FR2744174B1 - Agencement de paroi pour des parois de propulseurs refroidies par circulation de propergols - Google Patents
Agencement de paroi pour des parois de propulseurs refroidies par circulation de propergolsInfo
- Publication number
- FR2744174B1 FR2744174B1 FR9700656A FR9700656A FR2744174B1 FR 2744174 B1 FR2744174 B1 FR 2744174B1 FR 9700656 A FR9700656 A FR 9700656A FR 9700656 A FR9700656 A FR 9700656A FR 2744174 B1 FR2744174 B1 FR 2744174B1
- Authority
- FR
- France
- Prior art keywords
- propergols
- propeller
- circulation
- wall arrangement
- cooled walls
- 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
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
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Filling Or Discharging Of Gas Storage Vessels (AREA)
- Laminated Bodies (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DE19602731A DE19602731C1 (de) | 1996-01-26 | 1996-01-26 | Wandstruktur für treibstoffgekühlte Triebwerkswände |
Publications (2)
Publication Number | Publication Date |
---|---|
FR2744174A1 FR2744174A1 (fr) | 1997-08-01 |
FR2744174B1 true FR2744174B1 (fr) | 1999-12-10 |
Family
ID=7783722
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
FR9700656A Expired - Lifetime FR2744174B1 (fr) | 1996-01-26 | 1997-01-23 | Agencement de paroi pour des parois de propulseurs refroidies par circulation de propergols |
Country Status (4)
Country | Link |
---|---|
US (1) | US5899060A (fr) |
JP (1) | JP3004930B2 (fr) |
DE (1) | DE19602731C1 (fr) |
FR (1) | FR2744174B1 (fr) |
Families Citing this family (22)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE19801407C2 (de) * | 1998-01-16 | 1999-12-02 | Daimler Chrysler Ag | Brennkammer für Hochleistungstriebwerke und Düsen |
DE19804232C2 (de) * | 1998-02-04 | 2000-06-29 | Daimler Chrysler Ag | Brennkammer für Hochleistungstriebwerke und Düsen |
DE19858197B4 (de) * | 1998-12-17 | 2005-05-04 | Eads Space Transportation Gmbh | Triebwerk |
DE10126923B4 (de) | 2001-06-01 | 2006-11-23 | Eads Space Transportation Gmbh | Raketentriebwerk mit Trennung von Innenmantel und Außenmantel |
DE10126926B4 (de) * | 2001-06-01 | 2015-02-19 | Astrium Gmbh | Brennkammer mit Innenmantel aus einem keramischen Komposit-Material und Verfahren zur Herstellung |
FR2836698B1 (fr) * | 2002-03-04 | 2005-02-11 | Eads Launch Vehicles | Chambre de combustion pour statoreacteur et statoreacteur pourvu d'une telle chambre de combustion |
DE60313455T2 (de) * | 2002-05-28 | 2008-01-03 | Volvo Aero Corp. | Wandkonstruktion |
ATE479017T1 (de) * | 2005-09-06 | 2010-09-15 | Volvo Aero Corp | Verfahren zur herstellung einer motorwandstruktur |
US7740161B2 (en) * | 2005-09-06 | 2010-06-22 | Volvo Aero Corporation | Engine wall structure and a method of producing an engine wall structure |
DE102005059502A1 (de) * | 2005-12-06 | 2007-06-14 | Deutsches Zentrum für Luft- und Raumfahrt e.V. | Heißkammer |
WO2008069705A1 (fr) | 2006-12-06 | 2008-06-12 | Volvo Aero Corporation | Chemise destinée à une section de turbine, section de turbine, moteur à turbine à gaz et un avion muni de celle-ci |
DE102007048527B4 (de) * | 2007-10-10 | 2014-03-27 | Bayern-Chemie Gesellschaft Für Flugchemische Antriebe Mbh | Schubtriebwerk |
US8453456B2 (en) * | 2009-03-25 | 2013-06-04 | United Technologies Corporation | Fuel-cooled flexible heat exchanger with thermoelectric device compression |
RU2517949C2 (ru) * | 2012-02-02 | 2014-06-10 | Федеральное государственное бюджетное образовательное учреждение высшего профессионального образования "Воронежский государственный технический университет" | Камера жидкосного ракетного двигателя |
RU2513059C2 (ru) * | 2012-02-02 | 2014-04-20 | Федеральное государственное бюджетное образовательное учреждение высшего профессионального образования "Воронежский государственный технический университет" | Тракт охлаждения теплонапряженных конструкций |
RU2516678C2 (ru) * | 2012-02-03 | 2014-05-20 | Федеральное государственное бюджетное образовательное учреждение высшего профессионального образования "Воронежский государственный технический университет" | Тракт регенеративного охлаждения камеры жидкостного ракетного двигателя |
RU2515576C2 (ru) * | 2012-02-03 | 2014-05-10 | Федеральное государственное бюджетное образовательное учреждение высшего профессионального образования "Воронежский государственный технический университет" | Сопло камеры жидкостного ракетного двигателя |
RU2516723C2 (ru) * | 2012-02-03 | 2014-05-20 | Федеральное государственное бюджетное образовательное учреждение высшего профессионального образования "Воронежский государственный технический университет" | Способ изготовления тракта регенеративного охлаждения камеры жидкостного ракетного двитателя |
US10471542B1 (en) * | 2017-06-27 | 2019-11-12 | United States Of America As Represented By The Administrator Of Nasa | Cladding and freeform deposition for coolant channel closeout |
JP7324096B2 (ja) * | 2019-09-13 | 2023-08-09 | 三菱重工業株式会社 | 冷却流路構造、バーナー及び熱交換器 |
EP3945245B1 (fr) * | 2020-07-27 | 2024-02-07 | Ansaldo Energia Switzerland AG | Composant de trajet de gaz chaud pour une turbine à gaz à échangeur de chaleur intégré |
CN113389657B (zh) * | 2021-07-27 | 2022-09-30 | 中国人民解放军国防科技大学 | 一种高温流体通道 |
Family Cites Families (18)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
NL69245C (fr) * | 1946-01-09 | |||
US3190070A (en) * | 1950-04-05 | 1965-06-22 | Thiokol Chemical Corp | Reaction motor construction |
DE1197689B (de) * | 1959-12-12 | 1965-07-29 | Boelkow Gmbh | Raketenbrennkammer |
US3242670A (en) * | 1962-08-27 | 1966-03-29 | United Aircraft Corp | Segmented baffle injector design |
US3267664A (en) * | 1963-03-19 | 1966-08-23 | North American Aviation Inc | Method of and device for cooling |
US3280850A (en) * | 1963-05-06 | 1966-10-25 | North American Aviation Inc | Hollow structural elements and methods for fabricating same |
US3493177A (en) * | 1967-07-26 | 1970-02-03 | Trw Inc | Method of and means for cooling the throat wall of rocket engine nozzle |
DE1751938B1 (de) * | 1968-08-21 | 1970-12-03 | Messerschmitt Boelkow Blohm | Verfahren zur Herstellung der Kuehlkanaele fuer Raketenbrennkammern mit konvergent-divergenter Schubduese |
US3798902A (en) * | 1968-08-21 | 1974-03-26 | Messerschmitt Boelkow Blohm | Arrangement of cooling channels for rocket engine combustion chambers |
DE2137109C3 (de) * | 1971-07-24 | 1980-04-30 | Messerschmitt-Boelkow-Blohm Gmbh, 8000 Muenchen | Herstellung einer regenerativ gekühlten Raketenbrennkammer |
US3832290A (en) * | 1972-09-14 | 1974-08-27 | Nasa | Method of electroforming a rocket chamber |
DE2418841C3 (de) * | 1974-04-19 | 1979-04-26 | Messerschmitt-Boelkow-Blohm Gmbh, 8000 Muenchen | Wärmetauscher, insbesondere regenerativ gekühlte Brennkammern für Flüssigkeitsraketentriebwerke und Verfahren zu ihrer Herstellung |
US4840226A (en) * | 1987-08-10 | 1989-06-20 | The United States Of America As Represented By The United States Department Of Energy | Corrosive resistant heat exchanger |
US5172548A (en) * | 1988-09-14 | 1992-12-22 | Societe Europeene De Propulsion | Device for tapping off hot gases from a combustion chamber and injector head equipped with such a device |
FR2664585B1 (fr) * | 1990-07-13 | 1993-08-06 | Europ Propulsion | Structures refractaires refroidies et procede pour leur fabrication. |
DE4115403A1 (de) * | 1991-05-10 | 1992-11-12 | Mtu Muenchen Gmbh | Duesenwand |
DE4137638C2 (de) * | 1991-11-15 | 1994-08-11 | Mtu Muenchen Gmbh | Bauteil mit einer vor thermischer Belastung zu schützenden Wand |
DE4443864A1 (de) * | 1994-12-09 | 1996-06-13 | Abb Management Ag | Gek}hltes Wandteil |
-
1996
- 1996-01-26 DE DE19602731A patent/DE19602731C1/de not_active Expired - Lifetime
-
1997
- 1997-01-22 US US08/787,389 patent/US5899060A/en not_active Expired - Lifetime
- 1997-01-23 FR FR9700656A patent/FR2744174B1/fr not_active Expired - Lifetime
- 1997-01-24 JP JP9011487A patent/JP3004930B2/ja not_active Expired - Lifetime
Also Published As
Publication number | Publication date |
---|---|
JP3004930B2 (ja) | 2000-01-31 |
FR2744174A1 (fr) | 1997-08-01 |
US5899060A (en) | 1999-05-04 |
JPH09217654A (ja) | 1997-08-19 |
DE19602731C1 (de) | 1997-07-10 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
PLFP | Fee payment |
Year of fee payment: 20 |