CN111305944A - Eccentric birotor transmission device - Google Patents

Eccentric birotor transmission device Download PDF

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Publication number
CN111305944A
CN111305944A CN202010234421.6A CN202010234421A CN111305944A CN 111305944 A CN111305944 A CN 111305944A CN 202010234421 A CN202010234421 A CN 202010234421A CN 111305944 A CN111305944 A CN 111305944A
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CN
China
Prior art keywords
rotor
cylinder
piston
wall
outer rotor
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CN202010234421.6A
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Chinese (zh)
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杨平
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Individual
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Individual
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Priority to CN202010234421.6A priority Critical patent/CN111305944A/en
Publication of CN111305944A publication Critical patent/CN111305944A/en
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    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02B—INTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
    • F02B61/00—Adaptations of engines for driving vehicles or for driving propellers; Combinations of engines with gearing
    • F02B61/06—Combinations of engines with mechanical gearing
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01M—LUBRICATING OF MACHINES OR ENGINES IN GENERAL; LUBRICATING INTERNAL COMBUSTION ENGINES; CRANKCASE VENTILATING
    • F01M1/00—Pressure lubrication
    • F01M1/02—Pressure lubrication using lubricating pumps
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02B—INTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
    • F02B75/00—Other engines
    • F02B75/02—Engines characterised by their cycles, e.g. six-stroke
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02B—INTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
    • F02B75/00—Other engines
    • F02B75/16—Engines characterised by number of cylinders, e.g. single-cylinder engines
    • F02B75/18—Multi-cylinder engines
    • F02B75/22—Multi-cylinder engines with cylinders in V, fan, or star arrangement
    • F02B75/222—Multi-cylinder engines with cylinders in V, fan, or star arrangement with cylinders in star arrangement
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02F—CYLINDERS, PISTONS OR CASINGS, FOR COMBUSTION ENGINES; ARRANGEMENTS OF SEALINGS IN COMBUSTION ENGINES
    • F02F1/00—Cylinders; Cylinder heads 
    • F02F1/18—Other cylinders
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02F—CYLINDERS, PISTONS OR CASINGS, FOR COMBUSTION ENGINES; ARRANGEMENTS OF SEALINGS IN COMBUSTION ENGINES
    • F02F3/00—Pistons 
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02M—SUPPLYING COMBUSTION ENGINES IN GENERAL WITH COMBUSTIBLE MIXTURES OR CONSTITUENTS THEREOF
    • F02M35/00—Combustion-air cleaners, air intakes, intake silencers, or induction systems specially adapted for, or arranged on, internal-combustion engines
    • F02M35/10—Air intakes; Induction systems
    • F02M35/10006—Air intakes; Induction systems characterised by the position of elements of the air intake system in direction of the air intake flow, i.e. between ambient air inlet and supply to the combustion chamber
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16H—GEARING
    • F16H21/00—Gearings comprising primarily only links or levers, with or without slides
    • F16H21/10—Gearings comprising primarily only links or levers, with or without slides all movement being in, or parallel to, a single plane
    • F16H21/16—Gearings comprising primarily only links or levers, with or without slides all movement being in, or parallel to, a single plane for interconverting rotary motion and reciprocating motion
    • F16H21/18—Crank gearings; Eccentric gearings
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02B—INTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
    • F02B75/00—Other engines
    • F02B75/02—Engines characterised by their cycles, e.g. six-stroke
    • F02B2075/022—Engines characterised by their cycles, e.g. six-stroke having less than six strokes per cycle
    • F02B2075/025—Engines characterised by their cycles, e.g. six-stroke having less than six strokes per cycle two
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02B—INTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
    • F02B75/00—Other engines
    • F02B75/16—Engines characterised by number of cylinders, e.g. single-cylinder engines
    • F02B75/18—Multi-cylinder engines
    • F02B2075/1804—Number of cylinders
    • F02B2075/1812—Number of cylinders three

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  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Transmission Devices (AREA)

Abstract

The invention discloses an eccentric dual-rotor transmission device which comprises an outer rotor, an inner rotor, a cylinder, a piston and a piston rod, wherein the closed end of the cylinder is installed on the inner wall of the annular outer rotor through an outer rotor installation seat and can swing within the angle range of 1-20 degrees, the piston is installed in the cylinder, the first end of the piston rod is connected with the piston, the second end of the piston rod extends out of the opening end of the cylinder and then is connected with the annular or circular inner rotor through an inner rotor installation seat, the piston rod can swing within the angle range of 1-20 degrees, and the circle center of the inner rotor and the circle center of the outer rotor are located on the same plane and do not. The simplified structure of the eccentric double-rotor transmission device can select application occasions according to actual requirements, and is not limited to the application of producing engine cylinder blocks; the eccentric double-rotor transmission device refines a combustion working structure on the basis of simplifying the structure, can be used for producing an engine cylinder body, solves the problem of the traditional engine, and forms an engine with a brand new structure.

Description

Eccentric birotor transmission device
Technical Field
The invention relates to a transmission device for outputting rotary power, in particular to an eccentric dual-rotor transmission device based on rotary transmission.
Background
In rotary power equipment such as an engine and the like, the most common transmission structure is to convert the reciprocating motion of a piston into the rotary motion, namely, a crankshaft is driven to rotate by the piston through a crank-connecting rod mechanism.
In addition to the above-mentioned engine using a crank mechanism to rotate a crankshaft, there is a wankel engine using a triangular rotor to rotate in an elliptical space, which has a large power, but has a problem of air tightness that has been difficult to solve, and has limited the positive development of the engine.
Disclosure of Invention
The invention aims to solve the problems and provide an eccentric dual-rotor transmission device based on inner rotors and outer rotors with different circle centers.
The invention realizes the purpose through the following technical scheme:
the utility model provides an eccentric birotor transmission, includes external rotor, inner rotor, cylinder, piston and piston rod, the blind end of cylinder is installed through the external rotor mount pad annular just can swing at 1-20 angle within range on the inner wall of external rotor, the piston is installed in the cylinder, the first end of piston rod with the piston is connected, the second end of piston rod stretches out behind the open end of cylinder with circle ring shape or circular shape the inner rotor passes through the inner rotor mount pad and connects just the piston rod can swing at 1-20 angle within range, the centre of a circle of inner rotor with the centre of a circle of external rotor is located the coplanar and does not coincide, and its interval is decided according to actual need. The outer rotor mounting seat and the inner rotor mounting seat can be easily realized by the prior art, such as a universal seat structure.
Further, in order to facilitate auxiliary compression of gas, an auxiliary cylinder body is further arranged at the opening end of the cylinder, one end of the auxiliary cylinder body is opened and is in butt joint with the opening end of the cylinder, the other end of the auxiliary cylinder body is closed, and the piston rod penetrates through the closed end.
Further, in order to realize the function of driving the outer rotor to rotate and outputting the rotating power by combustion of oil and gas in the cylinder, the eccentric dual-rotor transmission device further comprises a shell, a planetary gear and a power output gear, wherein a cavity and a power output cavity separated by a partition wall are arranged in the shell, the outer rotor, the inner rotor and the planetary gear are all arranged in the cavity of the shell, the power output gear is arranged in the power output cavity, two ends of a central shaft of the power output gear are respectively arranged on the inner wall of the first end of the shell and the partition wall through bearings, two ends of the central shaft of the planetary gear are respectively arranged on the inner wall of the second end of the shell and the partition wall through bearings, the central shaft of the planetary gear penetrates through the partition wall and then is arranged in the power output cavity and is provided with a transmission gear, and the gear teeth of the transmission gear are meshed with the gear teeth of the power output gear, the center shaft output rotary power of power take-off gear, the centre of a circle of power take-off gear with the centre of a circle coincidence of outer rotor, be located on the circumference inner wall of outer rotor the position next door of cylinder is equipped with the outer rotor teeth of a cogwheel, at least two planetary gear is located the outer rotor with between the power take-off gear and at circumferencial direction evenly distributed, planetary gear's the teeth of a cogwheel with the teeth of a cogwheel meshing of outer rotor teeth of a cogwheel, inner rotor is ring shape and is connected with the inner rotor center pin, the inner rotor center pin be hollow shaft and its axial with inner rotor place plane mutually perpendicular, install respectively through the bearing at the both ends of inner rotor center pin the second end inner wall of shell with on the partition wall, the piston rod is hollow rod, the center through-hole of, An oil pipe is arranged in an inner channel formed by mutually communicating central through holes of the piston rod, the outer end of the oil pipe is an oil inlet end, the inner end of the oil pipe penetrates through the through hole in the piston and then is arranged on the end surface of the piston, an oil sprayer is arranged at the inner end of the oil pipe, the outlet of the oil sprayer is positioned in a cavity between the piston and the closed end of the cylinder, a spark plug is arranged at the position beside the oil sprayer on the piston, an air inlet pipe is arranged at one side of the outer wall of the joint of the cylinder and the auxiliary cylinder body, an air storage cylinder is arranged at the other side of the outer wall of the joint of the cylinder and the auxiliary cylinder body, the air storage cylinder is communicated with the auxiliary cylinder, the air storage cylinder is communicated and connected with a first end of an air conveying pipe, a second end of the air conveying pipe penetrates through the cylinder wall, the control end of the oil sprayer, the control end of the spark plug and the control end of the air injection switch are respectively connected with the first ends of the corresponding control wires, three power receiving contact pieces are arranged on the inner rotor or the inner rotor mounting seat, the second ends of the three control wires penetrate through the central through hole of the piston rod and then are respectively connected with the three power receiving contact pieces, three power supply contact pieces are arranged at positions, corresponding to the three power receiving contact pieces, on the inner wall of the second end of the shell, the three power receiving contact pieces can be respectively in contact connection with the three power supply contact pieces in the rotating process, the closed end of the air cylinder is provided with an exhaust valve, the inner end of the exhaust valve is arranged in the air cylinder, the outer end of the exhaust valve penetrates through the outer rotor and then is arranged outside the outer rotor, the outer end of the exhaust valve is opened after being pressed and closed after being decompressed, and a connecting straight line between the circle center of the Handing over and keeping away from the point of inner rotor is A point, be close to on the pelvic cavity inner wall of shell the position of A point is equipped with to being close to the bellied evagination segmental arc of outer rotor direction, the radian of evagination segmental arc with the excircle radian of outer rotor is unanimous, exhaust valve's outer end is being rotated to can be pushed down when the evagination segmental arc and open, the pelvic cavity inner wall of shell is equipped with inside and outside communicating gas vent and air inlet, the gas vent is located region outside the outer rotor, the air inlet is located position within the outer rotor, be located on the pelvic cavity inner wall of shell the gas vent with position between the evagination segmental arc is equipped with exhaust groove or exhaust hole, the air inlet with the intake pipe communicates with each other.
The eccentric double-rotor transmission device with the structure can form an engine cylinder body structure, and correspondingly, the output shaft rotates for one circle after the piston reciprocates once, which is equivalent to a two-stroke engine cylinder body; and can be used as a four-stroke engine cylinder body according to requirements.
Furthermore, in order to realize good lubricating and heat dissipation functions, an annular engine oil channel is arranged in the annular wall of the outer rotor, a cylinder ring is fixedly arranged at a position, close to the closed end, on the cylinder, a through hole is formed in one side of the cylinder ring and is communicated with the engine oil channel, the engine oil channel is communicated with an engine oil storage chamber, an engine oil pump chamber is arranged between the cylinder ring and the piston, a plurality of engine oil holes are formed in the piston on one side of the inner surface of the piston ring and are communicated with an engine oil pipeline in the piston rod, the engine oil pump chamber is connected with an inlet of heat dissipation equipment through the engine oil pipeline in the piston rod, and an outlet of the heat dissipation equipment is communicated with the engine oil pump chamber.
Preferably, one cylinder, one piston rod, one outer rotor mounting seat and one inner rotor mounting seat are a group of connecting devices, and the eccentric dual-rotor transmission device comprises three groups of connecting devices which are uniformly distributed along the circumferential direction. This structure corresponds to a three-cylinder engine block.
The invention has the beneficial effects that:
the outer rotor and inner rotor structure of the invention is a structure which integrates the crankshaft guide reciprocating motion mode to expand the crankshaft application, replaces the crankshaft with the rotor structure form, and is another embodiment of the reciprocating motion; the outer rotor and the inner rotor are connected through the air cylinder, the piston and the piston rod, the circle centers of the outer rotor and the inner rotor are on the same plane and do not coincide, the maximum distance and the minimum distance between the outer rotor and the inner rotor correspond to each other when a certain point on the outer rotor and the inner rotor rotates to the connecting line of the two circle centers, the outer rotor and the inner rotor respectively rotate around the respective circle centers, the function of applying work of the air cylinder and the piston is realized through the principle of changing the distance between the certain point on the circumference of the outer rotor and the circle center of the inner rotor, the second end of the piston rod is connected with the inner rotor, so the outer rotor only can do circumferential motion around the inner rotor, the air cylinder is pushed by the combustion explosive force of oil gas in the air cylinder to expand outwards in the opposite direction, namely the outer rotor is pushed to move, the outer rotor only moves in the direction far away, the engine produced by the device has the advantages of the traditional crankshaft type engine and the Wankel engine, and is suitable for popularization and application. The simplified structure of the eccentric double-rotor transmission device can select application occasions such as an engine, a pressure pump and a generator according to actual needs, and is not limited to the application of producing an engine cylinder block; the refining structure of the eccentric double-rotor transmission device is suitable for producing engine cylinder bodies, solves the problems of the traditional engine, forms an engine with a brand new structure, and can be applied to the field of commercial aviation. The same transmission structure principle can realize a plurality of working modes.
Drawings
Fig. 1 is a schematic structural view of an eccentric double-rotor transmission device according to embodiment 1 of the present invention;
fig. 2 is a schematic structural diagram of an eccentric double-rotor transmission device in embodiment 2 of the invention, wherein a power output gear is in a power output cavity on the other side of a partition wall, but for the convenience of understanding, the effect is shown in a cavity;
fig. 3 is a schematic structural view of the eccentric dual-rotor transmission device according to embodiment 2 of the present invention, in which the cylinder, the piston rod, the auxiliary cylinder, the air cylinder, and the inner rotor are removed, and the power output gear is in the power output cavity on the other side of the partition wall.
Detailed Description
The invention is further illustrated by the following examples and figures:
example 1:
as shown in fig. 1, the eccentric double-rotor transmission device comprises an outer rotor 1, an inner rotor 8 and a cylinder 3, the auxiliary cylinder body 5, the piston 4 and the piston rod 6, the closed end of the cylinder 3 is installed on the inner wall of the circular outer rotor 1 through the outer rotor installation seat 2 and can swing within the angle range of 1-20 degrees, the piston 4 is installed in the cylinder 3, one end of the auxiliary cylinder body 5 is opened and is in butt joint with the open end of the cylinder 3, the other end of the auxiliary cylinder body 5 is closed, the first end of the piston rod 6 is connected with the piston 4, the second end of the piston rod 6 extends out of the open end of the cylinder 3 and the closed end of the auxiliary cylinder body 5 and then is connected with the circular or round inner rotor 8 through the inner rotor installation seat 7, the piston rod 6 can swing within the angle range of 1-20 degrees, and the circle center of the inner rotor 8 and the circle; the eccentric double-rotor transmission device comprises three groups of connecting devices which are uniformly distributed along the circumferential direction, wherein one cylinder 3, one piston 4, one piston rod 6, one outer rotor mounting seat 2 and one inner rotor mounting seat 7 form one group of connecting devices.
When the device is used, the outer rotor 1 and the inner rotor 8 rotate synchronously around the circle center of the outer rotor and the inner rotor respectively, the piston 4 and the piston rod 6 reciprocate synchronously in the cylinder 3 in the rotating process, and the rotating power can be output from the outer rotor 1 or the inner rotor 8 according to requirements.
The eccentric double-rotor transmission device is of a simplified structure, can select application occasions according to actual requirements, and is not limited to the application of producing engine cylinder blocks.
Example 2:
as shown in fig. 2 and fig. 3, an eccentric dual-rotor transmission device comprises an outer rotor 1, an inner rotor 8, a cylinder 3, an auxiliary cylinder body 5, a piston 4, a piston rod 6, a housing 9, a planetary gear 25 and a power output gear 24, wherein a closed end of the cylinder 3 is mounted on the inner wall of the circular outer rotor 1 through an outer rotor mounting seat 2 and can swing within an angle range of 1-20 degrees, the piston 4 is mounted in the cylinder 3, one end of the auxiliary cylinder body 5 is open and is butted with the open end of the cylinder 3, the other end of the auxiliary cylinder body 5 is closed, a first end of the piston rod 6 is connected with the piston 4, a second end of the piston rod 6 extends out of the open end of the cylinder 3 and the closed end of the auxiliary cylinder body 5 and is connected with the circular inner rotor 8 through an inner rotor mounting seat 7, the piston rod 6 can have a clattering inner wall within an angle range of 1-20 degrees, a cavity (not marked in the figure) and a power output cavity (not shown) which are separated by a partition wall are arranged in the shell 9, the outer rotor 1, the inner rotor 8 and the planetary gear 25 are all arranged in an inner cavity of the shell 9, the power output gear 24 is arranged in the power output cavity, two ends of a central shaft 27 of the power output gear 24 are respectively arranged on the inner wall of a first end (namely the front end in the figure) of the shell 9 and the partition wall through bearings (not shown), two ends of a central shaft of the planetary gear 25 are respectively arranged on the inner wall of a second end (namely the rear end in the figure) of the shell 9 and the partition wall through bearings (not shown), the central shaft of the planetary gear 25 passes through the partition wall and then is arranged in the power output cavity, and is provided with a transmission gear (not shown, the shape and the size of the planetary gear 25 are the same or similar) and the gear teeth, a central shaft 27 of the power output gear 24 outputs rotary power, the circle center of the power output gear 24 coincides with the circle center of the outer rotor 1, outer rotor gear teeth 22 are arranged at positions beside (on the front side in the figure) the cylinder 3 on the circumferential inner wall of the outer rotor 1, three (or two or more) planetary gears 25 are arranged between the outer rotor 1 and the power output gear 24 and are uniformly distributed in the circumferential direction, the gear teeth of the planetary gears 25 are meshed with the gear teeth 23 of the outer rotor gear teeth 22, the inner rotor 8 is connected with a central shaft (not shown) of the inner rotor, the central shaft of the inner rotor is a hollow shaft, the axial direction of the central shaft of the inner rotor is vertical to the plane of the inner rotor 8, two ends of the central shaft of the inner rotor are respectively arranged on the inner wall of the second end of the shell 9 and the partition wall through, An oil pipe 20 is arranged in an inner channel formed by mutually communicating a central through hole of the inner rotor 8 and a central through hole of the piston rod 6, the outer end of the oil pipe 20 is an oil inlet end, the inner end of the oil pipe 20 passes through the through hole in the piston 4 and then is arranged on the end surface of the piston 4, an oil sprayer 16 is arranged at the inner end of the oil pipe 20, the outlet of the oil sprayer 16 is arranged in a cavity between the piston 4 and the closed end of the cylinder 3, a spark plug 17 is arranged at the position beside the oil sprayer 16 on the piston 4, two air inlet pipes 18 (in the figure, the two air inlet pipes 18 are matched with the I-shaped piston 4, the pistons 4 with other shapes can be adopted, one air inlet pipe 18 and one air storage cylinder 19 are arranged at the other side, a one-way valve only allowing air to enter is arranged on the air inlet pipe 18, the air storage cylinder 19 is communicated with the, the air cylinder 19 is communicated and connected with a first end of an air pipe 15, a second end of the air pipe 15 penetrates through the cylinder wall of the cylinder 3 and is positioned in the cylinder 3 and close to the closed end of the cylinder, an air injection switch (not shown in the figure) is arranged on the air pipe 15 and close to the second end of the air pipe, a control end of the oil injector 16, a control end of the spark plug 17 and a control end of the air injection switch are respectively connected with a first end of a corresponding control wire (not shown in the figure), three power supply contact blades 28 are arranged on the inner wall of the second end of the shell 9 and correspond to the three power supply contact blades 26, the three power supply contact blades 26 can be respectively contacted and connected with the three power supply contact blades 28 in the rotating process, the three power supply contact blades 28 are correspondingly connected with an external electric control board, the closed end of the cylinder 3 is provided with an exhaust valve 13, the inner end of the exhaust valve 13 is arranged in the cylinder 3, the outer end of the exhaust valve 13 penetrates through the outer rotor 1 and then is arranged outside the outer rotor 1, the outer end of the exhaust valve 13 is opened after being pressed and closed after being decompressed, the point where the connecting straight line of the circle center of the outer rotor 1 and the circle center of the inner rotor 8 intersects with the outer wall of the outer rotor 1 and is far away from the inner rotor 8 is a point A, the position on the inner wall of the cavity of the shell 9, which is close to the point A, is provided with an outer convex arc section 11 which is convex towards the direction close to the outer rotor 1, the radian of the outer convex arc section 11 is consistent with the radian of the outer circle of the outer rotor 1, the radian length of the outer convex arc section is set according to requirements, the outer end of the exhaust valve 13 can be, an air inlet 14 is positioned in the outer rotor 1, an exhaust groove 10 (also can be an exhaust through hole) is arranged on the inner wall of the cavity of the outer rotor 9 and positioned between an exhaust port 12 and an outer convex arc section 11, the air inlet 14 is communicated with an air inlet pipe 18 (a passage is formed by utilizing the space corresponding to the inner cavity of the outer rotor 1 in the outer rotor 1), a circular engine oil channel 21 is arranged in the annular wall of the outer rotor 1, a cylinder ring (not shown) is fixedly arranged on the position, close to the closed end, of the cylinder 3, a through hole is formed in one side of the cylinder ring and is communicated with the engine oil channel 21, the engine oil channel 21 is communicated with an engine oil storage chamber (not shown), an engine oil pump chamber (not shown) is arranged between the cylinder ring and the piston 4, a plurality of engine oil holes (not shown) are, the engine oil pump chamber is connected with an inlet of a heat dissipation device (not shown) through an engine oil pipeline in the piston rod 6, an outlet of the heat dissipation device is communicated with the engine oil pump chamber, the engine oil pump chamber formed between the cylinder ring and the piston 4 changes along with the change of the volume of the movement of the piston 4, the engine oil is sucked and pressed out through the one-way flow action of the one-way valve to drive the engine oil to circulate, the engine oil enters the engine oil pipeline arranged in the piston rod 6 and enters the heat dissipation device, and the engine oil after heat dissipation returns to the engine oil pump chamber through an oil return path, so that the cylinder 3 and the piston 4 are lubricated, and the heat dissipation problem is; the eccentric double-rotor transmission device comprises three groups of connecting devices which are uniformly distributed along the circumferential direction, wherein one cylinder 3, one piston 4, one piston rod 6, one outer rotor mounting seat 2 and one inner rotor mounting seat 7 form one group of connecting devices. Of these, the length of the piston 4 and the auxiliary cylinder 5 is preferably equal and the length of the cylinder 3 is preferably 2 times the length of the piston 4.
The eccentric double-rotor transmission device with the structure can form an engine cylinder body structure, and correspondingly, the output shaft rotates for one circle after the piston reciprocates once, which is equivalent to a two-stroke three-cylinder engine cylinder body; and can be used as a four-stroke engine cylinder body according to requirements.
As shown in fig. 2 and 3, the eccentric dual-rotor transmission device works according to the following principle:
when the piston 4 moves towards the direction close to the outer rotor 1, air enters the auxiliary cylinder 5 from the air inlet pipe 18, and when the piston 4 moves towards the direction close to the inner rotor 8, air in the auxiliary cylinder 5 is compressed and the compressed air enters the air storage cylinder 19 to be stored; when a certain air cylinder 3 is exhausted for a certain time, the corresponding power supply contact piece 28 is contacted with the corresponding power receiving contact piece 26 on the inner rotor 8 corresponding to the air inlet switch corresponding to the air cylinder 3, the air inlet switch is opened, and compressed air in the air storage cylinder 19 enters the air cylinder 3, so that on one hand, waste gas is thoroughly exhausted, and on the other hand, the air in the air cylinder 3 is further compressed; when the cylinder 3 is at the end of the compression stroke, the corresponding power receiving contact 26 on the inner rotor 8 corresponding to the fuel injector 16 corresponding to the cylinder 3 contacts the corresponding power supply contact 28, the fuel injector 16 starts injecting fuel, the outer rotor 1 continues to rotate to compress fuel, the fuel injection is finished when the outer rotor 1 rotates until the corresponding power receiving contact 26 is separated from the power supply contact 28, the power receiving contact 26 corresponding to the spark plug 17 corresponding to the cylinder 3 contacts the power supply contact 28, the spark plug 17 ignites, the fuel-air mixture in the cylinder 3 burns to do work, the outer rotor 1 rotates along with the inertia force, the power of the fuel gas burning explosion pushes the piston 4 and the cylinder 3 to push in opposite directions, only the cylinder 3 outwards expands as the piston 4 is connected with the inner rotor 8 through the piston rod 6 and the inner rotor 8 cannot move, but the outer rotor 1 keeps rotating continuously under the guidance of the inertia force, gradually enlarging the distance between the inner rotor 8 and the outer rotor 1 in the rotating advancing direction from the minimum distance (corresponding to a top dead center), expanding the explosive force in the cylinder 3, extending the cylinder 3 in the opposite direction to push the outer rotor 1 to rotate at an accelerated speed, drawing the piston 4 and the piston rod 6 by the cylinder 3 to synchronously rotate, pushing the exhaust valve 13 by the convex arc section 11 arranged on the shell 9 when the cylinder 3 rotates to a point A (corresponding to a bottom dead center), opening the exhaust valve 13, discharging the waste gas in the cylinder 3 into the exhaust groove 10, and then discharging the waste gas to the outside through the exhaust port 12 on the shell 9; when the air cylinder 3 is exhausted for a certain time and is about to finish, the air inlet switch is turned on, the compressed air in the air storage cylinder 19 enters the air cylinder 3, and the process is repeated and repeated; the operating principle of the other cylinders 3 is the same.
The eccentric double-rotor transmission device is of a refined structure, is suitable for producing engine cylinder bodies, solves the problems of the traditional engine, and forms an engine with a brand new structure.
The above embodiments are only preferred embodiments of the present invention, and are not intended to limit the technical solutions of the present invention, so long as the technical solutions can be realized on the basis of the above embodiments without creative efforts, which should be considered to fall within the protection scope of the patent of the present invention.

Claims (6)

1. An eccentric birotor transmission device is characterized in that: including external rotor, inner rotor, cylinder, piston and piston rod, the blind end of cylinder is installed through the external rotor mount pad annular just can swing at 1-20 angle within range on the inner wall of external rotor, the piston is installed in the cylinder, the first end of piston rod with the piston is connected, the second end of piston rod stretches out behind the open end of cylinder with circle ring shape or circular shape the inner rotor passes through the inner rotor mount pad and connects just the piston rod can swing at 1-20 angle within range, the centre of a circle of inner rotor with the centre of a circle of external rotor is located the coplanar and does not coincide.
2. The eccentric dual rotor transmission of claim 1, wherein: the opening end of the cylinder is also provided with an auxiliary cylinder body, one end of the auxiliary cylinder body is opened and is in butt joint with the opening end of the cylinder, the other end of the auxiliary cylinder body is closed, and the piston rod penetrates through the closed end.
3. The eccentric dual rotor transmission of claim 2, wherein: the eccentric dual-rotor transmission device further comprises a shell, a planetary gear and a power output gear, a pelvic cavity and a power output cavity which are separated by a partition wall are arranged in the shell, the outer rotor, the inner rotor and the planetary gear are arranged in the pelvic cavity of the shell, the power output gear is arranged in the power output cavity, two ends of a central shaft of the power output gear are respectively installed on the inner wall of the first end of the shell and the partition wall through bearings, two ends of the central shaft of the planetary gear are respectively installed on the inner wall of the second end of the shell and the partition wall through bearings, one end of the central shaft of the planetary gear penetrates through the partition wall and then is arranged in the power output cavity, a transmission gear is installed on the gear teeth of the power output gear, the gear teeth of the transmission gear are mutually meshed with the gear teeth of the power output gear, and the, the circle center of the power output gear coincides with the circle center of the outer rotor, the position of the inner circumferential wall of the outer rotor, which is positioned beside the cylinder, is provided with outer rotor gear teeth, at least two planetary gears are positioned between the outer rotor and the power output gear and are uniformly distributed in the circumferential direction, the gear teeth of the planetary gears are meshed with the gear teeth of the outer rotor gear teeth, the inner rotor is in a circular ring shape and is connected with the central shaft of the inner rotor, the central shaft of the inner rotor is a hollow shaft, the axial direction of the central shaft of the inner rotor is vertical to the plane where the inner rotor is positioned, two ends of the central shaft of the inner rotor are respectively installed on the inner wall of the second end of the shell and the partition wall through bearings, the piston rod is a hollow rod, and an oil pipe is installed in an inner channel formed, the outer end of the oil pipe is an oil inlet end, the inner end of the oil pipe penetrates through a through hole in the piston and then is arranged on the end face of the piston, an oil sprayer is arranged at the inner end of the oil pipe, the outlet of the oil sprayer is positioned in a cavity between the piston and the closed end of the cylinder, a spark plug is arranged at the position, beside the oil sprayer, on the piston, an air inlet pipe is arranged on one side of the outer wall of the joint of the cylinder and the auxiliary cylinder body, an air storage cylinder is arranged on the other side of the outer wall of the joint of the cylinder and the auxiliary cylinder body, the air storage cylinder is communicated with the auxiliary cylinder and is connected with a first end of an air delivery pipe, a second end of the air delivery pipe penetrates through the cylinder wall of the cylinder and is positioned in the position, close to the closed end of the cylinder, an air injection switch is arranged on the position, close to the second end, on the air delivery pipe, the inner rotor or the inner rotor mounting seat is provided with three power receiving contact pieces, the second ends of the three control wires are respectively connected with the three power receiving contact pieces after penetrating through the central through hole of the piston rod, the inner wall of the second end of the shell is provided with three power supply contact pieces at positions corresponding to the three power receiving contact pieces, the three power receiving contact pieces can be respectively in contact connection with the three power supply contact pieces in the rotating process, the closed end of the air cylinder is provided with an exhaust valve, the inner end of the exhaust valve is arranged in the air cylinder, the outer end of the exhaust valve penetrates through the outer rotor and then is arranged outside the outer rotor, the outer end of the exhaust valve is opened after being pressed and closed after being decompressed, and the point A is set as the point A, wherein the point where the connecting straight line of the circle center of the outer rotor and the circle center, the inner wall of the cavity of the shell is provided with an outward convex arc section which is convex towards the direction close to the outer rotor, the radian of the outward convex arc section is consistent with the radian of the outer circle of the outer rotor, the outer end of the exhaust valve can be pressed and opened when rotating to the outward convex arc section, the inner wall of the cavity of the shell is provided with an exhaust port and an air inlet which are communicated with each other inside and outside, the exhaust port is positioned in the area outside the outer rotor, the air inlet is positioned in the position inside the outer rotor, the position on the inner wall of the cavity of the shell between the exhaust port and the outward convex arc section is provided with an exhaust groove or an exhaust through hole, and the air inlet is communicated with.
4. The eccentric dual rotor transmission of claim 3, wherein: the oil pump is characterized in that an annular engine oil channel is arranged in the annular wall of the outer rotor, an air cylinder ring is fixedly arranged at a position, close to the closed end, of the air cylinder, a through hole is formed in one side of the air cylinder ring and communicated with the engine oil channel, the engine oil channel is communicated with an engine oil storage chamber, an engine oil pump chamber is arranged between the air cylinder ring and the piston, a plurality of engine oil holes are formed in the piston on one side of the inner surface of the piston ring and communicated with an engine oil pipeline in the piston rod, the engine oil pump chamber is connected with an inlet of a heat dissipation device through the engine oil pipeline in the piston rod, and an outlet of the heat dissipation device is.
5. The eccentric dual rotor drive of any of claims 1-4, wherein: the eccentric dual-rotor transmission device comprises three groups of connecting devices which are uniformly distributed along the circumferential direction.
6. The eccentric dual rotor drive of any of claims 1-4, wherein: the cylinder and piston structure finally establishes a two-stroke mode of operation to achieve operation in the two-stroke mode under an eccentric dual rotor transmission configuration.
CN202010234421.6A 2020-03-30 2020-03-30 Eccentric birotor transmission device Pending CN111305944A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN202010234421.6A CN111305944A (en) 2020-03-30 2020-03-30 Eccentric birotor transmission device

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN202010234421.6A CN111305944A (en) 2020-03-30 2020-03-30 Eccentric birotor transmission device

Publications (1)

Publication Number Publication Date
CN111305944A true CN111305944A (en) 2020-06-19

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Family Applications (1)

Application Number Title Priority Date Filing Date
CN202010234421.6A Pending CN111305944A (en) 2020-03-30 2020-03-30 Eccentric birotor transmission device

Country Status (1)

Country Link
CN (1) CN111305944A (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN117526600A (en) * 2024-01-03 2024-02-06 上海时的科技有限公司 Rotor structure and brushless motor

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN117526600A (en) * 2024-01-03 2024-02-06 上海时的科技有限公司 Rotor structure and brushless motor
CN117526600B (en) * 2024-01-03 2024-03-08 上海时的科技有限公司 Rotor structure and brushless motor

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