FR2962493B1 - Chambre de propulsion de moteur-fusee et procede de fabrication d'une telle chambre - Google Patents

Chambre de propulsion de moteur-fusee et procede de fabrication d'une telle chambre

Info

Publication number
FR2962493B1
FR2962493B1 FR1055592A FR1055592A FR2962493B1 FR 2962493 B1 FR2962493 B1 FR 2962493B1 FR 1055592 A FR1055592 A FR 1055592A FR 1055592 A FR1055592 A FR 1055592A FR 2962493 B1 FR2962493 B1 FR 2962493B1
Authority
FR
France
Prior art keywords
chamber
manufacturing
engine propulsion
engine
propulsion 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
FR1055592A
Other languages
English (en)
Other versions
FR2962493A1 (fr
Inventor
Herve Goislot
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.)
Safran Aircraft Engines SAS
Original Assignee
SNECMA SAS
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 SNECMA SAS filed Critical SNECMA SAS
Priority to FR1055592A priority Critical patent/FR2962493B1/fr
Publication of FR2962493A1 publication Critical patent/FR2962493A1/fr
Application granted granted Critical
Publication of FR2962493B1 publication Critical patent/FR2962493B1/fr
Expired - Fee Related legal-status Critical Current
Anticipated expiration legal-status Critical

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
    • 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
    • F02K9/97—Rocket nozzles
    • F02K9/972—Fluid cooling arrangements for nozzles

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)
FR1055592A 2010-07-09 2010-07-09 Chambre de propulsion de moteur-fusee et procede de fabrication d'une telle chambre Expired - Fee Related FR2962493B1 (fr)

Priority Applications (1)

Application Number Priority Date Filing Date Title
FR1055592A FR2962493B1 (fr) 2010-07-09 2010-07-09 Chambre de propulsion de moteur-fusee et procede de fabrication d'une telle chambre

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR1055592A FR2962493B1 (fr) 2010-07-09 2010-07-09 Chambre de propulsion de moteur-fusee et procede de fabrication d'une telle chambre

Publications (2)

Publication Number Publication Date
FR2962493A1 FR2962493A1 (fr) 2012-01-13
FR2962493B1 true FR2962493B1 (fr) 2014-05-16

Family

ID=43727889

Family Applications (1)

Application Number Title Priority Date Filing Date
FR1055592A Expired - Fee Related FR2962493B1 (fr) 2010-07-09 2010-07-09 Chambre de propulsion de moteur-fusee et procede de fabrication d'une telle chambre

Country Status (1)

Country Link
FR (1) FR2962493B1 (fr)

Families Citing this family (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE102016215244A1 (de) * 2016-08-16 2018-02-22 Airbus Ds Gmbh Brennkammerstruktur, insbesondere für ein raketentriebwerk
CN106762227B (zh) * 2016-12-26 2018-02-06 西安航天发动机厂 一种液体火箭发动机推力室身部高温钎焊防变形转轴

Family Cites Families (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3780533A (en) * 1972-05-17 1973-12-25 Us Air Force Composite wall for a regeneratively cooled thrust chamber of a liquid propellant rocket engine
US4707225A (en) * 1986-01-06 1987-11-17 Rockwell International Corporation Fluid-cooled channel construction
US5075966A (en) * 1990-09-04 1991-12-31 General Electric Company Method for fabricating a hollow component for a rocket engine
EP1458968B1 (fr) * 2001-12-18 2007-07-18 Volvo Aero Corporation Composant destine a etre soumis a une charge thermique elevee au cours de son utilisation et procede de fabrication d'un tel composant
US6688100B1 (en) * 2002-07-16 2004-02-10 The Boeing Company Combustion chamber having a multiple-piece liner and associated assembly method

Also Published As

Publication number Publication date
FR2962493A1 (fr) 2012-01-13

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