CN108301876A - A kind of revolution curved tube rotor of rotary engine - Google Patents
A kind of revolution curved tube rotor of rotary engine Download PDFInfo
- Publication number
- CN108301876A CN108301876A CN201710793416.7A CN201710793416A CN108301876A CN 108301876 A CN108301876 A CN 108301876A CN 201710793416 A CN201710793416 A CN 201710793416A CN 108301876 A CN108301876 A CN 108301876A
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- China
- Prior art keywords
- curved tube
- rotor
- hollow out
- revolution
- revolution curved
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Pending
Links
- 238000002485 combustion reaction Methods 0.000 description 4
- 238000005516 engineering process Methods 0.000 description 3
- 239000002737 fuel gas Substances 0.000 description 3
- 239000007789 gas Substances 0.000 description 3
- 238000010586 diagram Methods 0.000 description 2
- 238000005265 energy consumption Methods 0.000 description 2
- 238000006243 chemical reaction Methods 0.000 description 1
- 239000012530 fluid Substances 0.000 description 1
- 238000002347 injection Methods 0.000 description 1
- 239000007924 injection Substances 0.000 description 1
- 239000007921 spray Substances 0.000 description 1
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
- F01D1/00—Non-positive-displacement machines or engines, e.g. steam turbines
- F01D1/34—Non-positive-displacement machines or engines, e.g. steam turbines characterised by non-bladed rotor, e.g. with drilled holes
Abstract
A kind of revolution curved tube rotor of rotary engine, is made of axis and rotor body, and rotor body is in flywheel shape, and one end is inlet end, and the other end is exhaust end；There is hollow out to turn round curved tube between inlet end and exhaust end, hollow out revolution curved tube is distributed in rotor body less than in the arc-shaped curved surface body circumferentially of outer diameter；The hollow out turns round curved tube U-shaped revolution in curved surface from air inlet to exhaust outlet, and multiple hollow outs turn round curved tube and are seen as isogonism distribution from the inlet end end face of rotor body.Engine burnup produced by the present invention is low, output torque is big.Engine is used suitable for middle-size and small-size rotating plasma aircraft, automobile, motor etc..
Description
Technical field
The present invention relates to a kind of revolution curved tube rotors of rotary engine, belong to engine technology.
Background technology
Piston internal-combustion engine, toggle and piston, which exist, to be moved back and forth, and engine overcomes movement portion
The reciprocating motion of part needs to consume a large amount of energy, and in-fighting is very big.Therefore, the thermal efficiency of piston internal-combustion engine is low is
Undisputable fact.
To overcome the disadvantage that energy consumption is high inside piston internal-combustion engine, there are many rotary engine design cases
Example.But there are easily worn parts in the complicated or even structure design of the rotary engine of the prior art.Such as notification number
A kind of slide plate engine etc. that CN1069888868A is disclosed.
Another kind of typical rotary engine, is turbojet or turbofan.But turbojet or turbofan, mainly with height
The reaction force of speed injection pushes the flight of the special vehicles such as aircraft.This kind of rotary engine is used for torque axis output
When way, high-temperature high-pressure air flow is discharged by the self inflation between open impeller blade of turbo blade expansion work, there is phase
When the hot-fluid gas of ratio fails to play a role.
Invention content
The purpose of the present invention is to provide a kind of revolution curved tube rotors of rotary engine.
Technical scheme of the present invention
A kind of revolution curved tube rotor of rotary engine, is made of axis and rotor body, rotor body be in flywheel shape, one
End is inlet end, and the other end is exhaust end；There is hollow out to turn round curved tube between inlet end and exhaust end, hollow out revolution curved tube is distributed in
Rotor body is less than in the arc-shaped curved surface body circumferentially of outer diameter；The hollow out turns round curved tube from air inlet to exhaust
U-shaped revolution mouthful in curved surface, meander sections are towards the direction of rotation of rotor；The hollow out revolution curved tube quantity must be multiple to engrave more than 2
Backlash turns curved tube and is seen as isogonism distribution from the inlet end end face of rotor body or exhaust end end face.
The first distribution mode of air inlet/exhaust outlet of hollow out revolution curved tube of the present invention：Air inlet is in air inlet
The end face at end, exhaust outlet is in the end face of exhaust end.
Second of distribution mode of air inlet/exhaust outlet of hollow out revolution curved tube of the present invention：Air inlet is in air inlet
The end face at end, outer wall of the exhaust outlet in exhaust end.
The third distribution mode of air inlet/exhaust outlet of hollow out revolution curved tube of the present invention：Air inlet is in air inlet
The outer wall at end, exhaust outlet is in the end face of exhaust end.
4th kind of distribution mode of air inlet/exhaust outlet of hollow out revolution curved tube of the present invention：Air inlet is in air inlet
The outer wall at end, outer wall of the exhaust outlet in exhaust end.
The cross section of hollow out of the present invention revolution curved tube, a kind of scheme are circle.
The cross section of hollow out revolution curved tube of the present invention, another scheme are rectangle.
The revolution curved tube rotor of rotary engine of the present invention, the sectional area that hollow out turns round the meander sections of curved tube are
The 80% of air inlet section product；The sectional area of air inlet is the 80% of exhaust outlet sectional area.
The course of work of the present invention
The technical spirit of the present invention is to be changed to revolution curved tube rotor to the turbine of turbojet or turbofan, is sprayed using whirlpool
Or the combustion technology of fanjet obtains high-temperature high-pressure fuel gas, high-temperature high-pressure fuel gas turns from the air inlet impact rotor of rotor
It is dynamic, using spouting from exhaust outlet after meander sections, repetition promotion revolution curved tube rotor.
The invention has the advantages that
1, the shortcomings that exporting rotary engine rotor as axis, not only overcoming energy consumption in existing piston-mode motor height,
And vulnerable components are not present in structure.
2, high-temperature high-pressure fuel gas from the air inlet impact rotor of rotor rotate, using after meander sections from exhaust outlet spray and
Go out, repeats to push revolution curved tube rotor.Its burnup is low, output torque is big.The present invention be suitable for middle-size and small-size rotating plasma aircraft, automobile,
Motor etc. uses engine.
Description of the drawings
It further illustrates the present invention below in conjunction with the accompanying drawings.
Fig. 1 is that air inlet of the present invention shows in the rotor three-dimensional appearance of the end face of inlet end, exhaust outlet in the end face of exhaust end
It is intended to.
Fig. 2 is that air inlet of the present invention shows in outer wall, the exhaust outlet of inlet end in the rotor three-dimensional appearance of the outer wall of exhaust end
It is intended to.
In figure：
1- axis, 2- inlet ends, 3- exhaust ends, 4- rotor bodies
G1- air inlets, g2- meander sections, g3- exhaust outlets
Embodiment
Embodiment 1
1、2A kind of revolution curved tube rotor of rotary engine, is made of axis 1 and rotor body 4,
Rotor body 4 is in flywheel shape, and one end is inlet end 2, and the other end is exhaust end 3；There is hollow out to return between inlet end 2 and exhaust end 3
Turn curved tube g1, g2, g3, hollow out revolution curved tube g1, g2, g3 are distributed in the arc circumferentially that rotor body 4 is less than outer diameter
In the body of curved surface；The hollow out turns round curved tube g1, g2, g3 U-shaped revolution in curved surface from air inlet g1 to exhaust outlet g3, revolution
G2 is towards the direction of rotation of rotor for section；Described hollow out revolution curved tube g1, g2, g3 quantity be 9,9 hollow outs turn round curved tube g1,
G2, g3 are from 40 ° each other of angle of distribution in terms of 3 end face of 2 end face of inlet end or exhaust end of rotor body 4.
Embodiment 2
The revolution curved tube rotor of rotary engine as shown in Figure 1, described in hollow out revolution curved tube g1, g2, g3 into
Gas port g1 is distributed in the end face of inlet end 2, and exhaust outlet g3 is distributed in the end face of exhaust end 3.
Embodiment 3
The air inlet g1 of the revolution curved tube rotor of the rotary engine, hollow out revolution curved tube g1, g2, g3 is distributed in
The end face of inlet end 2, exhaust outlet g3 are distributed in the outer wall (no schematic diagram) of exhaust end 3.Embodiment 4
The air inlet g1 of the revolution curved tube rotor of the rotary engine, hollow out revolution curved tube g1, g2, g3 is distributed in
The outer wall of inlet end 2, exhaust outlet g3 are distributed in the end face (no schematic diagram) of exhaust end (3).
Embodiment 5
As shown in Figure 1, 2, the revolution curved tube rotor of the rotary engine, hollow out turn round curved tube g1, g2, g3 into
Gas port g1 is distributed in the outer wall of inlet end 2, and exhaust outlet g3 is distributed in the outer wall of exhaust end 3.
Embodiment 6
As shown in Figure 1, 2, the revolution curved tube rotor of the rotary engine, hollow out turn round the cross of curved tube g1, g2, g3
Section is circle.
Embodiment 7
The revolution curved tube rotor of the rotary engine, the cross section that hollow out turns round curved tube g1, g2, g3 are rectangle.
Embodiment 8
As shown in Figure 1, 2, the revolution curved tube rotor of the rotary engine, hollow out turn round returning for curved tube g1, g2, g3
The sectional area for turning section g2 is the 80% of air inlet g1 sectional areas；The sectional area of air inlet g1 is the 80% of exhaust outlet g3 sectional areas.
Claims (8)
1. a kind of revolution curved tube rotor of rotary engine, is made of axis (1) and rotor body (4), it is characterized in that rotor body
(4) it is in flywheel shape, one end is inlet end (2), and the other end is exhaust end (3)；There is hollow out between inlet end (2) and exhaust end (3)
Curved tube (g1, g2, g3) is turned round, hollow out revolution curved tube (g1, g2, g3) is distributed in rotor body (4) less than outer diameter along circle
In the body of the arc-shaped curved surface in week；The hollow out revolution curved tube (g1, g2, g3) is from air inlet (g1) to exhaust outlet (g3) in song
The U-shaped revolution in face, meander sections (g2) are towards the direction of rotation of rotor；Described hollow out revolution curved tube (g1, the g2, g3) quantity is more than 2,
Multiple hollow out revolution curved tubes (g1, g2, g3) are seen as isogonism from inlet end (2) end face of rotor body (4) or exhaust end (3) end face
Distribution.
2. the revolution curved tube rotor of rotary engine described in claim 1, it is characterized in that the hollow out revolution curved tube (g1,
G2, g3) air inlet (g1) be distributed in the end faces of inlet end (2), exhaust outlet (g3) is distributed in the end face of exhaust end (3).
3. the revolution curved tube rotor of rotary engine described in claim 1, it is characterized in that the hollow out revolution curved tube (g1,
G2, g3) air inlet (g1) be distributed in the end faces of inlet end (2), exhaust outlet (g3) is distributed in the outer wall of exhaust end (3).
4. the revolution curved tube rotor of rotary engine described in claim 1, it is characterized in that the hollow out revolution curved tube (g1,
G2, g3) air inlet (g1) be distributed in the outer walls of inlet end (2), exhaust outlet (g3) is distributed in the end face of exhaust end (3).
5. the revolution curved tube rotor of rotary engine described in claim 1, it is characterized in that the hollow out revolution curved tube (g1,
G2, g3) air inlet (g1) be distributed in the outer walls of inlet end (2), exhaust outlet (g3) is distributed in the outer wall of exhaust end (3).
6. the revolution curved tube rotor of rotary engine described in claim 1, it is characterized in that hollow out revolution curved tube (g1, g2, g3)
Cross section be circle.
7. the revolution curved tube rotor of rotary engine described in claim 1, it is characterized in that hollow out revolution curved tube (g1, g2, g3)
Cross section be it is non-circular.
8. the revolution curved tube rotor of rotary engine described in claim 1, it is characterized in that the hollow out revolution curved tube (g1,
G2, g3) meander sections (g2) sectional area be air inlet (g1) sectional area 50-100%；The sectional area of air inlet (g1) is row
The 40-100% of gas port (g3) sectional area.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201710793416.7A CN108301876A (en) | 2017-08-31 | 2017-08-31 | A kind of revolution curved tube rotor of rotary engine |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201710793416.7A CN108301876A (en) | 2017-08-31 | 2017-08-31 | A kind of revolution curved tube rotor of rotary engine |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN108301876A true CN108301876A (en) | 2018-07-20 |
Family
ID=62869450
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201710793416.7A Pending CN108301876A (en) | 2017-08-31 | 2017-08-31 | A kind of revolution curved tube rotor of rotary engine |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN108301876A (en) |
Citations (9)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US4027995A (en) * | 1975-07-14 | 1977-06-07 | Berry Clyde F | Steam track turbine |
| FR2453976A1 (en) * | 1978-05-16 | 1980-11-07 | Bachl Herbert | TURBOMACHINE |
| US5237814A (en) * | 1991-06-11 | 1993-08-24 | Chen Suh P | Internal combustion rotary engine |
| EP0625629A1 (en) * | 1993-05-21 | 1994-11-23 | Shu Ping Chen | Turbine |
| CN101397915A (en) * | 2008-11-07 | 2009-04-01 | 陈效刚 | Airway type gas turbine |
| CN101592080A (en) * | 2009-06-30 | 2009-12-02 | 陈效刚 | A kind of annular bending type turbine engine |
| WO2011042863A2 (en) * | 2009-10-06 | 2011-04-14 | Cmt Systems-Ceramic Micro Turbine Technologies Ltd | Bladeless working wheel useful as a turbomachine component |
| KR20120138509A (en) * | 2011-06-15 | 2012-12-26 | (주)빅뱅지티에스 | Multi-stage turbine consisting of wheels with multiple through holes |
| CN105201560A (en) * | 2008-10-30 | 2015-12-30 | 电力技术发展基金公司 | Toroidal Boundary Layer Gas Turbine |
-
2017
- 2017-08-31 CN CN201710793416.7A patent/CN108301876A/en active Pending
Patent Citations (9)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US4027995A (en) * | 1975-07-14 | 1977-06-07 | Berry Clyde F | Steam track turbine |
| FR2453976A1 (en) * | 1978-05-16 | 1980-11-07 | Bachl Herbert | TURBOMACHINE |
| US5237814A (en) * | 1991-06-11 | 1993-08-24 | Chen Suh P | Internal combustion rotary engine |
| EP0625629A1 (en) * | 1993-05-21 | 1994-11-23 | Shu Ping Chen | Turbine |
| CN105201560A (en) * | 2008-10-30 | 2015-12-30 | 电力技术发展基金公司 | Toroidal Boundary Layer Gas Turbine |
| CN101397915A (en) * | 2008-11-07 | 2009-04-01 | 陈效刚 | Airway type gas turbine |
| CN101592080A (en) * | 2009-06-30 | 2009-12-02 | 陈效刚 | A kind of annular bending type turbine engine |
| WO2011042863A2 (en) * | 2009-10-06 | 2011-04-14 | Cmt Systems-Ceramic Micro Turbine Technologies Ltd | Bladeless working wheel useful as a turbomachine component |
| KR20120138509A (en) * | 2011-06-15 | 2012-12-26 | (주)빅뱅지티에스 | Multi-stage turbine consisting of wheels with multiple through holes |
Non-Patent Citations (1)
| Title |
|---|
| 张中洲等: "某型发动机喷管-排气管系统建模方法", 《导弹与航天运载技术》 * |
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Application publication date: 20180720 |
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