FR2588313B1 - DEVICE FOR COOLING THE WALLS OF A COMBUSTION CHAMBER - Google Patents

DEVICE FOR COOLING THE WALLS OF A COMBUSTION CHAMBER

Info

Publication number
FR2588313B1
FR2588313B1 FR8613375A FR8613375A FR2588313B1 FR 2588313 B1 FR2588313 B1 FR 2588313B1 FR 8613375 A FR8613375 A FR 8613375A FR 8613375 A FR8613375 A FR 8613375A FR 2588313 B1 FR2588313 B1 FR 2588313B1
Authority
FR
France
Prior art keywords
walls
cooling
combustion chamber
combustion
chamber
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 - Fee Related
Application number
FR8613375A
Other languages
French (fr)
Other versions
FR2588313A1 (en
Inventor
Schmidt Gunther
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Airbus Defence and Space GmbH
Original Assignee
Messerschmitt Bolkow Blohm AG
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by Messerschmitt Bolkow Blohm AG filed Critical Messerschmitt Bolkow Blohm AG
Publication of FR2588313A1 publication Critical patent/FR2588313A1/en
Application granted granted Critical
Publication of FR2588313B1 publication Critical patent/FR2588313B1/en
Anticipated expiration legal-status Critical
Expired - Fee Related legal-status Critical Current

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
FR8613375A 1985-10-07 1986-09-25 DEVICE FOR COOLING THE WALLS OF A COMBUSTION CHAMBER Expired - Fee Related FR2588313B1 (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DE19853535779 DE3535779C1 (en) 1985-10-07 1985-10-07 Arrangement for the cooling of rocket engine walls

Publications (2)

Publication Number Publication Date
FR2588313A1 FR2588313A1 (en) 1987-04-10
FR2588313B1 true FR2588313B1 (en) 1994-01-28

Family

ID=6282980

Family Applications (1)

Application Number Title Priority Date Filing Date
FR8613375A Expired - Fee Related FR2588313B1 (en) 1985-10-07 1986-09-25 DEVICE FOR COOLING THE WALLS OF A COMBUSTION CHAMBER

Country Status (3)

Country Link
JP (1) JPH0656134B2 (en)
DE (1) DE3535779C1 (en)
FR (1) FR2588313B1 (en)

Families Citing this family (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE4015204C1 (en) * 1990-05-11 1991-10-17 Mtu Muenchen Gmbh
DE4315256A1 (en) * 1993-05-07 1994-11-10 Mtu Muenchen Gmbh Device for distributing and supplying and removing a coolant to a wall of a turbo, in particular turbo ramjet engine
DE4321393C2 (en) * 1993-06-26 1996-08-22 Daimler Benz Aerospace Ag Wall structure, in particular for a ramjet engine
DE19617916B4 (en) * 1996-05-03 2007-02-01 Airbus Deutschland Gmbh Evaporator for evaporating a cryogenic liquid medium
DE19801407C2 (en) * 1998-01-16 1999-12-02 Daimler Chrysler Ag Combustion chamber for high-performance engines and nozzles
DE19804232C2 (en) 1998-02-04 2000-06-29 Daimler Chrysler Ag Combustion chamber for high-performance engines and nozzles
JP4844337B2 (en) * 2006-10-12 2011-12-28 浜名湖電装株式会社 Solenoid device and manufacturing method thereof

Family Cites Families (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE1019865B (en) * 1940-03-09 1957-11-21 Bayerische Motoren Werke Ag Cooling device for rocket motors
GB794660A (en) * 1954-08-30 1958-05-07 Havilland Engine Co Ltd Heat exchangers
US2975590A (en) * 1957-12-02 1961-03-21 Thiokol Chemical Corp Proportional coolant flow thrust chamber
DE1273907B (en) * 1966-10-27 1968-07-25 Boelkow Gmbh Thermally highly stressed components, such as rocket combustion chambers, with sweat cooling and processes for their production
US3578030A (en) * 1967-09-27 1971-05-11 Hitco Ablative and insulative structures
DE1751180A1 (en) * 1968-04-18 1971-04-29 Messerschmitt Boelkow Blohm Design and arrangement of an inlet ring or outlet collecting ring for thrust nozzles or combustion chambers of rocket engines, in particular liquid rocket engines
US3759443A (en) * 1971-06-16 1973-09-18 Nasa Thermal flux transfer system
DE2356572C3 (en) * 1973-11-13 1979-03-29 Messerschmitt-Boelkow-Blohm Gmbh, 8000 Muenchen Liquid-cooled rocket combustion chamber with thrust nozzle

Also Published As

Publication number Publication date
FR2588313A1 (en) 1987-04-10
JPS6293478A (en) 1987-04-28
DE3535779C1 (en) 1987-04-09
JPH0656134B2 (en) 1994-07-27

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Legal Events

Date Code Title Description
CA Change of address
CD Change of name or company name
ST Notification of lapse