DE69525518D1 - Herstellung von Raketenkammern - Google Patents
Herstellung von RaketenkammernInfo
- Publication number
- DE69525518D1 DE69525518D1 DE69525518T DE69525518T DE69525518D1 DE 69525518 D1 DE69525518 D1 DE 69525518D1 DE 69525518 T DE69525518 T DE 69525518T DE 69525518 T DE69525518 T DE 69525518T DE 69525518 D1 DE69525518 D1 DE 69525518D1
- Authority
- DE
- Germany
- Prior art keywords
- manufacture
- rocket chambers
- rocket
- chambers
- 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.)
- Expired - Lifetime
Links
- 238000004519 manufacturing process Methods 0.000 title 1
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02K—JET-PROPULSION PLANTS
- F02K9/00—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof
- F02K9/42—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof using liquid or gaseous propellants
- F02K9/60—Constructional parts; Details not otherwise provided for
- F02K9/62—Combustion or thrust chambers
- F02K9/64—Combustion or thrust chambers having cooling arrangements
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
- Y10T29/00—Metal working
- Y10T29/49—Method of mechanical manufacture
- Y10T29/49346—Rocket or jet device making
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
- Y10T29/00—Metal working
- Y10T29/49—Method of mechanical manufacture
- Y10T29/4935—Heat exchanger or boiler making
- Y10T29/49364—Tube joined to flat sheet longitudinally, i.e., tube sheet
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Pressure Welding/Diffusion-Bonding (AREA)
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US08/346,646 US5546656A (en) | 1994-11-30 | 1994-11-30 | Fabrication of rocket thrust chambers |
Publications (2)
Publication Number | Publication Date |
---|---|
DE69525518D1 true DE69525518D1 (de) | 2002-03-28 |
DE69525518T2 DE69525518T2 (de) | 2002-11-28 |
Family
ID=23360381
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
DE69525518T Expired - Lifetime DE69525518T2 (de) | 1994-11-30 | 1995-11-27 | Herstellung von Raketenkammern |
Country Status (4)
Country | Link |
---|---|
US (1) | US5546656A (de) |
EP (1) | EP0720876B1 (de) |
JP (1) | JP3702376B2 (de) |
DE (1) | DE69525518T2 (de) |
Families Citing this family (13)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2733581B1 (fr) * | 1995-04-27 | 1997-07-18 | Europ Propulsion | Enceinte de combustion avec refroidissement par transpiration |
DE19845336A1 (de) | 1998-10-01 | 2000-04-06 | Behr Gmbh & Co | Mehrkanal-Flachrohr |
US6134782A (en) * | 1998-11-30 | 2000-10-24 | United Technologies Corporation | Method of forming a rocket thrust chamber |
US6131280A (en) * | 1998-11-30 | 2000-10-17 | United Technologies Corporation | Method of repairing a rocket thrust chamber |
DE19915082C1 (de) * | 1999-04-01 | 2000-07-13 | Daimler Chrysler Ag | Verfahren zur Herstellung einer gekühlten Düse für ein Raketentriebwerk |
US6421998B1 (en) * | 2000-06-13 | 2002-07-23 | The Boeing Company | Thruster device responsive to solar radiation |
EP1352169B1 (de) * | 2001-01-11 | 2008-04-30 | Volvo Aero Corporation | Raketentriebwerksglied und ein verfahren zur herstellung eines raketentriebwerksglieds |
US7213392B2 (en) | 2003-06-10 | 2007-05-08 | United Technologies Corporation | Rocket engine combustion chamber |
US7219505B2 (en) * | 2004-10-22 | 2007-05-22 | York International Corporation | Control stability system for moist air dehumidification units and method of operation |
EP3717768B1 (de) * | 2017-12-02 | 2022-12-14 | Aerojet Rocketdyne, Inc. | Kupferlegierungbrennkammer, die an der einspritzdüse durch einen nicht-kupfer-schweissübergangsring befestigt ist |
CN109604436B (zh) * | 2018-11-29 | 2020-11-03 | 湖北三江航天江北机械工程有限公司 | 液体火箭发动机推力室身部变截面异形单管的成形方法 |
DE102020124542A1 (de) * | 2020-09-21 | 2022-03-24 | Arianegroup Gmbh | Brennkammer mit schwingungsdämpfender Innenwandform und Verfahren zum Herstellen eines Brennkammerabschnitts |
CN114233516B (zh) * | 2021-12-23 | 2023-05-09 | 南京航空航天大学 | 一种具有再生冷却功能的复合材料爆震发动机燃烧室结构 |
Family Cites Families (15)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2968918A (en) * | 1949-08-22 | 1961-01-24 | California Inst Res Found | Rocket motor shell construction |
US3190070A (en) | 1950-04-05 | 1965-06-22 | Thiokol Chemical Corp | Reaction motor construction |
US3208132A (en) | 1962-04-13 | 1965-09-28 | William J D Escher | Method of making a multi-walled chamber |
US3349464A (en) * | 1962-06-29 | 1967-10-31 | Aerojet General Co | Method of making rocket combustion chamber |
DE1911642A1 (de) * | 1968-03-15 | 1969-10-16 | Man Turbo Gmbh | Verfahren zur Herstellung der Brennkammer und/oder der Schubduese eines Raketentriebwerkes |
FR2012723A1 (de) | 1968-07-11 | 1970-03-20 | Messerschmitt Boelkow Blohm | |
US3897316A (en) * | 1972-05-17 | 1975-07-29 | Us Air Force | Method for manufacturing a composite wall for a regeneratively cooled thrust chamber of a liquid propellant rocket engine |
JPS6082602A (ja) * | 1983-10-07 | 1985-05-10 | Natl Aerospace Lab | ロケツト燃焼器外筒製作法 |
JPS6082603A (ja) * | 1983-10-07 | 1985-05-10 | Natl Aerospace Lab | ロケツト燃焼器製作法 |
US4942653A (en) * | 1989-08-25 | 1990-07-24 | Rockwell International Corporation | Production method for a channeled wall thrust nozzle |
FR2669966B1 (fr) * | 1990-11-30 | 1993-03-26 | Europ Propulsion | Procede de fabrication de paroi de chambre de combustion, notamment pour moteur-fusee, et chambre de combustion obtenue par ce procede. |
US5386628A (en) * | 1991-12-23 | 1995-02-07 | United Technologies Corporation | Method of making a diffusion bonded rocket chamber |
US5371945A (en) * | 1991-12-23 | 1994-12-13 | United Technologies Corporation | Method of making a tubular combustion chamber construction |
US5375325A (en) * | 1992-05-26 | 1994-12-27 | United Technologies Corporation | Method of making a rocket chamber construction |
US5249357A (en) * | 1993-01-27 | 1993-10-05 | The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration | Method of fabricating a rocket engine combustion chamber |
-
1994
- 1994-11-30 US US08/346,646 patent/US5546656A/en not_active Expired - Lifetime
-
1995
- 1995-11-27 DE DE69525518T patent/DE69525518T2/de not_active Expired - Lifetime
- 1995-11-27 EP EP95308496A patent/EP0720876B1/de not_active Expired - Lifetime
- 1995-11-28 JP JP33121095A patent/JP3702376B2/ja not_active Expired - Fee Related
Also Published As
Publication number | Publication date |
---|---|
EP0720876A2 (de) | 1996-07-10 |
EP0720876B1 (de) | 2002-02-20 |
JP3702376B2 (ja) | 2005-10-05 |
EP0720876A3 (de) | 1996-12-04 |
JPH08210184A (ja) | 1996-08-20 |
US5546656A (en) | 1996-08-20 |
DE69525518T2 (de) | 2002-11-28 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
8364 | No opposition during term of opposition |