Multi-purpose self-support idling four-gear disc type pole dance operation engine

Abstract

To provide an engine structure optimal for hybrid.SOLUTION: Upper and lower pistons are provided in place of a piston. A cylinder inner skin inward ring is fitted between a disc type engine upper outer wall cylinder inner skin inside recess and a disc type engine lower outer wall cylinder inner skin inside recess, and a cylinder inner skin outward ring is provided between a disc type engine upper outer wall cylinder inner skin outside recess and a disc type engine lower outer wall cylinder inner skin outside recess, thereby improving airtightness. Regarding an operation process, at the time of middle operation of an opposite side second cylinder and an extrusion bar, the operation is reinforced by second ignition separately from first ignition and further, blades in a guide ring are moved by an exhaust gas from an exhaust movable hole as exhaust operation, thereby assisting operation. Smooth rotation is made possible by using two alternate gears and disc type engine upper and lower inner two alternate gears at the time of a low speed and using a half gear double and a disc type engine upper inner gear for eccentric operation at the time of a high speed, and smooth switching is made possible by a variable induction gear, thereby attaining cooling effect improvement and reduction of weight.SELECTED DRAWING: Figure 57

Description

Technical Field

[0001] The present invention relates to a multi-purpose engine with a structure that reexamines the shapes and movable strokes of all parts such as the engine body, pistons, and cylinders, which are the power units of all machines such as automobiles and air motors. Compared with the previous Japanese Patent Application No. 2013-235136, it further improves airtightness for fuel, and uses a play 4-gear for the ratchet gear part that is easily damaged, and relates to a stable and movable multi-purpose disc-type PDOU4GE engine.

Background Art

[0002] In recent years, with the soaring gasoline prices, the market has entered an era of multi-purpose use of electric vehicles, hybrid vehicles, and hydrogen fuel vehicles. In hybrid vehicles, the goal is to be lightweight, and in electric vehicles, the goal is to have a coordinated structure. Therefore, in order to further improve fuel efficiency, it is necessary to reexamine the basic structure of the engine to achieve weight reduction and high efficiency, and to easily form a hybrid structure. Additionally, it is considered whether it can be applied to air motors related to tools and medical equipment, engines of large vehicles and heavy machinery, and generators to automobiles for multiple purposes.

[0003] Also, in conventional piston engines, there are generally vertical multi-cylinder engines, horizontal engines, and rotary engines. These are known to have a structure that is prone to bulkiness due to the block shape because the vertical and horizontal movable ranges of the pistons, connecting rods, and crankshafts are large.

Prior Art Documents

Patent Documents

[0004]

Patent Document 1

Non-Patent Documents

[0005]

Non-Patent Document 1

Summary of the Invention

Problems to be Solved by the Invention

[0006] Upper retaining burring (73) The structure of FIG. 4 is such that the ring hole is one size larger than the disk-type engine guide ring (4), and the outer shape is a ring-shaped retaining bar ring (71) that can be fitted into the pipe guiding ring groove (153) on the side of the mounting pedestal. Two disk retaining bars (75) are facing each other. The upper side of the half-gear double (95) which is the eccentric shortest position of the eccentric rotational movement, the inner gear (22) in the upper part of the disk-type engine, or the lower side of the half-gear double (95) and the inner gear (24) in the lower part of the disk-type engine, and the upper stopper bar (150) on the outer wall of the upper part of the disk-type engine or the lower stopper bar (151) on the outer wall of the lower part of the disk-type engine on the same side, with a length in a state where they are closer to the center, and the pipe guiding ring (72) The structure of FIG. 3 is a pipe guiding hole (76) which is a hole for guiding each circular movement caused by the eccentric rotation of the axial fuel branch pipe (13) near the tip of the pipe guiding bar (77) extending from the inner four sides of the pipe guiding retaining ring (78) having the same shape as the above-mentioned retaining bar ring (71). A part provided with an escape hole (156) which is a cut-out part for escape when the main body drops at low speed, and the guide ring shaft guiding part (126) The structure of FIG. 1 is such that the outer ring size is the same as the above-mentioned retaining bar ring (71). The inner side of the ring is a guide ring bearing holding part (102) provided with a through hole of the vertical guide (101) of the disk-type engine guide ring bearing on the inner four sides of the guide ring bearing outer ring (107) with a size one size larger than the eccentric circular movement orbit of the disk-type engine guide ring shaft (100). A cylindrical part is held and fixed to the guide ring bearing holding part (102), and an extended through hole of the vertical guide (101) of the disk-type engine guide ring bearing is provided. A guide ring shaft play window (106) for the movable protrusion range of the disk-type engine guide ring shaft (100) during eccentric limit rotation is provided at a position above the middle of the cylindrical part. A guide ring shaft guide assist (104) part provided with a quarter inner circle protrusion for guiding the circular movement during eccentric limit rotation of the spring-type stopper (129) above the guide ring shaft play window (106), and a quarter inner circle protrusion in the same horizontal direction as above is provided at the lower part of the guide ring shaft play window (106). A part provided with a left-right alignment inclination (103) of a vertical semi-circular inclination for bringing the left and right distortions to the center at the low-speed movable position, and further, a quarter ball inner hole guide ring shaft guiding ball-type hole (105) for correcting the front-back displacement in the extension,A component with a guide ring shaft guide part (126) structure provided with a guide ring bearing inner ring (108) composed of each guide part for returning to a low-speed movable circular movable range at the center, and the structure of the guide ring shaft lifting guide ring (117) in FIG. 2 is as follows: First, the guide ring shaft guide body (116) is rotatably housed inside each guide protrusion part (104·105) of the guide ring bearing inner ring (108). The inner side is a low cylindrical shape with a hole at the bottom, which provides a space for the eccentric rotation range of the disk-shaped engine donut piston part (154) combined with the outer walls (1·2) of the upper and lower parts of the disk-shaped engine and the disk-shaped engine guide ring (4). It is a part of the slide mechanism gear (109) of the gear with a hole at the bottom. At the upper part, protrusions of the slide stopper (111) are provided on four sides, and a honeycomb-shaped stopper dance floor (113) is provided, which is the space for the eccentric rotation range of the honeycomb-shaped stopper (129). Immediately beside it, a return stopper (121) part with a spring protrusion structure is provided. Immediately beside it, a slide inclination (110) of the inclined part for lifting is provided, and a bottom at the low-speed position is provided. At this time, a recess is provided at the lower part of the next slide stopper (111) at the height of the honeycomb-shaped stopper (129) and provided on four sides. Furthermore, the disk holding bar (75) is provided in a folded manner by a spring (115) for a retractable guide bar near the center of the honeycomb-shaped stopper dance floor (113). The structure of the installation box (94) in FIG. 34, which is the installation space on the main body side, is as follows: It has a normal movable circle (93) and, by rephrasing the normal movable point (209) at its center as an eccentric point (208), this part that depicts an eccentric movable circle (124) outside the outer peripheral end of the idle gear reference (18) is installed inside, and this part becomes the installation bottom (91). A cylindrical side surface, the installation side (92), is provided on the outer periphery. A hole for the shaft is provided at the bottom of the cylindrical tea can shape, a pipe guiding ring (72), an upper holding bar ring (73), and a guide ring shaft guiding mechanism part (138) are arranged and fixed at appropriate positions from above, and an installation box (94) ASSY with a built-in self-supporting disk-shaped idle 4-gear PDO movable engine (209). The structure of the disk receiving bearing pedestal (19) for the fuel tank in FIGS. 32·42 is as follows: A round recess is provided between the inner and outer sides of the surface where the corners of the upper inner peripheral surface of the ring shape are cut to near the bottom, and this part becomes the pedestal bearing ring (53).A disc receiving bearing pedestal (19) ASSY with a structure in which around 3 to several tens of portions are provided circumferentially with portions where a ball-shaped pedestal bearing ball (52) that is slightly smaller than the depression is rotatably fitted; a honeycomb-shaped fuel tank (10) ASSY with a structure in which around 2 to several tens of slightly smaller hollow portions are provided circumferentially with airfoil cooling fuel tank portions (213) which are airfoil cavities from the center of the thicker blades of the fan, and an axial fuel main pipe (59) is provided at the upper center; a component with a structure from a pipe from the honeycomb-shaped fuel tank (10), from the fixed portion inside the shaft to the pipe distribution portion in all directions from the upper half gear double (95) of the variable gear box (88) for the structure of the axial fuel main pipe (59) in FIG. 38; a component with a structure in which a cross groove is formed on the upper side of a pipe material having a hole for the axial fuel main pipe (59) and the in-shaft axial wiring (14) to form a pipe holding shaft pipe receiver (123) for the structure of the pipe holding shaft (122) in FIG. 38; the in-shaft axial wiring (14) is a component that is wired along the axial fuel main pipe (59) from below the guide ring shaft lifting induction ring (117) to the installation side; a component with a structure in which a pipe holding shaft pipe fixing portion (202) with protrusions on the outer circumference in all directions is provided at the lower cylindrical portion of the idler gear four spacer (120) in FIG. 48, the idler gear four holder holes (203) of the receiving portion of the idler gear four holder (119) are fixed, and a structure is formed on which the lower portion of the propeller portion gear (9) is fixed; a component with a structure in which a half gear double (95) in FIG. 33 has a half holding gear portion (96) with no teeth on the gear in a half cylindrical portion and a half transmission gear (97) with teeth, and two lower half gears (99) are fixed with their tooth positions shifted so as not to overlap, and a hole for rotatably holding the pipe holding shaft (122) is provided; the fixed shaft (121) is a fixed shaft (121) ASSY with the axial fuel main pipe (59) and the in-shaft axial wiring (14) built therein in the pipe holding shaft (122); the structure of the operating shaft (54) is an operating shaft (54) ASSY which connects a movable shaft gear (15) to the upper portion of the half gear double (95), connects a pipe-shaped pipe shaft (55) to the lower portion of the half gear double (95), and is composed of a portion provided with hexagonal upper and lower portions (215·216) in a nut shape at the lower portion; the structure of the pipe built-in shaft pipe (181) is a pipe built-in shaft pipe (181) ASSY with a structure in which the fixed shaft (121) is rotatably built in the through hole of the operating shaft (54).Movable shaft gear (15) Figure 21 shows a component with a hole for fitting onto the pipe shaft (55). The structure of the idle gear four (11) in Figure 21 is a dumbbell silhouette with gears connected by a shaft. The upper gear meshes with the propeller gear (9) attached to the lower part of the propeller (51). The lower gear meshes with the movable shaft gear (15) to transmit rotation. The idle gear four is rotatably fitted onto the shaft between the gears by the idle gear four holder (119), and the opposite-side idle gear four holder (119) is fixed to the pipe holding shaft (122) by the idle gear four spacer (120). Further, it is fixed to the lower part of the upper propeller gear (9). The structure of the idle gears one and two (16, 17) in Figure 21 is a gear with a smaller diameter than the idle gear three (18). One and two are the same, and they are named due to the difference in the position of the attachment part. The structure of the idle gear three (18) in Figure 21 is a cylindrical shape and is a component provided for stable holding in the upper and lower internal gears (22, 24) of the disc-type engine. The shape of the variable induction gear (84) in Figure 35 is such that the inner peripheral end gear teeth of the variable induction gear (84) with an oblique cylindrical shape, which is obtained by shifting the non-contact central axis interval by shifting the interval between the center shaft hole (85) at the bottom of the right-angled triangle shape of the upper half teeth (205) of the two-change receiving gear (197) on the upper part of the shaft to a right-angled isosceles triangle shape of teeth around the center shaft, and the outer peripheral gear teeth and the half gear double (95) are provided at both ends and do not mesh, are aligned and fixed with the gear teeth of the half gear double (95). This part is the vertical rotation part of the half gear double (95) at high speed. With this as the axis, the restricted operation disc-type engine guide ring (4), and the outer walls (1, 2) of the upper and lower parts of the disc-type engine are components with an alternating rotation and eccentric movement structure. The structure of the two-change gear (201) ASSY in Figure 44 is first a two-change gear connection hole part (210) in the shape of a hexagonal column is provided above and below the center of the disc-shaped plate, and it becomes a two-change gear spring part (212) with the two-change gear spring (199) set above and below the spring fixing part (200). Next, it is a part with gear teeth in the shape of a right-angled triangle provided on the outer periphery of the shallow cylindrical lid shape, and a two-change gear connection convex (211) in the shape of a hexagonal column protrusion that is slightly larger than the two-change gear connection hole part (210) in the center inside this part, which forms the upper and lower internal two-change receiving gears (197, 198) of the disc-type engine.The two-change gear (201) ASSY has a structure in which it is telescopically fitted to the two-change gear connection protrusion (211) of the two-change receiving gears (197, 198) inside the upper and lower parts of the disc-shaped engine, which are fitted to the two-change gear connection hole part (210) of the two-change gear spring part (212) set earlier. The structure of the variable gear box (88) ASSY in Fig. 21 is such that a bearing (213) is provided at the lower part of the operating shaft (54), and the two-change gear connection hole (210) meshes with the hexagonal upper and lower parts (215, 216) at the upper part thereof. A variable induction gear (84) is fixed to the upper part thereof. The variable induction gear (84) is fixed to the upper part of the one-half gear double (95), and the lower part of the movable shaft gear (15) is fixed to the variable induction gear (84). A free gear three (18) is provided opposite to the upper one-half of the variable induction gear (84) of the one-half gear double (95), a free gear one (16) is provided on the left side, and a free gear two (17) is rotatably provided on the right side. A part of the fixed shaft (121) of the shaft fixing part has a free gear four holder (119) fitted into the free gear four holder hole (203) of the free gear four spacer (120). The propeller part gear (9) is rotatably fitted to the upper part of the free gear four spacer (120). The movable shaft gear (15) meshes with the lower part of the propeller relay gear (11), and the upper part of the propeller relay gear (11) meshes with the propeller part gear (9). The structure of the central side on the front side of the outer walls (1, 2) of the upper and lower parts of the disc-shaped engine is such that the part where the angel cake-shaped cake batter enters is semi-circular, or the flat part from the central hole of the upper and lower cylinder covers (157) cut horizontally leaving a hollow donut-shaped hole to the inner concave part is the disc gear holding part (158). Vent holes (56) for allowing the flow of air from the cooling movable fins (40) are provided on all four sides thereof. Further, on the outer periphery of the central hole of the disc gear holding part (158), there are the inner gears (22, 24) of the upper and lower parts of the disc-shaped engine, and below that, there is a part consisting of the two-change gears (23, 25) of the upper and lower parts of the disc-shaped engine with gear teeth shaped like half of the gear teeth of the inner gears (22, 24) of the upper and lower parts of the disc-shaped engine provided on all four sides. Next, the structure of the cooling movable fins (40) on the outer periphery of the cylinder on the front side of the outer walls (1, 2) of the upper and lower parts of the disc-shaped engine is such that crescent shapes larger than the donut semi-circle of the upper outer wall (1) of the disc-shaped engine are provided at an angle from the outer gears (23, 25) of the upper and lower parts of the disc-shaped engine to the inner gears (22, 24) of the upper and lower parts of the disc-shaped engine, with the number ranging from 1 to several tens. The air flow is a flow taken in from the center.The structure where air flows from the center to the side by the cooling movable fins (40) on the lower outer wall (2) of the disk-shaped engine on the opposite side, and next, the operating mechanism part receiver (159) of the structure on the outer side of the circle on the front side of the upper and lower outer walls (1, 2) of the disk-shaped engine, the upper and lower stopper bar (150, 151) parts of the disk-shaped engine outer wall, the intake and exhaust extrusion head (132, 131) parts, the commutator (28, 29) parts, the first and second stopper head (57, 58) parts, the upper and lower movable ring groove (63, 64) parts, and the disk-shaped engine with a shape in which a gently inclined right-angled triangular prism provided at the bottom of the upper and lower movable ring grooves (63, 64) is laid down, The structural part consisting of the upper and lower outer wall one-way gears (225, 226), the ring rail (161), the exhaust movable hole (139), and the exhaust passage (136), and the structure of the disk-shaped engine outer wall upper and lower stopper bars (150, 151) of the outer inclined part of the disk during the high-speed movement of the actuator mechanism receiver (159) is a cylindrical bar provided in the middle of the outer inclination of the upper and lower outer walls (1, 2) of the disk-shaped engine. The upper outer wall (1) of the disk-shaped engine is a disk holding bar (75), and the lower outer wall (2) of the disk-shaped engine is a retractable guide bar (114), which is a part of the mechanism that alternately creates a movable standby state. The arrangement positions of the intake and exhaust extrusion heads (132, 131) of the above-mentioned actuator mechanism receiver (159) are such that the intake extrusion head (132) is provided on the left side and the exhaust extrusion head (131) is provided on the right side below the disk-shaped engine outer wall upper and lower stopper bars (150, 151). The arrangement positions of the commutators (28, 29) of the actuator mechanism receiver (159) are a structural part where a plus brush (28) is provided in the upper left and a minus brush for the brush (29) is provided in the lower right between the lower parts of the above-mentioned intake and exhaust extrusion heads (132, 131). The ignition of the second plug (147) is arranged slightly to the left. The structure of the first and second stopper heads (57, 58) of the actuator mechanism receiver (159) is a structure with an inclined part provided on the left side of the block shape, which is provided outside the lower part of the commutator part (28, 29). Each actuator mechanism receiver (159) is located on the outer four sides of the circle on the front side of the upper outer wall (1) of the disk-shaped engine, and the lower outer wall (2) of the disk-shaped engine is arranged in an inverted manner. The structure of the upper and lower movable ring grooves (63, 64) in Fig. 28 is such that the upper movable ring groove (63) is rotatably fitted to the inner upper rail (166) of the ring of the disk-shaped engine guide ring (4), and the lower movable ring groove (64) is rotatably fitted to the inner lower rail (167). The structure of the ring rail (161) is to prevent the side guard from falling off the upper and lower movable ring grooves (63, 64), and the exhaust passage (136) is formed by cutting out the side arc vertically from each actuator mechanism receiver (159) to the vicinity of the exhaust extrusion head (131). The exhaust passage (136) is a part where the inner honeycomb rail hole (185) of the guide ring inner honeycomb (65) of the following is cut out from the shape of the ring rail (161) to form the intermediate exhaust port part (184).Furthermore, the structural part where the exhaust flow reaches up to the final exhaust hole (152) provided in the lower right part near the axial fuel branch pipe (13) of the disk-shaped engine guide ring (4), and the structure of the exhaust movable hole (139) are the structural part provided on the lower side surface of the outer side of the ring rail (161) from the exhaust valve hole (133) of each operating mechanism receiving part (159). The exhaust movement moves one-third of a rotation of one stroke in four strokes during the first half of the movement. During exhaust, dozens of the inner springs (65) 3 in the guide ring of the disk-shaped engine guide ring (4) move. At that time, the exhaust path switches from the ring rail (161) to the exhaust passage (136) from the position where the upper and lower outer walls (1) of the disk-shaped engine have moved. The inner spring ring rail hole (185) of the inner spring (65) and the intermediate exhaust port part (184) are formed. In the second half of the exhaust, it is the structural part where the exhaust is discharged from the final exhaust hole (152). The disk-shaped engine outer wall outer ring leakage prevention ring (143) on the inner side of the outer circle of the upper and lower outer walls (1, 2) of the disk-shaped engine is installed between the leakage prevention ring outer grooves (144) of the upper outer wall (1) of the disk-shaped engine and the lower outer wall (2) of the disk-shaped engine, and is the structural part that prevents leakage and misalignment on the outside. The leakage prevention ring outer groove (144) is the installation hole part of the disk-shaped engine outer wall outer ring leakage prevention ring (143) provided on the inner and outer sides of the upper and lower outer walls (1, 2) of the disk-shaped engine, and is the structural part where the outer wall outer ring bearing balls (145) are installed rotatably between the outer wall outer ring bearing grooves (165) of the upper and lower outer walls (1, 2) of the disk-shaped engine provided on the lower circumference inside the ring rail (161) with respect to the disk shape. Next, the structure of the piston semi-circular ring (3) around the combustion chamber on the inner side of the upper and lower outer walls (1, 2) of the disk-shaped engine is the same as that of the piston ring, and is the part for being installed in the piston ring semi-groove (60) of the upper and lower outer walls (1, 2) of the disk-shaped engine as shown in FIG. 39. The structure of the upper and lower piston walls (5, 8) is in the shape of a thick disk, and its outer circumference is fitted into a groove. It is the structural part that is fitted and welded together with the piston wall groove (186) and the piston ring semi-groove (60) provided on the inner four sides of the upper and lower outer walls (1, 2) of the disk-shaped engine. The structure of the extrusion bar (61) is the part that bends along the combustion chamber like a banana in the left center of the upper piston wall (5) when viewed from the inside of the upper outer wall (1) of the disk-shaped engine, and the tip is rounded. The structure of the second cylinder (118) is slightly larger than the extrusion bar (61).The inner peripheral surface has a banana tube shape with an intake groove (149) in the groove part without a groove from the top of the cylinder to the bottom as it goes deeper. At the center of the bottom, there is a firing pin receiver (148), a first plug (146) near the outer periphery adjacent to it, a second plug (147) provided near the outer periphery of the second cylinder (118), and a structure part. The disc-shaped engine outer wall inner ring leakage prevention ring (162) on the central side inside the outer walls (1, 2) of the upper and lower parts of the disc-shaped engine is installed between the leakage prevention ring inner grooves (155) of the upper outer wall (1) and the lower outer wall (2) of the disc-shaped engine, and is a structure part for preventing inner leakage and misalignment. The leakage prevention ring inner groove (155) is the installation hole part of the disc-shaped engine outer wall inner ring leakage prevention ring (162) provided on the inner center side of the upper and lower outer walls (1, 2) of the disc-shaped engine, and is a structure part for rotatably installing an outer wall inner ring bearing ball (163) between the outer wall inner ring bearing grooves (164) of the upper and lower outer walls (1, 2) of the disc-shaped engine, where the inside from the vent hole is provided on the lower circumference of the disc shape. The structure of the lower outer wall (2) of the disc-shaped engine is the disc-shaped engine lower outer wall (2) ASSY with the inverted arrangement structure of the upper outer wall (1) of the disc-shaped engine above. The shapes of the disc-shaped engine guide rings (4) in FIGS. 12, 13, and 14 are ring-shaped, with a rounded outer periphery and a hollow inner periphery. It consists of an upper side surface (192) of the inner ring upper rail (166) with the same length as the length of the inner ring rail (187) part, a surface part (193) that enters the inside with approximately the same length as the upper movable ring groove (63), a part (195) with the same length as the inner surface part of the outer ring rail (161), the length (194) of the upper surface part of the outer ring rail (161), and the length (196) of the side surface of the upper rail side of the hollow part inside the guide ring. It forms a ring inner upper rail (166) of the protruding inner peripheral part and a part consisting of a ring inner lower rail (167) provided at the lower part. The ring inner upper and lower rails (166, 167) have a structure with right-angled triangular gear teeth provided on the convex surface, which meshes with the one-way gears (225, 226) of the upper and lower outer walls of the disc-shaped engine to prevent reverse rotation. It becomes a honeycomb-shaped protrusion provided on the side surface of the disc-shaped engine guide ring (4) on the side of the guide ring operating mechanism part (188), and a honeycomb-shaped stopper ball (128), which is a ball roller for movement from the outside of the lower part of the honeycomb-shaped stopper (129), is installed so that its head protrudes.The honeycomb stopper (129) ASSY consists of a part provided with a cylindrical bar-shaped disk-type engine guide ring shaft (100) at the central height position on the outer side surface of the honeycomb stopper (129). The structure of the axial fuel branch pipe (13) extends upward from the middle position of each guide ring operating mechanism part (188) of the disk-type engine guide ring (4), bends in an L shape at approximately the same height as the axial fuel main pipe (59), and is connected to the axial fuel main pipe (59) from the rubber hose (21). The structure of the brush part of the guide ring operating mechanism part (188) provided on the four sides of the disk-type engine guide ring (4) is a plus brush (28) with a longer left side and a minus brush for brush (29) with a shorter right side near the upper inner side of the disk-type engine guide ring (4). It is provided at an appropriate angle where sliding contact is possible with the plus for commutator (26) and the plus brush (28), and the minus for commutator (27) and the minus brush for brush (29). The structure of the switching ring bar (7) forms a first lock and a second lock with the claws at both ends in bar shape, serving as a mechanism for preventing return for the expansion standby state and the upper and lower piston walls (5, 8) and expansion receiving, and an alternating mechanism part by the push bar (61). The structure of the honeycomb inside the guide ring (65) is provided with 3 to several tens of pieces at intervals of 1 / 8 of the guide ring operating mechanism part (188) on the inner peripheral surface of the disk-type engine guide ring (4). Its shape consists of a part connecting the inner peripheral side surface (206) of the disk-type engine guide ring in Fig. 45 and the outer peripheral side surface of the outer ring rail on the upper and lower outer walls of the disk-type engine outer wall (207). The exhaust passage (136) formed from the cross-section of the arc of the honeycomb inside the guide ring (65), the side surface of the ring rail for the upper outer wall of the disk-type engine (190), or the side surface of the ring rail for the lower outer wall of the disk-type engine (191) and the ring rail (161) becomes the honeycomb exhaust hole inside the guide ring (62). The final exhaust hole (152) is a part that becomes the final exhaust part provided at the lower part on the right side of each guide ring operating mechanism part (188) of the disk-type engine guide ring (4). The guide ring operating mechanism part (188) at the upper part of the disk-type engine guide ring (4) has a lower inversion arrangement structure except for the axial fuel branch pipe (13). The structure of the guide ring shaft guiding mechanism part (138) ASSY in Figs. 11 and 16 is a structural part with the guide ring shaft lifting and guiding ring (117) built into the guide ring shaft guiding part (126).The (197·198) of the above two-replacement gear (201) always moves in a constant direction during operation at low speed. However, when the two-replacement gear (23) inside the upper part of the disk-type engine and the two-replacement gear (25) inside the lower part of the disk-type engine rotate forward in the rotational direction, then the two-replacement receiving gear (197) inside the upper part of the shaft, and then the two-replacement receiving gear (198) inside the lower part of the shaft behind it, when the two-replacement receiving gear (197) inside the upper part of the shaft operates, the two-replacement gear (23) inside the upper part of the disk-type engine and the two-replacement gear (25) inside the lower part of the disk-type engine rotate together by 85°. At the remaining 5°, due to the inclination of the gear teeth of the two-replacement receiving gear (198) inside the lower part of the shaft waiting for operation, the two-replacement gear (25) inside the lower part of the disk-type engine escapes inward, so that the two-replacement gear (23) inside the upper part of the disk-type engine and the two-replacement gear (25) inside the lower part of the disk-type engine overtake, and the next operation becomes the two-replacement receiving gear (198) inside the lower part of the shaft. By repeating this, it is a mechanism part that alternately transmits rotation to the shaft. The structure of the disk-type free 4-gear PDO movable engine fixing part is the structure of the honeycomb-type fuel tank (10) part installed so as to be placed on the disk receiving bearing pedestal (19) fixed to the installation bottom (91) from below, and the structure part from the axial fuel main pipe (59) fixed to the center upper part of the honeycomb-type fuel tank (10) to the tip of the axial fuel main pipe (59) of the fixed shaft (121). The structure of the semi-fixed limit movable part during high-speed operation of the disk-type free 4-gear PDO movable engine is the structure from the rubber hose (21) fitted to the tip of the above axial fuel main pipe (59) to the disk-type engine guide ring (4) fitted to the axial fuel branch pipe (13), and it is a structure part that becomes a fixed part at low speed. The exhaust mechanism part (181) is composed of an exhaust pipe and an exhaust slide switch bar (179), and the exhaust extrusion head (131) has the same structure part except for the inclined part provided from the lower left side. The structure part is composed of the inner pipes of the upper and lower outer walls of the disk-type engine from the intake holes (31·177) of the upper outer wall of the disk-type engine in Fig. 46 to the lower part of the intake valve hole (134). The part where the rubber hose (21) connects between the tip of the above axial fuel main pipe (59) and the axial fuel branch pipe (13), and from the rounded root at the upper outer circumference of the disk-type engine guide ring (4), it branches up and down like Fig. 29 for the disk-type engine guide ring (4), and pipes extend from each position around the center to the left. The upper part is,The lower part of the intake hole (141) for the upper guide ring of the disk-shaped engine is the structural part that becomes the intake pipe inside the ring up to the part connected to the intake hole (142) for the lower guide ring of the disk-shaped engine. The intake mechanism structure (180) first has a hole in an appropriate position of the operating mechanism part receiver (159) provided on all four sides of the outer walls (1, 2) of the upper and lower parts of the disk-shaped engine, where the valve spring (135) can be built in so as to be able to expand and contract from the outside. It becomes a small hole where the valve bar can slide at the middle position, and the hole becomes thicker from the position immediately below to the combustion chamber. The lower part consists of the intake valve hole (134) part, which is a through hole with a size that can hide the intake valve (130), and the intake extrusion head, The intake extrusion head (132) is provided with an inclined part from the upper left side. When the intake slide switch bar (178) is turned on, it opens the intake valve (130). Next, the intake extrusion head (132) is connected to the upper part of the intake valve hole (134) on the outside, and the valve bar is connected from the lower part of the intake extrusion head (132). The valve spring (135) is slidably held in the middle hole of the intake valve hole (134) from above the valve bar, and the intake valve (130) is fixed to the tip of the valve bar with a space left at the lower part of the intake hole. The above is the structure of the parts and the ASSY part.

[0007] The airtight structure of the cylinder part is as follows: First, in the inner combustion chamber side of the outer circumferential airtight part of the disk in Fig. 53, a concave groove part is provided in the outer wall of the upper part of the disk-shaped engine (1) in the outer ring bearing groove (165). The inner side of the cylinder inner skin of the outer wall of the upper part of the disk-shaped engine has a concave (238). Between the inner side of the cylinder inner skin of the outer wall of the lower part of the disk-shaped engine (2) in the outer ring bearing groove (165) where a concave groove part is provided on the inner combustion chamber side, there is a part where the cylinder inner skin outward ring (235) is fitted. Between the inner side of the cylinder inner skin of the outer wall of the upper part of the disk-shaped engine (1) in the inner ring bearing groove (164) where a concave groove part is provided on the inner combustion chamber side, the inner side of the cylinder inner skin of the outer wall of the upper part of the disk-shaped engine has a concave (237). Between the inner side of the cylinder inner skin of the outer wall of the lower part of the disk-shaped engine (2) in the inner ring bearing groove (164) where a concave groove part is provided on the inner combustion chamber side, there is a part where the cylinder inner skin inward ring (236) is fitted. Between the upper part of each upper piston wall (5) of the outer wall of the upper part of the disk-shaped engine (1) and the piston semi-circular ring (3) part, the outward root of the piston semi-circular ring (3) of the upper piston wall (5), the double-ring contact part of the cylinder inner skin outward ring (235), the inward root of the piston semi-circular ring (3) of the upper piston wall (5), the double-ring contact part of the cylinder inner skin inward ring (236), between the lower part of each lower piston wall (8) of the outer wall of the upper part of the disk-shaped engine (1) and the piston semi-circular ring (3) part, the outward root of the piston semi-circular ring (3) of the lower piston wall (8), the double-ring contact part of the cylinder inner skin outward ring (235), the inward root of the piston semi-circular ring (3) of the lower piston wall (8), and the double-ring contact part of the cylinder inner skin inward ring (236), each engaging disk's inner circumference part that becomes the airtight part of each combustion chamber. The structure of the intake slide switch bar (178) is to create an intake stroke in the standby state next to the exhaust slide switch bar (179). It is an intake slide switch bar (178) with a short length, and there is a part with a mirror-image arrangement on the front and back. The structure of the exhaust slide switch bar (179) in Fig. 6 is that the bar that presses the exhaust extrusion head (131) within the moving range during the exhaust section is the exhaust slide switch bar (179), and there is a part with a mirror-image arrangement on the front and back. The shaft operating stroke at high speed: The idle gear one (16), idle gear two (17), and idle gear three (18) of the upper part of the variable gearbox (89) are a rotation stabilization mechanism and rotate freely.When the upper part of the half gear double (95) and the inner gear (22) of the upper part of the disc-shaped engine are operating, the half gear double (95) transmits rotation through the half transmission gear (97). At this time, the upper part is held by the upper holding barring (73) and the disc-shaped engine outer wall upper stopper bar (150) of the disc-shaped engine upper outer wall (1), and by the retractable guide bar (114) and the disc-shaped engine outer wall lower stopper bar (151) of the disc-shaped engine lower outer wall (2), creating a state of not moving while being eccentric (4). The inner disc-shaped engine lower inner gear (24) idles without transmitting rotation through the lower half holding gear part (96) of the half gear double (95), and in the next stroke, it transmits rotation in the reverse direction and operates alternately. In the first stroke A diagram of Figure 6, the first combustion chamber (32) starts to expand due to the first ignition, the second combustion chamber (33) exhausts, the third combustion chamber (34) intakes, the fourth combustion chamber (35) compresses, the first B combustion chamber (36) operates halfway through the second ignition, the second B combustion chamber (37) exhausts, the third B combustion chamber (38) intakes, the fourth B combustion chamber (39) compresses, and each exhaust is in the exhaust operating state. Next, in the first stroke B diagram, during operation, and then in the first stroke C, the first combustion chamber (32) and the push bar (61) during the expansion operation of the first B combustion chamber (36) push the striker receiver (148) in front of the second combustion chamber (33) and the second B combustion chamber (37). With this momentum, the switching ring bar (7) moves from the anti-return part on the left to the waiting tooth on the right, and the first stopper head (57) of the disc-shaped engine lower outer wall (2) moves to maintain a fixed position, and the waiting and operating states are switched, repeating the return to the first stroke A of Figure 6. The process of Figure 7 is repeated 8 times for two rounds, and each of the upper and lower outer walls (1, 2) of the disc-shaped engine rotates once, and the shaft rotates 4 times. In the high-speed shaft operation stroke, the idle gear one (16), idle gear two (17), and idle gear three (18) of the upper part of the variable gearbox (89) are rotation stability mechanisms and idle. When the upper part of the half gear double (95) and the inner gear (22) of the upper part of the disc-shaped engine are operating, the half gear double (95) transmits rotation through the half transmission gear (97). At this time, the upper part is held by the upper holding barring (73) and the disc-shaped engine outer wall upper stopper bar (150) of the disc-shaped engine upper outer wall (1), and by the retractable guide bar (114) and the disc-shaped engine outer wall lower stopper bar (151) of the disc-shaped engine lower outer wall (2), creating a state of not moving while being eccentric (4).The inner disc-shaped lower engine inner gear (24) is the lower half holding gear portion (96) of the half gear double (95), idles without transmitting rotation, and in the next stroke, conversely transmits rotation and operates alternately in this alternating manner, and The fully fixed part is a structural part provided with a disk receiving bearing pedestal (19) on the installation bottom (91) of the installation box (94), a pipe guiding ring (72), an upper holding bar ring (73), and a slide mechanism gear (109) at appropriate positions on the installation side surface (92); the semi-fixed part is a structural part of the connection part of the honeycomb fuel tank (10), the pipe holding shaft (122), and the axial fuel main pipe (59); the alternately movable part is a structural part in which the upper outer wall (1) and the lower outer wall (2) of the disk-shaped engine are held by a disk-shaped engine guide ring (4) so as to be rotatable alternately in one direction; the fixation at low speed is a structural part from the fixed shaft (121) to the disk-shaped engine guide ring (4); the restricted movable part at high speed is a structural part from the rubber hose (21) to the disk-shaped engine guide ring (4); the first ignition stroke is a structural part in which the first plug (146) ignites the combustion chamber during compression; the second ignition stroke for enhancing operation is that the second plug (147) ignites on the second cylinder (118) on the opposite side of the above-mentioned first ignition stroke, with the push bar (61) slightly separated, and at this time, the commutator is switched and shifted slightly later; the exhaust stroke is a structural part in which the exhaust push head (131) and the exhaust slide switch bar (179), which are operating auxiliary mechanisms for exhaust movement, move the honeycombs (65) inside the guide ring from 4 to several sheets by exhaust gas from the exhaust movable hole (139), and at the position where they move one-eighth, the exhaust gas is exhausted to the outside through the exhaust hole formed by the ring rail side surface (190) for the upper outer wall of the disk-shaped engine or the ring rail side surface (191) for the lower outer wall of the disk-shaped engine of each honeycomb (65) and the exhaust passage (136) to the final exhaust hole (152); the axial fuel branch pipe (13) and the rubber hose restricted operation stroke at high speed are such that due to the eccentric operation of the half gear double (95) and the upper and lower internal gears (22, 24) of the disk-shaped engine and the restriction of the restricted movement of the disk-shaped engine guide ring (4), each axial fuel branch pipe (13) draws a small circle in a regular manner through the pipe guiding hole (76) so as to draw a small circle; the operating stroke of the disk-shaped engine guide ring (4) at high speed is a structural part in which, with respect to the eccentrically operating upper and lower outer walls (1, 2) of the disk-shaped engine, due to the restricted movement of the disk-shaped engine guide ring (4), each honeycomb stopper ball (128) moves in a circular pattern on the honeycomb stopper dance floor (113).During eccentric operation at high speed, the waiting operation stroke of the disk holding bar (75) and the retractable guide bar (114) is such that when the upper outer wall (1) of the disk-type engine rotates during operation, the lower outer wall (2) of the disk-type engine is in a standby state. The lower outer wall stopper bar (151) of the disk-type engine outer wall of the retractable guide bar (114) and the lower outer wall (2) of the disk-type engine moves out of the middle position of the retractable guide bar (114) to the inner tip at a quarter rotation as shown in Fig. 25, and slides without transmitting rotation through the lower half holding gear portion (96) of the half gear double (95), and repeats this for the next replacement. At low speed, it comes under the upper outer wall stopper bar (150) of the upper outer wall (1) of the disk-type engine from the disk holding bar (75) without interference, and the retractable guide bar (114) is folded so that the disk-type engine guide ring (4) can be pushed down, and it does not interfere with the lower outer wall stopper bar (151) of the lower outer wall (2) of the disk-type engine. The structure of the lifting part of the slide mechanism (242) is a part fixed at an appropriate position on the side surface (92) by installing the outer circumference of the guide ring bearing outer ring (107) of the guide ring shaft guiding part (126). It is rotatably held on the upper part of the slide mechanism gear (109) of the guide ring shaft lifting guide ring (117), goes up to the spring-type stopper dance floor (113) at a quarter left rotation, the upper inner gear (22) of the disk-type engine comes to a position meshing with the upper part of the half gear double (95), the lower inner gear (24) of the disk-type engine comes to a position meshing with the lower part of the half gear double (95), and goes down to the low-speed hold position (241) at a quarter right rotation. The upper inner two-change gear (23) of the disk-type engine comes to a position meshing with the upper inner two-change receiving gear (197) of the shaft, and the lower inner two-change gear (25) of the disk-type engine comes to a position meshing with the lower inner two-change receiving gear (198) of the shaft. Each ASSY and operation stroke are composed of such a structure.

[0008] The engagement of the entire self-standing type four-gear disk type engine is as follows: Place the semi-fixed part (10) on the disk receiving bearing pedestal (19) of the complete fixing part. The part where the honeycomb fuel tank (10) is welded to the lower part of the axial fuel main pipe (59), the part where the operating shaft (54) is rotatably installed inside the fixed shaft (121), the bearing (213) at the lower part of the operating shaft (54), align the positions of the hexagonal lower part (216) above this, the two-way receiving gear (198) inside the lower part of the shaft, the hexagonal upper part (215), and the two-way receiving gear (197) inside the upper part of the shaft. Fit the part of the two-way gear (201) fitted in the center of the spring fixing part (200). The part fitted into the part which is actually a vertical hole but becomes the shaft hole (85) on the opposite side of the upper inclination from the central shaft hole (85) at the lower part of the variable induction gear (84), and the variable gear box (88) part provided with each induction gear around it. The fixed part of the disk type engine guide ring (4) at low speed, the structure part where the disk type engine guide ring (4) for high-speed limit operation and the axial fuel branch pipe (13) connect the axial fuel main pipe (59) with a rubber hose (21). The upper movable ring groove (63) on the upper outer wall (1) of the disk type engine and the upper rail (166) inside the ring of the disk type engine guide ring (4), and the lower movable ring groove (64) on the lower outer wall (2) of the disk type engine and the lower rail (167) inside the ring of the disk type engine guide ring (4) are rotatably fitted in one direction by the one-way gear (227) on the guide ring, the one-way gear (225) on the upper outer wall of the disk type engine, the one-way gear (226) on the lower outer wall of the disk type engine, and the one-way gear (228) under the guide ring. When the position of the guide ring shaft play window (106) of the slide mechanism (243) at low speed is at the low-speed hold position (241), the part held by its own weight between the upper outer side of the bearing (213), the internal gear (24) inside the lower part of the disk type engine on the lower outer wall (2) of the disk type engine, and the vent hole (56). The part meshed with the upper half teeth (205) of the two-way gear of the two-way gear (23) inside the upper part of the disk type engine and the two-way receiving gear (197) inside the upper part of the shaft, and also meshed with the upper half teeth (205) of the two-way gear of the two-way gear (25) inside the lower part of the disk type engine and the two-way receiving gear (198) inside the lower part of the shaft respectively. When the position of the guide ring shaft play window (106) of the slide mechanism (243) at high speed is at the honeycomb stopper dance floor (113),The structure consists of a state part where the disk-shaped engine doughnut piston part (154) is placed by its own weight on the honeycomb-shaped stopper dance floor (113) in a limited operation state with the honeycomb-shaped stopper ball (128) of the honeycomb-shaped stopper (129).

[0009] Figure 36 of the shaft improvement structure of Japanese Patent Application No. 2013-235136 is a multi-purpose swing and twist triple piston engine characterized by having all of these structures and functions above, by replacing the disk-shaped engine operation pipe part ratchet gear (6) with a variable gear box (88) to improve durability.

Advantages of the Invention

[0010] By rotating and moving from most of the first chamber to the eighth chamber corresponding to the combustion chamber, the cooling efficiency is increased. Furthermore, the cooling effect is enhanced by the cooling movable fins. By making it disk-shaped, the height can be reduced and the weight can be lightened. Additionally, hybridization is possible by providing a motor part directly below.

Brief Description of the Drawings

[0011]

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Modes for Carrying Out the Invention

[0012] Hereinafter, embodiments of the present invention will be described in sequence with reference to the improvement points of Japanese Patent Application No. 2013-235136 shown in FIG. 36 of the accompanying drawings, the structural diagrams of each part in FIGS. 1 to 5, 48, 33, and 8 to 12, 24, 26 to 30, 32, 34, 35, 37 to 47, 49 to 53 of the ASSY diagrams, the operating stroke diagrams in FIGS. 6, 7, 9, 10, 11, 25, 31, 54, the installation pedestal diagram, and the multi-purpose self-supporting free 4-gear disc-shaped pole dance operating engine.

[0013] The shaft improvement structure of Japanese Patent Application No. 2013-235136 increases durability by replacing the disc-shaped engine operating pipe part ratchet gear (6) with a variable gear box (88).

[0014] The structure of the upper holding burring (73) in Fig. 4 is such that the ring hole is one size larger than the disk-shaped engine guide ring (4), and the outer shape is a ring-shaped holding bar ring (71) that can be fitted into the pipe guiding ring groove (153) on the side of the installation pedestal. Two disk holding bars (75) face each other. The upper side of the half-gear double (95), which is the shortest eccentric position of the eccentric rotational motion, is connected to the inner gear (22) in the upper part of the disk-shaped engine, or the lower side of the half-gear double (95) is connected to the inner gear (24) in the lower part of the disk-shaped engine. The length of the structure is such that the upper stopper bar (150) on the outer wall of the disk-shaped engine on the same side or the lower stopper bar (151) on the outer wall of the disk-shaped engine is closer to the center.

[0015] The structure of the pipe guiding ring (72) in Fig. 3 is provided with a pipe guiding hole (76), which is a hole for guiding each circular motion caused by the eccentric limit rotation of the axial fuel branch pipe (13), near the tip of the pipe guiding bar (77) extending from the inner four sides of the pipe guiding holding ring (78) having the same shape as the above-mentioned holding bar ring (71). A pull-out hole (156), which is a cut-out part for pulling out when the main body drops at low speed, is provided.

[0016] The structure of the guide ring shaft guiding portion (126) in Fig. 1 is such that the outer ring size is the same as that of the above-mentioned ring for the holding bar (71). Inside the ring, a guide ring bearing holding portion (102) is provided with a through-hole of the disk-type engine guide ring shaft vertical guide (101) on the inner four sides of the guide ring bearing outer ring (107) with a hole size that is one size larger than the eccentric circular motion orbit of the disk-type engine guide ring shaft (100). A cylindrical portion is held and fixed in the guide ring bearing holding portion (102), and an extended through-hole of the disk-type engine guide ring shaft vertical guide (101) is provided. A guide ring shaft play window (106) for the movable overhang range of the disk-type engine guide ring shaft (100) during eccentric limit rotation is provided at a position above the middle of the cylindrical portion. A guide ring shaft guide assist (104) portion is provided with a quarter inner circle protrusion for guiding the circular motion during eccentric limit rotation of the spring-type stopper (129) above the guide ring shaft play window (106). A portion is provided with a quarter inner circle protrusion in the same lateral direction as above at the lower part of the guide ring shaft play window (106), and a left-right alignment inclination (103) with a vertical semi-circular inclination for bringing the left and right distortions to the center at the low-speed movable position is provided. Further, its extension, a quarter ball inner hole guide ring shaft guiding ball-type hole (105) corrects the front and rear displacements, and a guide ring shaft bearing inner ring (108) consisting of each guiding portion for returning to the circular movable range of low-speed movement is provided in the center, forming the structure of the guide ring shaft guiding portion (126).

[0017] The structure of the guide ring shaft lifting guide ring (117) in Fig. 2 is as follows: First, the guide ring shaft guide body (116) is rotatably accommodated inside each guiding protrusion (104, 105) of the guide ring bearing inner ring (108). The inner part is a low cylindrical shape with a hole at the bottom, which provides a space for the eccentric rotation range of the disc-shaped engine donut piston part (154) formed by combining the upper and lower outer walls (1, 2) of the disc-shaped engine and the disc-shaped engine guide ring (4). It also has a gear slide mechanism gear (109) part. At the upper part, there are protrusions of the slide stopper (111) on four sides, and a honeycomb-shaped stopper dance floor (113) is provided in the space of the eccentric rotation range of the honeycomb-shaped stopper (129). Immediately beside it, there is a return stopper (121) part with a spring structure where the protrusion sticks out. Immediately beside that, there is a slide slope (110) for the lifting slope. A bottom part at a low speed position is provided. At this time, a depression is provided at the lower part of the next slide stopper (111) on the height of the honeycomb-shaped stopper (129) and is provided on four sides. Furthermore, the disc holding bar (75) is provided in a foldable manner near the center of the honeycomb-shaped stopper dance floor (113) by a spring (115) for the retractable guide bar.

[0018] The structure of the guide ring shaft guiding mechanism part (138) ASSY in Fig. 11.16 is a structure in which the guide ring shaft lifting guide ring (117) is built into the guide ring shaft guiding part (126).

[0019] The movable stroke of the high-speed eccentric movable state in the upward view of Fig. 16 and the low-speed circular movable state in the downward view of Fig. 22 is a structure in which the disc-shaped engine donut piston part (154) is lifted and lowered by rotating the guide ring shaft lifting guide ring (117) by one-fourth turn.

[0020] The structure of the idle gear three (18) in Fig. 21 is cylindrical and is provided for stable holding of the inner gears (22, 24) of the upper and lower parts of the disc-shaped engine.

[0021] The structures of the idle gears one and two (16, 17) in Fig. 21 are gears with a smaller diameter than the idle gear three (18). One and two are the same, and they are named according to the difference in the position of the mounting part.

[0022] The structure of the fourth idle gear (11) in Fig. 21 is in the shape of a dumbbell silhouette with gears connected by a shaft. The upper gear meshes with the propeller part gear (9) attached to the lower part of the propeller (51). The lower gear meshes with the movable shaft gear (15) to transmit rotation. The gears are rotatably fitted into the fourth idle gear holder (119) through the shaft, and the opposite-side fourth idle gear holder (119) is fixed to the pipe holding shaft (122) with the fourth idle gear spacer (120), and further fixed to the lower part of the propeller part gear (9) at the upper part.

[0023] The shape of the fourth idle gear spacer (120) in Fig. 48 is such that at the lower cylindrical part, there is a pipe holding shaft pipe fixing part (202) with protrusions on the four-sided outer periphery and a fourth idle gear holder hole (203) for receiving the fourth idle gear holder (119). It is fixed, and on it, it is fixed to the lower part of the propeller part gear (9).

[0024] The movable shaft gear (15) in Fig. 21 has a structure with a hole for fitting onto the pipe shaft (55).

[0025] The shape of the variable induction gear (84) in Fig. 35 is such that at the upper part inside the shaft, the inner peripheral end gear teeth of the variable induction gear (84) with an oblique cylindrical shape are fixed with the gear teeth of the half gear double (95) aligned. This part is the vertical rotation part of the half gear double (95) at high speed. With this as the axis, the restricted operation disk-type engine guide ring (4) and the outer walls of the upper and lower parts of the disk-type engine rotate eccentrically alternately. The center shaft hole (85) at the bottom has a shape where the right-angled triangle shape of the upper half teeth (205) of the two-alternation receiving gear (197) in the upper part of the shaft is changed to a right-angled isosceles triangle shape with teeth provided around it. The radius of the center shaft is half of the radius of the gear double (95), and the outer peripheral gear teeth and the gear double (95) are provided at both ends with a non-contact interval between them, and the interval of the non-contact center shaft is shifted.

[0026] The structure of the half gear double (95) in Fig. 33 is such that in the cylindrical half part, two lower half gears (99) are provided with a half holding gear part (96) without teeth on the gear and a half transmission gear (97) with teeth. They are fixed with the tooth positions shifted so as not to overlap, and a hole for rotatably holding the pipe holding shaft (122) is provided.

[0027] The structure of the two - alternating gear (201) in FIG. 44 is as follows: First, a hexagonal - column - shaped two - alternating gear connection hole part (210) is provided above and below the center of a disc - shaped plate. A two - alternating gear spring part (212) is formed by setting two - alternating gear springs (199) above and below a spring fixing part (200). Next, it consists of a part with right - angled triangular gear teeth provided on the four outer sides of the shallow cylindrical lid - shaped outer periphery, and a two - alternating gear connection convex (211) of a hexagonal - column - shaped protrusion that is slightly larger than the two - alternating gear connection hole part (210) at the central part inside this part, which forms a two - alternating receiving gear (197·198) inside the upper and lower parts of the disc - type engine. The two - alternating gear connection convex (211) of the two - alternating receiving gear (197·198) inside the upper and lower parts of the disc - type engine is telescopically fitted into the two - alternating gear connection hole part (210) of the two - alternating gear spring part (212) that was set earlier.

[0028] The above - mentioned two - alternating gears (197·198) of the two - alternating gear (201) always move in a certain direction during low - speed operation. When the two - alternating gear (23) inside the upper part of the disc - type engine and the two - alternating gear (25) inside the lower part of the disc - type engine rotate forward, then the two - alternating receiving gear (197) inside the upper part of the shaft, and then the two - alternating receiving gear (198) inside the lower part of the shaft behind it, when the two - alternating receiving gear (197) inside the upper part of the shaft operates, the two - alternating gear (23) inside the upper part of the disc - type engine and the two - alternating gear (25) inside the lower part of the disc - type engine rotate together by 85°. At the remaining 5°, due to the inclination of the gear teeth of the two - alternating receiving gear (198) inside the lower part of the shaft that is waiting for operation, the two - alternating gear (25) inside the lower part of the disc - type engine escapes inward. In this way, the two - alternating gear (23) inside the upper part of the disc - type engine and the two - alternating gear (25) inside the lower part of the disc - type engine overtake each other, and the next operation becomes the two - alternating receiving gear (198) inside the lower part of the shaft. By repeating this, a mechanism is formed to alternately transmit rotation to the shaft.

[0029] The structure of the variable gear box (88) ASSY is as follows: a bearing (213) is provided at the lower part of the operating shaft (54), and at the upper part, two alternating gear connection holes (210) are engaged with the hexagonal upper and lower parts (215·216). A variable induction gear (84) is fixed to the upper part thereof. The variable induction gear (84) is fixed to the lower part of the movable shaft gear (15) above the one-half gear double (95). A free gear three (18) is provided opposite to the one-half gear double (95) at the upper part of the variable induction gear (84), a free gear one (16) is provided on the left side, and a free gear two (17) is rotatably provided on the right side. A free gear four spacer (120) is fitted into the free gear four holder hole (203) of the free gear four holder (119) at the fixed shaft (121) of the shaft fixing part. A propeller part gear (9) is rotatably fitted to the upper part of the free gear four spacer (120), and is engaged with the lower part of the movable shaft gear (15) and the propeller relay gear (11). The upper part of the propeller relay gear (11) is engaged with the propeller part gear (9).

[0030] The structure of the axial fuel main pipe (59) in FIG. 38 is a structure from the pipe from the honeycomb fuel tank (10), through the fixed part inside the shaft, to the one-half gear double (95) at the upper part of the variable gear box (88), and then to the pipe distribution part in four directions.

[0031] The part where a rubber hose (21) is connected between the tip of the above-mentioned axial fuel main pipe (59) and the axial fuel branch pipe (13), and the part where it branches above and below the disk-shaped engine guide ring (4) from the rounded root at the upper outer circumference of the disk-shaped engine guide ring (4) as shown in FIG. 29. The pipes extend from their respective positions around the center to the left. The upper part is connected to the intake hole (141) of the guide ring for the upper part of the disk-shaped engine, and the lower part is connected to the intake hole (142) of the guide ring for the lower part of the disk-shaped engine, which together form the intake pipe inside the ring.

[0032] The intake mechanism structure (180) is, first, a hole in an appropriate position of the operating mechanism part receiver (159) provided on the four sides of the outer walls of the upper and lower parts of the disk-shaped engine (1·2), through which a valve spring (135) can be built in so as to be expandable and contractible from the outside. It is a small hole where the valve bar can slide at the middle position, and the hole becomes thicker from the position immediately below to the combustion chamber. The lower part is a through hole with a size where the intake valve (130) is hidden, which forms the intake valve hole (134).

[0033] The intake extrusion head (132) is provided with an inclined portion from above on the left side, and is turned on by the intake slide switch bar (178) to open the intake valve (130).

[0034] Next, an intake valve hole (134) is provided on the outside, and a valve bar is connected from the lower part of the intake extrusion head (132) to the upper part of the intake valve hole (134). A valve spring (135) is slidably held in the middle hole of the intake valve hole (134) from above the valve bar, and an intake valve (130) is fixed to the tip of the valve bar with a space left at the lower part of the intake hole.

[0035] It consists of the inner piping of the upper and lower outer walls of the disk-shaped engine from the following to the intake valve hole (134) lower part from the intake holes (31, 177) of the upper outer wall of the disk-shaped engine in FIG. 46 of the upper and lower outer walls of the disk-shaped engine.

[0036] The exhaust mechanism part (181) has the same structure except that the exhaust pipe, the exhaust slide switch bar (179), and the exhaust extrusion head (131) are provided with an inclined portion from below on the left side.

[0037] The shaft inner axial wiring (14) is wired along the axial fuel main pipe (59) to the installation side from below the guide ring shaft lifting induction ring (117).

[0038] The structure of the pipe holding shaft (122) in FIG. 38 consists of a cross groove on the upper side of a pipe material having holes for the axial fuel main pipe (59) and the shaft inner axial wiring (14), and a pipe receiver (123) of the pipe holding shaft.

[0039] The fixed shaft (121) becomes a fixed shaft (121) ASSY incorporating the axial fuel main pipe (59) and the shaft inner axial wiring (14) in the pipe holding shaft (122).

[0040] The structure of the operating shaft (54) consists of connecting the movable shaft gear (15) to the upper part of the half gear double (95), connecting the pipe-shaped tube shaft (55) to the lower part of the half gear double (95), and having a nut-shaped hexagonal upper and lower part (215·216) provided at the lower part.

[0041] The structure of the shaft tube with built-in pipe (181) is a structure in which the fixed shaft (121) is rotatably built into the through hole of the operating shaft (54).

[0042] The structure of the central side on the front side of the outer walls of the upper and lower parts of the disk-shaped engine (1·2) is such that the part for the angel cake-shaped cake batter is semi-circular, or the flat part from the central hole of the upper and lower cylinder covers (157) cut horizontally leaving a hollow donut-shaped hole to the inner concave part is the disk gear holding part (158). Ventilation holes (56) for allowing the flow of air from the cooling movable fins (40) are provided on four sides thereof. Further, on the outer periphery of the central hole of the disk gear holding part (158), there are the inner gears (22·24) of the upper and lower parts of the disk-shaped engine, and below that directly, there are the inner 2 alternating gears (23·25) of the upper and lower parts of the disk-shaped engine provided with gear teeth in the shape of half of the gear teeth of the inner gears (22·24) of the upper and lower parts of the disk-shaped engine on four sides.

[0043] Next, the structure of the cooling movable fins (40) on the outer periphery of the cylinder on the front side of the outer walls of the upper and lower parts of the disk-shaped engine (1·2) is such that it is angled from the outer gears (23·25) of the upper and lower parts of the disk-shaped engine to the inner gears (22·24) of the upper and lower parts of the disk-shaped engine, and a crescent shape with a semi-circular outer periphery larger than the donut semi-circle of the upper outer wall (1) of the disk-shaped engine is provided in numbers from 1 to several tens. The air flow is a flow taken in from the center, and by the cooling movable fins (40) of the lower outer wall (2) of the disk-shaped engine on the opposite side, the air flows out from the center to the side.

[0044] Next, the structure of the outer circumference of the disc-shaped engine upper and lower outer walls (1, 2) on the front side, including the actuator mechanism receiver (159), the disc-shaped engine outer wall upper and lower stopper bars (150, 151), the intake and exhaust extrusion heads (132, 131), the commutator (28, 29), the first and second stopper heads (57, 58), the upper and lower movable ring grooves (63, 64), the disc-shaped engine upper and lower outer wall one-way gear (225, 226) parts in the shape of a gently inclined right-angled triangular prism lying on the bottom of the upper and lower movable ring grooves (63, 64), the ring rail (161) part, the exhaust movable hole (139) part, and the exhaust passage (136) part.

[0045] The structure of the disc-shaped engine outer wall upper and lower stopper bars (150, 151) at the outer inclined part of the disc during the high-speed movement of the actuator mechanism receiver (159) is a cylindrical bar provided in the middle of the outer inclination of the disc-shaped engine upper and lower outer walls (1, 2). The upper outer wall (1) of the disc-shaped engine is a disc holding bar (75), and the lower outer wall (2) of the disc-shaped engine is a retractable guide bar (114), which alternately forms a mechanism for making a movable standby state.

[0046] The arrangement position of the intake and exhaust extrusion heads (132, 131) of the actuator mechanism receiver (159) is such that the intake extrusion head (132) is on the left side under the disc-shaped engine outer wall upper and lower stopper bars (150, 151). The exhaust extrusion head (131) is provided on the right side.

[0047] The arrangement position of the commutator (28, 29) of the actuator mechanism receiver (159) is a structure in which a plus brush (28) is provided in the upper left and a minus brush (29) is provided in the lower right between the lower parts of the above intake and exhaust extrusion heads (132, 131).

[0048] The ignition of the second plug (147) is arranged slightly to the left.

[0049] The structure of the first and second stopper heads (57, 58) of the actuator mechanism receiver (159) is a structure with an inclined part provided on the left side in the shape of a block, and it is provided at the outer lower part of the commutator part (28, 29).

[0050] Each actuator part receiver (159) is located at the four outer sides of the outer circumference on the front side of the upper outer wall of the disk-shaped engine (1), and the lower outer wall of the disk-shaped engine (2) is arranged in an inverted manner.

[0051] Regarding the structure of the upper and lower movable ring grooves (63 and 64) in Fig. 28, the upper movable ring groove (63) is rotatably fitted to the upper rail (166) inside the ring of the disk-shaped engine guide ring (4), and the lower movable ring groove (64) is rotatably fitted to the lower rail (167) inside the ring.

[0052] The structure of the ring rail (161) prevents the side guards of the upper and lower movable ring grooves (63 and 64) from falling off, and the exhaust passage (136) is formed by cutting out the rounded part on the side vertically from each actuator part receiver (159) to near the exhaust extrusion head (131).

[0053] The exhaust passage (136) is formed by cutting out a part from the shape of the ring rail (161) of the inner rib (65) inside the guide ring, which becomes the intermediate exhaust port (184) in the middle, and further, the flow of the exhaust gas goes to the final exhaust hole (152) provided at the lower right part near the axial fuel branch pipe (13) of the disk-shaped engine guide ring (4).

[0054] The structure of the exhaust movable hole (139) is provided on the lower side surface outside the ring rail (161) from the exhaust valve hole (133) of each actuator part receiver (159).

[0055] During the first half of the exhaust movement, the exhaust movable part moves one-third of a rotation of one stroke every four minutes. During the exhaust process, it moves several tens of pieces from the inner rib (65) inside the guide ring of the disk-shaped engine guide ring (4). At this time, the exhaust passage switches from the ring rail (161) to the exhaust passage (136) at the position where the upper and lower outer walls (1) of the disk-shaped engine move. The inner rib ring rail hole (185) of the inner rib (65) inside the guide ring and the intermediate exhaust port (184) are formed, and during the second half of the exhaust, the exhaust gas is exhausted from the final exhaust hole (152).

[0056] The anti-leakage ring (143) for the outer ring of the disc engine outer wall, which is the structure on the outer side of the circle inside the upper and lower outer walls (1, 2) of the disc engine, is installed between the anti-leakage ring outer grooves (144) of the upper outer wall (1) and the lower outer wall (2) of the disc engine to prevent leakage and displacement on the outer side.

[0057] The anti-leakage ring outer groove (144) is the installation hole for the anti-leakage ring (143) of the outer ring of the disc engine outer wall provided on the inner and outer sides of the upper and lower outer walls (1, 2) of the disc engine.

[0058] Inside the ring rail (161) with respect to the disc shape, the outer ring bearing balls (145) of the outer walls of the upper and lower outer walls (1, 2) of the disc engine provided on the lower circumference are internally installed so as to be rotatable and movable between the outer wall outer ring bearing grooves (165).

[0059] Next, the structure of the piston semi-circular ring (3) around the combustion chamber inside the upper and lower outer walls (1, 2) of the disc engine is the same as that of the piston ring, and it is a name for being installed in the piston ring semi-groove (60) of the upper and lower outer walls (1, 2) of the disc engine as shown in Fig. 39.

[0060] The structure of the upper and lower piston walls (5, 8) is in the shape of a thick disc, and its outer circumference is fitted into a groove. A structure in which the piston wall groove (186) and the piston ring semi-groove (60) provided on the inner four sides of the upper and lower outer walls (1, 2) of the disc engine are combined and fitted and welded.

[0061] The structure of the extrusion bar (61) bends along the combustion chamber like a banana at the upper left center of the upper piston wall (5) as seen from the inside of the upper outer wall (1) of the disc engine, and the tip is rounded.

[0062] The structure of the second cylinder (118) is slightly larger than the extrusion bar (61), and has a banana tube shape with an intake groove (149) in the shape of a groove without a groove on the inner peripheral surface that goes deeper from the top of the cylinder to the bottom. At the center of the bottom, there is a firing pin receiver (148), a first plug (146) near the outer periphery adjacent to it, and a second plug (147) provided near the outer periphery of the second cylinder (118).

[0063] The anti-leakage ring (162) of the inner ring of the outer wall of the disk-shaped engine, which is the structure on the central side inside the upper and lower outer walls (1, 2) of the disk-shaped engine, is installed between the anti-leakage ring inner grooves (155) of the upper outer wall (1) and the lower outer wall (2) of the disk-shaped engine to prevent inner leakage and misalignment.

[0064] The anti-leakage ring inner groove (155) is the installation hole for the anti-leakage ring (162) of the inner ring of the outer wall of the disk-shaped engine provided on the inner center side of the upper and lower outer walls (1, 2) of the disk-shaped engine.

[0065] Inside the disk-shaped structure, the outer wall inner ring bearing balls (163) are installed rotatably between the outer wall inner ring bearing grooves (164) of the upper and lower outer walls (1, 2) of the disk-shaped engine provided on the lower circumference from the vent.

[0066] The structure of the lower outer wall (2) of the disk-shaped engine is the inverted arrangement structure of the upper outer wall (1) of the above disk-shaped engine.

[0067] In FIGS. 12, 13, and 14, the shape of the disk-shaped engine guide ring (4) is a ring shape, with a rounded outer circumference, a hollow inner circumference, and a ring inner upper rail (166) upper side surface (192) having the same length as the length of the inner ring rail (187) part, a surface part (193) that enters the inner side with approximately the same length as the upper movable ring groove (63), a part (195) having the same length as the inner surface part of the outer ring rail (161), a length (194) of the upper surface part of the outer ring rail (161), and a length (196) of the side surface of the upper rail side of the hollow part inside the guide ring. It consists of the ring inner upper rail (166) of the protruding inner circumference formed therefrom and the ring inner lower rail (167) provided at the lower part.

[0068] The ring inner upper and lower rails (166, 167) are provided with right-angled triangular gear teeth on the convex surface and engage with the one-way gears (225, 226) of the upper and lower outer walls of the disk-shaped engine to prevent reverse rotation.

[0069] It is a honeycomb-shaped stopper (129) which is a honeycomb-shaped protrusion provided on the side surface of the disk-shaped engine guide ring (4) on the side of the guide ring operating mechanism section (188). The honeycomb-shaped stopper (129) ASSY consists of a part in which a honeycomb-shaped stopper ball (128), which is a ball roller for movement from outside the lower part of the honeycomb-shaped stopper (129), is installed so that its head protrudes, and a part in which a disk-shaped engine guide ring shaft (100) in the shape of a cylindrical bar is provided at the height of the center of the disk-shaped engine guide ring (4) on the outer side surface of the honeycomb-shaped stopper (129).

[0070] The structure of the axial fuel branch pipe (13) extends upward from the middle position of each guide ring operating mechanism section (188) of the disk-shaped engine guide ring (4), bends in an L shape at approximately the same height as the axial fuel main pipe (59), and is connected to the axial fuel main pipe (59) from the rubber hose (21).

[0071] The structure of the intake slide switch bar (178) is located to the immediate right of the exhaust slide switch bar (179) and creates an intake stroke in the standby state. It is an intake slide switch bar (178) with a short length, and the front and back surfaces are arranged in a mirror image.

[0072] The structure of the exhaust slide switch bar (179) in Fig. 6 is such that the bar that presses the exhaust extrusion head (131) within the movement range during the exhaust section is the exhaust slide switch bar (179), and the front and back surfaces are arranged in a mirror image.

[0073] The two-cycle intake and exhaust slide switch bar (229) poses a problem for the next two-cycle movement.

[0074] The structure of the brush part of the guide ring operating mechanism section (188) provided on the four sides of the disk-shaped engine guide ring (4) is such that on the upper inner side of the disk-shaped engine guide ring (4), the left side has a long positive brush (28) and the right side has a short negative brush (29). It is provided at an appropriate angle where sliding contact is possible between the commutator positive (26) and the positive brush (28), and between the commutator negative (27) and the negative brush (29).

[0075] The structure of the switching ring bar (7) forms a mechanism for preventing return for the inflation standby state and (5·8), and for receiving inflation, with a first lock and a second lock by the claws at both ends of the bar shape, and an alternating mechanism by the extrusion bar (61).

[0076] The structure of the guide ring inner spring (65) is provided with 3 to several tens of pieces at 1 / 8 of the guide ring operating mechanism part (188) on the inner peripheral surface of the disc-shaped engine guide ring (4). Its shape is formed by a plate shape connecting the inner peripheral side surface (206) of the disc-shaped engine guide ring in Fig. 45 and the side surface of the outer peripheral side surface of the outer ring rail on the upper and lower outer walls of the disc-shaped engine outer wall (207).

[0077] This guide ring inner spring (65) and the side surface of the ring rail for the upper outer wall of the disc-shaped engine (190) or the side surface of the ring rail for the lower outer wall of the disc-shaped engine (191), and the exhaust passage (136) formed from the cross-section of the rounded part of the ring rail (161) become the guide ring inner spring exhaust holes (62).

[0078] The final exhaust hole (152) is the final exhaust part provided at the lower part on the right side of each of the guide ring operating mechanism parts (188) of the disc-shaped engine guide ring (4).

[0079] The guide ring operating mechanism part (188) at the upper part of the disc-shaped engine guide ring (4) has a lower inversion arrangement structure except for the axial fuel branch pipe (13).

[0080] The structure of the installation box (94), which is the installation space on the main body side in Fig. 34, has a normal movable circle (93) and, by rephrasing the normal movable point (209) at its center as an eccentric point (208), the part that draws an eccentric movable circle (124) outside the outer peripheral end of the idle gear reference (18) is installed inside, and this part becomes the installation bottom (91). A cylindrical side surface, the installation side (92), is provided on this outer periphery. A hole for the shaft, a pipe guiding ring (72), an upper holding bar ring (73), and a guide ring shaft guiding mechanism part (138) are arranged and fixed at appropriate positions from above, and a self-supporting disc-shaped idle 4-gear PDO movable engine (209) is built-in.

[0081] The structure of the disc receiving bearing pedestal (19) for the fuel tank in Fig. 25 is such that a round recessed portion is provided between the inner and outer sides of a surface where the corners of the ring-shaped upper inner peripheral surface are cut almost to the bottom, and this portion becomes the pedestal bearing ring (53). Around this, there are provided 3 to dozens of places with a structure where ball-shaped pedestal bearing balls (52) that are slightly smaller than the recess are rotatably fitted.

[0082] The shape of the fuel tank in Figs. 32 and 42 is a hollow structure that is slightly smaller in circumference, with 2 to dozens of wing-shaped cooling fuel tank parts (243), which are wing holes, provided around the center of the relatively thick blades of the fan. Also, it is a honeycomb-shaped fuel tank (10) with an axial fuel main pipe (59) provided at the upper center.

[0083] The structure of the disc-shaped play 4-gear PDO movable engine fixing part is the structure from the part of the honeycomb-shaped fuel tank (10) placed on the disc receiving bearing pedestal (19) fixed to the installation bottom (91) from below, to the tip of the axial fuel main pipe (59) of the fixed shaft (121) where the axial fuel main pipe (59) is pipe-fixed to the upper center of the honeycomb-shaped fuel tank (10).

[0084] The structure of the semi-fixed limit movable part when the disc-shaped play 4-gear PDO movable engine is moving at high speed is the structure from the rubber hose (21) fitted to the tip of the above axial fuel main pipe (59) to the disc-shaped engine guide ring (4) fitted to the axial fuel branch pipe (13), and it becomes a fixed part at low speed.

[0085] The disc-shaped play 4-gear PDO movable engine rotor part consists of a 2-alternating rotor part, a fixed shaft (121) part, and an operating shaft (54) part.

[0086] The structure of the 2-alternating rotor part is such that the upper inner rail (166) of the disc-shaped engine guide ring (4) and the upper movable ring groove (63) of the upper outer wall (1) of the disc-shaped engine, as well as the lower inner rail (167) and the lower movable ring groove (64) of the lower outer wall (2) of the disc-shaped engine, are rotatably engaged.

[0087] The airtight structure of the cylinder part is as follows: First, between the outer peripheral airtight part (1) of the disk in Fig. 53 and the concave groove part provided on the combustion chamber side inside the outer wall outer ring bearing groove (165), there is a concave part (238) on the outer side of the cylinder inner skin of the upper outer wall of the disk-shaped engine. And between the concave part (240) on the outer side of the cylinder inner skin of the lower outer wall of the disk-shaped engine with a concave groove part provided on the combustion chamber side inside the outer wall outer ring bearing groove (165), there is a part where the cylinder inner skin outward ring (235) is fitted. Also, between the concave part (237) on the inner side of the cylinder inner skin of the upper outer wall of the disk-shaped engine with a concave groove part provided on the combustion chamber side inside the outer wall inner ring bearing groove (164) of the upper outer wall of the disk-shaped engine (1), and the concave part (239) on the inner side of the cylinder inner skin of the lower outer wall of the disk-shaped engine with a concave groove part provided on the combustion chamber side inside the outer wall inner ring bearing groove (164) of the lower outer wall of the disk-shaped engine (2), there is a part where the cylinder inner skin inward ring (236) is fitted. Then, between the upper part of each upper piston wall (5) of the upper outer wall of the disk-shaped engine (1) and the piston semi-circular ring (3) part, the outward root of the piston semi-circular ring (3) of the upper piston wall (5), the double-ring contact part of the cylinder inner skin outward ring (235), the inward root of the piston semi-circular ring (3) of the upper piston wall (5), the double-ring contact part of the cylinder inner skin inward ring (236), between the lower part of each lower piston wall (8) of the upper outer wall of the disk-shaped engine (1) and the piston semi-circular ring (3) part, the outward root of the piston semi-circular ring (3) of the lower piston wall (8), the double-ring contact part of the cylinder inner skin outward ring (235), the inward root of the piston semi-circular ring (3) of the lower piston wall (8), and the double-ring contact part of the cylinder inner skin inward ring (236), each engagement disk forms the airtight part of each combustion chamber on the inner circumference of the combustion chamber.

[0088] Figure 6, One-stroke A diagram: The expansion of the first combustion chamber (32) starts due to the first ignition, the A2 combustion chamber (33) is for exhaust, the A3 combustion chamber (34) is for intake, the A4 combustion chamber (35) is for compression, the B1 combustion chamber (36) is in mid-operation due to the second ignition, the B2 combustion chamber (37) is for exhaust, the B3 combustion chamber (38) is for intake, the B4 combustion chamber (39) is for compression, and each exhaust is in the exhaust operation state.

[0089] Next, the one-stroke B diagram shows the mid-operation.

[0090] Next, in one stroke C, the push bar (61) during the expansion operation of the first A1 combustion chamber (32) and the second B1 combustion chamber (36) presses the striker receiver (148) in front of the second A2 combustion chamber (33) and the second B2 combustion chamber (37). With this momentum, the switching ring bar (7) moves from the left anti-return part to the right standby claw, and the first stopper head (57) of the lower outer wall (2) of the disk-shaped engine moves to the standby claw, maintaining a fixed position. The standby and operating states are switched, and it returns to one stroke A in Figure 6 and repeats this process. The process in Figure 7 is repeated 8 times for two rounds, and the upper and lower outer walls (1, 2) of each disk-shaped engine rotate once each, and the shaft rotates 4 times.

[0091] During the shaft operation stroke at high speed, the idle gear one (16), idle gear two (17), and idle gear three (18) of the upper part of the variable gearbox (89) are in an idling state due to the rotation stabilization mechanism. When the upper part of the half-gear double (95) and the inner gear (22) of the upper part of the disk-shaped engine are operating, the half-gear double (95) transmits rotation through the half-gear transmission gear (97). At this time, the upper part is held by the upper holding bar ring (73) and the disk-shaped engine outer wall upper stopper bar (150) of the upper outer wall (1) of the disk-shaped engine, and the retractable guide bar (114) and the disk-shaped engine outer wall lower stopper bar (151) of the lower outer wall (2) of the disk-shaped engine create a state where it moves eccentrically (4) but does not move. The inner lower inner gear (24) of the disk-shaped engine idles without transmitting rotation through the lower half-holding gear part (96) of the half-gear double (95), and in the next stroke, it transmits rotation in the reverse direction and operates alternately in this way.

[0092] The fully fixed part has a structure in which a disk receiving bearing pedestal (19) is provided on the installation bottom (91) of the installation box (94), and a pipe guiding ring (72), an upper holding bar ring (73), and a slide mechanism gear (109) are provided at appropriate positions on the installation side (92).

[0093] The semi-fixed part is the structure of the part where the honeycomb fuel tank (10), the pipe holding shaft (122), and the fuel pipe of the axial fuel main pipe (59) are connected.

[0094] The interactive movable part has a structure in which the upper outer wall (1) of the disk-shaped engine and the lower outer wall (2) of the disk-shaped engine are held by the disk-shaped engine guide ring (4) so as to be rotatable in one direction alternately.

[0095] The fixation at low speed is a structure from the fixed shaft (121) to the disk-shaped engine guide ring (4).

[0096] The restricted movable part at high speed is a structure from the rubber hose (21) to the disk-shaped engine guide ring (4).

[0097] The first ignition stroke is a structure in which the combustion chamber during compression is ignited by the first plug (146).

[0098] The second ignition stroke for enhancing operation is that the second cylinder (118) on the opposite side of the above-mentioned first ignition stroke and the second plug (147) secondarily ignite with the push bar (61) slightly separated. At this time, the commutator is switched and shifted slightly later.

[0099] The exhaust stroke is that due to the exhaust movable part which is an operation assist mechanism, the exhaust push head (131) and the exhaust slide switch bar (179) move the honeycombs (65) inside the guide ring from the exhaust movable hole (139) by the exhaust gas by several pieces from 4, and at the position where it has moved one-eighth, the honeycombs (65) inside each guide ring are exhausted to the outside through the exhaust hole formed by the ring rail side surface (190) for the upper outer wall of the disk-shaped engine or the ring rail side surface (191) for the lower outer wall of the disk-shaped engine and the exhaust passage (136) to the final exhaust hole (152).

[0100] The axial fuel branch pipe (13) and the rubber hose restricted operation stroke at high speed are such that due to the eccentric operation of the half gear double (95) and the upper and lower internal gears (22·24) of the disk-shaped engine and the restriction of the restricted movement of the disk-shaped engine guide ring (4), each axial fuel branch pipe (13) also draws a small circle regularly like drawing a small circle by the piping induction hole (76) so that the center draws a small circle.

[0101] During the operating stroke of the disc-shaped engine guide ring (4) at high speed, with respect to the outer walls (1, 2) of the upper and lower parts of the eccentrically-operating disc-shaped engine, due to the restricted movement of the disc-shaped engine guide ring (4), each honeycomb-shaped stopper ball (128) moves in a circular motion on the honeycomb-shaped stopper dance floor (113).

[0102] During the operating stroke of the standby of the disc holder bar (75) and the retractable guide bar (114) during eccentric operation at high speed, when the upper outer wall (1) of the disc-shaped engine is operating and rotating, the lower outer wall (2) of the disc-shaped engine is in a standby state. When the retractable guide bar (114) and the lower outer wall stopper bar (151) of the disc-shaped engine outer wall of the lower outer wall (2) of the disc-shaped engine rotate by one-quarter as shown in Fig. 25, it slides without transmitting rotation through the lower half holding gear part (96) of the one-half gear double (95) from the middle position of the retractable guide bar (114) to the inner tip, and this process is repeated for the next replacement.

[0103] At low speed, it comes under the upper outer wall stopper bar (150) of the upper outer wall (1) of the disc-shaped engine from the disc holder bar (75) without interference, and the retractable guide bar (114) is folded so that the disc-shaped engine guide ring (4) can be pushed downwards without interfering with the lower outer wall stopper bar (151) of the lower outer wall (2) of the disc-shaped engine.

[0104] The structure of the lifting part of the slide mechanism (242) is composed of a part fixed at an appropriate position on the side surface (92) by installing the outer ring (107) of the guide ring bearing of the guide ring shaft guiding part (126) on the outer circumference, and a part rotatably held on the upper part of the slide mechanism gear (109) of the guide ring shaft lifting guide ring (117). It rises to the honeycomb-shaped stopper dance floor (113) by rotating one-quarter to the left. The upper inner gear (22) of the disc-shaped engine comes to a meshing position with the upper part of the one-half gear double (95), and the lower inner gear (24) of the disc-shaped engine comes to a meshing position with the lower part of the one-half gear double (95). Also, it descends to the low-speed hold position (241) by rotating one-quarter to the right. The upper inner two-change gear (23) of the disc-shaped engine comes to a meshing position with the upper inner two-change receiving gear (197) of the shaft, and the lower inner two-change gear (25) of the disc-shaped engine comes to a meshing position with the lower inner two-change receiving gear (198) of the shaft.

[0105] The engagement of the entire self-standing four-gear disc-type engine is as follows: Place the semi-fixed part (10) on the disc receiving bearing pedestal (19) of the fully-fixed part. The part where the honeycomb fuel tank (10) is welded to the lower part of the axial fuel main pipe (59), the part where the operating shaft (54) is rotatably installed inside the fixed shaft (121), the bearing (213) at the lower part of the operating shaft (54), align the positions of the hexagonal lower part (216) above it, the two-way receiving gear (198) inside the lower part of the shaft, the hexagonal upper part (215), and the two-way receiving gear (197) inside the upper part of the shaft. Fit the part of the two-way gear (201) fitted in the center of the spring fixing part (200). The part actually fitted into the central shaft hole (85) at the lower part of the variable induction gear (84), which is actually a vertical hole but becomes the shaft hole (85) on the opposite side of the upper inclination. The part around it is the variable gear box (88) with each induction gear provided. The fixed part of the disc-type engine guide ring (4) at low speed, the structure part where the disc-type engine guide ring (4) for high-speed limited operation is connected to the axial fuel main pipe (59) from the axial fuel branch pipe (13) by a rubber hose (21). The upper movable ring groove (63) on the outer wall of the upper part of the disc-type engine and the upper rail (166) inside the ring of the disc-type engine guide ring (4), and the lower movable ring groove (64) on the outer wall of the lower part of the disc-type engine and the lower rail (167) inside the ring of the disc-type engine guide ring (4). The part rotatably fitted in one direction by the one-way gear (227) on the guide ring, the one-way gear (225) on the outer wall of the upper part of the disc-type engine, the one-way gear (226) on the outer wall of the lower part of the disc-type engine, and the one-way gear (228) under the guide ring. When the position of the play window (106) of the guide ring shaft of the slide mechanism (243) at low speed is at the low-speed hold position (241), the part held by its own weight between the outer upper part of the bearing (213), the internal gear (24) of the lower part of the disc-type engine on the outer wall of the lower part of the disc-type engine, and the vent hole (56). The part meshed with the upper half teeth (205) of the two-way gear of the two-way gear (23) inside the upper part of the disc-type engine and the two-way receiving gear (197) inside the upper part of the shaft, and also the part meshed with the upper half teeth (205) of the two-way gear of the two-way gear (25) inside the lower part of the disc-type engine and the two-way receiving gear (198) inside the lower part of the shaft. When the position of the play window (106) of the guide ring shaft of the slide mechanism (243) at high speed is at the honeycomb stopper dance floor (113),The structure consists of a state part where the disk - type engine doughnut piston part (154) is placed by its own weight on the honey - type stopper dance floor (113) in a state where the operation can be restricted by the honey - type stopper ball (128) of the honey - type stopper (129).

Industrial Applicability

[0106] The multi - purpose disk - type induction 4 - gear E - engine according to the present invention has the possibility of wide application ranging from a stirrer to large objects such as automobiles, engines, and machines, or small objects such as medical devices.

Explanation of Symbols

[0107] 1 Disk - type engine upper outer wall (PDOU4GE upper outer wall), 2 Disk - type engine lower outer wall (PDOU4GE lower outer wall), 3 Piston semi - circular ring, 4 Disk - type engine guide ring, 5 Upper piston wall, 6 Disk - type engine operation pipe part ratchet gear, 7 Switching ring bar, 8 Lower piston wall, 9 Propeller part gear, 10 Honey - type fuel tank, 11 Propeller relay gear (idle gear four), 12 Axial fuel pipe shaft, 13 Axial fuel branch pipe, 14 Inner - shaft axial wiring in the shaft, 15 Movable shaft gear, 16 Idle gear one (first holding gear), 17 Idle gear two (second holding gear). 18 Play gear three (third holding gear), 19 Disc receiving bearing pedestal, 20 Shaft, 21 Rubber hose, 22 Disc-shaped engine upper inner gear, 23 Disc-shaped engine upper inner two-change gear, 24 Disc-shaped engine lower inner gear, 25 Disc-shaped engine lower inner two-change gear, 26 For commutator plus 27 For commutator minus, 28 Brush for plus, 29 Brush for minus, 30 Wiring ring part receiver, 31 Disc-shaped engine upper outer wall intake hole, 32 Combustion chamber A1 (first combustion chamber), 33 Combustion chamber A2 (second combustion chamber), 34 Combustion chamber A3 (third combustion chamber), 35 Combustion chamber A4 (fourth combustion chamber), 36 Combustion chamber B1 (fifth combustion chamber), 37 Combustion chamber B2 (sixth combustion chamber), 38 Combustion chamber B3 (seventh combustion chamber), 39 Combustion chamber B4 (eighth combustion chamber), 40 Cooling movable fin, 41 Combustion chamber upper space, 42 Combustion chamber lower space, 43 Hexagonal shaft, 44 Movable lock holding bar, 45 Holding alternation switching part, 46 Exhaust holding bar, 47 Exhaust holding bar support, 48 Hollow part, 49 Outer ring connection groove, 50 Inner ring connection part, 51 Propeller, 52 Bearing balls for pedestal, 53 Pedestal bearing ring, 54 Operating shaft 55 Pipe shaft, 56 Vent hole, 57 First stopper head, 58 Second stopper head, 59 Axial fuel main pipe, 60 Piston ring semi-groove, 61 Extrusion bar (piston head firing pin), 62 Movable ring rail, 63 Upper movable ring groove, 64 Lower movable ring groove, 65 Guide ring inner spring, 66 Play gear two holding part, 67 Variable gear integrated shaft 68 Hexagonal shaft part, 69 Disc-shaped engine guide ring holding arm, 70 Multi-purpose disc-shaped U4E engine, Ring for the holding bar, 72 Ring for pipe guidance, 73 Upper holding bar ring, 74 Exhaust blowout hole, 75 Disk holding bar, 76 Pipe guidance hole, 77 Pipe guidance bar, 78 Pipe guidance holding ring, 79 Quarter transmission gear, 80 Quarter gear teeth, 81 Quarter holding gear part, 82 Upper quarter transmission gear, 83 Lower quarter transmission gear, 84 Variable induction gear, 85 Shaft hole, 86 Gear support, 87 Lower part of variable gear box, 88 Variable gear box, 89 Upper part of variable gear box, 90 Gear holding part, 91 Mounting bottom, 92 Mounting side, 93 Normal movable circle, 94 Mounting box (U4E black box), 95 Half gear double, 96 Half holding gear part, 97 Half transmission gear, 98 Upper half gear, 99 Lower half gear, 100 Disk-type engine guide ring shaft, 101 Vertical guide for the bearing of disk-type engine guide ring, 102 Guide ring bearing holding part, 103 Left-right alignment inclination, 104 Guide for guide ring shaft auxiliary, 105 Guide ball-type hole for guide ring shaft, 106 Play window for guide ring shaft, 107 Outer ring of guide ring bearing, 108 Inner ring of guide ring bearing, 109 Slide mechanism gear, 110 Slide inclination, 111 Slide stopper, 112 Return stopper, 113 Spring-type stopper dance floor, 114 Retractable guide bar, 115 Spring for retractable guide bar, 116 Guide body for guide ring shaft, 117 Guide ring for lifting and lowering of guide ring shaft, 118 Second cylinder, 119 Idler gear four-holder, 120 Idler gear four-spacer (pipe holding shaft spacer), 121 Fixed shaft, 122 Pipe holding shaft, 123 Pipe receiver for pipe holding shaft, 124 Eccentric movable circle, 125 Disk-type idle 4-gear PDO movable engine, 126 Guide part for guide ring shaft, 127 Exhaust valve, 128 Spring-type stopper ball, 129 Spring-type stopper, 130 Intake valve, 131 Exhaust extrusion head, 132 Intake extrusion head, 133 Exhaust valve hole, 134 Intake valve hole, 135 Spring for valve, 136 Exhaust passage, 137 Gear box shaft, 138 Guide mechanism part for guide ring shaft, 139 Exhaust movable hole, 140 Final exhaust port, 141 Intake hole for guide ring for upper part of disk-type engine, 142 Intake hole for guide ring for lower part of disk-type engine, 143Disc-shaped engine outer wall outer ring leakage prevention ring, 144 leakage prevention ring outer groove, 145 outer wall outer ring bearing ball, 146 first plug, 147 second plug, 148 firing pin receiver, 149 intake groove, 150 disc-shaped engine outer wall upper stopper bar, 151 disc-shaped engine outer wall lower stopper bar, 152 final exhaust hole, 153 pipe guiding ring groove, 154 disc-shaped engine donut piston part, 155 leakage prevention ring inner groove, 156 escape hole, 157 upper and lower cylinder covers, 158 disc gear holding part, 159 operating mechanism part receiver, 160 operating mechanism part, 161 outer ring rail, 162 disc-shaped engine outer wall inner ring leakage prevention ring, 163 outer wall inner ring bearing ball, 164 outer wall inner ring bearing groove 165 outer wall outer ring bearing groove, 166 ring inner upper rail, 167 ring inner lower rail, 177 disc-shaped engine lower outer wall intake hole, 178 intake slide switch bar, 179 exhaust slide switch bar, 180 intake and exhaust mechanism part structure, 181 pipe built-in shaft pipe, 182 external pipe, 183 disc-shaped engine guide ring shaft inner pipe, 184 intermediate exhaust port part, 185 inner spring rail hole, 186 piston wall groove, 187 inner ring rail, 188 guide ring operating mechanism part, 189 installation side wall, 190 disc-shaped engine upper outer wall ring rail side surface, 191 disc-shaped engine lower outer wall ring rail side surface, 192 ring inner upper rail upper side surface, 193 surface part that enters inside, 194 length of outer ring rail upper surface part, 195 part with the same length as the inner surface part of the outer ring rail, 196 length of guide ring inner cavity upper rail side side surface, 197 shaft upper inner 2 change receiving gear, 198 shaft lower inner 2 change receiving gear, 199 2 change gear spring, 200 spring fixing part, 201 2 change gear, 202 pipe holding shaft pipe fixing part, 203 idle gear four holder holes, 204 propeller gear fitting hole, 205 2 change gear upper half teeth, 206 inner circumferential side surface of disc-shaped engine guide ring, 207 outer circumferential side surface side of disc-shaped engine outer wall upper and lower outer ring rails, 208 eccentric point, 209 self-supporting disc-shaped idle 4 gear PDO movable engine, 210 2 change gear connection hole part, 211 2 change gear connection convex 212 Two-stroke gear spring part, 213 Bearing, 214 Hexagon, 215 Upper hexagon, 216 Lower hexagon, 217 Guide ring upward return prevention gear, 218 Guide ring downward return prevention gear, 219 Outer ring rail upward return prevention gear, 220 Outer ring rail downward return prevention gear, 221 A-one upper piston wall, 222 A-two upper piston walls, 223 A-three upper piston walls, 224 A-four upper piston walls, 225 Disc-type engine upper outer wall one-way gear, 226 Disc-type engine lower outer wall one-way gear, 227 Guide ring upper one-way gear, 228 Guide ring lower one-way gear, 229 Two-stroke intake and exhaust slide switch bar, 230 Two-stroke gear lower half teeth, 231 B-one lower piston wall, 232 B-two lower piston walls, 233 B-three lower piston walls, 234 B-four lower piston walls, 235 Cylinder inner skin outward-facing ring, 236 Cylinder inner skin inward-facing ring, 237 Disc-type engine upper outer wall cylinder inner skin inner side concave, 238 Disc-type engine upper outer wall cylinder inner skin outer side concave, 239 Disc-type engine lower outer wall cylinder inner skin inner side concave, 240 Disc-type engine lower outer wall cylinder inner skin outer side concave, 241 Low-speed hold position, 242 Slide mechanism, 243 Feather-type cooling fuel tank part, 244 Rotation extraction gear,

Claims

[Claim 1] The structure of the upper retaining bar ring (73) in Figure 4 is a ring hole that is one size larger than the disk-shaped engine guide ring (4), and the outer shape is a ring-shaped retaining bar ring (71) that can be fitted into the pipe guide ring groove (153) on the side of the installation base. Two disk retaining bars (75) are arranged facing each other, and the upper half gear double (95) and the disk-shaped engine upper inner gear (22), which are the shortest positions of eccentricity in the eccentric rotational motion, or the lower half gear double (95) and the disk-shaped engine lower inner gear (24), and the upper stopper bar (150) of the outer wall of the disk-shaped engine on the same side, or the lower half gear double (95) and the outer wall of the disk-shaped engine The structure of FIG. 3 is a part having a length in which the stopper bar (151) is located toward the center, and a piping guide ring (72). The structure of FIG. 3 is a part having a piping guide hole (76) near the tip of the piping guide bar (77) extending from the four inner sides of the piping guide holding ring (78) having the same shape as the holding bar ring (71), which is a hole for guiding each circular motion due to the eccentric limited rotation of the axial fuel branch pipe (13), and a part having an escape hole (156) that is a cut part for escape when the main body descends at low speed, and a guide ring shaft guide part (126). The structure of FIG. 1 is a part having an outer ring size of the above-mentioned holding bar ring (71). The inner side of the ring is the same as that of the outer ring (107) of the guide ring bearing, which has a hole one size larger than the eccentric circular motion orbit of the disc-type engine guide ring shaft (100). A guide ring bearing holder (102) is provided on the inner four sides of the outer ring (107) of the guide ring bearing, which has a through hole for the disc-type engine guide ring bearing vertical guide (101). The cylindrical part is held and fixed to the guide ring bearing holder (102). An extended through hole for the disc-type engine guide ring bearing vertical guide (101) is provided at a position above the middle of the cylindrical part, and the movable extension of the disc-type engine guide ring shaft (100) during eccentric limited rotation is A guide ring shaft play window (106) is provided in the extension range, and a guide ring shaft guide auxiliary (104) portion is provided with a quarter inner circle protrusion at the top of the guide ring shaft play window (106) to guide the circular motion of the blade-type stopper (129) during eccentric limited rotation, and a portion is provided with the same horizontal quarter inner circle protrusion as above at the bottom of the guide ring shaft play window (106), and a left-right shifting inclination (103) with a vertical semicircular inclination is provided to move the left-right distortion to the center at the low-speed movable position, and further, a quarter ball inner hole guide ring shaft guide ball type hole (105) is provided as an extension of this to correct the front-to-back misalignment,The guide ring shaft guide part (126) structure part has a guide ring bearing inner ring (108) in the center, which is composed of each guide part for returning the circular range of low speed movement, and the guide ring shaft lift guide ring (117). The structure of Figure 2 is as follows: First, the guide ring shaft guide body (116) is rotatably accommodated inside each guide protrusion part (104, 105) of the guide ring bearing inner ring (108), and the inside is the disc-shaped engine upper and lower outer walls (1, 2) and the disc-shaped engine guide ring (4) combined with the disc-shaped engine donut piston part (154). The slide mechanism gear (109) is a gear with a hole in the bottom of a low cylindrical shape with a space in the range, and the protrusions of the slide stopper (111) are provided on all four sides of the top, and a blade-type stopper landing (113) is provided, which is the space for the eccentric rotational motion range of the blade-type stopper (129). Immediately next to it is a return stopper (121) with a structure in which the protrusions protrude with a spring, and immediately next to it is a slide incline (110) for ascending and descending, and a bottom for a low speed position is provided, and at this time, the height of the blade-type stopper (129) is below the next slide stopper (111). The structure of FIG. 34 is a part in which a normally movable circle (93) and its center normally movable point (209) are connected to the eccentric point (208) to form an eccentric movable circle (124) on the outer periphery of the idler gear (18). The part is the mounting bottom (91), and the cylindrical side of the mounting side is connected to the outer periphery of the idler gear (18). (92) is provided, and a hole for the shaft is provided at the bottom of the cylindrical tea canister shape, and a pipe guide ring (72), an upper holding bar ring (73), and a guide ring shaft guide mechanism (138) are arranged and fixed at appropriate positions from above, to form an installation box (94) ASSY having a structure that incorporates a self-supporting disk-type 4-gear PDO movable engine (209), and a disk support bearing base (19) for the fuel tank (Figures 32 and 42.The structure of the ring-shaped upper inner surface is such that the corners of the upper inner surface are cut down to near the bottom, and a round recess is provided between the inside and outside of the surface, which becomes the base bearing ring (53).The disk bearing base (19) ASSY has a structure in which a ball-shaped base bearing ball (52) one size smaller than the recess is rotatably fitted in three to several tens of places around the circumference, and the fuel tank Fig. 32 and 42 has a hollow structure just one size smaller than the center of the thick fan blades, with two to several tens of blade-shaped cooling fuel tank parts (213) around the circumference, which are the hollow parts of each blade. The blade-type fuel tank (10) ASSY has a structure in which the axial main fuel pipe (59) is installed at the top center, and the structure of the axial main fuel pipe (59) Fig. 38 is a piping from the blade-type fuel tank (10) to the shaft. The structure of the variable gear box (88) from the upper half gear double (95) to the piping distribution section on all four sides, the piping support shaft (122) (Figure 38) is a part of the structure consisting of a pipe support shaft (123) with a cross groove on the upper side of the pipe material with a hole for the axial fuel main pipe (59) and the axial wire (14) in the shaft, the axial wire (14) in the shaft is wired from under the guide ring shaft lift guide ring (117) to the installation side along the axial fuel main pipe (59), and the idle gear spacer (120) (Figure 48) is a cylindrical lower part with a protrusion on the outer circumference on all four sides, The fixed part (202), the idle gear 4 holder hole (203) of the idle gear 4 holder (119) receiving part is fixed, and the propeller part gear (9) is fixed on top of it. The half gear double (95) is a part with a cylindrical half, and the half holding gear part (96) with no gear teeth and the half transmission gear (97) with teeth are fixed to the lower half gear (99) with two lower half gears (99) shifted so that the teeth do not overlap. The fixed shaft (121) is a part with a hole for rotatably holding the piping holding shaft (122). The piping holding shaft (122) is fixed to the piping holding shaft (122). the movable shaft (54) has a structure in which a movable shaft gear (15) is connected to the upper part of a half gear double (95), a tubular shaft (55) is connected to the lower part of the half gear double (95), and a hexagonal upper and lower parts (215, 216) in the shape of nuts are provided at the lower part of the movable shaft (54) ASSY; the piping-integrated shaft pipe (181) has a structure in which a fixed shaft (121) is rotatably incorporated in a through hole of the movable shaft (54) ASSY;The movable shaft gear (15) in Figure 21 is a part with a hole that fits into the pipe shaft (55), and the idle gear (11) in Figure 21 has a dumbbell silhouette with the gears connected by a shaft. The upper gear engages with the propeller gear (9) attached to the bottom of the propeller (51), and the lower gear engages with the movable shaft gear (15), transmitting rotation. The idle gear holder (119) is fitted between the gears so that they can rotate on the shaft. The idle gear holder (119) on the opposite side is fixed to the pipe holding shaft (122) with the idle gear spacer (120), and the propeller is attached to the top. The structure of the idler gears 1 and 2 (16 and 17) in Fig. 21 is a gear with a smaller diameter than the idler gear 3 (18), and the first and second are the same, with the name being derived from the difference in the location of the attachment part. The structure of the idler gear 3 (18) in Fig. 21 is a cylindrical part that is provided for stable support of the upper and lower internal gears (22 and 24) of the disk-shaped engine. The shape of the variable induction gear (84) in Fig. 35 is a right-angled triangular shape of the two alternating gear upper half teeth (205) of the shaft upper internal two alternating receiving gear (197) with teeth in the shape of a right-angled isosceles triangle around it. The inner peripheral end gear teeth of the variable induction gear (84) of the oblique cylindrical shape, which has a radius of the half gear double (95) from the bottom of the central shaft hole (85) to the upper central axis, and the outer peripheral gear teeth and the half gear double (95) are provided at both ends and shifted by the interval of the non-contact central axis, which is the interval where they do not mesh, are fixed in line with the gear teeth of the half gear double (95). This part is the vertical rotating part at high speed of the half gear double (95), and this is the axis around which the limited operation disc-type engine guide ring (4) and the upper and lower outer walls (1, 2) of the disc-type engine are parts with a structure that can rotate eccentrically in an alternating manner. The structure of the two-shift gear (201) ASSY (Figure 44) is as follows: first, a two-shift gear spring (212) is provided with a two-shift gear connection hole (210) in the shape of a hexagonal column at the top and bottom of the center of a disk-shaped plate, and a two-shift gear spring (199) is set above and below the spring fixing part (200); next, a part with right-angled triangular gear teeth on all four sides of the outer periphery of a shallow cylindrical lid, and a two-shift gear connection protrusion (211) in the shape of a hexagonal column, which is slightly larger than the two-shift gear connection hole (210), is provided at the center of the inside of this part. This makes up two-shift receiving gears (197, 198) in the upper and lower parts of the disk-shaped engine.The two-shift gear (201) ASSY, which is fitted to the two-shift gear connection protrusion (211) of the two-shift receiving gear (197, 198) in the upper and lower parts of the disk-shaped engine in an expandable manner to the two-shift gear connection hole part (210) of the two-shift gear spring part (212) set earlier, and the variable gear box (88) ASSY (Figure 21) has a structure in which the bearing (213) is attached to the lower part of the moving shaft (54), and the two-shift gear connection hole (210) is engaged with the upper and lower hexagonal parts (215, 216) at the upper part, the variable induction gear (84) is fixed to the upper part, the half gear double (95) is attached to the upper part, and the movable shaft gear (15) is attached to the lower part. The variable induction gear (84) is fixed, and the variable induction gear (84) has a portion on the opposite side of the upper half gear double (95) on which the idler gear 3 (18) is rotatably arranged, the idler gear 1 (16) on the left side, and the idler gear 2 (17) on the right side. The idler gear 4 holder (119) is fitted into the idler gear 4 holder hole (203) of the idler gear 4 spacer (120) on the fixed shaft (121) of the shaft fixing portion. The propeller part gear (9) is rotatably fitted into the upper part of the idler gear 4 spacer (120). The movable shaft gear (15) and the lower part of the propeller relay gear (11) are engaged, and the upper part of the propeller relay gear (11) and the propeller relay gear (11) are engaged. The variable gear box (88) ASSY consisting of the part that meshes with the propeller gear (9), and the structure of the center of the front side of the upper and lower outer walls (1, 2) of the disk-shaped engine are as follows: the part where the cake batter of the angel cake type is placed is semicircular, or the flat part from the central hole of the upper and lower cylinder covers (157) cut horizontally leaving a hollow donut-shaped hole to the inner recess is the disk gear holding part (158), and on all four sides there are provided ventilation holes (56) for passing the air flow from the cooling movable fins (40). Furthermore, the disk-shaped engine upper and lower inner gears (22, The structure of the cooling movable fins (40) on the outer periphery of the cylinder on the front side of the outer wall of the upper and lower disc-type engine (1 and 2) is such that the fins are angled from the outer gears (23 and 25) to the inner gears (22 and 24) and have one to several dozen crescent shapes on the outer periphery of a semicircle larger than the donut semicircle of the outer wall of the upper disc-type engine (1), and the air flow is drawn in to the center,A structural part in which air flows from the center to the side by the movable cooling fins (40) on the lower outer wall (2) of the disk-shaped engine on the opposite side, and then the outer circular structure on the front side of the upper and lower outer walls (1, 2) of the disk-shaped engine, which includes the operating mechanism receiver (159), the upper and lower stopper bars (150, 151) of the outer wall of the disk-shaped engine, the intake and exhaust push-out heads (132, 131), the commutator (28, 29), the first and second stopper heads (57, 58), the upper and lower movable ring grooves (63, 64), and the disk-shaped engine in the shape of a gently sloping right-angled triangular prism laid down at the bottom of the upper and lower movable ring grooves (63, 64); The structure of the upper and lower outer wall one-way gears (225, 226), the ring rail (161), the exhaust movable hole (139), and the exhaust passage (136), and the upper and lower stopper bars (150, 151) on the outer inclined part of the disk when the operating mechanism receiver (159) is moving at high speed, are cylindrical bars provided midway on the outer inclination of the upper and lower outer walls (1, 2) of the disk-type engine, and the upper outer wall (1) of the disk-type engine is a disk holding bar (75), and the lower outer wall (2) of the disk-type engine is a retractable guide bar (114), which alternately create a movable standby state. The position of the intake and exhaust push heads (132, 131) on the operating mechanism receiver (159) is a part where the intake push head (132) is provided on the left side and the exhaust push head (131) is provided on the right side under the upper and lower stopper bars (150, 151) on the outer wall of the disk-shaped engine. The position of the commutators (28, 29) on the operating mechanism receiver (159) is a structural part where a positive brush (28) is provided on the upper left and a negative brush (29) is provided on the lower right between the lower parts of the intake and exhaust push heads (132, 131). The ignition plug for the second plug (147) is The part located slightly to the left, the structure of the first and second stopper heads (57, 58) of the operating mechanism receiver (159) is a structure with an inclined part on the left side of the block shape, the part located on the outer lower part of the commutator part (28, 29), each operating mechanism receiver (159) is on the outer four sides of the circle on the front side of the upper outer wall of the disc-type engine (1), the lower outer wall of the disc-type engine (2) is inverted, and the structure of the upper and lower movable ring grooves (63, 64) in Figure 28 is that the upper movable ring groove (63) is attached to the inner upper rail (166) of the disc-type engine guide ring (4), and the lower movable The movable ring groove (64) is a structural portion for being rotatably fitted into the inner ring lower rail (167), and the structure of the ring rail (161) is such that the upper and lower movable ring grooves (63, 64) prevent the side guards from falling off, and the exhaust passage (136) is formed by cutting out the curved side surface vertically from each operating mechanism receiver (159) to the vicinity of the exhaust push-out head (131), and the exhaust passage (136) is formed by cutting out the shape of the ring rail (161) of the inner flange ring rail hole (185) of the guide ring inner flange (65) described below, which becomes the intermediate exhaust port portion (184),Furthermore, the exhaust flow extends from the exhaust valve hole (133) of each operating mechanism receiver (159) to the final exhaust hole (152) located at the lower right near the axial fuel branch pipe (13) of the disc-shaped engine guide ring (4), and the structure of the exhaust movable hole (139) is a structural part located at the outer lower side of the ring rail (161), and the exhaust movable hole is moved by 1 / 3 of a 1 / 4 rotation in one stroke during the first half of the movement, and when exhausting, several dozen blades are moved from the guide ring inner blade (65) 3 of the disc-shaped engine guide ring (4), and from the position where the upper and lower outer walls (1) of the disc-shaped engine move, the exhaust flows from the ring rail (161) to the position where the upper and lower outer walls of the disc-shaped engine move. The exhaust passage (136) is switched to the inner flange rail hole (185) of the guide ring inner flange (65), and the intermediate exhaust port (184) is formed, and the exhaust is exhausted from the final exhaust hole (152) in the latter half of the exhaust. The outer ring leakage prevention ring (143) of the outer wall of the disk-type engine, which is a circular outer structure inside the upper and lower outer walls (1 and 2) of the disk-type engine, is installed between the leakage prevention ring outer grooves (144) of the upper outer wall (1) of the disk-type engine and the lower outer wall (2) of the disk-type engine, to prevent leakage from the outside and to prevent misalignment. The leakage prevention ring outer groove (144) is installed between the upper and lower outer walls of the disk-type engine. The disk-shaped engine outer wall outer ring leak prevention ring (143) installation hole portion provided on the inside and outside of the outer wall (1, 2), the outer wall outer ring bearing groove (165) of the upper and lower outer walls (1, 2) of the disk-shaped engine provided on the lower circumference inside the ring rail (161) for the disk shape, the outer wall outer ring bearing ball (145) is installed between the outer wall outer ring bearing grooves (165) of the upper and lower outer walls (1, 2) of the disk-shaped engine so that it can rotate and move, and the piston semicircular ring (3) around the combustion chamber inside the upper and lower outer walls (1, 2) of the disk-shaped engine has the same structure as a piston ring, and is inserted into the piston ring half groove (60) of the upper and lower outer walls (1, 2) of the disk-shaped engine as shown in Figure 39. The structure of the upper and lower piston walls (5, 8) is a thick disc shape, fitted into a groove on its outer circumference, and fitted and welded to the piston wall groove (186) and the piston ring half groove (60) provided on the four inner sides of the upper and lower outer walls (1, 2) of the disc-type engine. The structure of the push-out bar (61) is a banana-like curved part along the combustion chamber in the center left of the upper piston wall (5) seen from the inside of the upper outer wall (1) of the disc-type engine, with a rounded tip. The structure of the second cylinder (118) is one size larger than the push-out bar (61),The inner circumferential surface is in the shape of a banana tube, with an intake groove (149) of a grooved portion without a groove as it goes deeper from the top of the cylinder to the bottom, and the center of the bottom is provided with a firing pin receiver (148), a first plug (146) adjacent to it near the outer periphery, and a second plug (147) near the outer periphery of the second cylinder (118). The inner leakage prevention ring (162) of the outer wall of the disk-type engine, which is structured on the inner center side of the upper and lower outer walls of the disk-type engine (1, 2), is installed between the leakage prevention ring inner grooves (155) of the upper outer wall of the disk-type engine (1) and the lower outer wall of the disk-type engine (2), and is structured to prevent leakage on the inside and to prevent misalignment. The structure of the lower outer wall of the disc-type engine (2) is a disc-type engine lower outer wall (2) ASSY having an inverted arrangement structure of the upper outer wall of the disc-type engine (1) and a disc-type engine lower outer wall (2) ASSY having an inverted arrangement structure of the upper outer wall of the disc-type engine (1). The structure of the lower outer wall of the disc-type engine (2) is a disc-type engine lower outer wall (2) ASSY having an inverted arrangement structure of the upper outer wall of the disc-type engine (1). The structure of the lower outer wall of the disc-type engine (2) is a disc-type engine lower outer wall (2) ASSY having an inverted arrangement structure of the upper outer wall of the disc-type engine (1). The guide ring (4) shown in Figs. 12, 13 and 14 has a ring shape with a rounded outer circumference and a hollow inner circumference. The ring inner upper rail (166) of the protruding inner circumference is formed by an upper side surface (192) of the ring inner upper rail (166) having the same length as the inner ring rail (187) portion, a surface portion (193) that is recessed inward and has approximately the same length as the upper movable ring groove (63), a portion (195) having the same length as the inner surface portion of the outer ring rail (161), the length (194) of the upper surface portion of the outer ring rail (161), and the length (196) of the side surface side of the upper rail of the hollow inside the guide ring. ), a portion consisting of an inner ring lower rail (167) provided at the bottom, a portion having a structure in which right-angled triangular gear teeth are provided on the convex surfaces of the inner ring upper and lower rails (166, 167) and which meshes with the upper and lower outer wall one-way gears (225, 226) of the disk-shaped engine to prevent reverse movement, and a portion which becomes a blade-shaped stopper (129) which is a blade-shaped protrusion provided on the side of the disk-shaped engine guide ring (4) on the guide ring operating mechanism part (188) side and has a blade-shaped stopper ball (128) which is a ball roller for movement and is installed so that its head protrudes from the outside of the lower part of the blade-shaped stopper (129).The blade-type stopper (129) ASSY is composed of a portion provided with a cylindrical bar-shaped disk-type engine guide ring shaft (100) provided at the center height of the disk-type engine guide ring (4) on the outer side of the blade-type stopper (129), and the axial fuel branch pipe (13) has a structure that extends upward from the middle position of each guide ring operating mechanism part (188) of the disk-type engine guide ring (4), bends in an L shape at approximately the same height as the axial fuel main pipe (59), and is connected to the axial fuel main pipe (59) by a rubber hose (21), and the guide ring operating mechanism parts (188) provided on the four sides of the disk-type engine guide ring (4) are provided with a cylindrical bar-shaped disk-type engine guide ring shaft (100). The brush section of the mechanism section (188) is structured such that the left side of the brush for plus (28) is long and the right side of the brush for minus (29) is short, located on the upper inside of the disc-shaped engine guide ring (4), and the commutator for plus (26) and the brush for plus (28), the commutator for minus (27) and the brush for minus (29) are arranged at an appropriate angle to allow sliding contact. The structure of the switching ring bar (7) is structured such that the claws at both ends of the bar shape allow the first and second locks to be used for the expansion standby state and the upper and lower piston walls (5, 8) and the return prevention mechanism for the expansion receiver, and the push-out bar (61) is used. The structure of the mechanism and the guide ring inner blade (65) that are replaced is such that three to several tens of pieces are provided on the inner circumferential surface of the disc-shaped engine guide ring (4) between one-eighth of the guide ring operating mechanism (188), and the shape of the guide ring is a plate-shaped part that connects the inner circumferential side surface (206) of the disc-shaped engine guide ring in FIG. 45 and the outer circumferential side surface (207) of the upper and lower outer ring rails of the outer wall of the disc-shaped engine, and the guide ring inner blade (65), the side surface of the ring rail for the upper outer wall of the disc-shaped engine (190) or the side surface of the ring rail for the lower outer wall of the disc-shaped engine (191), and the radius of the ring rail (161). The exhaust passage (136) formed from the cross section becomes the guide ring inner flap exhaust hole (62), the final exhaust hole (152) becomes the final exhaust part provided at the bottom on the right side of the guide ring operating mechanism part (188) of the disc-shaped engine guide ring (4), the guide ring operating mechanism part (188) at the top of the disc-shaped engine guide ring (4) has a lower inverted arrangement structure except for the axial fuel branch pipe (13), and the structure of the guide ring shaft guide mechanism part (138) ASSY Figures 11 and 16 is a structural part in which the guide ring shaft lift guide ring (117) is built into the guide ring shaft guide part (126),The above-mentioned two-shift gear (201) (197, 198) always moves in a fixed direction when operating at low speed, but the upper inner 2-shift gear (23) of the disk-shaped engine and the lower inner 2-shift gear (25) of the disk-shaped engine are in front of the rotation direction, followed by the upper inner 2-shift receiving gear (197) of the shaft, and behind that, the lower inner 2-shift receiving gear (198) of the shaft. When the upper inner 2-shift receiving gear (197) is operating, the upper inner 2-shift gear (23) of the disk-shaped engine and the lower inner 2-shift gear (25) of the disk-shaped engine rotate together by 85°, and the lower inner 2-shift receiving gear of the shaft waiting to operate at the remaining 5°. The inclination of the gear teeth of the disk-shaped engine lower inner 2 shift gear (25) (198) causes the disk-shaped engine upper inner 2 shift gear (23) and the disk-shaped engine lower inner 2 shift gear (25) to overtake, and the next operation becomes the shaft lower inner 2 shift receiving gear (198). This repeats the mechanism part that transmits rotation to the shaft alternately, and the structure of the disk-shaped 4-gear PDO movable engine fixed part is the blade-shaped fuel tank (10) part that is installed so that the disk receiving bearing base (19) fixed to the installation bottom (91) can be placed on it, and the blade-shaped fuel tank (1 The structure of the semi-fixed limited movable part during high speed operation of the disk-shaped 4-gear PDO movable engine is the structure from the rubber hose (21) fitted to the tip of the axial main fuel pipe (59) to the disk-shaped engine guide ring (4) fitted to the axial fuel branch pipe (13), which is the fixed part during low speed operation. The exhaust mechanism part (181) is the exhaust pipe and the exhaust slide switch bar (179), and the exhaust push-out head (131) is inclined downward from the left side. The structural part is the same except for the part where the upper and lower outer walls of the disk-shaped engine are provided, and the structural part is made up of the piping inside the upper and lower outer walls of the disk-shaped engine (1 and 2) from the upper outer wall intake hole (31 and 177) of the disk-shaped engine in Figure 46 to the lower part of the intake valve hole (134), and the part where the tip of the above-mentioned axial fuel main pipe (59) and the axial fuel branch pipe (13) are connected with a rubber hose (21), and the piping branches out from the base of the curve at the top of the outer periphery of the disk-shaped engine guide ring (4) to the top and bottom of the disk-shaped engine guide ring (4) as shown in Figure 29, and from each position, the piping extends around the center to the left, and the upper part is,The lower part of the guide ring intake hole (141) for the upper part of the disk-shaped engine is connected to the guide ring intake hole (142) for the lower part of the disk-shaped engine, and the structural part of the intake mechanism part (180) is an intake valve hole (134) part consisting of a hole in which the valve spring (135) can be inserted from the outside in an expandable manner at an appropriate position of the operating mechanism part receiver (159) provided on the four sides of the outer walls of the upper and lower parts of the disk-shaped engine (1, 2), a small hole in the middle where the valve bar can slide, and a hole that is widened from the position just below to the combustion chamber, and a hole of a size large enough to hide the intake valve (130) at the lower part, and an intake push-out head (, The intake valve (132) has an inclined portion at the top left side, which is turned on by the intake slide switch bar (178) to open the intake valve (130), and then on the outside, the intake push head (132) is connected to the top of the intake valve hole (134), and the valve bar is connected from the bottom of the intake push head (132), and from above the valve bar, the valve spring (135) is held in a slidable manner in the middle hole of the intake valve hole (134), and the intake valve (130) is fixed to the tip of the valve bar with a gap between the bottom of the intake hole, and the airtight structure of the cylinder part is as follows: First, the outer peripheral airtight part of the disk-type engine upper outer wall (1) in Figure 53, the outer wall outer A portion in which a cylinder inner skin outward ring (235) is fitted between a cylinder inner skin outer recess (238) of the upper outer wall of the disk-type engine having a recessed groove portion on the inner combustion chamber side of the outer wall outer ring bearing groove (165) of the disk-type engine lower outer wall (2) and a cylinder inner skin outer recess (240) of the lower outer wall of the disk-type engine having a recessed groove portion on the inner combustion chamber side of the outer wall outer ring bearing groove (165) of the lower outer wall of the disk-type engine (2), a cylinder inner skin inner recess (237) of the upper outer wall of the disk-type engine having a recessed groove portion on the inner combustion chamber side of the outer wall inner ring bearing groove (164) of the upper outer wall of the disk-type engine (1), and a cylinder inner skin outer recess (237) of the lower outer wall of the disk-type engine having a recessed groove portion on the inner combustion chamber side of the outer wall inner ring bearing groove (164) of the outer wall of the disk-type engine A portion where the cylinder inner skin inward ring (236) is fitted between the cylinder inner skin inner concave (239) of the lower outer wall of the disk-type engine, which has a recessed groove portion on the inner combustion chamber side of the bearing groove (164), the upper piston wall (5) of the upper outer wall of the disk-type engine and the piston semicircular ring (3) portion, the double ring contact portion of the outward root of the piston semicircular ring (3) of the upper piston wall (5) and the cylinder inner skin outward ring (235), the inward root of the piston semicircular ring (3) of the upper piston wall (5) and the double ring contact portion of the cylinder inner skin inward ring (236), The upper outer wall (1) of the disk-type engine, the lower part of each lower piston wall (8) and the piston semicircular ring (3), the outward root of the piston semicircular ring (3) of the lower piston wall (8) and the double ring contact part of the cylinder inner skin outward ring (235), the inward root of the piston semicircular ring (3) of the lower piston wall (8) and the double ring contact part of the cylinder inner skin inward ring (236) are the inner circumference of each engagement disk, which becomes the airtight part of each combustion chamber, and the structure of the intake slide switch bar (178) is located to the right of the exhaust slide switch bar (179) in the intake stroke standby state,The structure of the exhaust section is that the bar that holds the exhaust push head (131) in the moving range in the exhaust section is the exhaust slide switch bar (179), and the opposite and reverse mirror surfaces are arranged. The shaft operating stroke at high speed is that the idle gear 1 (16), idle gear 2 (17), and idle gear 3 (18) of the upper part of the variable gear box (89) are idling with the rotation stabilization mechanism, and when the upper part of the half gear double (95) and the disk-shaped engine upper internal gear (22) are operating, the two The half-gear double (95) transmits rotation through a half-transmission gear (97), and at the same time, the upper part is eccentrically moved by the upper retaining barring (73) and the upper stopper bar (150) of the outer wall of the disk-shaped engine on the upper outer wall of the disk-shaped engine (1), and the retractable guide bar (114) and the lower stopper bar (151) of the outer wall of the disk-shaped engine on the lower outer wall of the disk-shaped engine (2), creating a state where the disk-shaped engine is not moving from (4). The inner half-gear double (95) lower half-retaining gear part (96) does not transmit rotation and spins freely, and in the next process it transmits rotation in the opposite direction, alternating between these two. In the first stroke A of FIG. 6, the A1 combustion chamber (32) starts expanding due to the first ignition, the A2 combustion chamber (33) exhausts, the A3 combustion chamber (34) intakes, the A4 combustion chamber (35) compresses, the B1 combustion chamber (36) operates midway due to the second ignition, the B2 combustion chamber (37) exhausts, the B3 combustion chamber (38) intakes, the B4 combustion chamber (39) compresses, and each exhaust is in an exhaust operating state. Next, in the first stroke B, the operation is in progress, and next, in the first stroke C, the A1 combustion chamber (32) and the B1 combustion chamber (36) are in an expansion operating state with the push bar (61), the A2 combustion chamber (33) and the front of the B2 combustion chamber (37) The firing pin receiver (148) of the variable gear box is pushed, and the force of the force moves the first stopper head (57) of the lower outer wall (2) of the disk-shaped engine from the return prevention part on the left side of the switching ring bar (7) to the standby claw on the right side, where it maintains its fixed position and switches between standby and operating states. This process returns to step A in FIG. 6 and is repeated eight times, making two revolutions, with the upper and lower outer walls (1 and 2) of the disk-shaped engine each making one rotation and the shaft making four rotations. During the high-speed shaft operation process, the idler gears 1 (16), 2 (17) and 3 (18) of the upper part of the variable gear box (89) are idled by the rotation stabilization mechanism.When the upper half-gear double (95) and the upper inner gear of the disk-type engine (22) are in operation, the upper half-gear double (95) transmits rotation through the half-transmission gear (97). At that time, the upper half is eccentrically moved by the upper retaining barring (73) and the upper stopper bar (150) of the outer wall of the disk-type engine (1), the retractable guide bar (114) and the lower stopper bar (151) of the outer wall of the disk-type engine (2), and the lower inner gear of the disk-type engine (4) is not moving. A (24) is the lower half holding gear part (96) of the half gear double (95), which rotates idly without transmitting rotation, and in the next process transmits rotation in the opposite direction, and these parts operate alternately. The completely fixed part is a structural part in which the disk receiving bearing base (19) is provided on the mounting bottom part (91) of the mounting box (94), and the piping guide ring (72), the upper holding bar ring (73), and the slide mechanism gear (109) are provided at appropriate positions on the mounting side (92). The semi-fixed part is the blade-type fuel tank (10), the piping holding shaft (122), and the axial fuel tank. The structural part of the part where the fuel main pipe (59) is connected to the fuel pipe, the alternating movable part is a structural part that holds the disk-shaped engine upper outer wall (1) and the disk-shaped engine lower outer wall (2) by the disk-shaped engine guide ring (4) so ​​that they can rotate alternately in one direction, the fixed part at low speed is a structural part from the fixed shaft (121) to the disk-shaped engine guide ring (4), the limited movable part at high speed is a structural part from the rubber hose (21) to the disk-shaped engine guide ring (4), and the first ignition stroke is a first plug (146) that ignites the combustion chamber at the time of compression. The structural part and the second ignition stroke for enhanced operation are performed by the second plug (147) performing the second ignition with the second cylinder (118) on the opposite side of the first ignition stroke and the push bar (61) slightly separated, and the commutator at this time is switched and shifted slightly later. The structural part and the exhaust stroke are performed by the exhaust push head (131) and the exhaust slide switch bar (179) for the exhaust movement, which is an operation assistance mechanism, and the exhaust gas moves four or several inner blades (65) of the guide ring from the exhaust movable hole (139),A structural part that exhausts the exhaust from the exhaust hole formed by the side surface (190) of the ring rail for the upper outer wall of the disk-type engine or the side surface (191) of the ring rail for the lower outer wall of the disk-type engine of each guide ring inner blade (65) and the exhaust passage (136) to the final exhaust hole (152) at the 1 / 8th movement position, and the axial fuel branch pipe (13) and the rubber hose limited operation stroke at high speed are the structural part that each axial fuel branch pipe (13) also draws small circles regularly by the piping guide hole (76) so that the center draws a small circle due to the eccentric operation of the half gear double (95) and the disk-type engine upper and lower inner gears (22, 24) and the limited movement of the disk-type engine guide ring (4), and the circle at high speed The operation process of the disc-type engine guide ring (4) is as follows: With respect to the eccentrically operated upper and lower outer walls of the disc-type engine (1, 2), the disc-type engine guide ring (4) is limited in movement, and each blade-type stopper ball (128) moves in a circular motion on the blade-type stopper landing (113). During eccentric operation at high speed, the standby operation process of the disc retaining bar (75) and the retractable guide bar (114) is as follows: When the upper outer wall of the disc-type engine (1) is rotating, the lower outer wall of the disc-type engine (2) is in a standby state, and the retractable guide bar (114) and the lower stopper bar (151) of the disc-type engine outer wall of the disc-type engine (2) rotate in a quarter turn as shown in Figure 25. The retractable guide bar (114) moves from the middle position to the inner end as if it is coming out, and slides without transmitting rotation to the lower half holding gear part (96) of the half gear double (95), and the next exchange is repeated. At low speeds, the retractable guide bar (114) is folded up so that it comes under the upper stopper bar (150) of the disk-shaped engine outer wall of the disk-shaped engine upper outer wall (1) from the disk holding bar (75) and does not interfere, and the disk-shaped engine guide ring (4) goes down and pushes it aside, and the retractable guide bar (114) is folded up and comes under the lower outer wall of the disk-shaped engine (2). The structure of the lifting part of the slide mechanism (242) is such that the outer circumference of the guide ring bearing outer ring (107) of the guide ring shaft guiding part (126) is fixed at an appropriate position on the installation side (92), and the guide ring shaft lifting guide ring (117) is rotatably held on the upper part of the slide mechanism gear (109), and goes up to the blade-type stopper landing (113) with a quarter left turn, and the upper internal gear (22) of the disc-type engine is connected to the upper part of the half gear double (95),The lower inner gear (24) of the disk-type engine comes to a position where it meshes with the lower part of the half-gear double (95), and then descends to the low-speed hold position (241) with a quarter turn to the right. The upper inner 2 shift gear (23) of the disk-type engine comes to a position where it meshes with the upper inner 2 shift receiving gear (197) of the shaft, and the lower inner 2 shift gear (25) of the disk-type engine comes to a position where it meshes with the lower inner 2 shift receiving gear (198) of the shaft. The engagement of the entire independent 4-gear disk-type engine is carried out by placing the semi-fixed part (10) on the completely fixed part of the disk receiving bearing base (19), and connecting the blade-type fuel tank (10) and the axial fuel tank. The part where the lower part of the main pipe (59) is welded, the part where the movable shaft (54) is rotatably mounted on the fixed shaft (121), the bearing (213) at the lower part of the movable shaft (54), the part where the lower hexagonal part (216) above it, the two-shift gear (198) in the lower part of the shaft, the upper hexagonal part (215) and the two-shift gear (197) in the upper part of the shaft are aligned to form the two-shift gear (201) fitted in the center of the spring fixing part (200), and the part where the central shaft hole (85) at the lower part of the variable induction gear (84) is actually a vertical hole, but the upper part is tilted to become the shaft hole (85) on the opposite side. a variable gear box (88) part with various induction gears around it; a fixed part of the disc-shaped engine guide ring (4) at low speeds, a structural part connecting the disc-shaped engine guide ring (4) operating at limited speeds and the axial fuel branch pipe (13) to the axial fuel main pipe (59) with a rubber hose (21); an upper movable ring groove (63) of the upper outer wall (1) of the disc-shaped engine and the upper rail (166) inside the ring of the disc-shaped engine guide ring (4), and a lower movable ring groove (64) of the lower outer wall (2) of the disc-shaped engine and the lower rail (166) inside the ring of the disc-shaped engine guide ring (4). a portion rotatably fitted to the rail (167) by the guide ring upper one-way gear (227), the disk-type engine upper outer wall one-way gear (225), the disk-type engine lower outer wall one-way gear (226), and the guide ring lower one-way gear (228), and a portion held by its own weight between the outer upper part of the bearing (213) and the disk-type engine lower inner gear (24) and the ventilation hole (56) of the disk-type engine lower outer wall (2) when the position of the guide ring shaft play window (106) of the slide mechanism (243) during low speed is in the low speed hold position (241);A structural part consisting of a part meshed with the upper half teeth (205) of the disc-type engine upper inner 2-shift gear (23) and the upper inner 2-shift receiving gear (197) of the shaft and with the upper half teeth (205) of the disc-type engine lower inner 2-shift gear (25) and the lower inner 2-shift receiving gear (198) of the shaft, and a part in which the disc-type engine donut piston part (154) is placed on the blade-type stopper landing (113) by its own weight so that it can be operated limitedly by the blade-type stopper ball (128) of the blade-type stopper (129), when the guide ring shaft play window (106) of the slide mechanism (243) at high speed is located on the blade-type stopper landing (113), and Figure 36 of the shaft improvement structure of 013-235136 shows the part where the ratchet gear (6) of the disk-shaped engine operating tube is replaced with a variable gear box (88) to increase durability. This is a multi-purpose swing and twist triple piston engine characterized by having all of the above structures and functions.

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