A gas powered device

Abstract

The present invention discloses a gas power device, comprising an outer ring and a core body, wherein at least one-step secondary flow channel is arranged between the nozzle and the exhaust port on the outer ring surface of the core body, gas enters from the air inlet channel, is ejected step by step through the nozzle of the core body and the secondary flow channel, acts on at least two driving recesses on the circumference of the outer ring, generates thrust on these driving recesses, drives the outer ring to rotate and do work, realizes power output, and finally, the gas is discharged through the exhaust port of the core body via the exhaust channel.

Description

Technical Field

[0001] The present invention discloses a gas power device, which belongs to the technical field of mechanical devices for generating power according to the International Patent Classification (IPC). Background Art

[0002] The original meaning of engine refers to a "mechanical device that generates power". It is a machine that converts a certain form of energy into mechanical energy, such as converting the chemical energy of liquid or gas combustion into heat energy after combustion, and then converting the heat energy into mechanical energy through expansion and outputting power to the outside. The current research direction of engines, especially pneumatic engines, is to develop compact, efficient and reliable small engines. Most of them are in the experimental and trial production stage and have not yet been widely used in commercial applications.

[0003] At present, most gas engine design prototypes are based on piston engines or vane pumps, which convert energy through heat exchangers to achieve power output, but their structures are complex and their efficiency is low, making it difficult to meet the requirements of endurance.

[0004] Chinese document CN201410167469.4 discloses a variable pressure jet air engine, including an impeller chamber and an impeller, the impeller chamber is provided with an injection hole for injecting compressed gas and an exhaust hole for ejecting compressed gas, the impeller is installed in the impeller chamber through a rotating shaft, the impeller includes an air gap along the rotating circumference and the inner surface of the impeller chamber, and the inner surface of the impeller chamber is also provided with a variable pressure jet groove. The structure of this document is similar to that of a vane pump, and the provision of the variable pressure jet groove leads to low engine speed and low efficiency.

[0005] Chinese document CN107083994A discloses a pneumatic engine, which is an invention of an air engine previously proposed by the inventor of this case. It is ejected through the intake air duct of the direct-drive power movement, acting on the groove surface of the outer ring, generating thrust to drive the rotating outer ring. It is a major disruptive change in the engine field. Its output torque can match that of existing automobile engines, and its equivalent cruising range is comparable to that of similar new energy vehicles currently available.

[0006] In order to further improve the engine performance and realize a compact, efficient and reliable gas power generation device, the inventor has proposed the present invention after many years of development and research. Summary of the invention

[0007] In view of the deficiencies in the prior art, the present invention provides a gas power device, which utilizes the energy of the gas multiple times through the multi-stage flow channels circumferentially arranged on the core body, and realizes power output by driving the rotating outer ring through the core body. The device has the advantages of compact structure, large torque, high speed, high transmission efficiency, energy saving and environmental protection.

[0008] To achieve the above object, the present invention is achieved through the following technical solutions:

[0009] A gas powered device comprising:

[0010] An outer ring, whose inner ring surface is circumferentially provided with a plurality of driving recesses;

[0011] A core body is coaxially arranged in the outer ring and can rotate relative to the outer ring, and the outer ring surface of the core body is provided with at least one nozzle, at least one discharge port, and at least one flushing channel located between the nozzle and the discharge port;

[0012] at least one air inlet passage connected to at least one nozzle; and

[0013] at least one exhaust passage connected to at least one exhaust port;

[0014] The gas enters from the air inlet channel, is ejected step by step through the nozzle of the core body and the secondary flow channel, and acts on at least two driving recesses on the circumference of the outer ring, generating thrust for these driving recesses to drive the outer ring to rotate and do work, thereby realizing power output. Finally, the gas is discharged through the exhaust channel through the exhaust port of the core body.

[0015] Furthermore, at least one air inlet channel, at least one nozzle, at least two driving recesses, at least one primary flow channel, at least one discharge port and at least one exhaust channel form an independent working unit, and the gas power device includes at least one independent working unit.

[0016] Furthermore, the nozzles and secondary flow channels on the core body are connected to the driving recesses corresponding to the outer ring. The secondary flow channels are arranged alternately and connected in sequence with the corresponding driving recesses. The secondary flow channels are arranged circumferentially along the core body or the outer ring.

[0017] Further, an intake passage and an exhaust passage are formed in the core.

[0018] Furthermore, the core includes:

[0019] An air inlet passage, which forms a nozzle on the peripheral surface of the core body, and whose direction is an arc line extending from the middle to the outside, and the nozzle is connected with the driving concave portion corresponding to the outer ring to form a first-stage flow channel;

[0020] The secondary flow channel is an arc line extending from the edge of the core body inward and then bending to the edge. Each secondary flow channel is connected with the front and rear driving recesses corresponding to the outer ring, forming N-step flow channels along the circumference of the core body, where N is a natural number ≥ 2;

[0021] Each step of the flow channel cooperates with the corresponding driving recess of the outer ring to form a multi-step stroke structure with decreasing gas energy.

[0022] Furthermore, the secondary flow channel includes a return channel and a communicating stroke channel, the return channel is communicated with a driving recess corresponding to the outer ring, and the stroke channel is communicated with another driving recess.

[0023] Furthermore, the direction of the core air inlet channel is a logarithmic spiral extending from the middle to the outside, the pole of the logarithmic spiral is set on the central axis of the core, and the direction angle of the logarithmic spiral is 15°-45°.

[0024] Furthermore, an air inlet channel is provided on the core body, and its direction is a logarithmic spiral extending from the middle to the outside, and the direction of the stroke channel of the secondary flow channel is a logarithmic spiral. The direction of the logarithmic spiral of the stroke channel of the secondary flow channel is roughly the same as the direction of the logarithmic spiral of the air inlet channel.

[0025] Furthermore, the gas power device also includes a shaft, and the outer ring and the core body are coaxially arranged on the shaft.

[0026] Furthermore, the gas power device also includes a shaft, the outer ring is coaxially arranged on the shaft with the core body, and the shaft is provided with inlet and outlet shaft passages which are respectively connected to the inlet channel and the exhaust channel of the core body.

[0027] The air inlet and outlet shaft passages in the shaft form an air inlet and an air outlet, and the air inlet and outlet shaft passages are non-connected structures.

[0028] Furthermore, the outer ring is matched with the shaft through the side plates to form a closed space, and the core body is arranged in the closed space and is connected and fixed to the shaft.

[0029] Furthermore, the air inlet channel, the nozzle, the driving recess, the secondary flow channel, the exhaust port and the exhaust channel in the independent working unit constitute a gas flow path.

[0030] Furthermore, the gas power device includes more than two independent working units to form a multi-stage driving structure, and is arranged along the circumference of the core or the outer ring.

[0031] Furthermore, more than two driving recesses are arranged on the inner ring surface of the outer ring, and each driving recess has a contour bottom surface and a driving surface. The contour line of the contour bottom surface is a logarithmic spiral line, and its pole is arranged at the center of the core body.

[0032] A gas pressure engine comprises the gas power device, wherein the gas is compressed gas or gas with a certain pressure.

[0033] A continuously variable transmission comprises the gas power device.

[0034] The gas power device of the present invention has a simple structure, large torque, high speed, high transmission efficiency, and low energy consumption, and can be widely used in vehicles, power generation equipment, and other fields requiring power output devices. The present invention has the following beneficial effects:

[0035] 1. The core body of the present invention is provided with a multi-stage flow channel, i.e., the air inlet channel is used as the first stage flow channel, and each secondary flow channel is used as the second, third, fourth... stage flow channel. The gas acts on the driving recess of the outer ring from the first stage flow channel, the driving recess is connected to the second stage flow channel, and then returns to the second stage flow channel and acts on another driving recess of the outer ring, and so on, until the gas is discharged from the exhaust channel. The whole process is carried out in the forward direction of the outer ring rotation direction, with large torque, high transmission efficiency, high gas utilization rate, and the output torque further increases with the increase of the rotation speed.

[0036] 2. The flow channels arranged circumferentially on the core of the present invention effectively reduce the volume of the overall device and can be flexibly matched with power generation or output equipment in various fields. At the same time, the more inlet flow channels are set on the core, the lower the overall weight is, which further improves the output speed and efficiency of the device. BRIEF DESCRIPTION OF THE DRAWINGS

[0037] Figure 1 It is a schematic diagram of the first embodiment of the present invention.

[0038] Figure 2 It is a side view along axis A of the first embodiment of the present invention.

[0039] Figure 3 It is a side view along axis B of the first embodiment of the present invention.

[0040] Figure 4 It is a cross-sectional view of the first embodiment of the present invention.

[0041] Figure 5 This is another layout diagram of the first embodiment of the present invention.

[0042] Figure 6 It is a schematic diagram of the second embodiment of the present invention.

[0043] Figure 7 It is a side view along axis C of the second embodiment of the present invention.

[0044] Figure 8 It is a side view along axis D of the second embodiment of the present invention.

[0045] Fig. 9 It is a radial cross-sectional view of the second embodiment of the present invention. DETAILED DESCRIPTION

[0046] The present invention will be further described below in conjunction with the accompanying drawings:

[0047] Example 1: Please refer to Figures 1 to 4A gas power device comprises an outer ring 1, the inner ring surface of which is provided with a plurality of driving recesses 11 in the circumferential direction; a core body 3, which is coaxially arranged in the outer ring 1 and can rotate relative to the outer ring, and the outer ring surface of the core body 3 is provided with at least one nozzle 301, at least one discharge port 302, and at least one primary flow channel 300 located between the nozzle and the discharge port;

[0048] At least one air inlet passage 31 connected to at least one nozzle 301; and

[0049] at least one exhaust passage 310 connected to at least one exhaust port 302;

[0050] The gas enters from the inlet channel 31, and is ejected step by step through the nozzle 301 of the core body 3 and the secondary flow channel 300, acting on at least two driving recesses 11 on the circumference of the outer ring 1, generating thrust on these driving recesses 11 to drive the outer ring 1 to rotate and do work, thereby achieving continuous power output, and finally, the gas is discharged through the exhaust channel through the exhaust port of the core body 3. The gas power device also includes a shaft 2, and the outer ring 1 and the core body 3 are coaxially arranged on the shaft 2.

[0051] like Figure 4 As shown, the air inlet channel 31 and the exhaust channel 310 are formed in the core body 3, and the nozzle 301 and the secondary flow channel 300 on the core body 3 are connected with the driving recess 11 corresponding to the outer ring 1, wherein the secondary flow channel 300 and the corresponding driving recess 11 are arranged alternately and connected in sequence, and the secondary flow channel 300 is arranged along the circumference of the core body or the outer ring.

[0052] like Figure 4 The core 3 includes: an air inlet channel 31, which forms a nozzle 31 on the peripheral surface of the core, and its direction is an arc line extending from the middle to the outside, and the nozzle 301 is connected with the driving recess 11 corresponding to the outer ring to form a first-stage flow channel;

[0053] The secondary flushing channel 300 is an arc line extending from the edge of the core 3 inward and then bending to the edge. Each flushing channel 300 is connected with the front and rear driving recesses 11 corresponding to the outer ring 1, forming N-stage flow channels along the circumference of the core, where N is a natural number ≥ 2. It should be noted that if it is a 2-stage flow channel, it includes the 1st stage flow channel (intake channel) and the 2nd stage flow channel (primary flushing channel); if it is a 3-stage flow channel, it includes the 1st stage flow channel (intake channel), the 2nd stage flow channel (primary flushing channel), the 3rd stage flow channel (another secondary flushing channel), ...

[0054] Each step of the flow channel cooperates with the corresponding driving recess of the outer ring to form a multi-step stroke structure with decreasing gas energy.

[0055] The gas power device can be designed according to the load requirements, in which the core 3 can be set to a 2-stage flow channel, a 3-stage flow channel, or more stages of intake flow channels. Each stage cycle performs work, fully utilizes energy, and maximizes the use efficiency to meet the output torque and speed requirements.

[0056] like Figure 5 Schematic diagram of a 4-stage flow channel. After the compressed gas enters from the 1st-stage flow channel 311, it passes through the 2nd, 3rd, and 4th-stage flow channels 312, 313, and 314, and is ejected to act on the corresponding driving recess 11, and finally is output through the exhaust flow channel 310; Figure 4 This is a schematic diagram of the 5-stage intake air duct. The working process is the same as Figure 5 The schematic is similar. Figure 5 The secondary flow channel 300 includes a return channel and a connected stroke channel, such as Figure 5 The return path 3131 and the connected stroke path 3132 in the third-stage flow channel, the return path 3131 is connected to the driving recess corresponding to the outer ring, and the stroke path 3132 is connected to another driving recess.

[0057] See also Figure 1 The gas power device also includes a shaft 2, and the outer ring 1 is coaxially arranged on the shaft 2 with the core 3. The shaft 2 is provided with inlet and outlet shaft channels 21 and 210, which are respectively connected to the inlet channel 31 and the exhaust channel 310 of the core 3. The inlet and outlet shaft channels in the shaft form an inlet (inlet port) and an outlet (outlet port), and the inlet and outlet shaft channels are non-connected structures. The outer ring 1 is matched with the shaft 2 through the side plates 41 and 42 to form a closed space, and the core 3 is arranged in the closed space and connected and fixed to the shaft 2. In the present invention, the core 3 is provided with at least two steps of flow channels, each step of the flow channel is connected to the driving recess corresponding to the outer ring, and finally the gas is discharged from the exhaust channel.

[0058] See also Figure 1 In the present invention, the core body 3 can be formed by the cooperation of a left core body and a right core body, and the cooperation surfaces of the left core body and the right core body are provided with an air intake channel 31 and an exhaust channel 310. The core body 3 can also be integrally cast.

[0059] See also Figure 1 , Figure 4 , this embodiment is a primary drive structure, a gas channel is arranged circumferentially on the core 3 to form a primary drive structure, the gas channel is also called an independent working unit, an air inlet channel 31, a nozzle 301, at least two driving recesses 11, at least one primary flow channel 300, a discharge port 302 and an exhaust channel 310 on the core 3 and the outer ring 1 form an independent working unit, and the gas power device includes at least one independent working unit. The air inlet channel 31, the nozzle 301, the driving recess 11, the secondary flow channel 300, the discharge port 302 and the exhaust channel 310 in the independent working unit constitute a gas flow path.

[0060] See also Figure 1 , Figure 4 or Figure 5 In the present invention, more than two driving recesses 11 are arranged on the inner ring surface of the outer ring 1, each driving recess has a contour bottom surface 111 and a driving surface 112, the contour line of the contour bottom surface 111 can be a common arc line or a spiral line, when the contour line of the contour bottom surface is a logarithmic spiral line, its pole is set on the axis, each driving recess 11 is also connected with the adjacent step flow channel so that the gas entering the previous step flow channel is discharged from the next step flow channel.

[0061] In the present invention, the direction of the air inlet channel of the core body 3, namely the first-stage flow channel, can be a common arc line or a spiral line, and the direction of each secondary flow channel, namely the stroke channel in the Nth-stage flow channel, can also be a common arc line or a spiral line.

[0062] like Figure 4 and Figure 5 The core body 3 of the present invention is provided with an air inlet channel 31, which runs in a logarithmic spiral extending from the middle to the outside. The stroke channel of the secondary flow channel 300 runs in a logarithmic spiral, and the logarithmic spiral of the stroke channel of the secondary flow channel runs in a direction substantially the same as the logarithmic spiral of the air inlet channel. The air inlet channel of the core body 3 runs in a logarithmic spiral extending from the middle to the outside, and the pole of the logarithmic spiral is set on the central axis of the core body. The logarithmic spiral runs in an angle of 15°-45°. The smaller the angle, the longer the flow channel and the more the loss. The larger the angle, the smaller the tangential component of the driving outer ring.

[0063] See also Figure 1 , Figure 2 and Figure 3 In the present invention, the inlet and outlet shaft channels 21, 210 in the shaft 2 form an inlet and an outlet, and the inlet and outlet shaft channels are non-connected structures. The inlet and outlet of the shaft can be set at one end or both ends of the shaft, the inlet shaft channel 21 is connected to the inlet channel 31 of the core body, and the shaft outlet extends axially to form the outlet shaft channel 210, which is connected to the exhaust channel 310 of the core body.

[0064] The gas power device involved in this application refers to a device that can convert gas energy into mechanical rotation, wherein the device may include other components in addition to the necessary outer ring, core body and its corresponding recessed structure or flow channel structure design; for example, it may include a housing and a sealing structure that provide external protection, or a coupling that provides torque transmission. The outer ring may have different specific forms according to different mechanical rotation output modes, such as an outer toothed structure formed on the outer side of the outer ring to facilitate the output of kinetic energy through gear transmission; another example is that the outer ring has a belt groove to output kinetic energy through belt transmission; another example is that the outer ring has a mounting flange to facilitate the installation of a coupling to output kinetic energy; and so on. The core body and the outer ring are made of hard materials, not limited to metals, metal alloys, plastics, and composite materials. The processing methods of the recessed structure or flow channel structure of the core body and the outer ring can be realized by all known production means, including but not limited to die casting, forging, extrusion, 3D printing, and so on. The gas pressure input to the power device may be generated by a compressor (such as an air pressure pump), a container of compressed fluid (such as a high-pressure gas cylinder), or the like.

[0065] Figure 1 and Figure 4 It should be noted that the air inlet channel 31 and the exhaust channel 310 of the core body and the air inlet shaft channel 21 and the air outlet shaft channel 210 do not correspond to each other according to the drawing rules, but for the sake of illustration, Figure 1 The air inlet channel and the exhaust channel of the core body refer to the air inlet channel and the exhaust channel. Figure 6 and Fig. 9 A similar schematic diagram is shown here.

[0066] Example 2: Please refer to Figures 6 to 9The gas power device includes two independent working units to form a two-stage driving structure, that is, two gas channels are arranged circumferentially on the core 3, each gas channel includes an intake channel 31 of more than one order and a secondary flow channel 300 and an exhaust channel 310 arranged circumferentially along the core 3. The gas power device comprises an outer ring 1, whose inner ring surface is provided with a plurality of driving recesses 11 on the circumference; a core body 3, which is coaxially arranged in the outer ring 1 and can rotate relative to the outer ring, and the outer ring surface of the core body is provided with two groups of nozzles and exhaust ports, and at least one primary flow channel is provided between each group of nozzles and exhaust ports; the core body is provided with two air inlet channels 31, 32, which correspond to the connected nozzles; and two exhaust channels 310, 320, which correspond to the connected exhaust ports; two streams of gas enter from the two air inlet channels of the core body respectively, and are ejected step by step through the nozzles of the core body 3 and the secondary flow channel 300, acting on the corresponding driving recesses 11 on the circumference of the outer ring, generating thrust on these driving recesses to drive the outer ring 1 to rotate and do work, realizing power output, and finally, the gas is discharged through the exhaust port of the core body through the exhaust channel. The above-mentioned one air inlet channel, one nozzle, a corresponding number of driving recesses and corresponding secondary flow channels, exhaust ports and one exhaust channel form an independent work unit.

[0067] The gas power device also includes a shaft 2, and the outer ring 1 is coaxially arranged on the shaft with the core 3. The shaft 2 is provided with air inlet shafts 21, 22 and air outlet shafts 210, 220 which are respectively connected to the air inlet channels 31, 32 and the air exhaust channels 310, 320 of the core. The shaft 2 is provided with two air inlets and two air outlets corresponding to the gas channels; the compressed gas enters from the two air inlets of the shaft 2, is ejected through the air inlet channel of the core 3, and acts on the driving recess 11 of the outer ring 1, generating thrust to drive the outer ring 1 to rotate and do work, and finally the compressed gas returns to the corresponding air outlet through the exhaust channel of the core 3, realizing the continuous output of power. The other structures are the same as those in Example 1 and will not be repeated.

[0068] Embodiment 3: The gas power device of the present invention includes 4 or more independent working units to form a multi-stage driving structure. Three or more gas channels are arranged circumferentially on the core body. Each gas channel includes more than one intake channel and secondary flow channel and exhaust channel arranged circumferentially along the core body. The intake channel and exhaust channel are arranged on the mating surfaces of the left and right core bodies. The shaft is provided with intake channels and exhaust channels corresponding to the number of gas channels. The compressed gas enters from the intake channel of the shaft, is ejected through the intake channel of the core body, and acts on the driving recess of the outer ring, pushing the outer ring to rotate and do work, realizing continuous power output. Finally, the compressed gas returns to the corresponding exhaust channel through the exhaust channels of the core body. The other structures are the same as those in Embodiment 1.

[0069] Embodiment 4:

[0070] Gas powered device prototype:

[0071] (I) Second-stage gas power device

[0072] 1. The main parameters are as follows:

[0073] (1) Gas pressure: 1.2MPa;

[0074] (2) Maximum speed: 8550r / min;

[0075] (3) Number of driving structure levels: 3;

[0076] (4) Inlet flow channel diameter: Φ5mm;

[0077] (5) Single-stage drive intake order: 2;

[0078] (6) Outer ring diameter: Φ140mm;

[0079] (7) Outer ring weight: 2.5KG

[0080] 2. Output torque

[0081]

[0082] (II) Fifth-order gas power device

[0083] 1. The main parameters are as follows:

[0084] (1) Gas pressure: 1.2MPa;

[0085] (2) Maximum speed: 17967r / min;

[0086] (3) Number of driving structure levels: 3;

[0087] (4) Inlet flow channel diameter: Φ5mm;

[0088] (5) Single-stage drive intake order: 5;

[0089] (6) Outer ring diameter: Φ140mm;

[0090] (7) Outer ring weight: 2.5KG

[0091] 2. Output torque

[0092]

[0093] It can be seen from the test that under the same conditions, increasing the number of driving intake stages can significantly increase the output torque and improve the acceleration performance. At the same time, it is also beneficial to increase the speed.

[0094] The above records are only embodiments of the present invention. Any modification or change made by a person familiar with the present technology using the present invention shall fall within the patent scope claimed by the present invention and shall not be limited to those disclosed in the embodiments.

Claims

1. A gas powered device, characterized in that: include: An outer ring, whose inner ring surface is provided with a plurality of driving recesses in the circumferential direction; A core body is coaxially arranged in the outer ring and can rotate relative to the outer ring, and the outer ring surface of the core body is provided with at least one nozzle, at least one discharge port, and at least one flushing channel located between the nozzle and the discharge port; at least one air inlet passage connected to at least one nozzle; and at least one exhaust passage connected to at least one exhaust port; At least one inlet channel, at least one nozzle, at least two driving recesses, at least one primary flushing channel, at least one discharge port and at least one exhaust channel form an independent working unit, and the gas power device includes at least one independent working unit; The air inlet channel is formed in the core body, and the air inlet channel forms a nozzle on the peripheral surface of the core body, and its direction is an arc line extending from the middle to the outside. The nozzle is connected with the driving concave part corresponding to the outer ring to form a first-stage flow channel; The gas enters from the air inlet channel, is ejected step by step through the nozzle of the core body and the secondary flow channel, and acts on at least two driving recesses on the circumference of the outer ring, generating thrust for these driving recesses to drive the outer ring to rotate and do work, thereby realizing power output. Finally, the gas is discharged through the exhaust channel through the exhaust port of the core body.

2. The gas powered device according to claim 1, characterized in that: The nozzle and the secondary flow channel on the core body are connected with the driving recess corresponding to the outer ring, and the secondary flow channel is arranged along the circumference of the core body or the outer ring.

3. The gas powered device according to claim 1, characterized in that: An exhaust passage is formed in the core.

4. The gas powered device according to claim 3, characterized in that: The core includes The secondary flow channel is an arc line extending from the edge of the core body inward and then bending to the edge. Each secondary flow channel is connected with the front and rear driving recesses corresponding to the outer ring, forming N-step flow channels along the circumference of the core body, where N is a natural number ≥ 2; Each step of the flow channel cooperates with the corresponding driving recess of the outer ring to form a multi-step stroke structure with decreasing gas energy.

5. The gas powered device according to claim 1, characterized in that: The secondary flow channel includes a return channel and a communicating stroke channel. The return channel is communicated with a driving recess corresponding to the outer ring, and the stroke channel is communicated with another driving recess.

6. The gas powered device according to claim 3, characterized in that: The direction of the core air inlet channel is a logarithmic spiral extending from the middle to the outside, the pole of the logarithmic spiral is set on the central axis of the core, and the direction angle of the logarithmic spiral is 15°-45°.

7. The gas powered device according to claim 5, characterized in that: An air inlet channel is arranged on the core body, and its direction is a logarithmic spiral extending from the middle to the outside, and the direction of the stroke channel of the secondary flow channel is a logarithmic spiral, and the direction of the logarithmic spiral of the stroke channel of the secondary flow channel is the same as the direction of the logarithmic spiral of the air inlet channel.

8. The gas powered device according to claim 1, characterized in that: The gas power device also includes a shaft, and the outer ring and the core body are coaxially arranged on the shaft.

9. The gas powered device according to claim 3, characterized in that: The gas power device also includes a shaft, on which the outer ring is coaxially arranged with the core body, and on which an inlet and an outlet shaft passage are opened, which are respectively connected to an inlet passage and an outlet passage of the core body.

10. The gas powered device according to claim 9, characterized in that: The air inlet and outlet shaft passages in the shaft form an air inlet and an air outlet, and the air inlet and outlet shaft passages are non-connected structures.

11. The gas powered device according to claim 8, characterized in that: The outer ring is matched with the shaft through the side plates to form a closed space, and the core body is arranged in the closed space and is connected and fixed to the shaft.

12. The gas powered device according to claim 1, characterized in that: The air inlet channel, the nozzle, the driving recess, the secondary flow channel, the exhaust port and the exhaust channel in the independent working unit constitute a gas flow path.

13. The gas powered device according to claim 1, characterized in that: The gas power device comprises more than two independent working units to form a multi-stage driving structure, and the units are arranged along the circumference of the core or the outer ring.

14. The gas powered device according to claim 1, characterized in that: More than two driving recesses are arranged on the inner ring surface of the outer ring, each driving recess has a contour bottom surface and a driving surface, the contour line of the contour bottom surface is a logarithmic spiral line, and its pole is arranged at the center of the core body.

15. A pneumatic engine, characterized in that: A gas powered device comprising any one of claims 1 to 14, wherein the gas is compressed gas or gas with a certain pressure.

16. A continuously variable transmission, characterized in that: A gas powered device comprising any one of claims 1-14.

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