CN104632465A - Stamping impinging stream engine - Google Patents
Stamping impinging stream engine Download PDFInfo
- Publication number
- CN104632465A CN104632465A CN201510005206.8A CN201510005206A CN104632465A CN 104632465 A CN104632465 A CN 104632465A CN 201510005206 A CN201510005206 A CN 201510005206A CN 104632465 A CN104632465 A CN 104632465A
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- punching press
- compression system
- pulse
- flow motor
- cavity
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Abstract
The invention discloses a stamping impinging stream engine. The stamping impinging stream engine comprises a pulse compression system, a cavity and a combustion chamber. The combustion chamber is arranged in the cavity. At least two spray tubes are arranged on the wall of the cavity and/or in the cavity, wherein the combustion chamber is used as the overall jet direction of the spray tubes, the jet streams of the spray tubes impinge one another, and working medium inlets of the spray tubes are communicated with a working medium high-pressure area of the gas inlet channel. The stamping impinging stream engine is simple in structure and high in efficiency.
Description
Technical field
The present invention relates to heat energy and dynamic field, especially a kind of punching press percussion flow motor.
Background technique
No matter be which kind of engine working substance all needs supercharging before being heated, in the name that on April 1st, 2010 applies for, the present inventor is called that gas piston pulse engine discloses and utilizes gas flow mutually to clash into, be heated (comprising burning) after making working medium produce high pressure, thus produce the thought of power.In order to the actual application level improving this kind of motor further needs to invent a kind of new motor.
Summary of the invention
In order to solve the problem, the technological scheme that the present invention proposes is as follows:
Scheme 1, a kind of punching press percussion flow motor, comprises pulse compression system, cavity and firing chamber, and described firing chamber is arranged in described cavity; Two or more is set on the wall of described cavity and/or in described cavity with described firing chamber for spraying overall sensing, and the jet pipe that jet flow is clashed into mutually; The working medium entrance of described jet pipe is communicated with the working medium zone of high pressure of described pulse compression system.
Scheme 2, on the basis of scheme 1, has at least a described jet pipe to be arranged in described cavity.
Scheme 3, on the basis of scheme 1, described cavity is set to propelling nozzle.
Scheme 4, on the basis of scheme 1, described cavity is set to Laval nozzle.
Scheme 5, on the basis of scheme 1, described pulse compression system is set to pressed engine pulse compression system.
Scheme 6, on the basis of scheme 5, described pulse compression system is set to pulse gas supplying formula displacement type compressor.
Scheme 7, on the basis of scheme 6, described pulse gas supplying formula displacement type compressor is set to piston compressor.
Scheme 8, on the basis of scheme 1, described pulse compression system is set to non-pulse displacement type compressor with pulse control valve or the non-pulse velocity profile gas compressor that is set to pulse control valve.
Scheme 9, on the basis of scheme 1, the sender property outlet of described cavity is communicated with the working medium entrance of acting mechanism.
Scheme 10, in scheme 1 to 9 either a program basis on, described pulse compression system and described cavity are arranged on solid of rotation.
In the present invention, so-called " acting mechanism " refers to that all can utilize gas working medium to expand and/or flow and produces the mechanism of power, such as piston type acting mechanism, turbine, lobed rotor motor etc.
In the present invention, so-called " with described firing chamber for spraying overall sensing " has both comprised with the central position of described firing chamber is completely accurate situation of spraying sensing, although also comprise the drift angle existed to a certain extent, substantially still with the situation that the central position of described firing chamber is pointed to for injection.
In the present invention, form combustion condition in described internal pressure of combustion chamber high moment, i.e. oil spout at this moment and/or light a fire at this moment.
In the present invention, fuel should be provided to described firing chamber, if need to light and should arrange ignition mechanism in described firing chamber.
In the present invention, according to the known technology of heat energy and dynamic field, necessary parts, unit or system etc. should be set in the place of necessity.
Beneficial effect of the present invention is as follows:
Punching press percussion flow engine structure disclosed in this invention is simple, efficiency is high.
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;
Shown in Fig. 4 is the structural representation of the embodiment of the present invention 4;
Shown in Fig. 5 is the structural representation of the embodiment of the present invention 5;
In figure:
1 pulse compression system, 2 cavitys, 3 firing chambers, 4 jet pipes, 5 working medium zone of high pressure, 6 Laval nozzles, 7 piston compressors, 8 solid of rotation.
Embodiment
Embodiment 1
Punching press percussion flow motor as shown in Figure 1, comprises pulse compression system 1, cavity 2 and firing chamber 3, and described firing chamber 3 is arranged in described cavity 2; The wall of described cavity 2 arranges two or more with described firing chamber 3 for spraying overall sensing, and the jet pipe 4 that jet flow is clashed into mutually; The working medium entrance of described jet pipe 4 is communicated with the working medium zone of high pressure 5 of described pulse compression system 1.
Embodiment 2
Punching press percussion flow motor as shown in Figure 2, comprises pulse compression system 1, cavity 2 and firing chamber 3, and described firing chamber 3 is arranged in described cavity 2; Two or more is set on the wall of described cavity 2 and in described cavity 2 with described firing chamber 3 for spraying overall sensing, and the jet pipe 4 that jet flow is clashed into mutually; The working medium entrance of described jet pipe 4 is communicated with the working medium zone of high pressure 5 of described pulse compression system 1.
As the mode of execution that can convert, also only described jet pipe 4 can be set in described cavity 2.
Embodiment 3
Punching press percussion flow motor as shown in Figure 3, the difference of itself and embodiment 1 is: described cavity 2 is set to Laval nozzle 6.
In the present invention, all mode of executions all can refer to the present embodiment, and described cavity 2 is set to Laval nozzle 6.
Embodiment 4
Punching press percussion flow motor as shown in Figure 4, the difference of itself and embodiment 1 is: described pulse compression system 1 is set to pulse gas supplying formula displacement type compressor, when specifically implementing, described pulse gas supplying formula displacement type compressor is set to piston compressor 7.
As the mode of execution that can convert, optionally described pulse compression system 1 can be set to the non-pulse displacement type compressor with pulse control valve.
As the mode of execution that can convert, also optionally described pulse compression system 1 can be set to the non-pulse velocity profile gas compressor with pulse control valve.
In the present invention, all mode of executions, all can refer to the present embodiment and arrange described pulse compression system 1.
Embodiment 5
Punching press percussion flow motor as shown in Figure 5, the difference of itself and embodiment 1 is: described pulse compression system 1 and described cavity 2 are arranged on solid of rotation 8.
In the present invention, all mode of executions, all can refer to the present embodiment, described pulse compression system 1 and described cavity 2 are arranged on solid of rotation 8.
In the present invention, all mode of executions, all optionally make the sender property outlet of the described cavity 2 of described punching press percussion flow motor be communicated with the working medium entrance of acting mechanism.
Obviously, the invention is not restricted to above embodiment, according to known technology and the technological scheme disclosed in this invention of related domain, can to derive or association goes out many flexible programs, all these flexible programs, also should think protection scope of the present invention.
Claims (10)
1. a punching press percussion flow motor, comprises pulse compression system (1), cavity (2) and firing chamber (3), it is characterized in that: described firing chamber (3) are arranged in described cavity (2); Two or more is set on the wall of described cavity (2) and/or in described cavity (2) with described firing chamber (3) for spraying overall sensing, and the jet pipe that jet flow is clashed into mutually (4); The working medium entrance of described jet pipe (4) is communicated with the working medium zone of high pressure (5) of described pulse compression system (1).
2. punching press percussion flow motor as claimed in claim 1, is characterized in that: have at least a described jet pipe (4) to be arranged in described cavity (2).
3. punching press percussion flow motor as claimed in claim 1, is characterized in that: described cavity (2) is set to propelling nozzle.
4. punching press percussion flow motor as claimed in claim 1, is characterized in that: described cavity (2) is set to Laval nozzle (6).
5. punching press percussion flow motor as claimed in claim 1, is characterized in that: described pulse compression system (1) is set to pressed engine pulse compression system.
6. punching press percussion flow motor as claimed in claim 5, is characterized in that: described pulse compression system (1) is set to pulse gas supplying formula displacement type compressor.
7. punching press percussion flow motor as claimed in claim 6, is characterized in that: described pulse gas supplying formula displacement type compressor is set to piston compressor (7).
8. punching press percussion flow motor as claimed in claim 1, is characterized in that: described pulse compression system (1) is set to non-pulse displacement type compressor with pulse control valve or the non-pulse velocity profile gas compressor that is set to pulse control valve.
9. punching press percussion flow motor as claimed in claim 1, is characterized in that: the sender property outlet of described cavity (2) is communicated with the working medium entrance of acting mechanism.
10. punching press percussion flow motor according to any one of claim 1 to 9, is characterized in that: described pulse compression system (1) and described cavity (2) are arranged on solid of rotation (8).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201510005206.8A CN104632465A (en) | 2014-01-06 | 2015-01-06 | Stamping impinging stream engine |
Applications Claiming Priority (5)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201410005357 | 2014-01-06 | ||
| CN2014100053579 | 2014-01-06 | ||
| CN201410018700 | 2014-01-15 | ||
| CN2014100187003 | 2014-01-15 | ||
| CN201510005206.8A CN104632465A (en) | 2014-01-06 | 2015-01-06 | Stamping impinging stream engine |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN104632465A true CN104632465A (en) | 2015-05-20 |
Family
ID=53211602
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201510005206.8A Pending CN104632465A (en) | 2014-01-06 | 2015-01-06 | Stamping impinging stream engine |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN104632465A (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109681344A (en) * | 2019-01-25 | 2019-04-26 | 北京星际荣耀空间科技有限公司 | Jet flow single point crash engine with compression and combustion and axial symmetry aircraft and lifting body aircraft |
Citations (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| EP1621753A1 (en) * | 2004-07-21 | 2006-02-01 | United Technologies Corporation | Energetic detonation propulsion |
| CN101205851A (en) * | 2007-12-05 | 2008-06-25 | 李文晓 | Combustion jet engine |
| CN101825041A (en) * | 2010-03-15 | 2010-09-08 | 靳北彪 | Gas piston pulse engine |
| CN101968012A (en) * | 2010-10-19 | 2011-02-09 | 靳北彪 | High-efficiency turbojet engine |
| CN103089486A (en) * | 2012-01-28 | 2013-05-08 | 摩尔动力(北京)技术股份有限公司 | Three-valve hot-air engine |
| CN103216358A (en) * | 2012-01-31 | 2013-07-24 | 摩尔动力(北京)技术股份有限公司 | Hot cylinder door control Stirling engine |
-
2015
- 2015-01-06 CN CN201510005206.8A patent/CN104632465A/en active Pending
Patent Citations (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| EP1621753A1 (en) * | 2004-07-21 | 2006-02-01 | United Technologies Corporation | Energetic detonation propulsion |
| CN101205851A (en) * | 2007-12-05 | 2008-06-25 | 李文晓 | Combustion jet engine |
| CN101825041A (en) * | 2010-03-15 | 2010-09-08 | 靳北彪 | Gas piston pulse engine |
| CN101968012A (en) * | 2010-10-19 | 2011-02-09 | 靳北彪 | High-efficiency turbojet engine |
| CN103089486A (en) * | 2012-01-28 | 2013-05-08 | 摩尔动力(北京)技术股份有限公司 | Three-valve hot-air engine |
| CN103216358A (en) * | 2012-01-31 | 2013-07-24 | 摩尔动力(北京)技术股份有限公司 | Hot cylinder door control Stirling engine |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109681344A (en) * | 2019-01-25 | 2019-04-26 | 北京星际荣耀空间科技有限公司 | Jet flow single point crash engine with compression and combustion and axial symmetry aircraft and lifting body aircraft |
| CN109681344B (en) * | 2019-01-25 | 2023-10-03 | 北京星际荣耀空间科技有限公司 | Jet single-point impact compression combustion engine, axisymmetric aircraft and lifting body aircraft |
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Application publication date: 20150520 |
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| RJ01 | Rejection of invention patent application after publication |