CN113374573A

CN113374573A - Circumferential flow turbine

Info

Publication number: CN113374573A
Application number: CN202110758882.8A
Authority: CN
Inventors: 黄涵
Original assignee: Individual
Current assignee: Individual
Priority date: 2021-07-05
Filing date: 2021-07-05
Publication date: 2021-09-10
Anticipated expiration: 2041-07-05
Also published as: CN113374573B

Abstract

The present application relates to a circumferential flow turbine. The working device of the circumferential flow type turbine comprises a second stator and a second rotor, wherein an ignition device, an air supply port, a fuel inlet and an air exhaust port are arranged on the second stator, a second main shaft of the second rotor is rotatably and coaxially arranged in the second stator, a second roller is eccentrically arranged in the second stator, the second main shaft is movably arranged in a second roller, a second fixed blade is fixedly arranged on the second main shaft, a plurality of second swinging blades are rotatably arranged on the second main shaft, the main planes of the second fixed blade and the plurality of second swinging blades are parallel to the main shaft, and the second fixed blade and the plurality of second swinging blades can divide an area formed by the second roller and the second stator into a plurality of second spaces of which the volumes are periodically and continuously changed along with the rotation of the second roller. The heat energy waste problem of the internal combustion engine can be improved, and the heat conversion efficiency is improved.

Description

Circumferential flow turbine

Technical Field

The application belongs to the technical field of internal combustion engines, and particularly relates to a circumferential flow type turbine.

Background

The internal combustion engine is a main mode for converting chemical energy into mechanical energy in the existing mechanical structure, and the existing internal combustion engine mainly comprises a reciprocating piston internal combustion engine, an eccentric rotor internal combustion engine, an axial flow type gas turbine internal combustion engine and the like. The principle of the internal combustion engine is that the air sucked into the volume is compressed, the mixed chemical fuel becomes a high-pressure working medium, the mixed gas is ignited to expand to do work, and the waste gas is discharged. The internal combustion engine is designed to optimize and control the above procedures under the prior art conditions so as to meet the application requirements and environmental protection requirements. The existing internal combustion engine has the technical problems of heat energy waste and low heat conversion efficiency, and also has larger improvement space.

Disclosure of Invention

In order to solve the technical problems, the invention provides a circumferential flow type turbine to solve the technical problems of heat energy waste and low heat conversion efficiency of the conventional internal combustion engine.

The technical scheme of the invention is as follows:

a circumferential flow turbine, characterized in that it comprises:

the working device comprises a second stator and a second rotor, an ignition device, an air supply port, a fuel inlet and an air exhaust port are arranged on the second stator, the second rotor comprises a second main shaft, a second fixed blade, a second swinging blade and a second roller, the second main shaft is rotatably and coaxially arranged in the second stator, the second roller is eccentrically arranged in the second stator, the second main shaft is movably arranged in the second roller, the second fixed blade is fixedly arranged on the second main shaft, a plurality of second swinging blades are rotatably arranged on the second main shaft, the main planes of the second fixed blade and the second swinging blades are parallel to the second main shaft, and the second fixed blade and the second swinging blades movably and hermetically penetrate through the circumferential surface of the second roller, and the second fixed blade and the plurality of second swinging blades can divide an area enclosed by the second roller and the second stator into a plurality of second spaces of which the volumes are periodically and continuously changed along with the rotation of the second roller.

In some embodiments, a side of the second stationary blade is provided with a third mounting ring fixedly disposed on the second main shaft;

and a fourth mounting ring is arranged on one side of each second swinging blade and movably sleeved on the second main shaft.

In some embodiments, a plurality of second through holes are formed at intervals on the circumferential surface of the second drum, a second hinge is disposed in each second through hole, and a gap through which the second fixed blade or the second swing blade passes is disposed in each second hinge.

In some embodiments, each of the second hinges comprises:

two second hinge shafts rotatably connected in both axial ends of the second drum, respectively;

the arc surfaces of the two second cylindrical bodies are respectively and rotatably arranged on two opposite side walls of the corresponding second through hole, two axial ends of the two second cylindrical bodies are respectively and rotatably connected in the two second hinge shafts, the planes of the two second cylindrical bodies are opposite to each other, a gap for the second fixed blade or the second swinging blade to pass through is formed, and a second mounting groove axially arranged along the opposite surface of the two second cylindrical bodies is formed;

the second roller pins are arranged corresponding to the second cylindrical bodies, the second roller pins can be rotatably arranged in the corresponding second mounting grooves of the second cylindrical bodies, and two axial ends of the second roller pins are respectively and rotatably connected to the two second hinge shafts.

In some embodiments, two opposing sidewalls of the second through-hole are provided with second slots;

a second hinge sealing sheet is arranged between the outer side of the second cylindrical body and the side wall of the second through hole, a second inserting plate is arranged on the outer side of the second hinge sealing sheet, the second inserting plate is embedded in the second slot at the same side, and a second elastic piece is arranged between the second inserting plate and the bottom of the second slot.

In some embodiments, the ignition device, the air supply port, and the fuel inlet port are disposed on a first side of a circumferential surface of the second stator at a minimum distance from the second drum; the exhaust port is provided on a second side surface of the circumferential surface of the second stator, the second side surface being disposed opposite to the first side surface.

As a preferable aspect of the present application, the circumferential flow type turbine further includes:

the air compressing device comprises a first stator and a first rotor, an air inlet and an air outlet are arranged on the first stator, the air outlet of the first stator is communicated with the air supply port of the second stator, the first rotor comprises a first main shaft, a first fixed blade, a first swing blade and a first roller, the first main shaft is rotatably and coaxially arranged in the first stator, the first roller is eccentrically arranged in the first stator, the first main shaft is movably arranged in the first roller, the first fixed blade is fixedly arranged on the first main shaft, a plurality of first swing blades are rotatably arranged on the first main shaft, the main planes of the first fixed blade and the plurality of first swing blades are all parallel to the first main shaft, the first fixed blade and the plurality of first swing blades are movably sealed and penetrate through the periphery of the first roller, the first fixed blade and the plurality of first swinging blades can divide an area enclosed by the first roller and the first stator into a plurality of first spaces with the volumes changing periodically and continuously along with the rotation of the first roller.

In some embodiments, a first mounting ring is disposed on one side of the first stationary blade, the first mounting ring being fixedly disposed on the first main shaft;

and each first swing blade is provided with a second mounting ring on one side, and the second mounting ring is movably sleeved on the first main shaft.

In some embodiments, the air inlet is disposed on a circumferential surface of the first stator, and one or more pressure regulating sliders are disposed on the air inlet and are operable to move on the air inlet in a circumferential direction of the first stator.

In some embodiments, a plurality of first through holes are formed at intervals on the circumferential surface of the first drum, a first hinge is arranged in each first through hole, and a gap through which the first fixed blade or the first swing blade passes is arranged in each first hinge.

As a preferable aspect of the present application, each of the first hinges includes:

two first hinge shafts rotatably connected in both axial ends of the first drum, respectively;

the arc surfaces of the two first columnar bodies are respectively and rotatably arranged on two opposite side walls of the corresponding first through hole, two axial ends of the two first columnar bodies are respectively and rotatably connected into the two first hinge shafts, the planes of the two first columnar bodies are opposite to each other, a gap for the first fixed blade or the first swinging blade to pass through is formed, and the opposite surfaces of the two first columnar bodies are provided with first mounting grooves arranged along the axial direction of the first columnar bodies;

the first roller pin and the first columnar body are correspondingly arranged, the first roller pin can be rotatably arranged in the corresponding first mounting groove of the first columnar body, and two axial ends of the first roller pin are respectively and rotatably connected in the two first hinge shafts.

In some embodiments, two opposing sidewalls of the first through-hole are provided with a first slot;

a first hinge sealing sheet is further arranged between the arc-shaped surface of each first cylindrical body and the corresponding side wall of the first through hole, and the first cylindrical bodies are rotatably arranged on the inner sides of the first hinge sealing sheets;

the outer side of the first hinge sealing piece is provided with a first plug board, the first plug board is embedded in the first slot at the same side, and a first elastic piece is arranged between the first plug board and the bottom of the first slot.

In some embodiments, the first stator and the second stator are fixedly connected coaxially, and the first spindle and the second spindle are fixedly connected coaxially.

The beneficial effects of the invention at least comprise:

the invention provides a circumfluence turbine which comprises an acting device, wherein the acting device comprises a second stator and a second rotor, the second stator is provided with a gas supply port, a fuel inlet, a gas exhaust port and an ignition device, high-pressure gas can be conveyed into the second stator through the gas supply port of the second stator, a combustion medium required by acting is conveyed into the second stator through the fuel inlet of the fuel inlet, and the high-pressure gas and the combustion medium form a working medium after being input into the second stator, and the working medium can be ignited and expanded by the ignition device.

Because the second main shaft is rotatably and coaxially arranged in the second stator, the second roller is eccentrically arranged in the second stator, and the second main shaft is movably arranged in the second roller, a crescent working space can be enclosed between the second roller and the second stator.

Because the second fixed blade is fixedly arranged on the second main shaft, the plurality of second swinging blades are rotatably arranged on the second main shaft, the main planes of the second fixed blade and the plurality of second swinging blades are parallel to the second main shaft, and the second fixed blade and the plurality of second swinging blades hermetically penetrate through the peripheral surface of the second roller and lean against the inner side wall of the second stator. Therefore, the crescent second space can be divided into a plurality of second spaces with the volumes periodically and continuously changed along with the rotation of the second roller by the first fixed blades and the first swinging blades, high-pressure gas and medium injected into a certain second space are ignited by the ignition device to generate expanded hot gas, the second fixed blades and the second swinging blades are pushed by the expanded hot gas to drive the second main shaft and the second roller to rotate, the working space is changed from small to large, when the working space is changed to the maximum, the working space is communicated with the exhaust port on the second stator, and waste gas after working is exhausted from the exhaust port on the second stator.

The medium and the high-pressure gas are continuously injected into a certain working space, so that the second rotor can be continuously driven to rotate, and the aim of continuously outputting power is fulfilled.

According to the circumferential flow type turbine, the acting device only achieves power output through the second fixed blade, the second swing blade, the second roller and the second main shaft in a circumferential motion mode, corresponding conversion of other motions is not needed in the whole process, the problem that heat energy is wasted in an internal combustion engine can be improved, heat conversion efficiency is improved, and the circumferential flow type turbine has good practical value.

Drawings

In order to more clearly illustrate the technical solutions in the embodiments of the present invention, the drawings needed to be used in the description of the embodiments will be briefly introduced below, and it is obvious that the drawings in the following description are only some embodiments of the present invention, and it is obvious for those skilled in the art to obtain other drawings based on these drawings without creative efforts.

FIG. 1 is a schematic structural diagram of a circumferential flow turbine according to the present embodiment;

FIG. 2 is an exploded view of FIG. 1;

fig. 3 is a schematic structural diagram of the air compressing device of the present embodiment;

FIG. 4 is a schematic structural diagram of the first cover plate in FIG. 3;

fig. 5 is an exploded view of the first drum of the present embodiment;

FIG. 6 is a schematic top view of the first roller in this embodiment;

FIG. 7 is a schematic structural view of a first stationary blade;

FIG. 8 is an exploded view of the first hinge of the present embodiment;

fig. 9 is a schematic structural diagram of the working device according to the present embodiment;

FIG. 10 is a schematic structural view of the fifth cover plate in FIG. 9;

fig. 11 is an exploded view of the second drum of the present embodiment;

FIG. 12 is a schematic top view of the second roller in this embodiment;

FIG. 13 is a schematic structural view of a second stationary blade;

fig. 14 is an exploded view of the first hinge of the present embodiment.

In the drawings:

a-a compressor, 1-a first stator, 101-a first cover plate, 102-a second cover plate, 103-a third cover plate, 104-a fourth cover plate, 105-a first stator wall casing, 106-a first positioning groove, 107-a second positioning groove, 201-a first main shaft, 202-a first fixed blade, 203-a first swinging blade, 204-a first roller, 205-a first mounting ring, 206-a first key, 207-a second mounting ring, 208-a first through hole, 209-a first hinge sealing sheet, 210-a first hinge shaft, 211-a first cylindrical body, 212-a first roller pin, 213-a first plug board, 214-a first elastic member, 215-a first roller sealing member, 216-a first tension sealing ring, 217-a first roller end cover, 218-first bearing, 2-first rotor, 3-air inlet, 4-air inlet, 5-first heat dissipation hole, 6-slider, b-power-applying device, 7-second stator, 701-fifth cover plate, 702-sixth cover plate, 703-seventh cover plate, 704-eighth cover plate, 705-second stator wall casing, 706-third positioning groove, 707-fourth positioning groove, 8-second rotor, 801-second spindle, 802-second fixed blade, 803-second swinging blade, 804-second roller, 805-third mounting ring, 806-second key, 807-fourth mounting ring, 808-second through hole, 809-second hinge sealing sheet, 810-second hinge shaft, 811-second cylindrical body, 812-second needle roller, 813-second plugboard, 814-second elastic element, 815-second roller sealing element, 816-second tension sealing ring, 817-second roller end cover, 818-second bearing, 9-ignition device, 10-air supply port, 11-fuel inlet port, 12-air exhaust port, 13-second heat dissipation hole, and 14-connecting pipe.

Detailed Description

In order to make the present application more clearly understood by those skilled in the art to which the present application pertains, the following detailed description of the present application is made with reference to the accompanying drawings by way of specific embodiments.

The embodiment provides a circumferential flow type turbine, which aims to solve the technical problems that the existing internal combustion engine wastes heat energy and is low in heat conversion efficiency.

Fig. 1 is a schematic structural view of a circumferential flow turbine according to the present embodiment, and fig. 2 is an exploded schematic view of fig. 1. With reference to fig. 1 and fig. 2, the circumferential flow turbine provided in this embodiment mainly includes a compressor a and a working device b, where the compressor a is used to provide high-pressure gas required for combustion to the working device b, and the working device b ignites the high-pressure gas and combustion medium delivered into the working device b to perform work.

First, the present embodiment first describes the air compressing device.

Fig. 3 is a schematic structural diagram of the air compressing device of the present embodiment. Referring to fig. 1 to 3, an air compressing device a of this embodiment includes a first stator 1 and a first rotor 2, an air inlet 3 and an air supply port 4 are disposed on a circumferential surface of the first stator 1, the first rotor 2 includes a first main shaft 201, a first fixed blade 202, a first swing blade 203 and a first roller 204, the first main shaft 201 is rotatably disposed coaxially in the first stator 1, the first roller 204 is eccentrically disposed in the first stator 1, the first main shaft 201 is movably disposed in the first roller 204, the first fixed blade 202 is fixedly disposed on the first main shaft 201, the plurality of first swing blades 203 are rotatably disposed on the first main shaft 201, main planes of the first fixed blade 202 and the plurality of first swing blades 203 are parallel to the first main shaft 201, the first fixed blade 202 and the plurality of first swing blades 203 are movably sealed through the circumferential surface of the first roller 204, and is abutted against the inner side wall of the first stator 1, and the first fixed blade 202 and the plurality of first swing blades 203 can divide the area enclosed by the first roller 204 and the first stator 1 into a plurality of first spaces of which the volumes are periodically and continuously changed along with the rotation of the first roller 204.

Because the air compressing device of this embodiment includes first stator 1 and first rotor 2, is provided with air inlet 3 and gives gas port 4 on the global of first stator 1, consequently, accessible air inlet 3 injects gas into first stator 1 is inside, forms high-pressure gas after the gas compression processing in first stator 1, and the high-pressure gas who forms is drawn forth to acting device through giving gas port 4.

Since the first spindle 201 of the first rotor 2 is rotatably and coaxially arranged in the first stator 1, the first roller 204 is eccentrically arranged in the first stator, and the first spindle 201 is movably arranged in the first roller 204, a crescent-shaped first space can be defined between the first roller 204 and the first stator 1.

Since the first fixed blade 202 is fixedly provided on the first main shaft 201, the plurality of first swing blades 203 are rotatably provided on the first main shaft 201, the major planes of the first fixed blade 202 and the plurality of first swing blades 203 are parallel to the first main shaft 201, the first fixed blade 202 and the plurality of first swing blades 203 are movably sealed through the circumferential surface of the first drum 204, and abuts against the inner side wall of the first stator 1, so that when the first main shaft 201 is controlled to rotate, the first main shaft 201 drives the first fixed blade 201 to rotate, the first fixed blade 201 drives the first roller 204 to rotate, and further drives the plurality of first swinging blades 203 to rotate, that is, the first fixed blade 202 and the plurality of first swing blades 203 are rotated with the first main shaft 201, the crescent-shaped first space may be divided into first spaces whose size and volume are continuously changed periodically with the rotation of the first roller 204.

In implementation, gas enters a certain first space from the gas inlet 3 of the first stator 1, the volume of the first space where the gas is sucked is reduced from large to small along with the rotation of the first main shaft 201, the gas sucked into the first space is compressed to form high-pressure gas, and when the compressed gas space is communicated with the gas outlet 4 of the first stator 1, the high-pressure gas is discharged from the gas outlet.

With the continuous rotation of the first main shaft 201, the gas continuously enters the first stator 1 from the gas inlet 3 of the first stator 1, and the high-pressure gas compressed in the first stator 1 is continuously discharged from the gas outlet of the first stator 1.

Referring to fig. 2, in the present embodiment, the first stator 1 includes a first cover plate 101, a second cover plate 102, a third cover plate 103, a fourth cover plate 104 and a first stator wall housing 105, wherein the first cover plate 101 and the third cover plate 103 are disposed opposite to each other, the circumferential surfaces of the first cover plate 101 and the third cover plate 103 are connected through the first stator wall housing 105, the second cover plate 102 is disposed inside the first cover plate 101, the first cover plate 102 is provided with a first positioning groove 106 (see fig. 4) matching the circumferential surface of one axial end of the first roller 204, one axial end of the first roller 204 movably passes through the second cover plate 102 and is rotatably disposed in the first positioning groove 106, similarly, the fourth cover plate 104 is disposed inside the third cover plate 103, the third cover plate 104 is provided with a second positioning groove 107 matching the circumferential surface of the other axial end of the second roller 204, the other axial end of the first roller 204 movably passes through the fourth cover plate 104, is rotatably disposed in the second positioning recess 107.

In this embodiment, the first cover plate 101 and the second cover plate 102 may be integrally formed, the third cover plate 103 and the fourth cover plate 104 may also be integrally formed, and the first cover plate 101 and the third cover plate 103 and the first stator wall housing 105 may be detachably and hermetically connected to facilitate the assembly of the first rotor 2 in the first stator 1.

In this embodiment, two ends of the first spindle 201 can respectively movably penetrate through two cover plates at the same end, so as to realize the rotatable arrangement of the first spindle 201 in the first stator 1.

Fig. 5 is an exploded schematic view of the first drum of this embodiment, fig. 6 is a schematic top view of the first drum of this embodiment, fig. 7 is a schematic structural view of the first fixed blade, and in combination with fig. 5-7, in this embodiment, a first mounting ring 205 is disposed on one side of the first fixed blade 202, and the first mounting ring 205 is fixedly disposed on the first spindle 201, that is, the first fixed blade 202 can rotate synchronously with the first spindle 201.

Referring to fig. 6 and 7, for the present embodiment, the first mounting ring 205 may be fixedly connected to the first spindle 201 by the first key 206, but the first mounting ring 205 may also be welded or integrally connected to the first spindle 201, which is not limited in the present embodiment.

Referring to fig. 6, in the present embodiment, a second mounting ring 207 is disposed on one side of each first swing blade 203, and the second mounting ring 207 is movably sleeved on the first main shaft 201, that is, the second mounting ring 207 is rotatably disposed on the first main shaft 201.

Further, in this embodiment, at least one second mounting ring 207 is disposed between both axial ends of the first mounting ring 205 and both axial ends of the first stator 1, so that the second mounting ring 207 is assembled on the first main shaft 201 by the limit of the first mounting ring 205 and the end of the first stator 1.

Referring to fig. 5, in the present embodiment, a plurality of first through holes 208 are formed at intervals on the circumferential surface of the first roller 204, a first hinge is disposed in each first through hole 208, a gap through which the first fixed blade 202 or the first swing blade 203 passes is disposed in the first hinge, and the first fixed blade 202 and the first swing blade 203 can swing in the corresponding first through hole 208. The first fixed blade 202 penetrates through one first hinge in a movable sealing mode, and the first swing blade 203 penetrates through the rest first hinges corresponding to the movable sealing mode, so that the inner side and the outer side of the first roller 204 can be kept sealed, and the conversion efficiency of gas treatment is improved.

Fig. 8 is an exploded view of the first hinge of the present embodiment. Referring to fig. 5 and 8, in this embodiment, each first hinge includes two first hinge shafts 210, two first cylindrical bodies 211 and first roller pins 212, wherein the two first hinge shafts 210 are rotatably connected to two axial ends of the first roller 204, the arc-shaped surfaces of the two first cylindrical bodies 211 are rotatably disposed on two opposite sidewalls of the corresponding first through hole 208, two axial ends of the two first cylindrical bodies 211 are rotatably connected to the two first hinge shafts 210, the planes of the two first cylindrical bodies 211 are opposite to each other, a gap is formed for the first fixed blade 202 or the first swing blade 203 to pass through, the opposite surfaces of the two first cylindrical bodies 211 are provided with first mounting grooves disposed along the axial direction thereof, the first roller pins 212 and the first cylindrical bodies 211 are correspondingly disposed, the first roller pins 212 are rotatably disposed in the first mounting grooves of the corresponding first cylindrical bodies 211, both axial ends of the first needle roller 212 are rotatably coupled in the two second hinge shafts 210, respectively. When the first fixed blade 202 or the first swing blade 203 swings between the two first columns 211, the first roller 212 may have rolling friction with the corresponding blade to improve the lifespan of the first hinge and the corresponding blade.

Further, with reference to fig. 5 and 8, in this embodiment, two opposite side walls of each first through hole 208 are provided with first insertion slots, a first hinge sealing piece 209 is further disposed between an arc-shaped surface of each first column 211 and the corresponding side wall of the first through hole 208, the first column 211 is rotatably disposed inside the first hinge sealing piece 209, a first insertion plate 213 is disposed outside the first hinge sealing piece 209, the first insertion plate 213 is embedded in the first insertion slot on the same side, and a first elastic element 214 is disposed between the first insertion plate 213 and the bottom of the first insertion slot. The first elastic member 214 can press the first insertion plate 213 and the first cylindrical body 211 against the corresponding blades to achieve a sealing effect.

In order to improve the sealing effect, in this embodiment, the first inserting plate 213 may be integrally formed with the first hinge sealing piece 209, and the first hinge sealing piece 209 is integrally formed in an arc shape, so as to realize the rotation of the first column 211 inside the first hinge sealing piece 209.

For this embodiment, the first elastic member 214 of this embodiment may have an arc shape, two ends of the first elastic member 214 are against two axial ends of the first socket plate 213, and a middle portion of the first elastic member 214 is against a middle position of the bottom of the first socket, so that the first elastic member 214 has sufficient supporting force to improve the sealing effect.

The first elastic member 214 of the present embodiment may also have other shapes, such as a strip shape, and the first cylindrical body 211 may have a semicircular shape, and in some embodiments, it may also have a full circle, or other angles, which is not limited in this embodiment.

Referring to fig. 5, in the present embodiment, the first drum 204 is provided with a stepped first seam allowance at both axial ends, a first drum seal 215 is disposed in the first seam allowance, and a first tension sealing ring 216 is disposed outside the first drum seal 215. First drum end covers 217 are arranged at two axial ends of the first drum 204, the first drum sealing element 215 and the first tension sealing ring 216 are arranged in the first drum end cover 217 at the same side, and the first drum end cover 217 is rotatably arranged in the first positioning groove 106 or the second positioning groove 107, so that the sealing performance of the first drum 204 and the first drum end cover 217 can be improved. Preferably, in this embodiment, the first drum seal 215 has two steps, and the two steps of the first drum seal 215 are respectively sleeved with a first tension seal ring 216, so as to further improve the reliability of the sealing.

Further, referring to fig. 2, in this embodiment, the axial end portion of the second cylinder 210 passes through the end cap of the same end, the first bearing 218 is disposed at the axial end portion of the second cylinder 210, the first bearing 218 can contact with the first positioning groove 106 or the second positioning groove 107, when the first cylinder 210 rotates, the first bearing 218 and the first positioning groove 106 or the second positioning groove 107 generate rolling friction, so as to reduce friction force and improve smoothness of the rotation of the first cylinder 204.

In this embodiment, the first hinge shaft 210 may pass through the first drum cover 217 at the same end, and the first bearing 218 is correspondingly mounted on the first hinge shaft 210.

Referring to fig. 3, in this embodiment, at least one first heat dissipation hole 5 may be disposed at an end of the first stator 1, the first heat dissipation hole 5 is communicated with the inside of the first drum 204, and when the first drum 204 rotates, air may be introduced through the heat dissipation hole 5 to dissipate heat generated when the first drum 204 rotates.

In this embodiment, the outer sides and two ends of the first fixed blade 202 and the first swing blade 204 are provided with sealing members contacting with the inner wall of the first stator, the sealing members can slide in the corresponding blades, the inner wall of the first stator is tightly propped against under the tension of the spring, the sealing members can automatically compensate under the tension of the spring after being worn, and the service life of the whole machine is prolonged.

In the present embodiment, the air inlet 3 and the air supply port 4 may be provided on the circumferential surface of the first stator 1, but may be provided on the end surface of the first stator 1, which is not limited in the present embodiment.

Preferably, in the present embodiment, the first drum 204 and the first stator wall 105 may be arranged tangentially, the air inlet 3 is arranged at a position of the first stator wall 105 close to where it is tangential to the first drum 204, and the air inlet 4 and the air inlet 3 are oppositely arranged on the first stator wall 105.

Further, referring to fig. 4, one or more pressure regulating sliders 6 may be disposed on the gas inlet 3, and at least one pressure regulating slider 6 may be operatively disposed on the gas inlet 3 and may move along the circumferential direction of the first stator 1, so that the pressure starting phase may be adjusted to change the pressure of the gas, so as to adapt to the gas processing operation under different pressures.

In this embodiment, the movement of the slide 6 can be performed by a controllable structure, such as a motor, to realize an automated adjustment scheme.

Again, the present embodiment describes a work-doing device.

Fig. 9 is a schematic structural diagram of the working device according to the present embodiment. Referring to fig. 1, 2 and 9, the working device of the present embodiment includes a second stator 7 and a second rotor 8, the second stator 7 is provided with an ignition device 9, an air supply port 10, a fuel inlet 11 and an exhaust port 12, the second rotor 8 includes a second main shaft 801, a second fixed blade 802, a second swing blade 803 and a second drum 804, the second main shaft 801 is rotatably and coaxially disposed in the second stator 7, the second drum 804 is eccentrically disposed in the second stator 7, the second main shaft 801 is movably disposed in the second drum 804, the second fixed blade 802 is fixedly disposed on the second main shaft 801, the plurality of second swing blades 803 are rotatably disposed on the second main shaft 801, the second fixed blade 802 and the plurality of second swing blades 803 are movably sealed through the circumferential surface of the second drum 804 and abut against the inner sidewall of the second stator 7, and the second fixed blade 802 and the plurality of second swing blades 803 divide the area surrounded by the second drum 804 and the second stator 7 into sections A plurality of second spaces having a volume continuously changed periodically with the rotation of the second drum 804.

In this embodiment, the power generating device b includes a second stator 7 and a second rotor 8, the second stator 7 is provided with a gas supply port 10, a fuel inlet 11, a gas exhaust port 8 and an ignition device 9, high-pressure gas can be supplied into the second stator 7 through the gas supply port 10 of the second stator 7, a combustion medium required for power generation can be supplied into the second stator 7 through the fuel inlet 11, the high-pressure gas and the combustion medium are supplied into the second stator 7 to form a working medium, and the working medium can be ignited and expanded by the ignition device 9.

In this embodiment, since the second main shaft 801 is coaxially and rotatably disposed in the second stator 7, the second roller 804 is eccentrically disposed in the second stator 7, and the second roller 804 is movably disposed outside the second main shaft 801, a crescent-shaped working space is also defined between the second roller 804 and the second stator 7.

Since the second fixed blade 802 is fixedly disposed on the second main shaft 801, the plurality of second swinging blades 803 are rotatably disposed on the second main shaft 801, the main planes of the second fixed blade 802 and the plurality of second swinging blades 803 are parallel to the second main shaft 801, and the second fixed blade 802 and the plurality of second swinging blades 803 are movably sealed through the circumferential surface of the second drum 804 and abut against the inner side wall of the second stator 7. Thus, the second fixed blade 802 and the second swinging blades 803 can divide the crescent second space into a plurality of second spaces, the volume of which is periodically and continuously changed along with the rotation of the second roller 804, after the high-pressure gas and the fuel injected into a certain second space are ignited by the ignition device 9, expansion hot gas is generated, the expansion hot gas is utilized to push the second fixed blade 802 and the second swinging blades 803 to drive the second main shaft 801 and the second roller 804 to rotate, so that the second space is changed from small to large, when the second space is changed to the maximum, the second space is communicated with the exhaust port on the second stator, and the waste gas after work is exhausted from the exhaust port on the second stator.

The medium and the high-pressure gas are continuously injected into a certain second space, so that the second rotor 8 can be continuously driven to rotate, and the aim of continuously outputting power is fulfilled.

Referring to fig. 2, in the present embodiment, the second stator 7 includes a fifth cover plate 701, a sixth cover plate 702, a seventh cover plate 703, an eighth cover plate 704, and a second stator wall casing 705, wherein the fifth cover plate 701 and the seventh cover plate 703 are disposed opposite to each other, the circumferential surfaces of the fifth cover plate 701 and the seventh cover plate 703 are connected through the second stator wall casing 705, the sixth cover plate 702 is disposed inside the fifth cover plate 701, the fifth cover plate 701 is provided with a third positioning groove 706 (see fig. 10) matching the circumferential surface of one axial end of the second roller 804, one axial end of the second roller 804 movably passes through the sixth cover plate 702 and is rotatably disposed in the third positioning groove 706, similarly, the eighth cover plate 704 is disposed inside the seventh cover plate 703, the seventh cover plate 703 is provided with a fourth positioning groove 707 matching the circumferential surface of the other axial end of the second roller 804, the other axial end of the second roller 804 movably passes through the eighth cover plate 704, and is rotatably disposed in the fourth positioning groove 707.

In this embodiment, the fifth cover plate 701 and the sixth cover plate 702 may be integrally formed, the seventh cover plate 703 and the eighth cover plate 704 may also be integrally formed, and the fifth cover plate 701 and the eighth cover plate 704 may be detachably and hermetically connected to the second stator wall casing 705, so as to facilitate the assembly of the second rotor 8 in the second stator 7.

In this embodiment, at least one second heat dissipation hole 13 may be disposed at an end of the first stator 1, the second heat dissipation hole 13 is communicated with the inside of the second drum 804, and when the second drum 804 rotates, air may be introduced through the second heat dissipation hole 13 to dissipate heat generated when the second drum 804 rotates.

With reference to fig. 2 and fig. 9, in the present embodiment, two ends of the second main shaft 801 can respectively movably penetrate through two cover plates at the same end, so as to realize the rotatable arrangement of the second main shaft 801 in the second stator 7.

Fig. 11 is an exploded view of the second drum of the present embodiment, fig. 12 is a top view of the second drum of the present embodiment, and fig. 13 is a structural view of the second stationary blade. With reference to fig. 11-13, in the present embodiment, a third mounting ring 805 is disposed on one side of the second fixed blade 802, and the third mounting ring 805 is fixedly disposed on the second main shaft 801, that is, the second fixed blade 805 can rotate synchronously with the second main shaft 801.

Referring to fig. 12, for the present embodiment, the third mounting ring 805 may be fixedly connected to the second main shaft 801 by a second key 806, and of course, the third mounting ring 805 may also be welded or integrally connected to the second main shaft 801, which is not limited in the present embodiment.

Referring to fig. 12, in the present embodiment, a fourth mounting ring 807 is disposed on one side of each second swinging blade 803, and the fourth mounting ring 807 is movably sleeved on the second main shaft 801, that is, the fourth mounting ring 807 is rotatably disposed on the second main shaft 801.

Further, in this embodiment, at least one fourth mounting ring 807 is disposed between both axial ends of the third mounting ring 805 and both axial ends of the second stator 7, so that the fourth mounting ring 807 is assembled on the second main shaft 801 by the limitation of the third mounting ring 807 and the end of the second stator 7.

With reference to fig. 11, in this embodiment, a plurality of second through holes 808 are disposed at intervals on the circumferential surface of the second drum 804, a second hinge is disposed in each second through hole 808, a gap through which the second fixed blade 802 or the second swing blade 803 passes is disposed in the second hinge, and the second fixed blade 802 and the second swing blade 803 swing in the corresponding second through hole 808. The second fixed blade 802 penetrates through one second hinge in a movable sealing mode, and the second swinging blade 803 penetrates through the rest second hinges corresponding to the movable sealing mode, so that the inner side and the outer side of the second roller 804 can be kept sealed, and the work doing efficiency is improved.

Specifically, in this embodiment, a second hinge is disposed in each second through hole 808, a gap through which the second fixed blade 802 or the second swing blade 803 passes is disposed in the second hinge, and the second fixed blade 802 and the second swing blade 803 swing in the corresponding second through hole 808.

Fig. 14 is an exploded view of the second hinge of the present embodiment. Referring to fig. 11 and 14, in the present embodiment, each of the second hinges includes two second hinge shafts 810, two second cylindrical bodies 811, and two needle rollers 812, wherein the two second hinge shafts 810 are rotatably connected to two axial ends of the second drum 804, the two second cylindrical bodies 811 are rotatably disposed on two opposite sidewalls of the corresponding second through hole 808, two axial ends of the two second cylindrical bodies 811 are rotatably connected to the two second hinge shafts 810, planes of the two second cylindrical bodies 811 are opposite to each other to form a gap through which the second fixed vane 802 or the second swing vane 803 passes, opposite surfaces of the two second cylindrical bodies 811 are provided with second mounting grooves axially disposed along the second cylindrical bodies, the second needle rollers 812 and the second cylindrical bodies 811 are correspondingly disposed, the second needle rollers 821 are rotatably disposed in the second mounting grooves of the corresponding second cylindrical bodies 811, both axial ends of the second needle roller 821 are rotatably coupled in the two second hinge shafts 810, respectively. When the second fixed blade 802 or the second swing blade 803 swings between the two second cylindrical bodies 811, the second needle roller 804 may have rolling friction with the corresponding blade to improve the lifespan of the second hinge and the corresponding blade.

Further, in this embodiment, two opposite side walls of each second through hole 808 are provided with a second slot, a second hinge sealing plate 809 is further provided between an arc-shaped surface of each second column 811 and the corresponding side wall of the second through hole 808, a second inserting plate 813 is provided on an outer side of the second hinge sealing plate 809, the second inserting plate 813 is embedded in the second slot on the same side, and a second elastic member 814 is provided between the second inserting plate 813 and the bottom of the second slot. The second elastic member 814 can press the second inserting plate 613 and the first cylindrical body 811 against the corresponding blades to achieve a sealing effect.

In order to improve the sealing effect, in this embodiment, the second plug plate 813 may be integrally formed with the second hinge sealing piece 809, and the second hinge sealing piece 809 is integrally arc-shaped, so as to realize the rotation of the first column 211 inside the first hinge sealing piece 209.

For this embodiment, the second elastic member 814 of this embodiment may have an arc shape, two ends of the second elastic member 814 are supported by two axial ends of the second socket plate 213, and a middle portion of the second elastic member 814 is supported by a middle position of the bottom of the second socket, so that the second elastic member 814 has sufficient supporting force to improve the sealing effect.

The second elastic member 814 of the present embodiment may have other shapes, such as a strip shape, etc., and the second cylinder 811 may have a semicircular shape, etc., and in some embodiments, it may also have a full circle, or other angles, etc., which is not limited in this embodiment.

In this embodiment, the second drum end covers 817 are disposed at two axial ends of the second drum 804, the second drum seal 815 and the second tension seal ring 816 are disposed in the same side of the second drum end cover 817, and the second drum end cover 817 is rotatably disposed in the third positioning groove 706 or the fourth positioning groove 707, so that the sealing performance of the second drum 804 and the second drum end cover 817 can be improved.

Preferably, in this embodiment, the second drum seal 815 has two steps, and two steps of the second drum seal 815 are respectively sleeved with one second tension sealing ring 816, so as to further improve the sealing reliability.

Further, referring to fig. 2, in this embodiment, the axial end of the fourth cylinder 810 passes through the end cap of the same end, and the second bearing 818 is disposed at the axial end of the fourth cylinder 810, and the second bearing 818 can contact with the third positioning groove 706 or the fourth positioning groove 707, so that when the second roller 804 rotates, the second bearing 818 can generate rolling friction with the third positioning groove 706 or the fourth positioning groove 707, which can reduce friction force and improve the smoothness of the rotation of the second roller 804.

In this embodiment, the second hinge shaft 810 may pass through the second drum end cover 817 of the same end, and the second bearing 818 is correspondingly fitted on the second hinge shaft 810.

In addition, in this embodiment, the outer sides and two ends of the second fixed blade 802 and the second swing blade 803 are provided with sealing elements contacting with the inner wall of the second stator 7, the sealing elements can slide in the corresponding blades, the inner wall of the first stator is tightly pressed under the tension of the spring, the sealing elements can automatically compensate under the tension of the spring after being worn, and the service life of the whole machine is prolonged.

The ignition device 9, the air supply port 10, and the fuel inlet port 11 of the present embodiment may be disposed on a first side of the circumferential surface of the second stator where the distance from the second drum is the smallest, and the exhaust port 12 may be disposed on a second side of the circumferential surface of the second stator, the second side being opposite to the first side, which may improve work efficiency.

Further, in this embodiment, the second drum 804 and the second stator wall 705 may be tangentially arranged, the air supply port 10 is arranged at a position of the second stator wall 705 close to the tangent of the second drum 804, and the air discharge port 12 and the air supply port 10 are oppositely arranged on the second stator wall 705.

In addition, the gas supply port 10 of the second stator 7 of the present embodiment may communicate with the gas supply port 4 of the first stator 1 through a connection pipe 14, and the high-pressure gas may be supplied into the second stator 7 through the first stator 1, but the gas supply port 10 of the second stator may also supply the high-pressure gas through other devices, and the fuel inlet 11 of the present embodiment may also be disposed on the connection pipe 14, which is not limited in the present embodiment.

In addition, in the embodiment, the number of the elastic sealing elements on the first roller and the second roller is consistent, and the distance is also set to be consistent, so that the first space and the second space can be divided into chambers with different sizes, and the air compressing device and the acting device can be ensured to act consistently and synchronously.

In this embodiment, the air compressing device a may be fixedly disposed with the work applying module b, that is, the first stator 1 of the air compressing device a may be coaxially and fixedly connected with the second stator 7 of the work applying module b, the first spindle 201 of the air compressing device a is fixedly connected with the second spindle 802 of the work applying module b, when the first spindle 201 of the air compressing device a is started, the first spindle 201 may be driven by the motor to rotate, and after the work applying module b is started, the first spindle 201 may be driven by the second spindle 801 to synchronously rotate, at this time, the motor may be disconnected from the first spindle 201.

On the air compressing device, the volume of a first space between adjacent blades is sucked in the process of changing from small to large, and then the air is compressed in the process of changing from large to small. On the acting device, the process that the volume of the second space between the adjacent blades is changed from small to large does work, and the process that the volume of the second space between the adjacent blades is changed from large to small is utilized to discharge waste gas.

When the gas is pressed to the minimum in the air compressing device, the compressed air is pressed into the work doing membrane block through the communicating pipe and is mixed with the sprayed fuel to form a high-pressure working medium, and the work doing cavity of the work doing machine is filled with the high-pressure working medium and rotates to a phase which is most beneficial to ignition to ignite the working medium. The pressure of the combustion expansion of the working medium pushes the blades and the roller to move towards the direction of the blades with larger stress surfaces to do work, and the volume is simultaneously changed from small to large. The expansion pressure generated by the expansion hot gas acts on the blades vertically along the circumferential direction to push the stressed blades to rotate around the shaft, the stressed blades push the second roller to rotate by utilizing the lever principle, and then other blades are driven to rotate, and the fixed blades drive the main shaft to rotate. The whole working process airflow flows along the circumferential direction in the working machine. After the work is done, the volume between the adjacent blades of the work doing cavity begins to be reduced, and waste gas is discharged in the process of reducing the volume.

In the working rotation process of the rotor of the working device, the main shaft drives the fixed blade of the rotor of the air compressing device to rotate, the fixed blade of the air compressing device drives the first roller to rotate, the first roller drives the swing blade to rotate, the adjacent blades suck air in the process that the volume is changed from small to large among the blades, the air is compressed in the process that the volume is changed from large to small, and the air flow in the compression process flows along the circumferential direction.

The existing reciprocating piston engine is composed of a cylinder, a piston, a connecting rod, a crankshaft, an intake valve and an exhaust valve. Because the four strokes of air suction and air compression working and air exhaust are all carried out in the same container with fixed volume, the expanded hot air can not fully work and is discharged as waste gas to waste partial heat energy, so the heat efficiency is not high. The complex connecting rod crankshaft mechanism and the intake and exhaust valve control mechanism also lead the structure of the whole machine to be complex, heavy and high in cost, and the crankshaft rotates for 4 strokes of the piston for two circles to do work once, thus leading to low power-weight ratio, heavy weight, high output power and low rotating speed. The process of converting from linear motion to rotary motion also introduces vibration and noise.

The existing gas turbine internal combustion engine adopts an axial flow type coaxial rotor structure, an air compressing blade and a working blade share a straight shaft, the blades and a main shaft form a certain included angle, the kinetic energy air compressing mode of an axial flow type turbine compressor and a centrifugal turbine compressor is adopted to compress air, the compressed air is mixed with fuel and then ignited to expand to work, the working machine adopts an axial flow type turbine, high-pressure hot gas flows along the axial direction to act on the turbine blades, and the circumferential component force pushes the turbine blades to rotate. The exhaust gas is directly ejected in the axial direction. Simple structure, high power-weight ratio, high rotation speed and low noise. The efficiency of compressing air is high when the engine is operated at high speed, so the thermal efficiency is higher than that of a reciprocating piston engine.

Because the kinetic energy compression mode of axial flow type compression and centrifugal type compression is adopted, the air can be compressed to the ideal air pressure only at high rotating speed, so that the high combustion efficiency is achieved, the air can not work in a high-power working area of high compression, and the air can not work at low rotating speed and idling, so that the axial flow type gas turbine internal combustion engine can not be suitable for occasions of medium and low power and rotating speed such as civil transportation tools. The high-temperature, high-pressure and high-speed working environment limits the manufacturing process requirements of the blade, so that the manufacturing cost is extremely high.

In this application, will do work cavity and pressure cavity fall into the cavity of variation in size through fixed blade and swing blade, improve in the heat engine efficiency by a wide margin, from lighting to the inflation exhaust process, the volume expansion ratio is enough big, does not have linear motion conversion circular motion's loss, also does not have the extra friction loss that the eccentric vibrations of bent axle brought, and the burning steam does work the stroke big, and the pump gas loss is little, can increase substantially heat engine efficiency.

This application will do work cavity and pressure cavity divide into the cavity of variation in size through fixed blade and swing blade, adopts the volume of becoming mode compressed air that calms the anger, does not receive the rotational speed restriction, under well low rotational speed and idle operating mode, equally can reach the compression ratio of ideal, satisfies the demand of high-efficient burning.

The rotor of the acting device and the rotor of the compression device are in the rotating process, in the acting or compression process, except for the volume change caused by the change of the distance between the outer wall of the roller and the inner wall of the stator, the included angle between the blades is also reduced by the size, the compression ratio is improved, and the acting efficiency and the compression efficiency can be improved.

In addition, the structure of the engine does not have gears and crankshafts to do work, and the engine is simple in structure like an axial-flow turbine internal combustion engine, so that the rotating speed is high, and the output torque is high.

The noise of the reciprocating internal combustion engine is low, the impact noise of a connecting rod to a crankshaft is avoided, the vibration noise of eccentric rotation is avoided, the noise of gear meshing is avoided, the structure is simple, the axial-flow internal combustion engine is similar to the axial-flow internal combustion engine with the same size in weight, the volume and the weight are extremely light, the manufacturing cost is far lower than that of a reciprocating internal combustion engine with a complex structure, the working conditions of a rotor blade and a roller barrel are better than that of the axial-flow internal combustion engine, and the manufacturing cost is far lower than that of the axial-flow internal combustion engine.

The air compressing device realizes the compression of air only through the circular motion of the first fixed blade, the first swing blade and the first roller, and the whole process has no conversion of other motions, so that the energy loss caused by the conversion is correspondingly reduced; the acting device realizes power output only through the circular motion of the second fixed blade, the second swing blade, the second roller and the second main shaft, and the whole process has no corresponding conversion of other motions, so that the problem of waste of heat energy of the internal combustion engine can be solved, the heat conversion efficiency is improved, and the working device has good practical value.

While the preferred embodiments of the present application have been described, additional variations and modifications in those embodiments may occur to those skilled in the art once they learn of the basic inventive concepts. Therefore, it is intended that the appended claims be interpreted as including preferred embodiments and all alterations and modifications as fall within the scope of the application.

It will be apparent to those skilled in the art that various changes and modifications may be made in the present application without departing from the spirit and scope of the application. Thus, if such modifications and variations of the present application fall within the scope of the claims of the present application and their equivalents, the present application is intended to include such modifications and variations as well.

Claims

1. A circumferential flow turbine, characterized in that it comprises:

2. The circumferential flow turbine as claimed in claim 1, wherein a third mounting ring is provided at one side of the second stationary blade, the third mounting ring being fixedly provided on the second main shaft;

3. The circumferential flow turbine according to claim 1, wherein a plurality of second through holes are provided at intervals on the circumferential surface of the second drum, a second hinge is provided in each of the second through holes, and a gap through which the second fixed blade or the second swing blade passes is provided in the second hinge.

4. The circumferential flow turbine of claim 3, wherein each of said second hinges comprises:

5. The circumferential flow turbine of claim 4, wherein two opposing side walls of the second through hole are provided with second slots;

6. The circumferential flow turbine according to claim 1, wherein the ignition device, the air supply port, and the fuel inlet port are provided on a first side surface of a circumferential surface of the second stator at which a distance from the second drum is smallest; the exhaust port is provided on a second side surface of the circumferential surface of the second stator, the second side surface being disposed opposite to the first side surface.

7. The circumferential turbine of any one of claims 1-6, further comprising:

8. The circumferential flow turbine as claimed in claim 7, wherein a first mounting ring is provided at one side of the first stationary blade, the first mounting ring being fixedly provided on the first main shaft;

9. The circumferential flow turbine of claim 7, wherein the inlet port is disposed on a circumferential surface of the first stator, and wherein the inlet port has one or more pressure regulating slides disposed thereon, the pressure regulating slides being operable to move circumferentially on the inlet port along the first stator.

10. The circumferential flow turbine according to claim 7, wherein a plurality of first through holes are provided at intervals on the circumferential surface of the first drum, a first hinge is provided in each of the first through holes, and a gap through which the first fixed blade or the first oscillating blade passes is provided in the first hinge.

11. The circumferential flow turbine of claim 10, wherein each of said first hinges comprises:

12. The air compressing device as recited in claim 10, wherein two opposite side walls of the first through hole are provided with first slots;

13. The circumferential flow turbine of claim 7, wherein said first stator and said second stator are fixedly connected coaxially and said first main shaft and said second main shaft are fixedly connected coaxially.