CN103057721A - Sealed barrel type steam catapult - Google Patents
Sealed barrel type steam catapult Download PDFInfo
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- CN103057721A CN103057721A CN2012102014283A CN201210201428A CN103057721A CN 103057721 A CN103057721 A CN 103057721A CN 2012102014283 A CN2012102014283 A CN 2012102014283A CN 201210201428 A CN201210201428 A CN 201210201428A CN 103057721 A CN103057721 A CN 103057721A
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- steam
- catapult
- turbo
- machine
- sealed
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Abstract
A sealed barrel type steam catapult is mainly applied to catapult-assisted take-off of a shipboard aircraft on an aircraft carrier. The sealed barrel type steam catapult has the advantages of being good in seal of the catapult process through adoption of a sealed barrel catapult method. Compared with an existing steam catapult which utilizes the sealed metal bar technology, the sealed barrel type steam catapult has the advantages of realizing technology and being simpler in structure, and more energy-saving through cyclic utilization of fresh water by adoption of a residue steam utilization method.
Description
Affiliated technical field
The present invention relates to a kind of ship-board aircraft catapult-launching gear, be mainly used in carrier-borne aircraft catapult-assisted take-off use on the aircraft carrier.
Background technology
Use at present the sliding formula deck technology that the jumps aircraft that takes off on China's aircraft carrier.The sliding formula deck start aircraft that jumps, have that the take-off process consume fuel is large, the early warning plane that can't take off, to problems such as weather are strict.Be difficult to solve the problems such as ejection process is airtight and disappointing and make steam catapult.
Summary of the invention
The objective of the invention is to solve fluting loses heart and sealing problem.The invention provides a kind of sealing cylindrical steam ejector, this sealing cylindrical steam ejector can not only solve fluting and lose heart and sealing problem, and can more save the energy resource consumption in the ejection process.
Above-mentioned purpose of the present invention is to realize by such technical scheme, it is a kind of sealing cylindrical steam ejector, it is characterized in that: in sealed chamber, use the Steam Actuation piston, piston conducts thrust to seesaw frame by power conduction frame, and seesaw frame is by the sealing cartridge type catapult technique of grapple cataplane.
The sealed chamber front end connects gas outlet, gas outlet will launch rear residual high pressure steam by aie escape valve control and send into turbo-machine, Steam Actuation turbo-machine, turbo-machine drive the electric generator generating, and steam condenses into the residual high pressure steam-electric power method that flows into steam generator behind the water by condenser.
Reverse valve connects strut bar, and strut bar forms the reverse anti-leakage valve device that reverse anti-leakage valve forms by stable plug connecting fluid press.
Connect the thermally induced flow pipe in the steam generator, the thermally induced flow pipe can be combined with nuclear reactor.
The invention has the beneficial effects as follows that can reduce ejection process steam seal and disappointing problem and reduce the ejection process degradation of energy, the while is simple in structure, the realization technology is simple.
Description of drawings
The present invention is further described below in conjunction with drawings and Examples.
Fig. 1 is the schematic diagram that the present invention seals the cylindrical steam ejector.
The specific embodiment
In Fig. 1, flight deck (1), deck (2), grapple (3), seesaw frame (4), buffer rack (5), cushion gas cylinder barrel (6), power conduction frame (7), reciprocal carriage (8), piston (9), cable wire (10), cable wire pulling gear (11), power-transfer clutch (12), motor (13), electric generator (14), condenser (15), reverse anti-leakage valve (16), thermally induced flow pipe (17), launch control cock (18), aie escape valve (19), turbo-machine (20), cylinder barrel (21), steam transmitter (22), reverse valve (23), launch control cock (24), strut bar (25), stable plug (26), hydraulic compressor (27), sealed chamber (28), gas outlet (29), reverse anti-leakage valve (30).
Sealing cartridge type catapult technique, the realization technical scheme is as follows: use Steam Actuation piston (9) in sealed chamber (28), piston (9) conducts thrust to seesaw frame (8) by power conduction frame (7), and seesaw frame (8) is by grapple (3) cataplane.
Residual high pressure steam-electric power method, the realization technical scheme is as follows: sealed chamber (28) front end connects gas outlet (29), gas outlet (29) will launch rear residual high pressure steam by aie escape valve (19) control and send into turbo-machine (20), Steam Actuation turbo-machine (20), turbo-machine (20) drives electric generator (14) generating, and steam flows into steam generator (22) after condensing into water by condenser (15).
Reverse anti-leakage valve device, realize that technical scheme is as follows: reverse valve (23) connects strut bar (25), and strut bar (25) forms reverse anti-leakage valve by stable plug (26) connecting fluid press (27).
Connect thermally induced flow pipe (17) in the steam generator (22), thermally induced flow pipe (17) can be combined with nuclear reactor.
Complete ejection process, specific implementation method: open reverse anti-leakage valve (30), the steam that steam transmitter (22) produces enters cylinder barrel (21), close reverse anti-leakage valve (30) after producing enough air pressure, open and launch control cock (24) and begin to launch, piston (9) is subject to the interior Steam Actuation of cylinder barrel (21), piston (9) conducts frame (7) with thrust by power thrust is passed to seesaw frame (4), seesaw frame (4) drives grapple (3) cataplane, seesaw frame (4) slides into flight deck (1) end and bangs into cushion gas cylinder barrel (6) damping by buffer rack (5), unclamps simultaneously grapple (3) and takes off.Open aie escape valve (19) after taking off, residual steam enters turbo-machine (20) and drives turbo-machine (20) rotation, turbo-machine (20) rotates and drives electric generator (14) generating, steam enters condenser (15) by turbo-machine (20) and condenses into water, and water enters steam generator by reverse anti-leakage valve (16).Electric generator (14) generating offers motor (13), motor (13) band running wire pulling gear (11) pulling cable wire (10), cable wire (10) retracts pre-ejection position with seesaw frame (4), closes to launch control cock (24) seized piston (9) and prepare to launch next time.
Claims (4)
1. a sealing cylindrical steam ejector is characterized in that, uses the Steam Actuation piston in sealed chamber, and piston conducts thrust to seesaw frame by power conduction frame, and seesaw frame is by the sealing cartridge type catapult technique of grapple cataplane.
2. one kind is sealed the cylindrical steam ejector, it is characterized in that, the sealed chamber front end connects gas outlet, gas outlet will launch rear residual high pressure steam by aie escape valve control and send into turbo-machine, the Steam Actuation turbo-machine, turbo-machine drives the electric generator generating, and steam condenses into the residual high pressure steam-electric power method that flows into steam generator behind the water by condenser.
3. a sealing cylindrical steam ejector is characterized in that reverse valve connects strut bar, and strut bar forms reverse anti-leakage valve by stable plug connecting fluid press.
4. a sealing cylindrical steam ejector is characterized in that connect the thermally induced flow pipe in the steam generator, the thermally induced flow pipe can be combined with nuclear reactor.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN2012102014283A CN103057721A (en) | 2012-06-04 | 2012-06-04 | Sealed barrel type steam catapult |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN2012102014283A CN103057721A (en) | 2012-06-04 | 2012-06-04 | Sealed barrel type steam catapult |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN103057721A true CN103057721A (en) | 2013-04-24 |
Family
ID=48100680
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN2012102014283A Pending CN103057721A (en) | 2012-06-04 | 2012-06-04 | Sealed barrel type steam catapult |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN103057721A (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN103420690A (en) * | 2013-08-27 | 2013-12-04 | 天紫环保投资控股有限公司 | System for using household garbage for making fertilizer rapidly |
| CN105964649A (en) * | 2013-08-27 | 2016-09-28 | 天紫环保投资控股有限公司 | Organic matter rubbish treatment system with arc-shaped guide plates |
Citations (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN2130985Y (en) * | 1992-04-10 | 1993-04-28 | 辽宁省铁岭阀门厂 | Liquid-controlled check butterfly valve |
| US5961069A (en) * | 1995-10-18 | 1999-10-05 | Dassault Aviation | Catapult exit shock absorber |
| CN102120497A (en) * | 2010-10-07 | 2011-07-13 | 朱炎炎 | Enclosed cylinder carrier aircraft steam catapult |
-
2012
- 2012-06-04 CN CN2012102014283A patent/CN103057721A/en active Pending
Patent Citations (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN2130985Y (en) * | 1992-04-10 | 1993-04-28 | 辽宁省铁岭阀门厂 | Liquid-controlled check butterfly valve |
| US5961069A (en) * | 1995-10-18 | 1999-10-05 | Dassault Aviation | Catapult exit shock absorber |
| CN102120497A (en) * | 2010-10-07 | 2011-07-13 | 朱炎炎 | Enclosed cylinder carrier aircraft steam catapult |
Non-Patent Citations (2)
| Title |
|---|
| 舰群: "蒸汽弹射器揭秘", 《舰载武器》, no. 12, 31 December 2008 (2008-12-31), pages 71 * |
| 野木惠: "水面舰艇核动力系统", 《现代舰船》, no. 12, 31 December 2010 (2010-12-31), pages 30 * |
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN103420690A (en) * | 2013-08-27 | 2013-12-04 | 天紫环保投资控股有限公司 | System for using household garbage for making fertilizer rapidly |
| CN103420690B (en) * | 2013-08-27 | 2015-10-07 | 天紫环保投资控股有限公司 | Utilize domestic refuse fast composting system |
| CN105964649A (en) * | 2013-08-27 | 2016-09-28 | 天紫环保投资控股有限公司 | Organic matter rubbish treatment system with arc-shaped guide plates |
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| DD01 | Delivery of document by public notice |
Addressee: Ye Feng Document name: Notification of Publication and of Entering the Substantive Examination Stage of the Application for Invention |
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| C53 | Correction of patent of invention or patent application | ||
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Address after: 510600 Guangdong State Taxation Bureau, 10 South Jing Road, Guangzhou, Guangdong, Tianhe District Applicant after: Ye Feng Address before: 516003, 8C, room 2, Xin Li Lou, third Xinxing garden, No. 13, Lake Zhang Road, Huicheng District, Guangdong, Huizhou Applicant before: Ye Feng |
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Addressee: Ye Feng Document name: Notification of Passing Examination on Formalities |
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| C53 | Correction of patent of invention or patent application | ||
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Address after: 516003, 8C, room 2, Xin Li Lou, third Xinxing garden, No. 13, Lake Zhang Road, Huicheng District, Guangdong, Huizhou Applicant after: Ye Feng Address before: 510600 Guangdong State Taxation Bureau, 10 South Jing Road, Guangzhou, Guangdong, Tianhe District Applicant before: Ye Feng |
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| DD01 | Delivery of document by public notice |
Addressee: Ye Feng Document name: Notification of Passing Examination on Formalities |
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| DD01 | Delivery of document by public notice |
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Application publication date: 20130424 |