Novel rotor engine

Abstract

The invention discloses a novel rotor engine, and relates to the technical field of rotor engines, the novel rotor engine comprises a novel rotor engine and a compressor for supplying high-pressure air to the novel rotor engine, and the novel rotor engine comprises a main shaft, a rotor mounted on the main shaft and a stator on the outer side of the rotor. The stator is provided with an annular shell, two blades are fixed in a rectangular groove in the inner wall to divide an annular air chamber into two semi-annular air chambers, the blades are provided with conical valves and communicated with a throttle valve and an air nozzle, the air nozzle is connected with a combustion chamber, and an oil nozzle and an igniter are arranged in the combustion chamber. The rotor is provided with two sets of moving blade mechanisms, a rotor groove structure can automatically compensate part abrasion, airflow, oil injection and water injection devices are controlled by a control cam on the main shaft, detonation is conducted four times every time the main shaft rotates by a circle, the air inflow and the rotating speed can be manually adjusted, and the engine performance is improved.

Description

TECHNICAL FIELD

[0001] The present application relates to the technical field of rotor engine, in particular to a new type of rotor engine. BACKGROUND

[0002] In the long-term use of the existing rotor engine, the sealing performance of the air chamber is often reduced due to the wear of the parts, and the air leakage phenomenon occurs, which affects the power output efficiency. In the traditional structure, the matching part of the stator and the rotor lacks effective automatic compensation mechanism, and the parts need to be frequently disassembled and maintained after wear, which is high in maintenance cost and complicated in operation.

[0003] In terms of power output, most rotor engines have low frequency of explosion, and the number of explosions per revolution of the main shaft is small, which leads to discontinuous power output and insufficient stability, and is difficult to meet the demand of high-power equipment. At the same time, the intake air control is mostly fixed mode, which cannot be flexibly adjusted according to the actual working condition, the speed regulation is limited, and the adaptability is poor.

[0004] In addition, the oil injection and water injection device of the existing engine is not accurate enough in control, which is difficult to realize efficient cooperation under different working conditions, not only affects the combustion efficiency, but also may cause overheating or performance degradation of the equipment due to improper cooling or pressure regulation. And the exhaust emission is not thorough enough, the residual exhaust gas can easily affect the combustion effect of the next cycle, further reducing the overall performance of the engine. These problems restrict the popularization and application of the rotor engine, and a new structure is needed to solve the above defects. SUMMARY

[0005] The present application provides a new type of rotor engine to solve the above technical problems.

[0006] A new type of rotor engine, comprising a new type of rotor engine and a compressor for supplying high-pressure air to the new type of rotor engine, the new type of rotor engine comprising a main shaft, a rotor installed on the main shaft, and a stator installed on the outer side of the rotor.

[0007] The stator mainly comprises a circular ring-shaped stator shell, the inner wall of which is provided with a row of rectangular grooves, the inner end of the two side walls of the stator shell is stepped outward, the outer surface of the rotor outer ring installed on the inner side of the stator shell is protruded outward, the inner side of the protrusion is also made into a stepped blocking table, the blocking table is matched with the outer side of the two side walls of the stator shell, and the annular air chamber is formed between the stator shell and the rotor outer ring. A left end cover and a right end cover are installed at the two ends of the stator shell, the middle of each end cover is protruded outward, and the inner part is provided with a roller slide disc, each roller slide disc is provided with a roller slide, and each roller slide is provided with a roller. The main shaft is installed in the center hole of the two end covers, and the contact part of the end cover and the stator shell is provided with a sub-port.

[0008] Two complete partitioned annular air chambers are fixed in the rectangular recess of the stator shell, and the annular air chamber is symmetrically divided into two half-annular air chambers. Two pairs of water injection ports and exhaust ports are arranged on the stator shell to communicate the half-annular air chambers. The water injection ports are connected with water injection devices, and the exhaust ports are connected with exhaust pipes.

[0009] A conical valve is arranged in each vane, and a throttle valve is connected to the rear of the conical valve, and a jet port is connected to the front of the conical valve. The jet port is connected to a combustion chamber, and the combustion chamber is provided with an oil nozzle and an igniter. The outlet of the combustion chamber is provided with a horn port, and the horn port faces the half-annular air chamber. A combined water injection nozzle is arranged around the horn port.

[0010] A rotor slot is arranged at the matching position of the two rotor step-shaped retaining tables of the rotor outer ring and the two stator step-shaped retaining tables of the stator shell. The first stator step-shaped retaining table of the stator is arranged in the rotor slot, and an arc-shaped alloy sheet, a small slider, a long small slider retaining table, a short small slider retaining table, a pull spring for pulling the small slider to the arc-shaped alloy sheet, and a pull spring hole are arranged in the rotor slot.

[0011] The arc-shaped alloy sheet is in a half-annular shape around the bottom of the rotor slot, is fixed to the first small slider at the front, and is pulled to the spoke of the rotor by the pull spring at the tail. There are two arc-shaped alloy sheets, one in each half-annular air chamber. A plurality of small sliders are arranged on the other side of the arc-shaped alloy sheet to push the arc-shaped alloy sheet to the stator step-shaped retaining table. The small sliders and the long small slider retaining table are arranged at intervals. The bottom edge of the small slider is pulled to the fixed point on the outer side of the rotor by the pull spring. The outer side of the small slider, the arc-shaped alloy sheet, the long small slider retaining table, and the outer diameter of the rotor outer ring are consistent. The width of the long small slider retaining table and the short small slider retaining table does not exceed the width of the sealing strip on the vane. The structure of the rotor slot can automatically compensate for the wear of the parts.

[0012] Further, the throttle valve is separately arranged for manual control of the air intake. The throttle valve includes a valve housing and a conical valve core arranged in the valve housing. A throttle valve spring is arranged below the conical valve core. A knife-edge shaped through hole is arranged in the conical valve core, and the through hole is connected with a conical valve at one side and a high-pressure air supply pipeline interface at the other side. A valve core adjusting handle is fixed to the upper end of the conical valve core for manual rotation to adjust the air flow.

[0013] Further, the rotor includes a hub arranged on the main shaft. The hub has ten spokes, and the spokes are arranged on the inner surface of the rotor outer ring. The hub, the spokes, and the rotor outer ring are integrated.

[0014] Two sets of moving vane mechanisms are symmetrically arranged on the rotor.

[0015] Two of the ten radial supports are selected, and the end faces of the two sides are connected by connecting plates, and the inner side of the rotor outer ring is connected, and the hub is not connected, to form a square frame. A rectangular hole is opened in the rotor outer ring opposite the square frame. The width of the rectangular hole is the same as the width of the semi-annular air chamber, and the upper and lower parts are consistent. The length is shorter than the distance between the two radial supports. The front surface of the moving blade is tightly attached to one end face of the rotor outer ring, and is erected in the rectangular hole. The inner side of the two connecting plates is designed as a moving blade sliding channel for the moving blade.

[0016] Further, in the middle part of the front surface of the moving blade, there is a positioning socket. On the back surface of the moving blade, there are three mechanism-like support rods. One of them is in the upper half of the moving blade, corresponding to the center of the semi-annular air chamber. A support rod shaft is provided to connect the support rod and the support rod shaft sleeve. The other end of the support rod is connected to the double top rod by a hinge shaft. On the outside of the hinge shaft, there is a fulcrum at the contact point of the support rod and the double top rod. The other end of the double top rod is fixed to the middle of the second support rod top shaft. The two shaft sleeves of the second support rod top shaft are on the two connecting plates. The left end of the second support rod top shaft is fixed with an L-shaped small crankshaft. The end of the L-shaped small crankshaft is installed with a roller sliding channel disc in the roller sliding channel. The right end of the second support rod top shaft extends out of the connecting plate.

[0017] The other two support rods and support rod sleeves are arranged above the first support rod sleeve. The ends of the double top rods are fixed to the first support rod top shaft by a key. The two shaft sleeves of the first support rod top shaft are also on the connecting plates. The right end of the first support rod top shaft is fixed with a rocker. An L-shaped small crankshaft is installed on the extended part of the right end of the second support rod top shaft. The end of the crankshaft is installed with a roller right in the roller sliding channel of the right roller sliding channel disc. A connecting rod is used to connect the shaft of the rocker one of the first support rod top shaft and the end shaft of the right end of the L-shaped small crankshaft installed on the extended part of the second support rod top shaft, forming a parallelogram.

[0018] Further, the top and both sides of the upper half of the moving blade in contact with the inner wall of the semi-annular air chamber have a sealing frame of the moving blade. The sealing frame is installed in the grooves opened on both sides and the top of the moving blade, and is fixed to the moving blade by square nails. The sealing frame has a movable space.

[0019] Further, the conical valve includes a conical valve seat, a conical valve hole in the center of the conical valve seat, a conical valve hole communicating with a jet nozzle, a conical valve body directly above the conical valve hole, a conical valve rod at the upper end of the conical valve body, and a conical valve rod with a diameter consistent with the diameter of the conical valve hole. The conical valve rod is matched with the conical valve rod sleeve in the stator. There is a conical valve spring between the conical valve body and the conical valve rod sleeve to keep the conical valve closed. The tail of the conical valve rod has a pull ring. Pulling the pull ring will open the conical valve. The pull ring is connected to the rocker two controlled by the main shaft control cam one.

[0020] Further, the diameter of the jet port is smaller than the diameter of the conical valve hole.

[0021] Further, the automatic control device of the new rotor engine airflow is driven by the control cam installed on the main shaft, the push rod is hinged on the control cam, the adjusting joint is hinged on the other end of the push rod, the rocker three is installed on the adjusting joint, the rocker shaft of the rocker three is fixed on the second season plastic machine, the other end of the rocker three is hinged with the connecting rod, the connecting rod is hinged with the rocker two, the rocker shaft of the rocker two is fixed on the shell of the new rotor engine, the other end of the rocker two is arranged in the pull ring at the tail of the conical valve, the main shaft drives the control cam to rotate half a circle in the clockwise direction, the two protrusions on the control cam and the two push rods on the two sides are lifted once, so as to drive the two conical valves to open once, the main shaft drives the cam to rotate one circle, and the two conical valves will be automatically opened four times, and the high-pressure air is supplied to the jet port four times, that is, the new rotor engine should be detonated four times.

[0022] Further, the oil nozzle is connected with the oil injection pump, the oil injection pump is automatically controlled by the control cam two installed on the main shaft, the water injection port and the combined water injection nozzle share or separately use the water injection pump, and the water injection pump is also automatically controlled by the control cam two installed on the main shaft, the control cam two used by the oil injection pump and the water injection pump, and the oil injection pump and the water injection pump should inject oil and water for a long time in each half circle of the main shaft.

[0023] The advantages of the present application: the new rotor engine of the technical solution has many beneficial effects. In the structure design, the stator and the rotor outer ring form an annular air chamber, which is divided into two half annular air chambers by the blade, and the high-efficiency gas compression and expansion are realized by cooperating with the moving blade mechanism, so that the working efficiency is improved.

[0024] The arc-shaped alloy piece, small sliding block and tension spring in the rotor groove can automatically compensate the wear of parts, reduce the air leakage phenomenon, ensure the air chamber sealing, and prolong the service life of the equipment.

[0025] The airflow automatic control device is driven by the control cam on the main shaft, the main shaft can make the two conical valves open four times in one revolution, realize four times of detonation, the power output is more continuous and stable, and the throttle can be manually adjusted to control the air intake, so as to control the engine speed.

[0026] The oil injection pump and the water injection pump are controlled by the control cam two, can work for a long time in half a circle of the main shaft, and the water injection can be adjusted according to the demand, which is helpful for temperature reduction and pressure adjustment. In addition, the two-stage air compressor provides high-pressure air, combined with the detonation design of the combustion chamber, the power is strong, the overall structure is compact, and the parts work cooperatively, so that the comprehensive performance of the engine is improved. BRIEF DESCRIPTION OF DRAWINGS

[0027] Figure 1 It is a structural schematic diagram of a new rotor engine.

[0028] Figure 2 is Figure 1 A-A sectional view in the middle;

[0029] Figure 3 is Figure 1 B-B sectional view in the middle;

[0030] Figure 4 is a structure diagram of the moving blade falling into the moving blade slide in the rotor;

[0031] Figure 5 is a structure diagram of the rotor slot;

[0032] Figure 6 is a structure diagram of the arc alloy piece and the small slide block;

[0033] Figure 7 is a structure diagram of the spring pulling the small slide block and the spring hole;

[0034] Figure 8 is a structure diagram of the marked area D;

[0035] Figure 9 is a structure diagram of the overall appearance of a new rotor engine;

[0036] Figure 10 is a structure diagram of the moving blade sealing frame;

[0037] Figure 11 is a structure diagram of the blade sealing strip one;

[0038] Figure 12 is a structure diagram of the control cam one;

[0039] Figure 13 is a structure diagram of the control cam two;

[0040] Figure 14 is Figure 2 a structure diagram of the marked area E in the middle;

[0041] Figure 15 is Figure 2 a structure diagram of the marked area G in the middle;

[0042] Figure 16 is a drawing diagram of the roller slide.

[0043] As shown in the figure: 1, stator step-shaped blocking table; 2, rotor outer ring; 3, rotor slot; 4, arc-shaped alloy piece; 5, small slider; 6, tension spring; 7, tension spring channel; 8, small ladder type slider; 9, first small slider; 10, blade; 11, moving blade; 12, long small slider blocking table; 13, stator shell; 14, cooling fin; 15, sealing frame; 16, left end cover; 17, right end cover; 18, rotor step-shaped blocking table; 19, strut top shaft No. 1; 20, strut top shaft No. 2; 21, strut No. 1; 22, strut shaft No. 1; 23, hinged shaft; 24, rotor; 25, rocker No. 1; 26, combined water jet nozzle; 27, oil injection pump; 28, throttle; 29, water injection pump; 30, generator; 31, air outlet; 32, air jet nozzle; 33, combustion chamber; 34, oil injection nozzle; 35, igniter; 36, output clutch; 37, main shaft; 38, left roller slide; 39, right roller slide; 40, left roller slide disc; 41, right roller slide disc; 42, air inlet; 43, connecting rod No. 1; 44, coupling; 45, bearing; 46, L-shaped small crankshaft left; 47, left roller; 48, control cam No. 1; 49, control cam No. 2; 50, rocker No. 2; 51, L-shaped small crankshaft right; 52, end shaft; 53, conical valve; 54, conical valve seat; 55, conical valve hole; 56, conical valve rod; 57, conical valve rod tail ring; 58, right roller; 59, moving blade slide; 60, exhaust port; 61, water injection port; 62, rotor key; 63, sealing strip No. 1; 64, valve housing; 65, valve core; 66, high-pressure air supply pipeline; 67, throttle spring; 68, knife-edge-shaped through hole; 69, valve core adjusting handle; 70, moving blade bayonet; 71, rotor outer ring hook table; 72, high-pressure air supply pipeline; 73, rocker shaft; 74, conical valve body; 75, conical valve rod sleeve; 76, conical valve spring; 77, push rod; 78, adjusting joint; 79, rocker No. 3; 80, connecting rod No. 2; 81, machine base; 82, air supply pipeline; 83, sealing strip No. 2; 84, strut shaft No. 2; 85, second-stage air compressor; 86, new rotor engine; 87, reinforced frame; 88, first-stage air compressor; 89, air duct; 90, air outlet; 91, air inlet; 92, pressure gauge; 93, starting motor; 94, starting gear; 95, air inlet fan; 96, air cleaner; 97, short small slider blocking table. DETAILED DESCRIPTION

[0044] The following description is made in conjunction with the accompanying drawings.

[0045] The present application provides a new rotor engine, which comprises a new rotor engine and a compressor for supplying high-pressure air to the new rotor engine, the new rotor engine comprising a main shaft, a rotor installed on the main shaft, and a stator installed on the outer side of the rotor.

[0046] The stator mainly comprises a circular stator shell 13, the inner wall of which is provided with a row of rectangular grooves, the outer side of the inner end of the two side walls of the stator shell is stepped, the rotor outer ring 2 is fitted and installed on the inner side of the stator shell, the outer surface of the two ends of the rotor outer ring 2 is outwardly protruded, the inner side of the protrusion is also formed as a rotor stepped blocking platform 18, the rotor stepped blocking platform 18 is fitted and blocked on the outer side of the two side walls of the stator shell 13, the stator shell 13 and the rotor outer ring 2 form an annular air chamber, the left end cover 16 and the right end cover 17 are installed on the two ends of the stator shell 13, the middle of each end cover is outwardly protruded, the inner side of each end cover is provided with a roller slide disc 40, each roller slide disc 40 is provided with a roller slide 38, each roller slide 38 is provided with a roller 47, the main shaft 37 is installed in the central hole of the two end covers, and the contact part of the end cover and the stator shell 13 is provided with a sub-port.

[0047] Two blades 10 which completely separate the annular air chamber are symmetrically fixed in the rectangular grooves of the stator shell 13, the annular air chamber is symmetrically divided into two half annular air chambers, two pairs of water injection ports 61 and exhaust ports 60 which communicate the half annular air chambers are formed on the stator shell 13, the outer end of the water injection port 61 is connected with a water injection device, and the outer end of the exhaust port 60 is connected with an exhaust pipe.

[0048] A conical valve 53 is arranged in each blade 10, the conical valve 53 is connected with the air throttle 28 at the rear side, connected with the air injection port 32 at the front side, the air injection port is connected with the combustion chamber 33, the combustion chamber 33 is provided with the oil injection nozzle 34 and the igniter 35, the outlet of the combustion chamber 33 is provided with a horn port, the horn port faces the half annular air chamber, and the periphery of the horn port is provided with a combined water injection nozzle 26.

[0049] A rotor groove 3 is formed at the fitting part of the two rotor stepped blocking platforms 18 of the rotor outer ring 2 and the two stator stepped blocking platforms 1 of the stator shell, the first stator stepped blocking platform 1 of the stator is arranged in the rotor groove, the stator stepped blocking platform 1 may be deformed and swing due to heat in operation, the rotor groove 3 must be widened, the widened rotor groove 3 may cause air leakage, therefore, the following methods are adopted, the arc-shaped alloy sheet 4 and the small sliding block 5 are arranged in the rotor groove 3, the long small sliding block blocking platform 12, the short small sliding block blocking platform 97 and the small spring 6 which pulls the small sliding block 5 to the arc-shaped alloy sheet 4 are fitted, and the small spring hole 7 is fitted.

[0050] In Figure 5The middle rotor slot 3 is wide, and an arc alloy sheet 4 is arranged on the step-shaped stop 1 of the stator and the bottom of the rotor slot 3. The arc alloy sheet 4 is semi-circular around the bottom of the rotor slot 3, is fixed on the first small slider 5 at the front, and is pulled on the spoke of the rotor by a spring at the tail. There are two arc alloy sheets, one in each semi-circular air chamber. A plurality of small sliders 5 are arranged on the other side of the arc alloy sheet 4 and are in close contact with the step-shaped stop 1 of the stator. The small sliders and the long small slider stop 12 are arranged at intervals. The bottom edge of the small slider 5 is pulled away from the fixed point on the outside of the rotor by a spring 6. The outside of the small slider 5, the arc alloy sheet 4, the long small slider stop 12 and the outer diameter of the rotor outer ring 2 are consistent. The long small slider stop 12 and the short small slider stop 97 are relatively narrow, and their width cannot exceed the width of the sealing strip 163 on the blade 10. The structure of the rotor slot 3 can automatically compensate for the wear of the parts.

[0051] The throttle valve 28 is separately arranged for manually controlling the air intake.

[0052] The throttle valve 28 comprises a valve shell 64 and a conical valve core 65 arranged in the valve shell. A throttle valve spring 67 is arranged below the conical valve core. A knife-edge-shaped through hole 68 is arranged in the conical valve core, and the through hole is connected with the tapered valve 53 at one end and connected with the high-pressure air supply pipeline interface 66 at the other end. The upper end of the conical valve core is fixed with a valve core adjusting handle 69 for manually rotating to adjust the air flow.

[0053] The rotor 24 comprises a hub arranged on the main shaft 37. The hub has 10 spokes arranged on the inner surface of the rotor outer ring. The hub, the spokes and the rotor outer ring are integrated,

[0054] Two sets of movable blades 11 mechanisms are symmetrically arranged on the rotor 24. Only one set is described herein, and the other set has the same structure.

[0055] Two of the 10 spokes are selected, and the end faces on both sides are connected by connecting plates and connected to the inner side of the rotor outer ring 2 without connecting the hub to form a square frame. A rectangular hole is arranged on the rotor outer ring 2 opposite the square frame. The width of the rectangular hole is the same as the width of the semi-circular air chamber and consistent in up and down directions. The length is shorter than the distance between the two spokes. The front surface of the movable blade 11 is in close contact with one end face of the rotor outer ring 2, and the two connecting plates in the rectangular hole are arranged in the movable blade channel 59 designed for the movable blade 11 in the diameter direction.

[0056] In the middle of the front face of the moving vane 11, there is a positioning socket 70, and in the back face of the moving vane 11, there are three identical support rods No. 1 21, one of which is in the upper half of the moving vane 11, corresponding to the center of the semi-annular air chamber, a support rod sleeve is arranged, a support rod shaft 22 is used to connect the support rod No. 1 21 and the support rod sleeve, the other end of the support rod No. 1 21 is connected with a double top rod through a hinge shaft 23, outside the hinge shaft, there is a fulcrum at the contact point of the support rod No. 1 21 and the double top rod, the other end of the double top rod is fixed to the middle of a support rod top shaft No. 2 20, the two sleeves of the support rod top shaft No. 2 20 are arranged on the two connecting plates, the left end of the support rod top shaft No. 2 20 is fixed with an L-shaped small crank 46, the end of the L-shaped small crank 46 is provided with a left roller 47 in the roller slide 38 of the left roller slide disc 40, the right end of the support rod top shaft No. 2 20 extends out of the connecting plate and is ready for use, see Figure 1 and Figure 2 .

[0057] The other two support rods No. 1 21 and support rod sleeves are arranged above the first support rod sleeve, the ends of the double top rods are fixed to a support rod top shaft No. 1 19 through keys, the two sleeves of the support rod top shaft No. 1 19 are also arranged on the connecting plates, the right end of the support rod top shaft No. 1 19 is fixed with a rocker 25 through a key, an L-shaped small crank 51 is arranged on the extended part of the right end of the support rod top shaft No. 2 20, a roller 58 in the roller slide 39 of the right roller slide disc 41 is arranged on the end shaft 52 of the end of the L-shaped small crank, a connecting rod 43 is used to connect the shaft 73 of the rocker 25 of the support rod top shaft No. 1 19 and the end shaft 52 of the right end of the L-shaped small crank arranged on the extended part of the support rod top shaft No. 2, to form a parallelogram, see Figure 3 .

[0058] The top and two sides of the moving vane 11 in contact with the inner wall of the semi-annular air chamber in the upper half of the moving vane 11 are provided with a sealing frame 15 of the moving vane, see Figure 10 , the sealing frame 15 is arranged in the grooves opened on the two sides and the top of the moving vane 11 and is fixed to the moving vane 11 through square nails, the sealing frame 15 can move within a certain range.

[0059] The conical valve 53 comprises a conical valve seat 54, a conical valve hole 55 in the center of the conical valve seat 54, the conical valve hole 55 being communicated with the air jet nozzle 32, a conical valve body 74 above the conical valve hole 55, an upper end of the conical valve body 74 being a conical valve rod 56, the diameter of the conical valve rod 56 being consistent with the diameter of the conical valve hole 55, the conical valve rod 56 being matched with a conical valve rod sleeve 75 in the stator, a conical valve spring 76 being arranged between the conical valve body 74 and the conical valve rod sleeve 75 to keep the conical valve 53 in a closed state, a pull ring 57 being arranged at the tail of the conical valve rod 56, the conical valve 53 being opened by pulling the pull ring 57, the pull ring being connected to the rocker 50 controlled by the hand shaft control cam 48, see Figure 2 , Figure 9 .

[0060] The diameter of the jet port 32 should be smaller than the diameter of the conical valve hole 55 of the conical valve 53, because the conical valve 53 is two, so the conical valve automatic control device is also two sets, the conical valve automatic control device is to automatically control the opening and closing of the conical valve during the operation of the new type of rotor engine, and to supply in time.

[0061] The automatic control device of the airflow of the new type of rotor engine is driven by the control cam 48 installed on the main shaft 37, as shown in Figure 9 A push rod 77 is hinged on the control cam 48, the other end of the push rod 77 is hinged with an adjusting joint 78, the adjusting joint 78 is installed with a rocker three 79, the rocker shaft of the rocker three 79 is fixed on the second season compression molding machine 85, the other end of the rocker three 79 is hinged with a connecting rod 80, the connecting rod 80 is hinged with the rocker two 50, the rocker shaft of the rocker two 50 is fixed on the shell of the new type of rotor engine 86, the other end of the rocker two 50 is arranged in the pull ring 57 at the tail of the conical valve, the main shaft 37 drives the control cam 48 to rotate half a circle in the clockwise direction, the two protrusions on the control cam 48 push up the two push rods 77 on both sides, each push up once, thereby pushing open the two conical valves 53 each time, the main shaft drives the cam to rotate a circle, the other conical valve 53 will be automatically opened 4 times, 4 times of high pressure air is supplied to the jet port 32, that is, the new type of rotor engine should be detonated 4 times, as shown in Figure 12 .

[0062] The oil nozzle 34 is connected with the oil injection pump 27, the oil injection pump 27 is automatically controlled by the control cam two 49 installed on the main shaft 37, the water jet port 61 and the combined water jet nozzle 26, and the water injection pump 29 behind them can be shared or used separately, the water injection pump 29 is also automatically controlled by the control cam two 49 installed on the main shaft 37, the control cam two 49 used by the oil injection pump 27 and the water injection pump 29 is as shown in Figure 13 They should spray oil and water for a long time in each half circle of the main shaft 37.

[0063] Figure 15 is Figure 2 the structure diagram of the marked area G in Figure 2 , which is cited because it cannot be marked in Figure 15 , and is specially marked,

[0064] Figure 3 is Figure 1 the B_B sectional view in , which shows the position and structure of the right roller 58, the right roller slide 39, the right L-shaped small crankshaft 51, the rocker one 25 and the connecting rod one 43.

[0065] In each blade 10, there is a pressure reducing valve.

[0066] The drawing method of the roller slide:

[0067] I draw the figure size is not accurate, also not in the same plane, now assume I draw the figure is correct, will Figure 2 、 Figure 16 、 Figure 4 all assume in the same plane, and the same scale, so good painting.

[0068] Quadrilateral 19 / 20 / 22 / 84 is a parallelogram, see Figure 2 、 Figure 14 , the main shaft 37 is clockwise operation, so Figure 16 is the right roller slide 39, put Figure 4 in the main shaft 37 axis 0, strut top shaft No. 19, strut top shaft No. 20, L-shaped small crank right 51, end axis 52, connecting rod 1 43, rocker 1 25, rocker 1 shaft 73 are all original position shift drawing in Figure 16 , L-shaped small crank right 51 and end axis 52 in Figure 2 , also according to the original position shift drawing to Figure 16 , 51 move Figure 16 in the dotted line 51 ', 52 move Figure 16 in the point 52 " indicates, strut top shaft No. 2 axis with "Z" in Figure 16In the middle, make the bisector zg of ∠52Z52' and make the perpendicular line ZH of z with radius oz, rotate ∠52Z52' and the bisector zg of the angle around z close to ZH to make zg and ZH coincide to get new end axes 52" and 52"'. In the rotation of ∠52Z52', the support rod top shaft No. 1 and No. 2 remain unchanged, draw the intersection line 052"'of the right roller 58 with a and b with 52"'as the center, connect 052', draw ox = o52"'on the extension line of the diameter 052" ', take x point as the center, draw the extension line of the intersection line ox' of the right roller 58 with c point and d point with o as the center, draw circles c and d respectively with oc and od because o is often used as the center of the concentric circle later, so don't say the center o later, just say the circle c and the circle d, take x as the center and xa as the radius to draw an arc intersecting circle c at c' point, connect xc', take x as the center and xb as the radius to draw an arc intersecting xc' at y point, make the straight line 0c' intersecting circle x at x' and circle d at d' with c' as the center, draw an arc connecting d'y, start from c' point, move 2 times the thickness of the moving blade in the clockwise direction to intersect circle c at e point, make the straight line oe intersecting circle d at f, circle x at x" and circle 52"'at q, take q as the center and qf as the radius to draw an arc intersecting circle b at s, connect qs, take q as the center and qe as the radius to draw an arc intersecting qs at y' point, make the diameter os of circle b intersecting circle 52"'at x"'and circle at y point, take s as the center and sy as the radius to draw an arc, connect y' r, take x", x"'as the center to draw the right roller 58 respectively connecting each contact point.

[0069] On the diameter od, make the right roller 58 and the centers v, a', b' and 52" ', a, b, x symmetrical with the center o as the center of symmetry, on the diameter od', make the right roller 58 and the centers v', c", d" and x', c', d' symmetrical with the center o as the center of symmetry, on the diameter of f, make the right roller 58 and the centers v", q', e', f' and x", q, e, f symmetrical with the center o as the center of symmetry, on the diameter of s, make the right roller 58 and the centers v" ', r', s' and x" ', r, s symmetrical with the center o as the center of symmetry, then according to the previous method, connect the points that should be connected with the axis, erase the unnecessary line segments, and the remaining curves connected in the annular groove on both sides of the 8 right rollers 58 are the right roller slide 39, in the rotation of ∠52Z52', the L-shaped small crankshaft left 46 also rotates and fixes accordingly, the structure of the left roller slide 38 and the right roller slide 39 is the same, only left and right, the drawing is the same, the installation should be synchronized to make the two rollers produce the maximum combined force.

[0070] As an improvement, a convex is made on the back of the moving blade 11 towards the top end, see Figure 14And in the convex, a slot is opened, and a sealing strip 83 is installed in the slot, so as to prevent the exhaust gas from leaking from the gap between the back of the moving blade 11 and the blade 10 to the next air chamber when the moving blade falls. The contact angle between the corresponding blade 10 and the two sides of the annular air chamber is also changed from a right angle to an arc shape, which cooperates with the arc on both sides of the top end of the moving blade 11. The sealing strip 83 always does not leave the back of the blade 10. The method of war game can be used, that is, the stator and rotor of the engine are installed, the moving blade, the support rod, the support rod top shaft, and the roller system are installed, and only the blade is not installed. Push the main shaft rotor in the clockwise direction. When the rotor rotates, the roller will move along the curved part of the roller slide, drive the sealing strip 83 on the moving blade 11 to fall and draw its moving track. The shape of the back of the blade can be made according to the moving track, and the perfect shape of the back of the blade can be obtained through correction. Figure 2

[0071] In Figure 8 , when the moving blade 11 is raised to the highest position, because of the two sides, two first small sliding blocks 9 are needed, a ladder-shaped slot is opened on the moving blade 11, a ladder-shaped small sliding block 8 is installed in the slot, the small sliding block 8 is as high as the moving blade 11, the tail is clamped by a spring and can move horizontally, and the two outer corners of the small sliding block 8 are arc-shaped. This structure can make the contact between the ladder-shaped small sliding block 8, the small sliding block 9, the arc-shaped alloy sheet 4, the moving blade 11, the sealing frame 15, and the inner wall of the semi-annular air chamber be a gap. In addition, the bayonet 70 in the moving blade 11 and the hook table 71 on the outer circle of the rotor are also the tightest at this time, which cooperates to ensure that the moving blade 11 does not leak.

[0072] A rotor engine mainly consists of a new type of rotor engine 86 and a two-stage air compressor. The new type of rotor engine 86 and the two-stage air compressor are installed on the same machine base 81, and the upper ends of the two are connected by a reinforcing frame 87. One end of the high-pressure air supply pipeline 72 is connected to the output end of the second-stage air compressor 85, and the other end is connected to the high-pressure air supply pipeline 66 of the "throttle valve 28" of the new type of rotor engine. A pressure gauge 92 is installed on the high-pressure pipeline. There is an air supply pipeline 82 between the first-stage and second-stage air compressors. There is a ventilation pipeline 89 between the first-stage air compressor 88 and the new type of rotor engine 86. A starting gear 94 is installed on the outer center shaft of the first-stage air compressor 88. The starting gear is connected to a starting motor 93 and a starting handle. There are an air inlet fan 95 and an air filter 96 in the direction of the main shaft. See Figure 2 ;

[0073] ​Upon startup, the throttle valve 28 is manually closed, which also shuts down the fuel injection pump 27 and water injection pump 29. The starter motor 93 is then turned on, causing the main shaft 37 to rotate clockwise. The new rotary engine 86, due to the pressure relief valve on the blades 10, can also rotate, and the intake fan 95 rotates as well. Air filtered by the air filter 96 is sent through the intake fan 95 to the air intake hole 91 on the right end cover of the compressor, entering the first-stage air compressor 88. A portion of this air is absorbed and compressed by the first-stage air compressor 88, and then travels through the air delivery pipe 82 to the second-stage air compressor 85, where it is compressed. After compression, the air is sent from the high-pressure air supply pipe 66 to the throttle valve 28. Because the throttle valve 28 is closed, the pressure on the pressure gauge 92 on the high-pressure air supply pipe 66 increases, but it will not exceed the set value. Once the pressure gauge exceeds the set value, the air will be discharged. Another part of the air entering the first-stage air compressor 88 passes through the rotor cavity to the air outlet 90 at the left end of the first-stage air compressor 88 and enters the ventilation pipe 89. It passes through the air inlet 42 on the right end cover of the new rotary engine 86 and enters the interior of the new rotary engine 86. Then it passes through the rectangular hole on the outer ring 2 of the rotor and enters the semi-annular air chamber, carrying some residual exhaust gas and being discharged from the exhaust port 60.

[0074] Because the throttle valve 28 is closed, although the main shaft rotates and the cone valve 53 opens and closes normally, there is no airflow, so combustion is impossible. When the pressure on the pressure gauge 92 reaches a certain value, the engine can be started. The throttle valve 28 can be manually started, which opens the fuel injection pump 27. High-pressure air enters the cone valve 53 through the high-pressure air delivery pipe 72. The cam 48 of the ignition pump 53 sends compressed air to the nozzle 32 on time according to the command. The fuel injection pump 21 is controlled by the cam 49 to send fuel to the nozzle 34. When the fuel and high-pressure air mix in the combustion chamber and are ignited by the igniter 53, they will explode, generating an impact force that bursts out of the flare and pushes the moving blade 11 to rotate around the main shaft 37. Adjusting the throttle valve 28 and the fuel pump 27 can change the speed. During operation, the combination of the water nozzle 26 and the water inlet 61 can be determined as needed to spray water or not, spray more or less. See Figure 2 and Figure 15 .

[0075] Working principle: such as Figure 2 , 4 16, assuming the roller is 58 on the right. Figure 16 At position 52”', that is, at the moving blade 11 Figure 2 At this position, the previous stroke of the new rotary engine has ended, the exhaust gas has been exhausted, and the moving blade 11 remains in its highest, upright position. Figure 8 and Figure 2 The three struts on the back of the moving blade 11 are also straightened, and the fulcrum at the hinge shaft of each strut is in contact. They can ensure that the struts are straighter and more sturdier, and can also prevent the moving blade from retracting.

[0076] Let the new rotor engine main shaft 37 run in the clockwise direction, the stator is not moving, the whole rotor 24 will run with the main shaft to the positive direction, because the roller slide 39 in the roller right 58 at 52 ", begin to bend outward, see Figure 16 , And arrive at x' point, the new roller right 58 will also arrive at x' point, under the control of the roller right 58, the three struts installed on the strut top shaft 1 19 and strut top shaft 2 20 will bend and pull the moving blade 11 into the moving blade slide 59, see Figure 2 , Figure 16 And Figure 4 The roller 47 in the left roller slide 38 will also work together to pull the moving blade 11 into the moving blade slide 59, at this time the moving blade has slid to the inside of the blade 10, the moving blade slide 59 in the rotor 24, the main shaft 37 continues to rotate, the roller right 58 will turn from x' to x", the moving blade 11 will also turn to the opposite side of the blade 10, see Figure 4 And Figure 16 The main shaft continues to rotate, the roller slide 39 will bend inward at x" and arrive at x'" point, the roller right 58 will also turn from x" to x'" point, under the control of the roller right 58, the three struts installed on the two strut top shaft 1 19 and strut top shaft 2 20 will straighten and pull out the moving blade 11 and push the moving blade 11 to the highest point and contact the bottom of the semi-annular air chamber slot, the left roller 47 will also work together to push the moving blade 11 to the highest point.

[0077] The strut roller structure movement described above is complex, but there is no load after the semi-annular air chamber is exhausted, so the wear is small.

[0078] When the roller right 58 reaches x'" point, the protrusions on the control cam 1 48 will contact the push rod 77, preparing to open the conical valve 53, the two protrusions on the control cam 2 49 will contact the oil injection pump 27 and the water injection pump 29, the main shaft 37 continues to rotate, the conical valve 53 opens, high-pressure air enters the combustion chamber 33 through the paint injection nozzle 32, the oil injection pump 27 also injects oil into the combustion chamber 33 through the oil injection nozzle 34, the igniter 35 ignites, the oil and gas are ignited, causing an explosion to form a strong pressure, pushing the moving blade 11 to rotate around the main shaft 37, at this time the main shaft 37 becomes the driving force, the jet continues, the oil continues to be injected, the combined water injection nozzle 26 sprays water as determined by the operator, and continues to ignite;

[0079] When the roller right 58 reaches Figure 16n position in the middle of the dynamic blade 11, that is, when the dynamic blade 11 reaches the exhaust port 60, the water injection port 61 stops injecting water, and the semi-annular air chamber discharges the exhaust gas to the outside through the exhaust port. When the roller reaches the V outer position, see Figure 16 , the exhaust is completed, and the entire stroke is completed. The main shaft 37 rotates one circle, and the two symmetrical semi-annular air chambers complete four strokes. In addition, although the exhaust is completed, the exhaust gas in the annular air chamber cannot be completely discharged. Therefore, a protrusion and a sealing strip 2 83 are added to the back of the dynamic blade 11, see Figure 14 , which can organize the exhaust gas to enter the next air chamber.

[0080] Automatic compensation for part wear and tear, prolonging the service life:

[0081] The rotor slot is provided with an arc-shaped alloy piece, a small sliding block, and a tension spring structure. The small sliding block tightly abuts the arc-shaped alloy piece to the stepped blocking table of the stator, and the tension spring continuously applies tension, which can automatically compensate for the gap caused by the wear and tear of the parts ("the rotor slot structure can automatically compensate for the wear and tear of the parts"). This design reduces the impact of wear and tear on the sealing performance of the air chamber, reduces the maintenance frequency, and prolongs the service life of the engine.

[0082] High air tightness, improving energy utilization efficiency

[0083] The movable sealing frame is installed on the top and both sides of the dynamic blade, which can tightly abut the inner wall of the semi-annular air chamber in cooperation with the hook table of the rotor outer ring and the positioning bayonet of the dynamic blade, thereby reducing air leakage.

[0084] The protrusion and the sealing strip 2 added to the back of the dynamic blade can prevent the exhaust gas from entering the next air chamber from the gap between the back of the dynamic blade and the stator blade ("prevent the exhaust gas from entering the next air chamber from the gap between the back of the dynamic blade and the stator blade").

[0085] The combination design of the arc-shaped alloy piece and the small sliding block further strengthens the sealing of the rotor and the stator at the joint, avoiding the leakage of high-pressure gas in the annular air chamber.

[0086] High air tightness ensures that the energy generated by combustion is more efficiently converted into power, reducing energy loss.

[0087] High energy output, excellent power performance:

[0088] Two blades are symmetrically arranged in the stator, dividing the annular air chamber into two semi-annular air chambers. Each blade corresponds to a set of combustion chamber and jet system. The main shaft rotates one circle, and the two conical valves are automatically opened four times, providing high-pressure air to the jet port four times, that is, the new rotor engine should be detonated four times. High-frequency detonation significantly improves the power output per unit time.

[0089] The combustion chamber outlet is equipped with a flared opening, which can concentrate the impact force generated by the deflagration and directly drive the moving blades to rotate. The energy conversion path is short and the power transmission efficiency is high.

[0090] Stable operation and strong controllability:

[0091] Airflow (conical valve), fuel injection (fuel injection pump), and water injection (water injection pump) are all automatically driven by control cams on the main shaft ("The automatic control device for airflow of the new rotary engine is driven by control cam one installed on the main shaft" and "The fuel injection pump and water injection pump are also automatically controlled by control cam two installed on the main shaft"). The actions of each system are coordinated and synchronized to ensure operational stability.

[0092] The throttle body allows for manual adjustment of the intake air volume ("The throttle body is a separate setting for manual control of the intake air volume"). In conjunction with the fuel injection pump adjustment, it can flexibly change the engine speed to adapt to different operating conditions.

[0093] The symmetrical design of the two semi-annular air chambers and the two sets of moving blade mechanisms can balance the forces, reduce vibration during operation, and improve stability.

[0094] Easy to start and highly adaptable to different environments:

[0095] The stator blades are equipped with pressure reducing valves, which can reduce the rotor rotation resistance during startup, making it easier for the starter motor to drive the main shaft ("The new rotor engine can rotate together because of the pressure reducing valves on the blades").

[0096] The two-stage air compressor provides high-pressure air, which, together with the air filter and intake fan, ensures that the air entering the combustion chamber is clean and the pressure is stable, enabling reliable start-up even in complex environments;

[0097] The water spraying device (spray nozzle and combined spray nozzle) can adjust the water spray volume according to the needs. By heating the water into steam to increase the pressure, it can not only help to improve power, but also cool down at high temperatures, adapting to different load conditions.

[0098] Optimize exhaust emissions to reduce residual impact:

[0099] The exhaust port is directly connected to the semi-annular air chamber, which can quickly discharge the exhaust gas after combustion;

[0100] The sealing strip on the back of the moving blade and the specially designed blade contact angle (changed from a right angle to an arc) can reduce the residue of exhaust gas in the gas chamber, avoid affecting the efficiency of the next combustion, and indirectly reduce harmful emissions.

[0101] In summary, this new rotary engine achieves advantages such as wear self-compensation, high airtightness, high power output, and stable controllability through structural innovation, while taking into account service life, performance, and adaptability, and has strong practical value.

[0102] The above describes the present application and its embodiments, which are not limited, and the drawings only show one of the embodiments of the present application, and the actual structure is not limited thereto. In general, if a person skilled in the art is inspired thereby, without departing from the purpose of the present application, without creative design, similar structure and embodiments of the technical solution are not creative, and should belong to the protection scope of the present application.

Claims

1. A novel rotary engine characterized by: The application relates to a new type of rotor engine and a compressor for supplying high-pressure air to the new type of rotor engine, wherein the new type of rotor engine comprises a main shaft, a rotor installed on the main shaft and a stator installed outside the rotor. The stator mainly comprises a circular annular stator shell, the inner wall of the stator shell is provided with a row of rectangular grooves, the inner end of the two side walls of the stator shell is stepped outward, the rotor outer ring is installed on the inner side of the stator shell, the two ends of the outer surface of the rotor outer ring are protruded outward, the two inner sides of the protrusions are also formed into stepped blocking tables, the blocking tables are matched and blocked on the two side walls of the stator shell, the annular air chamber is formed between the stator shell and the rotor outer ring, the left end cover and the right end cover are installed on the two ends of the stator shell, the middle of each end cover is protruded outward, the inner part is provided with a roller slide disc, one roller slide is arranged in each roller slide disc, one roller is arranged in each roller slide, the main shaft is installed in the center holes of the two end covers, the contact part of the end cover and the stator shell is provided with a nozzle, and the two end covers are provided with a roller slide disc. Two blades which completely separate the annular air chamber are fixed in the rectangular grooves of the stator shell in a symmetrical mode, the annular air chamber is symmetrically divided into two half annular air chambers, two pairs of water injection ports and exhaust ports which are connected with the half annular air chambers are arranged on the stator shell, the water injection ports are connected with water injection devices, and the exhaust ports are connected with exhaust pipes. A conical valve is arranged in each blade, the conical valve is connected with a throttle valve at the back and connected with a jet port at the front, the jet port is connected with a combustion chamber, the combustion chamber is provided with an oil nozzle and an igniter, a horn is arranged at the outlet of the combustion chamber, the horn is directed to the half annular air chamber, and a combined water injection nozzle is arranged around the horn. A rotor groove is arranged at the matched part of the two rotor stepped blocking tables of the rotor outer ring and the two stator stepped blocking tables of the stator shell, the first stator stepped blocking table of the stator is arranged in the rotor groove, an arc-shaped alloy sheet, a small slider, a matched long small slider blocking table, a short small slider blocking table, a pulling spring which pulls the small slider to the arc-shaped alloy sheet and a matched spring hole are arranged in the rotor groove. The arc-shaped alloy sheet is in a half annular shape around the bottom of the rotor groove, the front part is fixed on the first small slider, the tail part is pulled to the radial support of the rotor by the pulling spring, there are two arc-shaped alloy sheets, one in each half annular air chamber, a plurality of small sliders are arranged on the other side of the arc-shaped alloy sheet and are close to the stator stepped blocking table, the small sliders and the long small slider blocking table are arranged at intervals, the bottom edge of the small slider is pulled to the fixed point outside the rotor by the pulling spring, the outer side of the small slider is consistent with the outer diameter of the arc-shaped alloy sheet, the long small slider blocking table and the short small slider blocking table have a width which does not exceed the width of the sealing strip on the blade, and the structure of the rotor groove can automatically compensate the wear of parts.

2. A novel rotary engine as claimed in claim 1, wherein: The throttle valve is separately arranged and used for manually controlling the air intake, the throttle valve comprises a valve shell and a conical valve core installed in the valve shell, a throttle valve spring is arranged under the conical valve core, a knife-edge shaped through hole which is staggered by 180 DEG at two ends is arranged in the conical valve core, a conical valve is connected with one side of the through hole, a high-pressure air supply pipeline interface is connected with the other side of the through hole, and a valve core adjusting handle which can be manually rotated to adjust the air flow is fixed on the upper end of the conical valve core.

3. A novel rotary engine according to claim 2, characterized in that: The rotor comprises a hub installed on the main shaft, and the hub is provided with 10 spokes which are arranged on the inner surface of the outer ring of the rotor and are integrated with the hub and the outer ring of the rotor; The rotor is symmetrically provided with two sets of dynamic blade mechanisms; Two of the 10 spokes are selected, the end faces on both sides are connected by connecting plates, and the connecting plates are connected to the inner side of the outer ring of the rotor, and the hub is not connected, so as to form a square frame, a rectangular hole is formed on the outer ring of the rotor opposite to the square frame, the width of the rectangular hole is the same as the width of the semi-annular air chamber, the length of the rectangular hole is shorter than the distance between the two spokes, the front surface of the dynamic blade is tightly attached to one end face of the outer ring of the rotor, and the dynamic blade is vertically arranged in the rectangular hole, and the inner sides of the two connecting plates are designed as dynamic blade sliding channels for the dynamic blade.

4. A novel rotary engine according to claim 3, characterized in that: A positioning socket is arranged at the middle part of the front surface of the dynamic blade, three supporting rods No. 1 are arranged on the back surface of the dynamic blade, one of the supporting rods No. 1 is arranged at the upper half of the dynamic blade and corresponds to the center of the semi-annular air chamber, a supporting rod sleeve is arranged at the position, a supporting rod is arranged between the supporting rod No. 1 and the supporting rod sleeve, the other end of the supporting rod No. 1 is connected to a double-jack by a hinge shaft, a fulcrum is arranged at the contact position between the supporting rod and the double-jack on the outer side of the hinge shaft, the other end of the double-jack is fixed to the middle of a supporting rod shaft No. 2, two shaft sleeves of the supporting rod shaft No. 2 are arranged on the connecting plates, the left end of the supporting rod shaft No. 2 is fixed with an L-shaped small crank, a roller left in a roller sliding channel left of a roller sliding channel disc is arranged on the end of the L-shaped small crank, and the right end of the supporting rod shaft No. 2 extends out of the connecting plate; The other two supporting rods No. 1 and the supporting rod sleeves are arranged at positions above the first supporting rod sleeve, the ends of the double-jacks are fixed to a supporting rod shaft No. 1 by keys, two shaft sleeves of the supporting rod shaft No. 1 are arranged on the connecting plates, the right end of the supporting rod shaft No. 1 is fixed with a rocker, an L-shaped small crank is arranged on the extended part of the right end of the supporting rod shaft No. 2, a roller right in a roller sliding channel right of a roller sliding channel disc is arranged on the end of the small crank, and a connecting rod is arranged between the shaft of the rocker of the supporting rod shaft No. 1 and the end of the shaft of the L-shaped small crank arranged on the right end of the extended part of the supporting rod shaft No. 2, so as to form a parallelogram.

5. A novel rotary engine according to claim 4, characterized in that: The top and both sides of the upper half of the dynamic blade which are in contact with the inner wall of the semi-annular air chamber are provided with sealing frames of the dynamic blade, the sealing frames are arranged in the grooves arranged on the top and both sides of the dynamic blade and are fixed to the dynamic blade by square nails, and the sealing frames have a movable space.

6. A novel rotary engine according to claim 5, characterized in that: The conical valve comprises a conical valve seat, a conical valve hole in the center of the conical valve seat, a jet nozzle communicated with the conical valve hole, a conical valve body above the conical valve hole, a conical valve rod at the upper end of the conical valve body, the diameter of the conical valve rod is consistent with the diameter of the conical valve hole, the conical valve rod is matched with a conical valve rod sleeve in a stator, a conical valve spring is arranged between the conical valve body and the conical valve rod sleeve, the conical valve rod tail is provided with a pull ring, the conical valve is opened by pulling the pull ring, and the pull ring is connected to a rocker No. 2 controlled by a main shaft control cam No.

1.

7. A novel rotary engine according to claim 6, characterized in that: The diameter of the jet port is smaller than the diameter of the conical valve hole of the conical valve.

8. A novel rotary engine according to claim 7, characterized in that: The automatic control device of the new rotor engine air flow is driven by the control cam one installed on the main shaft, the push rod is hinged on the control cam one, the adjusting joint is hinged on the other end of the push rod, the rocker three is installed on the adjusting joint, the rocker shaft of the rocker three is fixed on the second season plastic machine, the other end of the rocker three is hinged with the connecting rod, the connecting rod is hinged with the rocker two, the rocker shaft of the rocker two is fixed on the shell of the new rotor engine, the other end of the rocker two is arranged in the pull ring of the tail part of the conical valve, the main shaft drives the control cam one to rotate half a circle in the clockwise direction, the two protrusions on the control cam one and the two push rods on the two sides are lifted once, so as to drive the two conical valves to open once, the main shaft drives the cam to rotate one circle, the two conical valves will be opened automatically four times, four times of high pressure air are supplied to the air injection port, that is, the new rotor engine should be detonated four times.

9. A novel rotary engine according to claim 8, characterized in that: The oil injection nozzle is connected with the oil injection pump, the oil injection pump is automatically controlled by the control cam two installed on the main shaft, the water injection port and the combined water injection nozzle share or separately use the water injection pump, the water injection pump is also automatically controlled by the control cam two installed on the main shaft, the control cam two used by the oil injection pump and the water injection pump, the oil injection pump and the water injection pump should inject oil and water for a long time in each half circle of the main shaft.

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