CN103573654A - Multi-stage stamping gas compressor and engine applying same - Google Patents
Multi-stage stamping gas compressor and engine applying same Download PDFInfo
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- CN103573654A CN103573654A CN201310470696.XA CN201310470696A CN103573654A CN 103573654 A CN103573654 A CN 103573654A CN 201310470696 A CN201310470696 A CN 201310470696A CN 103573654 A CN103573654 A CN 103573654A
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- ring rotation
- gas compressor
- described ring
- stage ram
- ram gas
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Abstract
The invention discloses a multi-stage stamping gas compressor, comprising a power source and at least two ring-shaped rotating structure bodies, wherein all the ring-shaped rotating structure bodies are arranged in a sleeved manner, the power source is used for outputting rotating power to the ring-shaped rotating structure bodies, two adjacent ring-shaped rotating structure bodies rotate along different directions, and diffusers are arranged in all the ring-shaped rotating structure bodies. The invention also discloses an engine applying the multi-stage stamping gas compressor. The rotating speed of rotors (namely the ring-shaped rotating structure bodies) can be effectively reduced, and the force for compressing gas is improved, so that the working efficiency of the gas compressor and the engine can be further improved, and the size and the weight of the gas compressor and the engine can be further reduced. The stamping engine can be widely applied to vehicles, boats and aircrafts.
Description
Technical field
The present invention relates to heat power field, relate in particular to a kind of Multi-stage ram gas compressor, the invention still further relates to the motor of this Multi-stage ram gas compressor of application.
Background technique
Pressed engine and rotary punching engine are simple in structure, movement parts is few, but must do high-speed motion and can obtain higher stamping pressure, and then the higher efficiency of acquisition, this has just seriously limited the application of pressed engine, if utilize the working principle of intake duct of the Diffuser of pressed engine, carry out multistage diffusion, just can utilize punching press principle to produce the gas compressor that pressure ratio is high, also can produce the pressed engine that efficiency is high.
Summary of the invention
In order to address the above problem, the technological scheme that the present invention proposes is as follows:
A kind of Multi-stage ram gas compressor, comprise power source and at least two ring rotation structures, all described ring rotation structure suits arrange, described power source is to described ring rotation structure outputting rotary power, two adjacent described ring rotation structures are pressed different direction rotation, in all described ring rotation structures, establish Diffuser.
The suction port of described Diffuser and relief opening are arranged successively from inside to outside.
The suction port of described Diffuser and relief opening successively ecto-entad are arranged.
Between two adjacent described ring rotation structures, establish ring-type static pressure chamber, between the sidewall in described ring-type static pressure chamber and described ring rotation structure, be slidably matched.
The present invention also comprises a kind of motor of applying described Multi-stage ram gas compressor, comprise that inside is provided with the ring rotation dynamic structure body of pressed engine, described ring rotation dynamic structure body is arranged on the outside of the outermost described ring rotation structure of described Multi-stage ram gas compressor; Or described ring rotation dynamic structure body is arranged on the inner side of the described ring rotation structure of inner side of described Multi-stage ram gas compressor.
The present invention also comprises the motor of the described Multi-stage ram gas compressor of another kind of application, described power source is made as the ring rotation dynamic structure body that inside is provided with pressed engine, and described ring rotation dynamic structure body is arranged on the outside of the outermost described ring rotation structure of described Multi-stage ram gas compressor; Or described ring rotation dynamic structure body is arranged on the inner side of the described ring rotation structure of inner side of described Multi-stage ram gas compressor.
The working principle of Multi-stage ram gas compressor of the present invention is: by described Diffuser be arranged on mutual sheathing and adjacent two mutually in the described ring rotation structure turning, so from inside to outside or ecto-entad, just formed the Multi-stage ram pattern of multistage Diffuser series operation, thereby reduce the movement velocity of single Diffuser, in the situation that single Diffuser movement velocity is not too high, still can obtain in other words higher total ram ratio.
In the present invention, so-called " Diffuser " refers to the intake duct of pressed engine, can, by rotatablely moving or straight line motion improves the passage of gas pressure, can be subsonic diffuser, supersonic diffuser or hypersonic diffuser.
In the present invention, so-called " static pressure chamber " refers to that volume space, its effect are that the fluid that makes to flow in this volume space reduces the higher static pressure of flow velocity formation as far as possible.
In the present invention, should, according to the known technology in heat power field, in necessary place, necessary parts, unit or system etc. be set.
beneficial effect of the present invention is as follows:
The present invention can effectively reduce rotor (being described ring rotation structure) rotating speed, improves the compression dynamics to gas, and then can improve the working efficiency of gas compressor and motor, reduces its volume and weight.Can make pressed engine be widely used on car, ship and aircraft.
Accompanying drawing explanation
Shown in Fig. 1 is the structural representation of the embodiment of the present invention 1;
Shown in Fig. 2 is the structural representation of the embodiment of the present invention 2;
Shown in Fig. 3 is the structural representation of the embodiment of the present invention 3;
Fig. 4 be in Fig. 3 shown in Multi-stage ram gas compressor along the sectional view of A-A face;
Shown in Fig. 5 is the structural representation of the embodiment of the present invention 4;
Fig. 6 be in Fig. 5 shown in Multi-stage ram gas compressor along the sectional view of B-B face;
Shown in Fig. 7 is the structural representation of the embodiment of the present invention 5;
Shown in Fig. 8 is the structural representation of the embodiment of the present invention 6;
In figure: 1 ring rotation structure, 2 Diffusers, 3 ring-type static pressure chambeies, 301 sidewalls, 4 ring rotation dynamic structure bodies.
Embodiment
Below technological scheme of the present invention and beneficial effect are further described.
Embodiment 1
Multi-stage ram gas compressor shown in Fig. 1, comprise power source and three ring rotation structures 1, all described ring rotation structure 1 suits arrange, described power source is to described ring rotation structure 1 outputting rotary power, two adjacent described ring rotation structures 1 are pressed different direction rotation, at the interior Diffuser 2 of establishing respectively of all described ring rotation structures 1, the suction port of described Diffuser 2 and relief opening are arranged successively from inside to outside.
Multi-stage ram gas compressor shown in Fig. 2, and embodiment 1 difference is: the suction port of described Diffuser 2 and relief opening successively ecto-entad are arranged replacement arrangement from inside to outside.
Multi-stage ram gas compressor shown in Fig. 3, Fig. 4, on embodiment 1 basis: establish the ring-type static pressure chamber 3 being surrounded by the described ring rotation structure 1 of these adjacent two and sidewall 301 between two adjacent described ring rotation structures 1, be slidably matched between the described sidewall 301 in described ring-type static pressure chamber 3 and described ring rotation structure 1.
Multi-stage ram gas compressor shown in Fig. 5, Fig. 6, and embodiment 3 difference is: the suction port of described Diffuser 2 and relief opening successively ecto-entad are arranged replacement arrangement from inside to outside.
Embodiment 5
Motor shown in Fig. 7, comprise the described Multi-stage ram gas compressor in embodiment 1, also comprise that inside is provided with the ring rotation dynamic structure body 4 of pressed engine, described ring rotation dynamic structure body 4 is arranged on the outside of the outermost described ring rotation structure 1 of described Multi-stage ram gas compressor.
As the mode of execution that can convert, between described ring rotation dynamic structure body 4 and outermost described ring rotation structure 1, described annular static pressure chamber 3 can be set.
Gas working medium enters the pressed engine of outermost described ring rotation dynamic structure body 4 inside from inside to outside after multistage described Diffuser 2 diffusions of described Multi-stage ram gas compressor.
Embodiment 6
Motor shown in Fig. 8, itself and embodiment's 5 difference is: the suction port of described Diffuser 2 and relief opening successively ecto-entad are arranged and replaced arranging from inside to outside, and the inner side of described ring rotation structure 1 that described ring rotation dynamic structure body 4 is arranged on the inner side of described Multi-stage ram gas compressor replaces being arranged on the outside of the outermost described ring rotation structure 1 of described Multi-stage ram gas compressor.
As the mode of execution that can convert, at described ring rotation dynamic structure body 4 and between the most described ring rotation structure 1 of inner side, described annular static pressure chamber 3 can be set.
Gas working medium ecto-entad enters the pressed engine of described ring rotation dynamic structure body 4 inside of inner side after multistage described Diffuser 2 diffusions of described Multi-stage ram gas compressor.
In embodiment 5, embodiment 6 and disposable mode of execution thereof, can the structure in described ring-type static pressure chamber 3 be set between two adjacent described ring rotation structures 1 with reference to embodiment 3, embodiment 4; Also described power source can be made as to described ring rotation dynamic structure body 4, now 4 pairs of described ring rotation structure 1 outputting powers of described ring rotation dynamic structure body.
As the mode of execution that can convert, in above all embodiments, described Multi-stage ram gas compressor can comprise two or four even more described ring rotation structures 1.
Obviously, the invention is not restricted to above embodiment, according to the known technology of related domain and technological scheme disclosed in this invention, can derive or association goes out many flexible programs, all these flexible programs, also should think protection scope of the present invention.
Claims (6)
1. a Multi-stage ram gas compressor, comprise power source and at least two ring rotation structures (1), it is characterized in that: all described ring rotation structures (1) suit arranges, described power source is to described ring rotation structure (1) outputting rotary power, adjacent two described ring rotation structures (1) are pressed different direction rotation, establish Diffuser (2) in all described ring rotation structures (1).
2. Multi-stage ram gas compressor as claimed in claim 1, is characterized in that: the suction port of described Diffuser (2) and relief opening are arranged successively from inside to outside.
3. Multi-stage ram gas compressor as claimed in claim 1, is characterized in that: the suction port of described Diffuser (2) and relief opening successively ecto-entad are arranged.
4. Multi-stage ram gas compressor as described in any one in claims 1 to 3, it is characterized in that: between adjacent two described ring rotation structures (1), establish ring-type static pressure chamber (3), between the sidewall (301) in described ring-type static pressure chamber (3) and described ring rotation structure (1), be slidably matched.
5. an application rights requires in 1 to 4 the motor of Multi-stage ram gas compressor described in any one, comprise that inside is provided with the ring rotation dynamic structure body (4) of pressed engine, is characterized in that: described ring rotation dynamic structure body (4) is arranged on the outside of the outermost described ring rotation structure (1) of described Multi-stage ram gas compressor; Or described ring rotation dynamic structure body (4) is arranged on the inner side of the described ring rotation structure (1) of inner side of described Multi-stage ram gas compressor.
6. an application rights requires in 1 to 4 the motor of Multi-stage ram gas compressor described in any one, it is characterized in that: described power source is made as the ring rotation dynamic structure body (4) that inside is provided with pressed engine, described ring rotation dynamic structure body (4) is arranged on the outside of the outermost described ring rotation structure (1) of described Multi-stage ram gas compressor; Or described ring rotation dynamic structure body (4) is arranged on the inner side of the described ring rotation structure (1) of inner side of described Multi-stage ram gas compressor.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201310470696.XA CN103573654B (en) | 2012-10-13 | 2013-10-10 | A kind of Multi-stage ram compressor and apply its electromotor |
Applications Claiming Priority (4)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201210388654.7 | 2012-10-13 | ||
| CN201210388654 | 2012-10-13 | ||
| CN2012103886547 | 2012-10-13 | ||
| CN201310470696.XA CN103573654B (en) | 2012-10-13 | 2013-10-10 | A kind of Multi-stage ram compressor and apply its electromotor |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CN103573654A true CN103573654A (en) | 2014-02-12 |
| CN103573654B CN103573654B (en) | 2016-07-06 |
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| Application Number | Title | Priority Date | Filing Date |
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| CN201310470696.XA Active CN103573654B (en) | 2012-10-13 | 2013-10-10 | A kind of Multi-stage ram compressor and apply its electromotor |
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Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106382258A (en) * | 2016-12-06 | 2017-02-08 | 深圳福世达动力科技有限公司 | Centrifugal contra-rotating ram compressor |
Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US6032458A (en) * | 1997-10-24 | 2000-03-07 | James; Robert G. | Turbine powerplant having rotors with concentric rows of impeller blades |
| CN1653252A (en) * | 2001-08-20 | 2005-08-10 | 创新能量股份有限公司 | Rotary heat engine |
| US20100158665A1 (en) * | 2008-12-23 | 2010-06-24 | General Electric Company | Supersonic compressor |
| CN101936306A (en) * | 2009-06-25 | 2011-01-05 | 通用电气公司 | The supersonic compressor that comprises radial flow path |
| CN102278233A (en) * | 2010-07-07 | 2011-12-14 | 靳北彪 | Supersonic rotor engine |
-
2013
- 2013-10-10 CN CN201310470696.XA patent/CN103573654B/en active Active
Patent Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US6032458A (en) * | 1997-10-24 | 2000-03-07 | James; Robert G. | Turbine powerplant having rotors with concentric rows of impeller blades |
| CN1653252A (en) * | 2001-08-20 | 2005-08-10 | 创新能量股份有限公司 | Rotary heat engine |
| US20100158665A1 (en) * | 2008-12-23 | 2010-06-24 | General Electric Company | Supersonic compressor |
| CN101936306A (en) * | 2009-06-25 | 2011-01-05 | 通用电气公司 | The supersonic compressor that comprises radial flow path |
| CN102278233A (en) * | 2010-07-07 | 2011-12-14 | 靳北彪 | Supersonic rotor engine |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106382258A (en) * | 2016-12-06 | 2017-02-08 | 深圳福世达动力科技有限公司 | Centrifugal contra-rotating ram compressor |
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| Publication number | Publication date |
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| CN103573654B (en) | 2016-07-06 |
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Effective date of registration: 20200525 Address after: 215000 south of Lianyang road and east of Chang'an Road, Wujiang Economic and Technological Development Zone, Suzhou City, Jiangsu Province (Science and technology entrepreneurship Park) Patentee after: Wujiang science and Technology Pioneer Park Management Service Co., Ltd Address before: 100101, Beijing, Chaoyang District Beiyuan Road, 168, Sheng Sheng building, 24 floor Patentee before: MOLECULE POWER BEIJING TECH Co. |
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