CN116677493B - Circumferential rotor engine - Google Patents

Circumferential rotor engine Download PDF

Info

Publication number
CN116677493B
CN116677493B CN202310962551.5A CN202310962551A CN116677493B CN 116677493 B CN116677493 B CN 116677493B CN 202310962551 A CN202310962551 A CN 202310962551A CN 116677493 B CN116677493 B CN 116677493B
Authority
CN
China
Prior art keywords
piston
cover body
cylinder body
engine
power transmission
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Active
Application number
CN202310962551.5A
Other languages
Chinese (zh)
Other versions
CN116677493A (en
Inventor
赖莉萍
赖毅杰
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Chengdu Technological University CDTU
Original Assignee
Chengdu Technological University CDTU
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Chengdu Technological University CDTU filed Critical Chengdu Technological University CDTU
Priority to CN202310962551.5A priority Critical patent/CN116677493B/en
Publication of CN116677493A publication Critical patent/CN116677493A/en
Application granted granted Critical
Publication of CN116677493B publication Critical patent/CN116677493B/en
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02BINTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
    • F02B53/00Internal-combustion aspects of rotary-piston or oscillating-piston engines
    • F02B53/14Adaptations of engines for driving, or engine combinations with, other devices
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02BINTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
    • F02B55/00Internal-combustion aspects of rotary pistons; Outer members for co-operation with rotary pistons
    • F02B55/02Pistons
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02BINTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
    • F02B55/00Internal-combustion aspects of rotary pistons; Outer members for co-operation with rotary pistons
    • F02B55/08Outer members for co-operation with rotary pistons; Casings
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02TCLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T10/00Road transport of goods or passengers
    • Y02T10/10Internal combustion engine [ICE] based vehicles
    • Y02T10/12Improving ICE efficiencies

Abstract

The application relates to the technical field of mechanical power, in particular to a circumferential rotor engine. The engine comprises a cylinder body, a cover body, a guide post, a protruding part and a piston. The cover body can do circular motion relative to the cylinder body, and when the piston moves to the protruding part, the piston reciprocates up and down along the outline of the protruding part. According to the application, the engine cover body circularly moves around the hollow guide post of the engine cylinder body, and the engine power transmission assembly outputs power transmitted by the piston in the engine cover body; compared with the traditional reciprocating straight cylinder engine, the reciprocating straight cylinder engine has the advantages that the situation that power is greatly subjected to negative working due to design factors is avoided from the integral structure, and the function of increasing mechanical efficiency is achieved.

Description

Circumferential rotor engine
Technical Field
The application relates to the technical field of mechanical power, in particular to a circumferential rotor engine.
Background
Currently, there are two main types of engines.
Firstly, a reciprocating piston engine does reciprocating linear motion in a cylinder during working and can not directly output power, so that the linear motion of a piston is required to be converted into circular motion, and a crank-link mechanism is required to indirectly output circular motion power;
meanwhile, the crank-link mechanism can be regarded as lever movement, the input power is unchanged, the length of the lever is set as a power arm L, the power applied to the power arm by the actual power is dynamically changed, namely, the input power is not perpendicular to the power arm and is changed at regular angles, and the force (tangential direction) actually applied to the power arm is presented: from small to large, calculating 50% of power loss through a series from the change trend from large to small;
according to the power p=fv=f (C/T), the same perimeter motion is equal for the same time, the linear velocity is equal, and the output power fsmeans is lost by 50%, i.e. the mechanical efficiency is lost by 50%. It is also known that the thermal efficiency of the engine does not substantially exceed 50%. Therefore, the reciprocating piston engine must use a crank-link mechanism to indirectly output circular motion power, and the power conversion process has power loss (doing negative work), so the design is not energy-saving.
Secondly, the rotor engine, on one hand, has the working principle that the eccentric rotary motion is then directly transmitted to the output shaft through the rotary power to do circular motion, and the circular motion power is also indirectly output; on the other hand, the pressure bearing surfaces of the piston in the cylinder are actually 2, one power front-end surface and the other power rear-end surface, the power rear-end surface is smaller than the power front-end surface, and the pressure bearing surfaces of the power rear-end surfaces can offset part of forward power, so that the mechanical efficiency of the engine is reduced. Therefore, the design is also not energy efficient.
Both of the above engines have a large duty cycle of power loss due to design.
Disclosure of Invention
It is an object of the present application to provide a circumferential rotary engine to ameliorate the above problems.
In order to achieve the above object, the embodiment of the present application provides the following technical solutions:
the embodiment of the application provides a circumferential rotor engine which comprises a cylinder body, a cover body, a guide post, a protruding part and a piston. The cylinder body is cylindrical; the cover body is circular, the outer diameter of the cover body is equal to the inner diameter of the cylinder body, the cover body is arranged in the cylinder body, and the top of the cover body is flush with the top of the cylinder body; the airtight space formed by the cylinder body and the cover body is used as an air cylinder; one end of the guide post is fixedly connected with the bottom plate of the cylinder body, and the other end of the guide post is contacted with the cover body; the protruding part is arranged on the bottom plate of the cylinder body, the highest position of the protruding part is in contact with the cover body, one side of the protruding part is connected with the guide post, and the other side of the protruding part is connected with the side wall of the cylinder body; the piston is arranged in the cylinder and is connected with the cover body;
the cover body can do circular motion relative to the cylinder body, and when the piston moves to the protruding part, the piston reciprocates up and down along the outline of the protruding part.
Optionally, a first through hole for the piston to pass through is formed in the cover body, and the contour of the first through hole is the same as that of the piston.
Optionally, the cover body is further provided with a return device, the return device and the piston are respectively arranged on two sides of the cover body, the return device comprises two fixing seats, two fixing seats are respectively arranged at two ends of the first through hole, each fixing seat comprises a transverse block, two vertical blocks are respectively arranged at two ends of the transverse block, the two vertical blocks are symmetrically arranged, the transverse block and the vertical blocks are vertically arranged, the two vertical blocks are respectively arranged on two sides of the first through hole, and each fixing seat is provided with a structure for the piston to return.
Optionally, a longitudinal groove is formed in the bottom of the piston, a rolling shaft capable of rolling in the groove is arranged in the groove, and the rolling shaft protrudes out of the piston.
Optionally, a first inclined plane and a second inclined plane are respectively arranged at two sides of the protruding part, the first inclined plane and the second inclined plane are arranged in a mirror image mode, three mounting through holes are formed in the first inclined plane, an air inlet valve, an ignition plug and an oil nozzle are respectively arranged in the three mounting through holes, and the heights of the air inlet valve, the ignition plug and the oil nozzle are lower than the surface of the first inclined plane; and an exhaust notch is arranged on the second inclined plane.
Optionally, a third inclined plane and a fourth inclined plane are respectively arranged at two sides of the bottom of the piston, the third inclined plane and the fourth inclined plane are mirror images, and the inclination angle of the third inclined plane is the same as that of the first inclined plane.
Optionally, the engine further includes power transmission assembly, the guide post middle part is provided with the confession power transmission assembly passes the second through-hole, power transmission assembly includes the power transmission shaft, the tip of power transmission shaft is provided with the power take off gear, the power transmission shaft passes the second through-hole with the lid links to each other, the power take off gear sets up the cylinder body outside.
Optionally, the power transmission shaft is further provided with a spline portion, the spline portion and the power output gear are respectively arranged at two ends of the power transmission shaft, the middle part of the cover body is provided with a spline installation through hole matched with the spline portion, and the spline portion is arranged in the spline installation through hole.
Optionally, a transmission shaft bearing is disposed in the second through hole, an inner tile of the transmission shaft bearing is fixedly connected with the power transmission shaft, and an outer tile of the transmission shaft bearing is fixedly connected with the inner wall of the second through hole.
Optionally, the protruding part is a fan-shaped boss, and the circle center of the protruding part coincides with the center axis of the cylinder body.
Optionally, two protruding portions are arranged in the cylinder body, the two protruding portions are respectively arranged on two sides of the cylinder body, the two protruding portions are arranged in a mirror image mode, the two pistons are arranged, and the two pistons are respectively arranged on two sides of a connecting line of the two protruding portions.
The beneficial effects of the application are as follows:
according to the application, the engine cover body circularly moves around the hollow guide post of the engine cylinder body, and the engine power transmission assembly outputs power transmitted by the piston in the engine cover body; compared with the traditional reciprocating straight cylinder engine, the reciprocating straight cylinder engine has the advantages that the situation that power is greatly subjected to negative working due to design factors is avoided from the integral structure, and the function of increasing mechanical efficiency is achieved.
Additional features and advantages of the application will be set forth in the description which follows, and in part will be apparent from the description, or may be learned by practice of the embodiments of the application. The objectives and other advantages of the application will be realized and attained by the structure particularly pointed out in the written description and claims thereof as well as the appended drawings.
Drawings
In order to more clearly illustrate the technical solutions of the embodiments of the present application, the drawings that are needed in the embodiments will be briefly described below, it being understood that the following drawings only illustrate some embodiments of the present application and therefore should not be considered as limiting the scope, and other related drawings may be obtained according to these drawings without inventive effort for a person skilled in the art.
FIG. 1 is a schematic diagram of a front axle side structure of an engine according to an embodiment of the present application;
FIG. 2 is a schematic view of the reverse side shaft side structure of an engine according to an embodiment of the present application;
FIG. 3 is a schematic front view of an engine according to an embodiment of the present application;
FIG. 4 is a schematic rear view of an engine according to an embodiment of the present application;
FIG. 5 is a schematic top view of an engine according to an embodiment of the present application;
FIG. 6 is a schematic view of an exploded construction of an engine according to an embodiment of the present application;
FIG. 7 is a schematic diagram of an assembled front view of an engine according to an embodiment of the present application;
FIG. 8 is a schematic A-A cross-sectional configuration of the engine depicted in FIG. 7;
FIG. 9 is a schematic diagram of a front axle side structure of an engine according to another embodiment of the present application;
fig. 10 is a schematic view of the reverse side shaft side structure of an engine according to another embodiment of the present application.
The marks in the figure: 1. a cylinder; 2. a cover body; 3. a power transmission assembly; 4. a protruding portion; 5. an exhaust notch; 6. an intake valve; 7. a spark plug; 8. an oil nozzle; 9. a threaded hole; 10. a drive shaft bearing; 11. a first through hole; 12. a spline portion; 13. a spline mounting through hole; 14. a piston; 15. a return device; 16. a rolling shaft; 17. a fixing seat; 18. a telescopic rod; 19. a reset mechanism; 20. a guide post; 21. a power take-off gear; 22. and a power transmission shaft.
Description of the embodiments
For the purpose of making the objects, technical solutions and advantages of the embodiments of the present application more apparent, the technical solutions of the embodiments of the present application will be clearly and completely described below with reference to the accompanying drawings in the embodiments of the present application, and it is apparent that the described embodiments are some embodiments of the present application, but not all embodiments of the present application. The components of the embodiments of the present application generally described and illustrated in the figures herein may be arranged and designed in a wide variety of different configurations. Thus, the following detailed description of the embodiments of the application, as presented in the figures, is not intended to limit the scope of the application, as claimed, but is merely representative of selected embodiments of the application. All other embodiments, which can be made by those skilled in the art based on the embodiments of the application without making any inventive effort, are intended to be within the scope of the application.
It should be noted that: like reference numerals or letters denote like items in the following figures, and thus once an item is defined in one figure, no further definition or explanation thereof is necessary in the following figures. Meanwhile, in the description of the present application, the terms "first", "second", and the like are used only to distinguish the description, and are not to be construed as indicating or implying relative importance.
Examples
The present embodiment shows a circumferential rotary engine, as shown in fig. 1 to 8, which includes a cylinder block 1, a cover 2, a guide post 20, a protrusion 4, and a piston 14. The cylinder body 1 is cylindrical; the cover body 2 is circular, the outer diameter of the cover body 2 is equal to the inner diameter of the cylinder body 1, the cover body 2 is arranged in the cylinder body 1, and the top of the cover body 2 is level with the top of the cylinder body 1; the airtight space formed by the cylinder body 1 and the cover body 2 is used as an air cylinder; one end of the guide post 20 is fixedly connected with the bottom plate of the cylinder body 1, and the other end of the guide post 20 is contacted with the cover body 2; the protruding part 4 is arranged on the bottom plate of the cylinder body 1, the highest position of the protruding part 4 is in contact with the cover body 2, one side of the protruding part 4 is connected with the guide post 20, and the other side is connected with the side wall of the cylinder body 1; the piston 14 is arranged in the cylinder, and the piston 14 is connected with the cover body 2; the cover 2 is movable in a circular motion relative to the cylinder 1, and when the piston 14 moves to the protrusion 4, the piston 14 reciprocates up and down along the contour of the protrusion 4.
According to the application, the engine cover body 2 performs circular motion around the hollow guide post 20 of the engine cylinder body 1, and the engine power transmission assembly 3 outputs power transmitted by the piston 14 in the engine cover body 2; compared with the traditional reciprocating straight cylinder engine, the reciprocating straight cylinder engine has the advantages that the situation that power is greatly subjected to negative working due to design factors is avoided from the integral structure, and the function of increasing mechanical efficiency is achieved.
Optionally, the cover 2 is provided with a first through hole 11 for the piston 14 to pass through, and the contour of the first through hole 11 is the same as that of the piston 14.
The first through hole 11 is through which the piston 14 passes, and when the piston 14 moves to the protrusion 4, it is required to reciprocate up and down along the contour of the protrusion 4. Due to the same contour, airtightness is ensured when the piston 14 reciprocates in the first through-hole 11.
Optionally, the cover 2 is further provided with a return device 15, the return device 15 and the piston 14 are respectively disposed on two sides of the cover 2, the return device 15 includes two fixing seats 17, two fixing seats 17 are respectively disposed on two ends of the first through hole 11, each fixing seat 17 includes a horizontal block, two vertical blocks are respectively disposed on two ends of the horizontal block, two vertical blocks are symmetrically disposed, the horizontal block and the vertical blocks are vertically disposed, two vertical blocks are respectively disposed on two sides of the first through hole 11, and each fixing seat 17 is provided with a structure capable of allowing the piston 14 to return.
Alternatively, the structure for returning the piston 14 may be that a through hole is formed in a transverse block of the fixed seat 17, a telescopic rod is arranged on the piston 14, a return mechanism 19 is sleeved on the telescopic rod, the telescopic rod passes through the through hole, when the piston 14 moves to the position of the protruding part 4, the piston 14 moves upwards along the track of the telescopic rod, after the piston 14 passes over the highest position of the protruding part 4, the piston 14 moves downwards under the action of the elastic force of the return mechanism 19, so as to realize the return effect, the return mechanism 19 may be a spring, a damper or the like, or an electric control hydraulic system, for example, when the piston 14 moves to the protruding part 4, the hydraulic system controls the piston 14 to shrink along the contour line of the protruding part 4, and when the piston 14 passes over the highest position of the protruding part 4, the hydraulic system controls the piston 14 to stretch along the contour line of the protruding part until the piston 14 is completely returned.
Alternatively, the structure for returning the piston 14 may be that a telescopic rod 18 is arranged on the piston 14, one end of the telescopic rod is connected with the piston 14, and the other end is connected with a transverse block on the fixed seat 17.
Optionally, the structure for returning the piston 14 may also be that a telescopic rod 18 is disposed on the piston 14, one end of the telescopic rod is connected with the piston 14, the other end is connected with a transverse block on the fixing seat 17, and a return mechanism 19 is sleeved on the telescopic rod 18, so that smooth rebound of the piston 14 can be ensured.
Optionally, a longitudinal groove is formed at the bottom of the piston 14, a rolling shaft 16 capable of rolling in the groove is disposed in the groove, and the rolling shaft 16 protrudes from the piston 14.
The rolling shaft 16 can better enable the piston 14 to move in the cylinder body 1, and air tightness can be ensured.
Optionally, a first inclined plane and a second inclined plane are respectively arranged at two sides of the protruding part 4, the first inclined plane and the second inclined plane are mirror images, three mounting through holes are formed in the first inclined plane, an air inlet valve 6, an ignition plug 7 and an oil nozzle 8 are respectively arranged in the three mounting through holes, and the heights of the air inlet valve 6, the ignition plug 7 and the oil nozzle 8 are lower than the surface of the first inclined plane; and an exhaust notch 5 is arranged on the second inclined plane.
Optionally, a third inclined plane and a fourth inclined plane are respectively disposed on two sides of the bottom of the piston 14, the third inclined plane and the fourth inclined plane are mirror images, and an inclination angle of the third inclined plane is the same as an inclination angle of the first inclined plane.
The arrangement of the first inclined plane, the second inclined plane, the third inclined plane and the fourth inclined plane can enable the piston to have buffering and obstacle avoidance effects when passing through the protruding portion 4, prevent the piston 14 from interfering with the sending motion of the protruding portion 4, and enable the piston 14 to pass through the protruding portion more smoothly.
Optionally, the protruding part 4 is a fan-shaped boss, and the center of the protruding part 4 coincides with the central axis of the cylinder body 1.
By providing this, the boundaries of the first inclined surface and the second inclined surface of the protruding portion 4 can be kept constant with the piston 14, and the resistance of the piston 14 to passing through the protruding portion 4 can be reduced.
Optionally, the engine further includes a power transmission assembly 3, a second through hole for the power transmission assembly 3 to pass through is provided in the middle of the guide post 20, the power transmission assembly 3 includes a power transmission shaft 22, a power output gear 21 is provided at an end of the power transmission shaft 22, the power transmission shaft 22 passes through the second through hole and is connected with the cover 2, and the power output gear 21 is disposed outside the cylinder 1.
Optionally, the power transmission shaft 22 is further provided with a spline portion 12, the spline portion 12 and the power output gear 21 are respectively disposed at two ends of the power transmission shaft 22, a spline mounting through hole 13 matched with the spline portion 12 is disposed in the middle of the cover 2, and the spline portion 12 is disposed in the spline mounting through hole 13.
Optionally, a transmission shaft bearing 10 is disposed in the second through hole, an inner tile of the transmission shaft bearing 10 is fixedly connected with the power transmission shaft 22, and an outer tile of the transmission shaft bearing 10 is fixedly connected with an inner wall of the second through hole.
Alternatively, in order to make the connection between the transmission shaft bearing 10 and the cover 2 and the power transmission assembly 3 tighter, threaded holes may be formed at two ends of the inner tile of the transmission shaft bearing 10, and simultaneously threaded holes 9 may be formed at corresponding positions of the cover 2 and the power output gear 21, so that the connection between the transmission shaft bearing 10 and the cover 2 and the power transmission assembly 3 is more stable through the cooperation of the bolts and the threaded holes 9.
The working process of the engine of the embodiment is as follows: after passing through the transmission shaft bearing 10 in the hollow guide post 20 on the engine cylinder body 1, the spline part 12 of the engine power transmission assembly 3 is matched with the spline installation through hole 13 on the engine cover body 2, the threaded hole 9 on the engine cover body 2 is locked with the threaded hole 9 on the inner tile close to the transmission shaft bearing 10 by bolts, and the threaded hole 9 on the engine power output gear 21 is locked with the threaded hole 9 on the inner tile close to the transmission shaft bearing 10 by bolts; the air inlet valve 6 is used for air intake, the oil injection nozzle 8 is used for oil injection, and the spark plug 7 is used for igniting mixed gas, so that the gas expansion of the combustion chamber drives the piston 14 to do circular motion around the hollow guide post 20, the engine cover body 2 is driven to do circular rotation motion, and the engine cover body 2 is matched with the spline part 12 of the engine power transmission assembly 3 to transmit power to the engine power output gear 21. In the process, the rolling shaft 16 of the piston 14 reduces friction power loss, when the piston 14 moves to the second inclined plane of the protruding part 4, the piston 14 rises under the buffer action of the second inclined plane of the protruding part 4, and the area of the exhaust notch 5 gradually increases to realize exhaust.
In the embodiment, the engine cover body 2 performs circular motion around the guide post 20 of the engine cylinder body 1, and the engine power transmission assembly outputs power transmitted by the piston 14 in the engine cover body 2; compared with the traditional reciprocating straight cylinder engine, the reciprocating straight cylinder engine has the advantages that the situation that power is greatly subjected to negative working due to design factors is avoided from the integral structure, and the function of increasing mechanical efficiency is achieved. The intake valve 6, the spark plug 7 and the oil nozzle 8 are embedded into the through hole of the first inclined plane of the protruding part 4, and the heights of the intake valve 6, the spark plug 7 and the oil nozzle 8 are lower than the inclined plane height of the first inclined plane, so that the internal space of the engine is optimized. The piston 14 rises when the piston 14 passes through the second inclined plane of the protruding part 4 under the action of the return device 15, descends when the piston 14 passes through the first inclined plane of the protruding part 4, and has the buffering obstacle avoidance function when passing through the protruding part 4, so that the normal operation of the engine is ensured.
The mechanical return device 15 such as a spring has the advantages of timely response, stable performance and low price. The spline part 12 is combined with the engine cover body 2 of the power input end in the engine power transmission assembly, so that the engine power transmission assembly has stronger stress bearing capacity and can reduce the abrasion of the power input contact part. The transmission shaft bearing 10 is sleeved in the guide post 20, so that the transmission friction force is reduced; screw holes 9 are formed in the two ends of the bearing inner tile, screw holes 9 corresponding to the screw holes 9 of the transmission shaft bearing 10 inner tile are formed in the end portions of the engine cover body 2 and the end portions of the engine power output gear 21, so that bolts are used for locking, and the power transmission assembly 3 can be effectively fixed with the engine cylinder body 1 and the cover body 2. The fan-shaped boss can better fit the regular movement of the piston 14 in the process that the piston 14 runs along the first inclined plane or the second inclined plane, and larger resistance and irregular shaking are reduced when the piston 14 moves to the protruding part 4.
As another embodiment, as shown in fig. 9 and 10, two protruding portions 4 are disposed in the cylinder 1, the two protruding portions 4 are disposed on two sides of the cylinder 1, the two protruding portions 4 are disposed in mirror images, the two pistons 14 are disposed, and the two pistons 14 are disposed on two sides of a line connecting the two protruding portions 4.
In this embodiment, the engine may be referred to as a 2-cylinder engine, and when the engine is running, the left and right weights on the engine cover 2 are uniform, so that running jolts can be reduced, and the engine is damaged.
The above is only a preferred embodiment of the present application, and is not intended to limit the present application, but various modifications and variations can be made to the present application by those skilled in the art. Any modification, equivalent replacement, improvement, etc. made within the spirit and principle of the present application should be included in the protection scope of the present application.
The foregoing is merely illustrative embodiments of the present application, but the scope of the present application is not limited thereto, and any person skilled in the art can easily think about variations or substitutions within the technical scope of the present application, and the application should be covered. Therefore, the protection scope of the application is subject to the protection scope of the claims.

Claims (10)

1. A circumferential rotary engine, comprising:
a cylinder body (1), wherein the cylinder body (1) is cylindrical;
the cover body (2), the cover body (2) is circular, the external diameter of the cover body (2) is equal to the internal diameter of the cylinder body (1), the cover body (2) is arranged in the cylinder body (1), and the top of the cover body (2) is flush with the top of the cylinder body (1); the airtight space formed by the cylinder body (1) and the cover body (2) is used as an air cylinder;
the guide column (20), one end of the guide column (20) is fixedly connected with the bottom plate of the cylinder body (1), and the other end of the guide column (20) is contacted with the cover body (2);
the protruding part (4) is arranged on the bottom plate of the cylinder body (1), the highest position of the protruding part (4) is in contact with the cover body (2), one side of the protruding part (4) is connected with the guide column (20), and the other side of the protruding part is connected with the side wall of the cylinder body (1); and
the piston (14) is arranged in the cylinder, and the piston (14) is connected with the cover body (2);
the cover body (2) moves circularly relative to the cylinder body (1), and when the piston (14) moves to the protruding part (4), the piston (14) reciprocates up and down along the outline of the protruding part (4).
2. A circumferential rotary engine according to claim 1, characterized in that the cover (2) is provided with a first through hole (11) through which the piston (14) passes, the first through hole (11) having the same contour as the piston (14).
3. The circumference rotary engine according to claim 2, characterized in that the cover body (2) is further provided with a return device (15), the return device (15) and the piston (14) are respectively arranged at two sides of the cover body (2), the return device (15) comprises two fixing seats (17), the two fixing seats (17) are respectively arranged at two ends of the first through hole (11), each fixing seat (17) comprises a transverse block, two vertical blocks are respectively arranged at two ends of the transverse block, the two vertical blocks are symmetrically arranged, the transverse block and the vertical blocks are vertically arranged, the two vertical blocks are respectively arranged at two sides of the first through hole (11), and a structure capable of allowing the piston (14) to return is respectively arranged on each fixing seat (17).
4. A circumferential rotary engine according to claim 1, characterized in that the bottom of the piston (14) is provided with a longitudinal groove, in which groove a rolling shaft (16) is provided which can roll in the groove, the rolling shaft (16) protruding from the piston (14).
5. The circumferential rotary engine according to claim 1, characterized in that both sides of the protruding portion (4) are provided with a first inclined surface and a second inclined surface, respectively, the first inclined surface and the second inclined surface are mirror images of each other, three mounting through holes are provided on the first inclined surface, an intake valve (6), a spark plug (7) and an oil nozzle (8) are provided in the three mounting through holes, respectively, and the heights of the intake valve (6), the spark plug (7) and the oil nozzle (8) are lower than the surface of the first inclined surface; and an exhaust notch (5) is arranged on the second inclined plane.
6. The rotary circumferential engine of claim 5, characterized in that the piston (14) is provided with a third bevel and a fourth bevel on each side of the bottom, the third bevel and the fourth bevel being mirror images of each other, the third bevel having the same angle of inclination as the first bevel.
7. The circumferential rotary engine according to claim 1, further comprising a power transmission assembly (3), wherein a second through hole for the power transmission assembly (3) to pass through is provided in the middle of the guide post (20), the power transmission assembly (3) comprises a power transmission shaft (22), a power output gear (21) is provided at the end of the power transmission shaft (22), the power transmission shaft (22) passes through the second through hole and is connected with the cover body (2), and the power output gear (21) is arranged outside the cylinder body (1).
8. The circumferential rotary engine according to claim 7, characterized in that the power transmission shaft (22) is further provided with a spline portion (12), the spline portion (12) and the power output gear (21) are respectively provided at both ends of the power transmission shaft (22), a spline installation through hole (13) matched with the spline portion (12) is provided at the middle part of the cover body (2), and the spline portion (12) is provided in the spline installation through hole (13).
9. The circumferential rotary engine of claim 7, wherein a drive shaft bearing (10) is disposed within the second through bore, an inner shoe of the drive shaft bearing (10) is fixedly coupled to the power drive shaft (22), and an outer shoe of the drive shaft bearing (10) is fixedly coupled to an inner wall of the second through bore.
10. The circumferential rotary engine according to claim 1, characterized in that two protruding parts (4) are arranged in the cylinder body (1), the two protruding parts (4) are respectively arranged at two sides of the cylinder body (1), the two protruding parts (4) are arranged in a mirror image mode, the two pistons (14) are arranged, and the two pistons (14) are respectively arranged at two sides of a connecting line of the two protruding parts (4).
CN202310962551.5A 2023-08-02 2023-08-02 Circumferential rotor engine Active CN116677493B (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN202310962551.5A CN116677493B (en) 2023-08-02 2023-08-02 Circumferential rotor engine

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN202310962551.5A CN116677493B (en) 2023-08-02 2023-08-02 Circumferential rotor engine

Publications (2)

Publication Number Publication Date
CN116677493A CN116677493A (en) 2023-09-01
CN116677493B true CN116677493B (en) 2023-09-26

Family

ID=87779515

Family Applications (1)

Application Number Title Priority Date Filing Date
CN202310962551.5A Active CN116677493B (en) 2023-08-02 2023-08-02 Circumferential rotor engine

Country Status (1)

Country Link
CN (1) CN116677493B (en)

Citations (35)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3902465A (en) * 1974-02-04 1975-09-02 Byron O Stookey Rotary engine
US5304048A (en) * 1991-10-15 1994-04-19 Charles Chao-peng Huang Scissor-action piston rotary engine with distributive arms
CN2243543Y (en) * 1995-08-06 1996-12-25 刘弘 Rotor engine
JPH09151710A (en) * 1995-11-30 1997-06-10 Aisin Seiki Co Ltd Valve opening/closing timing control device
KR19990081644A (en) * 1998-04-30 1999-11-15 최진희 Coaxial Reciprocating Engine
KR20000020411A (en) * 1998-09-21 2000-04-15 최진희 Coaxial type reciprocating engine
KR20030077864A (en) * 2002-03-27 2003-10-04 김동현 Sealing device for rotary engine
CN101033711A (en) * 2007-04-09 2007-09-12 曾庆仁 Curved cylinder rotary internal combustion engine without crankshaft
CN200955441Y (en) * 2006-09-12 2007-10-03 任国明 Rotary rotor IC engine
CN101067379A (en) * 2006-10-31 2007-11-07 黄庆培 Piston device with rotary blade
RU2007138650A (en) * 2007-10-15 2009-04-20 Иван Дмитриевич Федоров (RU) DIRECT ACTION ROTARY INTERNAL COMBUSTION ENGINE
CN201347797Y (en) * 2009-01-22 2009-11-18 丁杰 Cylinder body mechanism in circular motion piston type internal combustion engine
CN101684745A (en) * 2009-05-11 2010-03-31 郑福建 Rotary type internal combustion engine with two corner pistons
WO2010051794A2 (en) * 2008-11-04 2010-05-14 Waldemar Seidler Rotary piston engine, control system for actuating a counter piston and method for the cycle-controlled operation of a rotary piston engine
CN101818685A (en) * 2010-04-28 2010-09-01 北京航空航天大学 Four-corner rotating piston engine
CN102606291A (en) * 2011-01-23 2012-07-25 梁天宇 Engine
WO2012115379A2 (en) * 2011-02-21 2012-08-30 Heon-Kyu Kim Gear type connection device for transmitting rotating power of rotors of rotary engine to output gear shaft
CN103282603A (en) * 2010-12-31 2013-09-04 纳克多·加西亚·罗德里格斯 Rotary heat engine
CN203335230U (en) * 2013-01-09 2013-12-11 黄荣嵘 Turbine rotor energy-saving engine
CN103764951A (en) * 2011-03-25 2014-04-30 赖因哈德·迪姆 Combustion engine having a rotor that is rotatable about the axis thereof
CN103899413A (en) * 2014-03-21 2014-07-02 袁政 Novel rotor engine
CN103939202A (en) * 2014-04-15 2014-07-23 蒋祖贵 Reciprocating-rotation piston engine
CN204851429U (en) * 2015-04-21 2015-12-09 陕西融悟动力科技有限公司 Circle rotor formula internal -combustion engine
CN106285928A (en) * 2016-10-17 2017-01-04 龙建 Piston stops the continuous rotary engine of dynamic formula
RU2629525C1 (en) * 2016-04-11 2017-08-29 Руслан Идрисович Джанаралиев Orbital internal combustion engine
WO2018129639A1 (en) * 2017-01-16 2018-07-19 袁新文 Multi-trajectory rotor-type internal combustion engine
CN111140343A (en) * 2020-01-10 2020-05-12 谢华秋 Rotary disc type engine
WO2020141553A1 (en) * 2019-01-02 2020-07-09 Patel Vipulkumar D A radial opposed piston reciprocating internal combustion engine
CN111472882A (en) * 2020-05-27 2020-07-31 朱永明 Regular round rotor lever type rotary engine
CN211524953U (en) * 2019-12-10 2020-09-18 吕国良 Novel piston rotor type engine
CN211737282U (en) * 2020-01-10 2020-10-23 谢华秋 Rotary disc type engine
WO2021114438A1 (en) * 2019-12-13 2021-06-17 李炳强 Blade rotary engine
CN113513366A (en) * 2021-05-21 2021-10-19 唐良伦 Rotary valve rotor engine
CN114294106A (en) * 2022-01-27 2022-04-08 汪建 Circular cylinder internal combustion engine
KR20220100427A (en) * 2021-01-08 2022-07-15 엘지전자 주식회사 Rotor for rotary engine

Family Cites Families (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2004537011A (en) * 2001-07-25 2004-12-09 トーラス テク カンパニー リミテッド Torus crank mechanism
CN110439677A (en) * 2019-07-29 2019-11-12 江苏大学 A kind of rotary engine

Patent Citations (35)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3902465A (en) * 1974-02-04 1975-09-02 Byron O Stookey Rotary engine
US5304048A (en) * 1991-10-15 1994-04-19 Charles Chao-peng Huang Scissor-action piston rotary engine with distributive arms
CN2243543Y (en) * 1995-08-06 1996-12-25 刘弘 Rotor engine
JPH09151710A (en) * 1995-11-30 1997-06-10 Aisin Seiki Co Ltd Valve opening/closing timing control device
KR19990081644A (en) * 1998-04-30 1999-11-15 최진희 Coaxial Reciprocating Engine
KR20000020411A (en) * 1998-09-21 2000-04-15 최진희 Coaxial type reciprocating engine
KR20030077864A (en) * 2002-03-27 2003-10-04 김동현 Sealing device for rotary engine
CN200955441Y (en) * 2006-09-12 2007-10-03 任国明 Rotary rotor IC engine
CN101067379A (en) * 2006-10-31 2007-11-07 黄庆培 Piston device with rotary blade
CN101033711A (en) * 2007-04-09 2007-09-12 曾庆仁 Curved cylinder rotary internal combustion engine without crankshaft
RU2007138650A (en) * 2007-10-15 2009-04-20 Иван Дмитриевич Федоров (RU) DIRECT ACTION ROTARY INTERNAL COMBUSTION ENGINE
WO2010051794A2 (en) * 2008-11-04 2010-05-14 Waldemar Seidler Rotary piston engine, control system for actuating a counter piston and method for the cycle-controlled operation of a rotary piston engine
CN201347797Y (en) * 2009-01-22 2009-11-18 丁杰 Cylinder body mechanism in circular motion piston type internal combustion engine
CN101684745A (en) * 2009-05-11 2010-03-31 郑福建 Rotary type internal combustion engine with two corner pistons
CN101818685A (en) * 2010-04-28 2010-09-01 北京航空航天大学 Four-corner rotating piston engine
CN103282603A (en) * 2010-12-31 2013-09-04 纳克多·加西亚·罗德里格斯 Rotary heat engine
CN102606291A (en) * 2011-01-23 2012-07-25 梁天宇 Engine
WO2012115379A2 (en) * 2011-02-21 2012-08-30 Heon-Kyu Kim Gear type connection device for transmitting rotating power of rotors of rotary engine to output gear shaft
CN103764951A (en) * 2011-03-25 2014-04-30 赖因哈德·迪姆 Combustion engine having a rotor that is rotatable about the axis thereof
CN203335230U (en) * 2013-01-09 2013-12-11 黄荣嵘 Turbine rotor energy-saving engine
CN103899413A (en) * 2014-03-21 2014-07-02 袁政 Novel rotor engine
CN103939202A (en) * 2014-04-15 2014-07-23 蒋祖贵 Reciprocating-rotation piston engine
CN204851429U (en) * 2015-04-21 2015-12-09 陕西融悟动力科技有限公司 Circle rotor formula internal -combustion engine
RU2629525C1 (en) * 2016-04-11 2017-08-29 Руслан Идрисович Джанаралиев Orbital internal combustion engine
CN106285928A (en) * 2016-10-17 2017-01-04 龙建 Piston stops the continuous rotary engine of dynamic formula
WO2018129639A1 (en) * 2017-01-16 2018-07-19 袁新文 Multi-trajectory rotor-type internal combustion engine
WO2020141553A1 (en) * 2019-01-02 2020-07-09 Patel Vipulkumar D A radial opposed piston reciprocating internal combustion engine
CN211524953U (en) * 2019-12-10 2020-09-18 吕国良 Novel piston rotor type engine
WO2021114438A1 (en) * 2019-12-13 2021-06-17 李炳强 Blade rotary engine
CN111140343A (en) * 2020-01-10 2020-05-12 谢华秋 Rotary disc type engine
CN211737282U (en) * 2020-01-10 2020-10-23 谢华秋 Rotary disc type engine
CN111472882A (en) * 2020-05-27 2020-07-31 朱永明 Regular round rotor lever type rotary engine
KR20220100427A (en) * 2021-01-08 2022-07-15 엘지전자 주식회사 Rotor for rotary engine
CN113513366A (en) * 2021-05-21 2021-10-19 唐良伦 Rotary valve rotor engine
CN114294106A (en) * 2022-01-27 2022-04-08 汪建 Circular cylinder internal combustion engine

Non-Patent Citations (1)

* Cited by examiner, † Cited by third party
Title
新型转子发动机探索;袁政;;佛山科学技术学院学报(自然科学版)(第01期);23-28页 *

Also Published As

Publication number Publication date
CN116677493A (en) 2023-09-01

Similar Documents

Publication Publication Date Title
JP5090456B2 (en) Conversion mechanism between reciprocating linear motion and rotational motion
US20040231619A1 (en) Compression ratio variable device of internal combustion engine
EP1831503A1 (en) Internal-combustion engine with guided roller piston drive
US4974555A (en) Piston motor with parallel cylinders arranged around the driving shaft
CN106870156B (en) A kind of double ratchet wheels formula driving engine structure
CN116677493B (en) Circumferential rotor engine
CN110617146B (en) Link mechanism and engine
CN110566426A (en) Double-acting groove cam constant-flow reciprocating pump
JP3204412U (en) Cam-driven reciprocating engine
EP1813791B1 (en) Internal combustion engine
CN107956593B (en) Dual-motor type variable compression ratio piston
CN106014630A (en) Movable-type reciprocating piston-type internal combustion engine and assembly method and power output mechanism thereof
AU603278B2 (en) Refrigerant compressor with axial vibration absorption mechanism
RU2267016C1 (en) Axial internal combustion engine
US10865706B1 (en) Spherical linear two stroke engine
CN110671199A (en) Variable compression ratio mechanism and engine
CN110657024A (en) Variable compression ratio mechanism and engine
CN201288609Y (en) Free piston type rotary power engine
CN209129756U (en) A kind of internal combustion engine
CN217481517U (en) Hollow plunger structure
CN209781442U (en) Connecting rod structure
CN105971724A (en) Horizontally-opposed cylindrical cam engine
GB2038937A (en) Reciprocating Piston Engine
KR20080010950A (en) Mechanism for converting motions and inner combustion engine comprising thereof
CN112145288A (en) Double-crankshaft composite piston internal combustion engine

Legal Events

Date Code Title Description
PB01 Publication
PB01 Publication
SE01 Entry into force of request for substantive examination
SE01 Entry into force of request for substantive examination
GR01 Patent grant
GR01 Patent grant