Hydrostatic transmission system with electromagnetic control variations for vehicles including optional power generation and propulsion

Abstract

A geared electromagnetically controlled hydrostatic transmission system is disclosed for vehicles with optional electric power generation and propulsion. The system includes a generator / motor and one or more wheel or propeller type drives, the drive being formed by a supply case and a discharge case having a toroidal bore filled with spheres. The system allows thrust applied by a power source to be transferred to the drive and can be used in aircraft, marine or land vehicles.

Description

[Technical field]

[0001] The present invention relates to a hydraulic and electromagnetic circuit, both equipped with flexible and adaptable containing conduits, installed inside a vehicle, that allows the transmission of the thrust exerted by the rotational movement of its motor source to the propeller or propellers that propel it, and / or to one or more wheels that support and drive it, thanks to the variations available between both the motor and the drive support, in a transmission whose flow can be reversed during passage, thus reversing the vehicle direction while maintaining the motor rotation direction, or partially stopping this oil flow to avoid excessive friction. [Background technology]

[0002] The system comprises a generator integrated into a hydraulic circuit and an electromagnetic circuit, adapted to control the flow in the former and to supply the latter, as described below; the generator can also be used as a substitute engine for the vehicle in which it is installed.

[0003] The electromagnetically controlled hydraulic system presented herein has an internal flow direction reversible system which allows the driver to reverse in any vehicle as detailed below.

[0004] A bicycle in which the current transverse chain connecting the bottom bracket to the rear wheel is eliminated, which, taking into account the asymmetry of the forces exerted by the chain on both sides when the traction tension of the movement of the rear wheel from the pedals occurs, causes harmful stresses on the front and rear wheels; here the bottom bracket is constituted by a central disc between the two pedals and the wheel with an equally centered ring on the bicycle chassis; both parts are interconnected by a hydraulic circuit as described above and passed through by a balanced rotational power transmission fluid as will be described in detail.

[0005] In addition, the same method can provide optional synchronous drive to the front wheels, which is currently not possible, without losing any of the current quality and functionality.

[0006] On the other hand, having a generator integrated into the hydraulic circuit means that this energy can be used as an additional contribution to the force exerted by the cyclist, or alternatively, the electric motorcycle can recover energy when descending from any height.

[0007] The hydraulic and electrical circuits are integrated into the bicycle chassis, resulting in a higher aerodynamic coefficient than that of a conventional bicycle.

[0008] In any air, sea or land vehicle, the electromagnetically controlled hydraulic system presented here transfers energy by fluid pressure from the engine, whatever its source of power, to the propellers or wheels available on the vehicle that can be used for its propulsion and support; this allows the vehicle to be optimized in weight, since the transmission and generation of primary drive energy is reduced and the number of components is saved.

[0009] In land vehicles, any number of drive wheels may be at the operator's discretion.

[0010] In shipbuilding construction, hull penetrations suitable for shafts running from the engine to the propeller are avoided, as they sometimes cause unwanted waterways. In ships and aircraft, the flexibility of the propeller's power acquisition path allows it to be freely oriented in three dimensions on its support point, thus forming a steerable propeller for vertical lift or horizontal flight in aircraft, and for balancing horizontal thrust in ships with the rudder of any vehicle that integrates it.

[0011] Since, according to the research previously conducted, the device claimed herein does not currently exist, we hereby request, in view of its industrial applicability, to grant corresponding rights to the invention described below, the understanding of which is reinforced by a series of schematic drawings, in which a dotted line followed by a dot indicates the hollowness of the space through which the line is drawn, and where there are discontinuous lines, indicates that the part so indicated is hidden in the drawing.

[0012] For ease of explanation, it should be added above that the hydraulic transmission shown here occurs between a flow-emitting element, called a motor, and other receivers of said flow, generally called here action items, in any quantity described below; both motor and action elements are similar in their construction and are assumed to be installed opposite each other in two container bodies that are geometrically mirror images of each other, the difference being that one has a series of electric valves installed and the other does not, allowing a free flow as will be shown below; the first of such pairs receives the fluid and controls its circulation, while the second one discharges the same each time it receives it, and therefore these are called the supply casing and the discharge casing respectively.

[0013] Figure 1 is an exterior elevational view of the supply case with logo 0. The supply case (0) is constituted by a rigid, dense, pressure-resistant cylindrical container; its geometry is characterized in that it has:

[0014] Three equal projections, commonly called supply case hooks, under their respective designations in this figure, numbered 12, 13 and 14, each pierced by a respective threaded cylindrical hole.

[0015] A coaxial hole passing through the center of the cylindrical body of the same (0), hereafter referred to as the supply caseway and designated by the reference number 11.

[0016] A cylindrical cavity, on its hidden side in this view, of a certain depth and coaxial with it (11); here called the feed casing cavity, the concave surface shown with the number 1.

[0017] Laterally to said supply case (0) opens a lateral duct, designated 2 and hidden in this figure because it is located inside the supply case (0), which is called the supply duct; this (2) has its beginning outside the supply case (0) and communicates continuously with three solenoid valves, each located at a different radius of the cavity (1), designated in this figure as the low solenoid valve with the reference number 3, the intermediate solenoid valve with the reference number 4 and the high solenoid valve with the reference number 5.

[0018] A cylindrical hole, called the feed case counter, designated 101, runs parallel to and beyond the feed caseway (11) and connects the two bases of the feed case (0).

[0019] Figure 2 shows the side view of the discharge case. As mentioned before, except that the supply case (0) incorporates three solenoid valves (3, 4 and 5), for the purposes of illustration and to distinguish them diagrammatically, the geometries of both cases are mirror images of each other, and in all figures the annotation of the parts depicted on the discharge case differs from that shown in the previous figures, with their symbols preceded by the number 0.

[0020] A coaxial hole, designated 011 and henceforth referred to as the discharge caseway, runs through the centre of the cylindrical body of the discharge case (00).

[0021] Thus, Emblem 00 represents a right-hand view of the cut made by a line with an arrow to the left drawn in the previous diagram, and corresponds to its symmetrical twin sister, Supply Case (0).

[0022] So we: Three equal projections, two of which are not visible in this view, are pierced by respective threaded cylindrical holes commonly called discharge case couplings, the upper one of which is here designated by the number 012.

[0023] A cavity of fixed depth, cylindrical shape, and coaxial with the discharge case (00), called the discharge case cavity, designated by the number 01.

[0024] A coaxial hole, numbered 011, passes through the discharge case (00) through the center of its cylindrical body; this hole will hereafter be referred to as the discharge caseway.

[0025] Above the discharge caseway (011), there is a cylindrical hole that connects the two bases of the discharge caseway (00), which is called the discharge case counter and is designated by the symbol 0101.

[0026] The semi-toroidal channel opens into the wall of the discharge case sinus (01) and is concentric with it (01); it is called the discharge rolling channel and is indicated by the symbol 06 on its underside.

[0027] One can see the opening of the exhaust duct, designated 02, which starts from the outside of the exhaust case (00) and communicates with it (02) an opening conduit called the lower outlet, initialed 03, which is a channel at its opening towards the exhaust case cavity (01).

[0028] Behind the low outlet (03) and therefore not specified as hidden in this view, the intermediate and high outlets open successively from the exhaust duct (02); the three outputs, namely low (03), intermediate and high, are respectively opposite in their assemblies in the system with the low (3), intermediate (4) and high (5) solenoid valves located in the supply case (0), as can be seen.

[0029] Similarly, the openings correspond to a series of semi-toroidal grooves of different radii, made in the wall of the drainage cavity (01) and concentric with it (01), which are designated and known as: →Anagram 07 is a high-level discharge static joint channel. →Anagram 08 is a mid-high discharge static joint channel. →Anagram 09 is a mid-low discharge static joint channel. →Anagram 010 is a low discharge static joint channel.

[0030] Figure 3 shows a top view of the feed case cut by the line of the downward arrow shown in Figure 1; in the present figure the notation of Figure 1 is repeated, except that in Figure 1 a semi-toroidal channel has been added, opening into the wall of the feed case (0) and concentric with it (0), called the feed rolling channel, and indicated by the reference numeral 6 on its downward slope.

[0031] The diameter of both static rolling channels: supply (6) and discharge (06) is the same.

[0032] FIG. 4 shows an elevational view of the exterior of a cylindrical part, referred to as the motor rotor, designated by the numeral 29 and detailed therein.

[0033] It can be seen that there is a semi-toroidal opening, designated by the number 17 and called motor rolling channel one, centered on its side (29), which is hidden in this state.

[0034] The motor rotor (29) is centrally and coaxially pierced with a hexagonal opening referred to herein as a power take-off, designated by the numeral 30.

[0035] At the base of the motor rotor (29) is found a series of semi-toroidal recesses opening therein, designated and known as: Anagram 18 is the upper channel supply motor joint. Anagram 19 is a mid-high channel supply motor joint. Anagram 20 is a low to mid channel supply motor joint. ·Anagram 21 is the lower channel supply motor joint 21.

[0036] The central hexagonal hole that is coaxial with the motor rotor (29) is called the power takeoff and is indicated by the number 30.

[0037] The motor rotor (29) is traversed diagonally from base to base by three concentric series of holes, each set of separating blades being known as the large motor turbine, the medium motor turbine, and the small motor turbine. The illustration shows several spans identified by the following numbers: 22, 25 and 28 for the large motor turbine, 24 and 27 for the medium motor turbine, and 23 and 26 for the small motor turbine.

[0038] Above the power take-off (30) there is a cylindrical hole which vertically connects the two bases of the motor rotor (29); this is called the motor counter and is designated by the reference number 201.

[0039] The vertical line with the arrow on the left side indicates the cross section shown in the following figure.

[0040] Figure 5 shows a right side view of the aforementioned section of the motor rotor (29) with the same designation as in the previous figure, but now showing in the upper sector a new semi-toroidal opening called motor rolling channel two, designated by the number 17'. Both motor rolling channels (17 and 17') are identical to each other, symmetrical with respect to the motor rotor (29), and have a diameter equal to that of the bearing balls described below.

[0041] At the two bases of the motor rotor (29), it can be seen that the respective channels of the movable motor joint are open; the one located on the left is the one visible in the previous drawing, and the one located on the right is called the one located on the right side, and on their respective upper slopes are indicated as follows: Top channel discharge motor joint with anagram 18'. ·Middle-lower channel discharge motor joint shown in anagram 19'. ·Middle-high channel discharge motor joint shown in anagram 20'. ·Lower channel discharge motor joint indicated by anagram 21'.

[0042] In this illustration, some of the bays are shown, identified by numbers: 22, 25 and 28 for the large motor turbines, 24 and 27 for the medium motor turbines, and 23 and 26 for the small motor turbines. The openings (22) represent the inclination of all of them with respect to the base of the motor rotor (29).

[0043] In Fig. 6 an elevational view of the new rotor is shown, which is called the wheel rotor and designated by the anagram 129, and which is identical in physical construction to the motor rotor (29), except that the outer ring is rigidly fixed to it (129) and the power take-off (30) is replaced by a cylindrical opening called a vain and designated by the reference number 130. Being essentially the same as the motor rotor (29), the parts of the wheel rotor (129) are designated by the same numbers as the previous (29), but with the addition of a 1 in front of each number, and they are known by the same names, in that the term motor is replaced by wheel.

[0044] In the opening indicated by the reference numeral 130, a cylindrical hole is formed which vertically connects the two base parts of the wheel rotor (129), which is called a wheel counter and is indicated by the reference numeral 301.

[0045] FIG. 7 shows a view from the right side of the wheel rotor (129) cut along the line with the arrow to the left shown in the previous figure, repeating the notation with the addition of a symmetrical semi-toroidal slot to the wheel rotor (129), designated by the number 117', which is identical to wheel rolling channel one (117) and called wheel rolling channel two; both wheel rolling channels one (117) and two (117') have a diameter equal to the diameter of the bearing balls described below.

[0046] At the two bases of the wheel rotor (129) it can be seen that two channels of the movable motor joint are open; the one located on the left is the one visible in the previous drawing, while the one located on the right is called the one located on the right side and is indicated on the upper slope of each as follows: ·Top channel ejection wheel joint indicated by anagram 118'. · Upper mid channel ejection wheel joint with anagram 119'. ·Lower mid channel ejection wheel joint with anagram 120'. · Lower channel ejection wheel joint indicated by anagram 121'.

[0047] In this illustration, some of the openings are shown, identified by 125 and 128 for the large wheel turbine, 124 and 127 for the medium wheel turbine, and 123 and 126 for the small wheel turbine.

[0048] FIG. 8 is an elevational view of the new rotor, which in its physical configuration is the same as the wheel rotor (129), except that it does not have an outer ring rigidly fixed to it, but rather incorporates the fixed blades of a propeller in its center, therefore recognizing it as a propeller rotor, indicated by the anagram 229; reference number 230 denotes the opening between said blades, called the propeller path.

[0049] Being essentially the same as the motor rotor (29), the parts of the propeller rotor (229) are designated with the same numbers as the previous (29), but with the addition of a 2 before each number, and are known by the same names with the term motor replaced by propeller.

[0050] When the two bases of the propeller rotor (229) are connected vertically, a cylindrical orifice opens on a helical path (230), which is called the propeller counter and is indicated by the reference number 301.

[0051] In FIG. 9, a view from the right side of the propeller rotor (229) cut by the line with the arrow on the left side shown in the previous figure is shown, repeating the notation with the addition of a symmetrical semi-toroidal gap to the propeller rotor (229), designated with the number 217', which is identical to propeller rolling joint one (217) and which is called propeller rolling joint two; both propeller rolling joints one (217) and two (217') have a diameter equal to the diameter of the bearing balls described below.

[0052] At the two bases of the propeller rotor (229) it can be seen that two channels of the propeller rolling joint are open; the one located on the left side is the one visible in the previous drawing, while the one located on the right side is called, and on the upper slope of each is indicated as follows: ·Upper channel propeller discharge joint indicated by anagram 218'. · Mid-lower channel propeller discharge joint shown by anagram 219'. Mid-high channel propeller discharge joint with anagram 220'. ·Lower channel propeller discharge joint indicated by anagram 221'.

[0053] In this illustration, some of the bays can be seen, identified by 225 and 228 for large propeller turbines, 224 and 227 for medium propeller turbines, and 223 and 226 for small propeller turbines.

[0054] Fig. 10 is an external elevational view of the pinion, designated 16; it (16) has a rigid cylindrical center opening on its central axis by a six-point star gear, and six teeth made of a resistant but flexible material surrounding the cylindrical center and forming with it (16) a single immovable part, the length of which is sufficient to allow the pinion (16) to fit completely into the power take-off (30), as can be seen in Figs. 12, 13, 14 and 15.

[0055] FIG. 11 shows a side view of the pinion (16) and is designated with the same reference numerals as in the previous figures.

[0056] Figure 12 is a cross-sectional view of the motor rotor (29) seen in Figure 4, removed from the outer edge of the mid-high channel feed motor joint (19). In keeping with the designations and references in this figure, the pinion (16) is now mounted inside the power takeoff (30).

[0057] Figures 13, 14 and 15 are repeats of the previous ones, except for the respective arrows depicted in each. The reasons for this repetition of images and the variety of arrows will be discussed in the description.

[0058] FIG. 16 shows a rigid sphere, designated as 89 and called a sphere; the sphere (89) has the same diameter as the supply (6) and discharge (06) rolling channels of the motor rotors (17 and 17'), the wheel rotors (117 and 117'), and the propeller rotors (217 and 217').

[0059] FIG. 17 shows an elevational view of an O-ring, referred to herein collectively as a joint designated by the numeral 88; the joint (88) is capable of sealing against fluid leakage between the two bodies that house it.

[0060] FIG. 18 represents a side view of the joint of the same name.

[0061] FIG. 19 is a side view of a cylindrical threaded connection element, here generally called the anchor, designated by the number 15. The anchor (15) provides a rigid and immovable fixation between the two cases, the supply (0) and the discharge (00), and therefore has the same thread profile as the discharge hooks (012, 013 and 014) of each of those (00 and 0) cases and the supply (12, 13 and 14); moreover, both (0) and (00) are firmly and stably linked with the structure of the vehicle they serve. In view of the many repetitions in this description, in its specific designation the number 15 is used, with other numbers appended in subscripts and superscripts, as the following will explain.

[0062] FIG. 20 shows an elevational view of a pressure-resistant hydraulic fluid communication hose, which may optionally be rigid or flexible; known as a sleeve, designated by the number 31 and whose channel is indicated by the reference number 32; the conduit (31) is suitable to communicate, through either of its two ports, while remaining sealed from the outside, with the different elements constituting the hydraulic system claimed in this specification.

[0063] FIG. 21 is a vertical diametrical cross-sectional view of a swivel ball joint arrangement formed by:

[0064] a. A vehicle, so called and designated by the number 60; which (60) has a cylindrical hole on the right hand side, which is tightly closed by a ring, and therefore may be understood by marking its underside with the number 59.

[0065] Furthermore, the vehicle is marked with the number 67 in the visible area. 1 It is equipped with an electric motor with a 67 1 ) comprises a transmission gear with its blades in the open space between the carriage (60) and the ring (59); at the ends of their terminals are visible the symbols of their respective polarities.

[0066] b. A cylinder of rigid material, called a guide, numbered 60 1It has a gear at its right end and a director (67 1 )Same as the gear above.

[0067] In addition, the guide (60 1 ) are fitted with what are called electric motors; at the ends of their terminals the signs of their respective polarities can be seen.

[0068] At its left end, it rounds off its base and terminates in a hemisphere.

[0069] c. Rigid bond, no. 60 2 known as a bond; it consists of two prismatic bars forming a single body, a larger one on the left and a smaller one on the right.

[0070] The left end of the larger rod is convexly rounded, adjacent to which is a cylindrical hole into which the anchor (15) can be assembled; to the right of this is a guide (60 1 ) has rounded sides, this time concave, of the same radius as the concave surface of the hemisphere mentioned above.

[0071] From the center of the recess, the elevator (67 2 ) a smaller rod appears, with a fixed gear at its final end which is the same as the one in

[0072] Links(60 2 The arrow that appears on the elevator (67 2 ) operation guide (60 1 ) indicates the possibility of rotating relative to the

[0073] Guide(60 1 The arrows that appear on the 1 ) indicates the possibility of turning relative to the vehicle (60).

[0074] Fig. 22 is an elevational view of the pedal, which is here designated and known as 61. At its right end is shown a six-point star gear which meshes with the gear of the pinion (16) already mentioned.

[0075] Figures 23, 24, 25 and 26 represent elevational views of a parallelepiped made of a rigid, compact and pressure-resistant material known as an inverter, designated by the reference number 69. The body of the inverter (69) is traversed on the left and right by two parallel ducts perpendicular to the walls of the inverter (69).

[0076] Both ducts are subdivided by two centrally placed solenoid valves, detailed below, and the sectors of the ducts are known as: · An upper right channel, located above and to the right of the inverter (69) and designated by the number 70. · The upper left channel, located above and to the left of the inverter (69), designated by the number 71. · A lower right channel, located below and to the right of the inverter (69) and designated by the number 72. · The lower left channel, located below and to the left of the inverter (69) and designated by the number 73.

[0077] The top right channel (70) and the bottom left channel (75) are interconnected by a pipe, designated pipe a, indicated at 74, which passes over another pipe, designated pipe b, indicated at 75, which is used to connect the bottom right channel (72) to the top left channel (71); there is no connection between both pipes, a (74) and b (75).

[0078] The openings of the upper channel (70) and the lower channel (71), as already pointed out, are both connectable to the ends of the hydraulic conduits (31) and maintain a seal at their respective junctions, joining either its channel a (70) or its channel b (75) with the channel (32) of the hydraulic conduit (31) attached thereto.

[0079] The inverter (69) has the following solenoid valves: An upper valve, designated with the numeral 76, is located between the upper right channel (70) and the upper left channel (71). A lower valve, designated with the numeral 77, is located between the lower right channel (72) and the lower left channel (73). A reversing valve a, designated by the number 78, is installed inside the pipe a (74). A reversing valve b designated by the number 79 is installed inside the pipe b (75).

[0080] The differences between Figures 21, 22 and 23 will be noted in the following description.

[0081] FIG. 27 shows an elevational view of a body made of a rigid, compact, electrically insulating material, known as a generator / motor, designated by the numeral 36, and open:

[0082] Two ducts, parallel to each other, traverse each other to the left and right and are called respectively the free passage detailed as 38 and the energy passage indicated at 39 .

[0083] The electric heater thermostat, called heater, is designated 37 which also constitutes a watertight separation between the free passage (38) and the energy passage (39). The terminals with the plus and minus signs can be seen.

[0084] The heater (37) has a length such that it provides paths at its upper and lower ends such that the free passage (38) and the energy passage (39) communicate with each other and converge at both locations at a single opening.

[0085] Seen here is a cylindrical blind hole open only at its base, referred to herein as a rotational cavity, designated by the reference numeral 40.

[0086] The energy passage (39) is in tangential communication with the rotational cavity (40).

[0087] Fig. 28 shows an element known as an inductor, designated 42, consisting of a rigid, dense disk having a series of radial blades of equal thickness forming a unitary body with it (42). These blades are dense, rigid and magnetized, maintaining homogeneity in their particular magnetic field, so that their respective most radial poles are of the same sign.

[0088] The overall diameter of the inductor (42) is the same as the diameter of the rotation cavity (40) so that the inductor can rotate therein while maintaining a seal at their mutual contact areas.

[0089] FIG. 29 is an elevational view of the lid, a rigid, dense parallelepiped intended to cover and seal the rotating cavity (40); we will call it the lid here and denote it by the reference number 43.

[0090] FIG. 30 is an elevational view of a cell, on which are shown the two poles, respectively marked + and -; this is known as a battery, and is designated by the number 52.

[0091] FIG. 31 shows an elevational view of a multitasking electronic control device designated control at 53.

[0092] FIG. 32 shows an elevational view of an interactive electromagnetic data management screen designated as manager by the numeral 54.

[0093] FIG. 33 shows an elevational view of an electric coil, designated by the symbol 41 as an armature; the terminal ends of the armature are marked with the symbols for their respective polarities.

[0094] FIG. 34 shows an elevational view of an adjustable pitch solenoid valve, commonly referred to as a regulator, here designated by the numeral 50; the terminal ends are marked with their respective polarity symbols.

[0095] FIG. 35 shows an elevational view of a photocell, and as such is designated by the designation 100; the ends of the photocell are marked with the symbols for their respective polarities.

[0096] FIG. 36 shows an elevational view of the focal point of an electric lamp, designated by the reference numeral 110; the ends of the terminals are marked with the symbols for their respective polarities.

[0097] Figure 37 shows an elevation view in a horizontal position of an electronic level, which forms a fixed part of the vehicle structure on which it is installed and consists of a rigid, compact and electrically insulating parallelepiped, which will be referred to as the level, designated by the reference numeral 111, having two open spaces within its body without any openings to the outside.

[0098] The body of the level (111) is traversed by four vertical conductors, each designated at its end with its own electrical polarity.

[0099] The interior of these spaces contains an amount of dielectric liquid required to fill it halfway.

[0100] In the lower portions of both vessels, the dielectric contained therein is designated with the numbers 1131 and 1132 respectively, while the respective upper gas chambers are designated with the numbers 1121 and 1122.

[0101] FIG. 38 repeats the previous one, but now the level (111) is tilted to the right, the results of which are detailed in the description.

[0102] FIG. 39 repeats the previous one, but now the level (111) is tilted to the left, the results of which are detailed in the description.

[0103] Figure 40 shows an elevational view of the entire electrical device, with electrical interconnections typical of the system claimed herein. Its parts and components have already been described in detail in the previous figures and are here marked with the same reference numerals:

[0104] The generator / motor (36) having armature (41) fixedly integrated therein is mounted in the wall of a rotating cavity (40) which constitutes its stator; an inductor (42) is housed therein with a rotating capacitance.

[0105] The rotating cavity (40) thus arranged is said to be permanently isolated from the outside by the cover (43).

[0106] Located within the upper beginning of the free path (38) is a path regulator (50), which will be referred to herein as a free path regulator to distinguish it from its cousins, and located at the upper beginning of the energy path (39) is an energy step regulator, designated by the reference numeral 50'.

[0107] The sleeve (31) is connected to the top of the generator / motor (36) and keeps it sealed from the outside so that its channel (32) opens to the free (38) and energy (39) passages; it is referred to herein as the arrival sleeve.

[0108] A second sleeve, here indicated as 031, is connected to the lower part of the generator / motor (36) and keeps it sealed from the outside so that its channels, here indicated as 032, lead to the free (38) and energy passages (39); here referred to as the outlet sleeve. A battery (52) electrically connected to the generator / motor (36) and control (53). Electrically connected control (53): Electronic level(111). Manager(54). Low (3), intermediate (4), and high (5) motor rotor case solenoid valves. Solenoid valves in either the wheel or propeller case, low (03), mid (04) and high (05). Light bulbs (100). Photocell (110). Top valve(76). Lower valve (77). Reversing valve a(78). Reversing valve b(79). Free passage regulator (50). Energy Step Regulator (50'). Heater(37).

[0109] Figure 41 is an elevational view of an assembly including a supply case, designated by the numeral 0, inside which (0) is located a motor rotor (29) with a pinion (16) attached to its power takeoff (30). Of the solenoid valves in (0), the lower one (3) is shown.

[0110] Specify the name by adding a subscript number to the end of the existing name:

[0111] Also shown in the figure is the bay for the main motor turbine (28).

[0112] The three anchors are listed as 151 top, 152 bottom left, and 153 bottom right.

[0113] The trio (151, 152 and 153) constitute a rigid and stable mooring for the feed casing (0) with two sections of the vehicle detailed with the numbers 601 and 602 respectively.

[0114] A section of a portion of the sleeve (31) having its channel (32).

[0115] The light source (100) can be seen through the motor counter (201) mounted on the power supply counter (101) because the rotation angle of this (201) aligns its opening with (100).

[0116] For the purpose of introducing the motor rotor (29) inside (01) of the discharge casing (00), four toroidal holes appear, their respective joint channels being created by opposing each other; each of them has a board called and designated as follows:

[0117] · The upper discharge joint is shown on its underside with the number 884 and fills the toroidal joint created by the opposing channels of the upper discharge static joint (07) and the upper discharge motor joint (18').

[0118] The mid-high discharge joint is indicated on its underside with the number 813' and fills the toroidal joint created by the opposing channels of the static mid-high discharge joint (08) and the upper motor joint (219').

[0119] · The lower-middle discharge joint is shown on its underside with the number 812' and fills the toroidal joint created by the opposing lower-middle discharge static joint channel (09) and the upper motor joint channel (20').

[0120] The low discharge joint is indicated on its underside with the number 811' and fills the toroidal joint created by the opposing mid-high discharge static joint channel (10) and the upper motor joint channel (21).

[0121] The assembly is firmly and stably joined by three ties, of which only the upper one (155) is visible, resulting in a supply case (0) and a discharge case (00 1 ) passes through it (158) and houses the motor rotors (29) and their respective cavities (1 and 01) (0 1 and 00 1 ).

[0122] FIG. 42 is an elevational view corresponding to the assembly of the exhaust case (00) with the wheel rotor (129) partially disposed within the cavity (01) as its ring protrudes from it (00).

[0123] In the diagram, the following is shown: Discharge Case(00). Medium output (04). A sleeve section (31) is adjacent to the section seen in the previous figure, with its channel (32). The four joints already claimed in the previous diagram are identical in their respective categories and their numbering coincides with that already established. Bay of large motor turbines (28). Three anchors: top anchor 154, left bottom anchor 155, and right bottom anchor 156. The trio (154, 155 and 156) constitute a rigid and stable fixation of the vehicle's three section exhaust case (00) and are detailed with the numerals 601', 602' and 603' respectively.

[0124] The rotation angle of the wheel rotor (129) means that the opening does not coincide with the lighting device or sensor installed in the exhaust casing counter (0101), so the wheel counter (301) can be seen, but the light source cannot be seen through it.

[0125] It is marked with the number 500 and one can see the ground on which the wheel rotor (129) rests.

[0126] FIG. 43 is a side view representation of a diametric cross section of a complete motor arrangement formed by: Supply cases that can be monitored (0 1 ): Its supply duct (2). its low (3), middle (4), and high (5) solenoid valves. A sensor (110) disposed within the supply case counter (101). Motor rotor(29). Discharge Case (00) shows: The exhaust duct (02). Its low (03), medium (04) and high (05) outputs. A light bulb (100) placed in a discharge case counter (0101). Number 89 1 and 89 2and are part of a set of the same which fill the gap created by the opposing supply rolling channel (6) and the motor rolling one channel (17) I which appear for the purpose of introducing the motor rotor (29) inside (01) of the supply case (01).

[0127] Number 89 3 and 89 4 The two spheres are designated by the discharge case (00 1 ) for the purpose of inserting the motor rotor (29) on its inside (01), it is part of a set of the same filling the toroidal hole created by the opposing discharge rolling channel (06) and the motor rolling tool channel (17').

[0128] Supply Case (0 1 ) inside the cavity (1) of the rotor (29) four toroidal cavities appear, their respective joint channels being created by their opposition; in each of them there are joints called and designated as follows:

[0129] A high supply joint, indicated at its lower slope with the number 814, fills the channel of the high supply static joint (7) and the channel of the upper supply motor joint (18).

[0130] A mid-high supply joint, shown on the lower bevel with the number 883, fills the mid-high supply static joint channel (8) and the mid-high supply motor joint channel (19).

[0131] A low-middle feed joint, shown on the lower bevel with the number 882, fills the mid-high feed static joint channel (9) and the mid-low feed motor joint channel (20).

[0132] A mid-high feed seal, shown on the lower bevel at 881, fills the low feed static seal channel (10) and the low feed driven seal channel (21).

[0133] For the purpose of introducing the motor rotor (29) inside (01) of the discharge casing (00), four toroidal holes appear, their respective joint channels being created by opposing each other; in each of them there are boards called and designated as follows:

[0134] A high discharge joint, shown on its lower side with the number 88'4, fills the toroidal gap created by the opposing channels of the high discharge static joint (07) and the upper discharge motor joint (18').

[0135] A mid-high discharge joint, shown on the lower side with the number 88'3, fills the toroidal gap created by the opposing channels of the mid-high discharge static joint (08) and the upper motor joint (219').

[0136] The lower intermediate discharge joint, shown on the lower slope with the number 88'2, is connected to the lower intermediate discharge static joint channel (09) and the upper motor joint channel (20 1 ) and fill the toroidal gap created by their opposing forces.

[0137] A low discharge joint, shown on the lower side with the number 88'1, fills the toroidal gap created by the opposing channels of the mid-high discharge static joint (10) and the upper motor joint (21).

[0138] The assembly is firmly and stably joined by three ties, of which only the upper one (155) is visible, resulting in a supply case (0) and a discharge case (00 1 ) are traversed by it (158) and house the motor rotors (29) in their respective cavities (01 and 00 1 ).

[0139] The motor rotor (29) is here dominated by a pinion, hidden for the sake of graphic clarity, which is traversed by pedals (611 and 612) firmly attached thereto.

[0140] It can be seen how the assembly is secured to a section of the vehicle (60) by anchors (155).

[0141] Moreover, it is intimately connected to the outside world in its cohesion:

[0142] For the supply duct (2) there is a sleeve section (311) having the channel (321).

[0143] For its discharge conduit (02) there is a sleeve section (312) with its channel (322). Figure 44 shows the external side view of the motor assembly resulting from the combination of two complete motors; the assembly is rigidly and stably joined by three anchors, of which only the upper one (155) is visible, so that each supply (0 1 and 0 3 ) and discharge(00 1 and 00 3 The case is traversed by this (155) and aligned with the two drive rotors (291 and 292) (0 1 and 00 1 ) and (0 3 and 00 3 ) is housed.

[0144] It can be seen how the assembly is secured to the two sections of the vehicle (60) by anchors (155).

[0145] Therefore, the discharge casing of the element furthest to the left (00 1) are glued to the supply casing (03) of the element located on the right side and align the respective casing tracks, not seen here, and thus also the respective power intakes of the motor rotors (291 and 292), here occupied by their respective pinions and hidden for clarity of illustration, are traversed by pedals (613 and 614) firmly mounted thereon.

[0146] The light source (100) can also be seen, as can the discharge case (00 3 ) in the discharge case counter (101) and the sensor (110) is disposed in the supply case counter (101) of the supply case (01).

[0147] It also connects its supply duct (2) to the sleeve section (311) with its channel (321), maintaining intimate contact with the outside of their assembly.

[0148] For the supply conduit (2) there is a sleeve section (311) having the channel (321).

[0149] For the exhaust duct (02) there is a sleeve section (312) having the channel (322).

[0150] Both are continuations of the sleeves seen in the previous figure and are numbered the same.

[0151] FIG. 45 corresponds, for reasons of clarity of illustration, to an exterior elevation of the complete propeller assembly, excluding its case and supply ducts.

[0152] Supply casing and discharge casing, here designated 00 4 The assembly formed by the latter having the casings (00) is firmly and stably joined by three anchors, designated respectively by the numbers 157, 158, and 159, so that both casings house a propeller rotor (229) which can rotate within each cavity. The upper right anchor (157) is connected to the supply and discharge casings (004 ) to the orientation device (60 1 ) and the other link (60 2 ) is that (60 1 ) to the vehicle (60), so that the propeller device is controlled by the pilot of the aircraft, ship or utility vessel, as the case may be, in the form of a director (67 1 ) and / or elevators (67 2 ) may be used to orient in any direction.

[0153] The exhaust casing (00) is shown incorporating the propeller rotor (229) within its cavity (01) such that it (01) is hidden by it (229). Additionally, its elevated outlet (05) and exhaust conduit (02) are shown, which has a sleeve section (313) connected to the outside at its outlet to keep it in close contact with the surrounding environment, so that its channel (323) is an extension of it (02).

[0154] The same symbols used previously may be used to denote the different joints.

[0155] FIG. 46 is a diametrical cross-sectional view of a complete wheel arrangement formed by: Supply case that can be monitored (0 5 ): Its supply duct (2). The low (3), intermediate (4), and high (5) solenoid valves. Wheel rotor(129). Discharge Case (00 5 ) shows: The exhaust duct (02) Its low (03), medium (04) and high (05) outputs.

[0156] Number 89 2 and 89 4 The two spheres are designated by the discharge case (00 5) which fills the toroidal hole created by the opposing discharge rolling channel (06) and channel rolling wheel two (117') that appears when inserting the wheel rotor (129) inside the

[0157] By introducing the wheel rotor (129) inside (1) of the supply case (0), it appears that four toroidal holes are created by opposing joint channels; in each of them there are boards called and designated as follows:

[0158] The high feed seal is indicated at 884 on its underside and fills the high feed static seal channel (7) and the upper feed wheel seal channel (118).

[0159] A mid-high feed joint, shown on the lower slope with the number 883, fills the mid-high feed static joint channel (8) and the mid-high feed wheel joint channel (119).

[0160] A mid-low feed seal, shown at the bottom incline with numeral 882, fills the mid-high feed static seal channel (9) and the mid-low feed wheel seal channel (120).

[0161] A mid-high feed seal, shown at the bottom incline with numeral 881, fills the low feed static seal channel (10) and the low feed wheel seal channel (121).

[0162] For the purpose of inserting the wheel rotor (129) inside (01) of the discharge casing (00), four toroidal holes appear, their respective joint channels being created by opposing each other; in each of them there is a board called and designated as follows:

[0163] A high discharge joint, shown on its lower side with the numeral 884', fills the toroidal gap created by the opposing channels of the high discharge static joint (07) and the upper discharge wheel joint (118').

[0164] A mid-high discharge joint, shown on the lower side with the number 883', fills the toroidal gap created by the opposing channels of the mid-high discharge static joint (08) and the upper wheel joint (119').

[0165] A lower mid-discharge joint, shown on the lower bevel with numeral 882', fills the toroidal gap created by the opposing lower mid-discharge static joint channel (09) and the upper wheel joint channel (220').

[0166] A low discharge seal, shown on the lower side with the numeral 881', fills the toroidal cavity created by opposing channels of the mid-high discharge static sole (10) and the upper wheel seal (121).

[0167] The assembly is held together firmly and stably by three ties, of which only the upper one (154) is visible, and as a result, the supply casing (0 5 ) and exhaust casing (00 5 ) passes through the one provided by it (158) and houses the wheel rotors (229) and their respective cavities (1 and 01) (0 5 and 00 5 ).

[0168] It can be seen how the assembly is secured to a section of the vehicle (60) by link (155), as well as the other two links.

[0169] Moreover, it is intimately connected to the outside world in its cohesion:

[0170] For the supply duct (2) there is a sleeve section (315) having the channel (325).

[0171] For the discharge conduit (02) there is a sleeve section (316) with a channel (326). With the number 500 one can see the ground on which the wheel rotor (129) rests.

[0172] The upper anchor, currently designated 154, is the vehicle (60), where each code 0 5 and 00 5 As shown in Fig. 1, the supply and discharge casings are fixed and a director (60 1 ) while the wheel device is inserted, the pilot of the aircraft, ship or multi-purpose vehicle, depending on what it is, inserts the director (67 1 ) or elevator (67 2 ) to allow the link (60) to be oriented in any direction. 2 ) are both of them (60 and 60 1 ) to combine.

[0173] On this basis, one understands an electromechanical structure mounted on a vehicle intended to transmit energy hydraulically through a reciprocating closed circuit completely filled with oleo-hydraulic fluid, a driving force applied to a rotary motor device, which is fixed to the vehicle on which it is mounted and to a device for transmitting said force providing forward movement of said vehicle (60), which in the case of a land vehicle is a wheel device (129), in the case of an air or sea vehicle a propeller device (229), or in the case of a multi-purpose vehicle both (129 and 229).

[0174] Both the wheel assembly (129) and the propeller (229) are rigidly fixed to the vehicle (60) which they serve, but when connected to it (60), both (129 and 229) have the ability to pivot independently in three dimensions, since this joint is made up of respective electric rotational ball joints, as already shown in Figures 42, 45 and 46, which are capable of providing such orientation.

[0175] The drive unit can be powered in its rotation by energy applied by the cyclist pressing with his legs against the pedals (61 and 61') of the bicycle, which requires their appropriate placement (61 and 61') within the vehicle for effective pedalling, or by any type of motor suited to said main purpose, so that the position of the motor element depends on the vehicle in question.

[0176] Both the drive element and the propeller have essentially the same physical structure, but differ in that, as can be seen from the figure, the drive element incorporates several pedals (61) or pinions (16) with which the motor engages as the case may be, while the wheel incorporates a ring on its rotor (129) that allows it to propel itself stationary relative to the ground, and the propeller incorporates several blades on it (229) that are compressed behind them by the liquid or air fluid that surrounds them.

[0177] In this embodiment, the position and ability of the motor rotor (29), wheels (129) and propeller (229) to rotate properly in the aforementioned positions is determined by two series of balls (89 1 ~89 3 and 89 2 ~89 4 ), which spheres guide and separate the respective containers (0 and 00) at a distance, allowing the sealing action of two sets of joints located between the three elements as shown in Figures 43 and 46.

[0178] As seen in Figure 13, the motor rotor (29) has a pinion (16) mounted on its power take-off (30) and when it rotates (16) counterclockwise, its teeth come into contact with the apex of its power take-off (30) without the possibility of bending, so that the drive rotor (29) rotates with its thrust in that direction; whereas, as seen in Figure 14, when the pedal rotates clockwise, the teeth (16) bend and slide on the wall of the power take-off (30), so that the drive rotor (29) remains stationary; the same thing happens when the rotation of the drive rotor (29) is faster than that of the variable pinion (16), as shown in Figure 15, due to the deceleration or cessation of pedaling for the hydraulic traffic inside it (29). For example, as happens when a wheel rotor (129) rotates at high speed while descending a slope, or when an aircraft propeller rotor (229) descends in full flight.

[0179] Each of said devices therefore consists of a vessel made up of two casings, one for the supply and the other for the discharge (00); as is known, the first (0) has three solenoid valves after its supply duct (2), namely low (3), medium (4) and high (5), while the second (00) has low (3), medium (4) and high (5) outputs after its duct discharge (02).

[0180] In each of the three cases, both shells (0 and 00) are joined by anchors (15) which show the respective sinuses (1) and (01) facing each other, so that by inserting, statically or movably, the corresponding joint channels of the matching joints (88), three supply spaces and three discharge spaces, namely upper, middle and lower, are created.

[0181] In addition, the motor rotor (29), the wheels (129) and the propeller (229), inserted in each of the above-mentioned cases between both casings (0 and 00), each have three open turbines, the blades of which are arranged at different radii and obliques with respect to the base of the disk in which they are incorporated; these are:

[0182] The largest motor turbine (22, 25 and 28 in Figs. 4 and 5) communicates with the upper intake space and the upper discharge space.

[0183] An intermediate motor-turbine (24 and 27 in Figs. 4 and 5) communicating with the intermediate supply space and the intermediate discharge space.

[0184] A small motor turbine (23 and 26 in Figures 4 and 5) connects the lower intake space with the lower discharge space.

[0185] The largest turbine wheel (122, 125 and 128 in Figs. 6 and 7) communicates the upper intake space with the upper exhaust space.

[0186] A half-wheel turbine (124 and 127 in Figs. 6 and 7) communicating the intermediate supply space with the intermediate discharge space.

[0187] A minimum wheel turbine (123 and 126 in Figs. 6 and 7) communicating the lower intake space with the lower exhaust space.

[0188] The largest propeller turbine (222, 225 and 228 in Figs. 8 and 9) communicates the upper intake space with the upper discharge space.

[0189] A semi-propeller turbine (224 and 227 in Figs. 8 and 9) communicating with the intermediate supply space and the intermediate discharge space.

[0190] A small propeller turbine (223 and 226 in Figures 8 and 9) connects the lower intake space with the lower exhaust space.

[0191] The drive shown in FIG. 41 has its supply duct (2) connected by means of a hose (31) to the exhaust duct (02) of the wheel assembly shown in FIG. 42, just as the former has its exhaust duct, so that the exhaust connected to the second supply is created by means of a hose that is placed behind it (31) just like the one in the image (31), and a closed hydraulic circuit is created as shown in the first, the solenoid valves of both the supply casing, the motor and the wheel, serving to allow the circulation of the flow through one or another of their respective turbines, so that the control (53) to which all the solenoid valves are connected is responsible for opening only one of them in the drive, whatever the three, and another one of the three in the wheel assembly; the latter (54) can control the former (53), so that any selection can be made by the driver from the manager (54).

[0192] From the above, it can be deduced that there are nine different combinations of opening and closing between the solenoid valves of the drive and wheel units, providing the possibility of applying the same number of variations in the reception at the wheels of the power applied to the drive. This is because the three turbines of each unit have different specific diameters and therefore different relative volumes displaced by the rotation of the rotor in each of the said links.

[0193] The same thing happens when the links are under the same structure, the drive and the propeller.

[0194] As seen in FIG. 44, a multiplex configuration can be established in the motor device, such that multiple motor devices are coupled in parallel and their respective pinions share a single focal point of rotation (613 and 614) like a wheel or propeller device, as desired to be installed on a vehicle, maintaining the aforementioned changes and increasing the discharge in proportion to the receiver of the oleo hydraulic fluid.

[0195] The variants can be augmented by the number of traction wheels on land vehicles, propellers on aircraft and ships, or hybrid vehicles of both of the above.

[0196] The system described thus far requires an electronic control system, shown in FIG. 40, which incorporates a power source, a battery (52), which initially provides such power to a stationary vehicle; but in said hydraulic circuit is a generator-motor (36) capable of generating electrical energy by the powerful rotation of any one of its rotors (29, 129 or 229) and any one of its turbines, which in its rotation drives an oleohydraulic fluid and transmits the generated electricity to the battery (52) for simultaneous, subsequent or reserve use.

[0197] In addition, the motor-generator (36) is well suited due to its ability to optionally inject oleohydraulic fluid therethrough, as described below, to supply the battery (52) with electrical current therefrom to propel the vehicle as a supplement to or in lieu of the rotational primary power source of the drive elements previously described.

[0198] The genetic inductor-motor (36), as seen in FIG. 40, has an inductor (42) capable of rotating about an armature (41) surrounding it, producing a change in the magnetic field exerted by the first (42) on the second (41), and when this one (42) is included in the first one (36), the rotating cavity (40) is isolated by a lid (43) and is sealed from the outside thanks to the connection of its energized (39) and free (38) passages with the hydraulic circuit presented here by means of two hose sections (31 and 031), and the hydraulic flow is given to one (38) by its own regulator (50), respectively, and can be directed by these (39 and 38) by means of the electrical calibration of each flow given to the other (39) by the regulator (50).

[0199] Said optional identification by the driver of the vehicle is carried out electronically from the manager (54) through the control (53), enabling the transmission of:

[0200] Any flow through the energy path (39) where maximum power generation is achieved has a high positive resistance to motor action.

[0201] As has already been shown, any distribution of flow between the energized (39) paths and the free (38) paths, through which more or less current is available, is accompanied by a consequent increase in resistance.

[0202] All flow through the free passage (38) where no force is available is the absence of any of the resistance to motor operation.

[0203] The hydraulic circulation we have seen so far only occurs in one direction;

[0204] Additionally, the hydraulic system presented herein includes an electronic traffic inverter (69) inserted in the shuttle hose (31) between the drive rotor and the wheel or propeller rotor in the assembly.

[0205] As shown in FIG. 24, when the upper (76) and lower (77) valves are open and the reverse valves a (78) and b (79) are closed, the traffic on the circuit is as we have seen, and by rotating the pedals (61) in the driving direction, the wheel or propeller in question rotates forward.

[0206] As seen in FIG. 25, when the upper (76) and lower (77) valves are closed and the reverse valves a (78) and b (79) are open, the traffic in the circuit is reversed and when the pedal (61) in the driving direction, the wheel or propeller rotates backwards.

[0207] The inclusion of a heater thermostat (37) in the generator-motor (36) gives the system the ability to know the temperature of the oleo hydraulic fluid it contains, and the option via the manager (54) to heat it with electrical supply from the battery (52) at the command of the control (53) until the most optimal flow rate is reached.

[0208] If the system has a generator / motor (36) inserted in the flow or return duct connecting the wheel or propeller unit with the inverter (69), then it is assumed that when its upper (76), lower (77) valves, inverter a (78) are closed and inverter b (79) is opened, as seen in Figure 26, the traffic on the circuit is limited to the generator / motor (36) and the wheel or propeller unit, taking the drive unit out of the circuit. This occurs automatically by the control (53) when the electronic level (111), described below, detects a situation that allows the vehicle to lower, where potential energy is available for conversion into electricity by the generator / engine (36).

[0209] As can be seen in FIG. 37, the electronic level (111) is based on the presence of a dielectric liquid that fills each of the two chambers halfway, and is created in each of them:

[0210] The lower portion (1131 and 1132) is conductive, optically dense, and fluid.

[0211] The superior ones (1121 and 1122) are dry, gaseous and electrically insulating.

[0212] In the figure, the vehicle on which the level (111) is placed is horizontal, so that the surfaces of both conductive volumes (1131 and 1132) remain stable in the landscape state. This means that the inner ends of the two conductors (-1 and -2) housed in the lower part (1131 and 1132) are immersed in a dielectric, while the two conductors (+1 and +2) housed in the chambers (1121 and 1122) and surrounded by said gas are electrically insulated from them (-1 and -2), thus meaning that there is no electrical circulation between the electrodes (-1 and +1) and (-2 and +2), no signal reaches the control (53), and therefore the control (53) does not process any action on the electrical system.

[0213] An increase in the incline of a land vehicle carrying the level described herein or an increase in the height of an aircraft means that the vehicle on which the level (111) is placed is no longer level, as shown in Figure 38, and therefore the surfaces of both conductors (1131 and 1132) are no longer horizontal, and to the left of the Knivel (111), conductor (1131) adopts the shape of a wedge with a small apex to its left. This means that the two internal ends of the conductors (+1 and -1) housed therein remain electrically insulated without emitting any signal to the control (53); on the other hand, on the right side of it (111), the two conductors (+2 and -2) are immersed in a dielectric (1132) and therefore, if there is an electrical circulation between them (+2 and -2), it gives a signal of such rise to the control (53), which, upon receiving any command from the driver of the vehicle through the manager (54), processes the command on the electrical system to operate the generator / motor using the electrical energy from the battery (52), supporting the efforts made by the propulsion source of said vehicle.

[0214] Assistance, either full assistance by fully closing the free path regulator (50') and fully opening the energy path regulator (50') to provide full power to the vehicle, or partial assistance by allowing a voluntary play to open and close both regulators (50') and (50') in stages.

[0215] A downward incline of a land vehicle carrying the level described herein or a downward in height of an aircraft means that the vehicle on which the level (111) is placed is no longer level, as shown in Figure 39, and therefore the surfaces of both conductors (1131 and 1132) are no longer horizontal, and at the right side of the level (111), conductor (1131) adopts the shape of a wedge with a small apex to its right side. This means that the two internal ends of the conductors (+2 and -2) housed therein remain electrically insulated without emitting any signal to the control (53); on the other hand, on the left side of it (111), the two conductors (+1 and -1) are immersed in a dielectric (1131) and therefore, if there is an electrical circulation between them (+1 and -1), it gives a signal of such a downward movement to the control (53), and upon receiving any command from the driver of the vehicle through the manager (54), the latter (53) processes the command on the electrical system and operates the generator / motor in energy generating mode, for the battery (52), to take advantage of the decrease in the potential energy of the vehicle and store it for later use.

[0216] Full production with the free path regulator (50') completely closed and the energy path regulator (50') fully open, giving full or partial vehicle power with spontaneous play by gradually opening and closing both regulators (50') and (50'). Furthermore, the inverter (69) can be optionally used to limit the oleo hydraulic traffic to the wheels or propeller unit, as the case may be, and to the generator / motor (36), avoiding friction and power losses in the rest of the circuit.

[0217] For all devices, where applicable: Power supply housing (0) for spotlight (110).

[0218] The driving rotor (29), wheel (129) or propeller (229) of the counter (201).

[0219] Discharge casing (00) of photocell (100).

[0220] That is, if the former (29, 129 or 229) rotates in both (0 and 00) sinusoids (1 and 01) due to its impulse on the motorized pedal or due to a downward influence, which occurs at each revolution of the same (29), the light on the latter (100) flashes from the former (110) through the motor meter (201), since the focus (110) is always connected to the battery (52).

[0221] When the rhythms are processed through a periodic sequence, the frequency and speed of their respective rotations are obtained, which are also processed in the control (53) and reflected in the manager (54) for any purpose.

[0222] It is not considered necessary to make this description more extensive so that those skilled in the art will understand the scope of the invention and the advantages derived therefrom.

[0223] The terms used in this report should always be interpreted in a broad and non-limiting sense.

[0224] The material, shape and arrangement of the elements may be modified unless this implies a change in the essential characteristics of the invention presented herein according to the following.

Claims

1. 1. A hydrostatic transmission system with electromagnetic control variation for a vehicle including optional power generation and propulsion, comprising: An electrical component, comprising the following connected by a carrying cable: An adjustable electric motor / generator (36) including: - Free passage regulator (50). - Energy step regulator (50'). - Induction stator (41). - Rotating inductor (42). - Battery (52). Electronic control (53). - Electronic Manager (54). - Two low supply solenoid valves (3). - Two intermediate supply solenoid valves (4 and 04). - Two high level supply solenoid valves (5 and 05). - Top valve (76). - Lower valve (77). - Reversing valve a (78). - Reversing valve b (79). Orientation motor (67 １ ). Lift motor (67 ２ ). Light bulb ((100). - Photoelectric sensor (110). - Electronic level (111). - hydraulic components, consisting of four categories of rotating equipment: two of them are energy sources: the drive and the generator / motor; the former is responsible for supplying the rest of the circuit with the hydraulic pressure generated by the main source of rotational energy, whether artificial or an engine of any nature, while the latter, depending on the circumstances, performs a pressure increase to the rest of the hydraulic circuit, either as a complement or optional alternative to the propulsion action applied to the equipment motor, by optionally converting said pressure injected by the rotor into electricity, using the potential energy of the system during the descent of the vehicle, or using the electrical energy stored in the battery. Residual torque: the wheel arrangement and the propeller arrangement respectively have the task of releasing the pressure force supplied by both of the aforementioned injection arrangements onto the supporting medium in the case of land vehicles, or onto the envelope in the case of ships or aircraft, the effect of which, whatever its nature, is to propel the vehicle forward. As a result, the hydraulic circuit has: One or more drive units, thus giving the system the possibility of having one or more receivers for the hydraulic fluid discharged by it or them; the number of which depends on the quantity of these receivers to ensure an adequate supply of said fluid. - One or more wheel character devices, depending on the desired availability in the number of driven wheels of the vehicle. One or more propeller devices, depending on the desired availability in number of thrust propellers on the vehicle. One or more wheel and propeller arrangements depending on the desired versatility in various travel spaces and the availability of traction on both the vehicle. The configurations of the drive unit, wheel unit, and propeller unit are essentially the same since all three are made up of two vessel bodies, which are: Power supply casing installed (0): Discharge casing (00). ・Those two series (89 １ ~89 ３ and 89 ２ ~89 ４ ), each filling the toroidal gap resulting from the facing of each of the motor, wheel, and propeller devices present in the system: Supply bearing channel and bearing groove one. - Bearing channel and bearing groove in the discharge. A sufficient number of low-level power joints (88) to bridge the toroidal joint gaps of such magnitude that they are presented by their respective counterparts in each of the drive, wheel and propeller units present in the system. １ ). A sufficient number of lower intermediate feed gaskets (88) to fill the toroidal gasket gaps of such magnitude that they appear due to their respective opposition in each of the drive units, wheel units and propeller units present in the system. ２ ). A sufficient number of mid-high supply gaskets (88) to fill the toroidal gasket gaps of such magnitude that they are presented by their respective opposing drive, wheel and propeller units present in the system. ３ ). A sufficient number of high-level supply gaskets (88) to fill the toroidal gasket gaps of such magnitude that they appear due to their respective opposition in each of the drive units, wheel units and propeller units present in the system. ４ ). A sufficient number of low-level exhaust gaskets (88') to fill the toroidal gasket gaps of such magnitude that they are presented by their respective opposing drive, wheel and propeller units present in the system. １ ). A sufficient number of mid-lower discharge gaskets (88') to fill the toroidal gasket gaps of such magnitude that they are presented by their respective opposing motor, wheel and propeller units present in the system. ２ ). A sufficient number of mid-high exhaust gaskets (88') to fill the toroidal gasket gaps of this magnitude presented by the respective opposing motor, wheel and propeller units present in the system. ３ ). A sufficient number of high discharge joints (88') to fill the toroidal joint gaps of such magnitude that they appear due to their respective opposition in each of the drive, wheel and propeller units present in the system. ４ ). The three differ in that the motor arrangement also incorporates: - Drive rotor (29). -Pinion (16). 3 anchors for each drive (15 １ , 15 ２ and 15 ３ ) which are fixed in the correct order and in a fixedly stable manner to each other and to the vehicle (60), to the power supply (0) casing and the exhaust (00) casing or to the casings of the compound motor device comprising the system, and if one or more wheels and / or propeller devices are mounted in connection thereto, their numbers are coordinated as described above. ・Some pedals (60 １ and 60 ２ ) or motor. The wheel system includes: Rotor wheel (129). ・3 anchors (15 ７ , 15 ８ and 15 ９ ) which connect the supply casing and the discharge casing of the device to each other in a fixed and stable manner; anchors (15 ７ ) secures both housings to: Links (60 ２ ), which is the elevator (67 ２ ) articulates with ・Orient (60 １ ) connected to the vehicle (60) by a ring (59) and a director (67) １ ) engages. and a propeller device (229): - Propeller rotor (229). ・3 anchors (15 ７ , 15 ８ and 15 ９ ) which connect the supply casing and the discharge casing of the device to each other in a fixed and stable manner; anchors (15 ７ ) secures both housings to: Links (60 ２ ), which is the elevator (67 ２ ) articulates with ・Orient (60 １ ) connected to the vehicle (60) by a ring (59) and a director (67) １ ) engages. Considering the possible large number of wheels and propeller units connected to the corresponding drives: An electronic inverter (69) for each pair formed by the drive and a wheel or propeller in hydraulic communication. the hoses (31) necessary to connect the exhaust duct (02) of the corresponding motor unit and all the power lines (2) of the wheels and propeller units installed in the latter exhaust duct (02) with the corresponding supply (2) in the wheels and propeller units; in addition to the number of hoses (31) necessary to insert said hoses (31), each supply connection (2) and exhaust (02) contains, as already mentioned, its corresponding inverter (69); Hydrostatic transmission system.

2. 10. A hydrostatic transmission system with electromagnetic control variations for a vehicle including optional power generation and propulsion according to claim 1, comprising: Each hydraulic circuit is the result of the integration of the drive and the wheels or one spiral, separated from each other by separate hoses connected to the respective supply and discharge conduits; the channels are the extension of the respective supply ducts (2) and discharge (02) of both devices, and when counting, the first (2) with three solenoid valves (3, 4 and 5) and the second with three outputs (03, 04 and 05) facing each other (3 to 03, 4 to 04 and 5 to 05) form the paths for the small, medium and large turbines. The oleo hydraulic traffic is made by only one of them, the same as the one selected by the driver of the vehicle when giving said preference to the system through his delegation to the manager (54) which returns it to the control (53), which processes the command to open selected supply solenoid valves in the drives and wheels or propellers, while the rest remain blocked from circulation through them. This results in a combination of turbines of the same or different radii, with different power changes at each selection. With the generator / motor (36) inserted in one of the hydraulic circuits of the system and with a new branch in oleo hydraulic communication, the vehicle operator can also select the priority of moving through the free path (38) or the energy step (39) by means of a corresponding command to the manager (54) which returns it to the control (53), which processes the opening of the free path regulator (50) and the energy step (50') in greater or lesser degrees, thus resulting in a variation in the power generated by the generator / motor (36) but also in a change in the resistance to pedaling or to the action of the installed motor, as in this case. The set of regulators (50) and (50') also affects the oleo-hydraulic traffic when the driver, by means of the energy from the battery (52) and the command given to the control (53) by means of the manager (54), decides to rotate the inductor (42) and to force the circulation of the fluid that immerses it, an action that can be more or less violent and powerful, depending on the electrical intensity applied to the problem and on the opening of the regulators (50) and (50'). A hydrostatic transmission system comprising:

3. 10. A hydrostatic transmission system with electromagnetic control variations for a vehicle including optional power generation and propulsion according to claim 1, comprising: The system has a level (111) that determines the level or inclination of the vehicle's advance, and thus such information serves to control (53) the signal for operating the generator / engine in power generation function by closing the free passage (38) and opening the energy passage (39) at the request of the vehicle driver, by means of associated instructions to the manager (54). A hydrostatic transmission system comprising:

4. A hydrostatic transmission system with electromagnetic control variations for vehicles including optional power generation and propulsion according to claim 1, characterized in that: The wheels and propeller unit are connected to the vehicle by means of two rotating ball joints so that it can be steered in three-dimensional space, which are connected to the link (60) by anchors (157). ２ ) and a supply and discharge housing (0) and (00) connected to a link (60 ２ ) is connected to the vehicle (60) by a ring (59) and a director (67 １ ) engaged with the guide (60) １ ) to the elevator (67 ２ ) for articulation. The orientation of said wheel or propeller device is made according to the requirements of the vehicle driver by means of associated instructions to a manager (54), which in turn receives from the control (53) the lift (67) to orient the desired device in one direction or another. ２ ) or Director (67 １ ) to the desired degree. A hydrostatic transmission system comprising:

5. A hydrostatic transmission system with electromagnetic control variations for vehicles including optional power generation and propulsion according to claim 1, characterized in that: The direction of the oleo-hydraulic traffic can be reversed while maintaining the direction of pedaling or motor rotation; for this, the cyclist, pilot or driver acts at the discretion of the manager (54), which then controls opening and closing the upper (76), lower (77), inverter a (78) and inverter b (79) valves and directing the flow through its upper right (70), upper left (71), lower left (72), left (73), pipe a (74) and pipe b channels in one direction or the other as seen in the description. A hydrostatic transmission system comprising:

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