FR2309729A1 - Anneau collecteur de refrigerant pour propulseur-fusee - Google Patents

Anneau collecteur de refrigerant pour propulseur-fusee

Info

Publication number
FR2309729A1
FR2309729A1 FR7611709A FR7611709A FR2309729A1 FR 2309729 A1 FR2309729 A1 FR 2309729A1 FR 7611709 A FR7611709 A FR 7611709A FR 7611709 A FR7611709 A FR 7611709A FR 2309729 A1 FR2309729 A1 FR 2309729A1
Authority
FR
France
Prior art keywords
collection ring
cooling medium
sided
connecting flange
prevent displacement
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.)
Granted
Application number
FR7611709A
Other languages
English (en)
French (fr)
Other versions
FR2309729B1 (enExample
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 FR2309729A1 publication Critical patent/FR2309729A1/fr
Application granted granted Critical
Publication of FR2309729B1 publication Critical patent/FR2309729B1/fr
Granted legal-status Critical Current

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02KJET-PROPULSION PLANTS
    • F02K9/00Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof
    • F02K9/42Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof using liquid or gaseous propellants
    • F02K9/60Constructional parts; Details not otherwise provided for
    • F02K9/62Combustion or thrust chambers
    • F02K9/64Combustion 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)
  • Gasket Seals (AREA)
  • Connection Of Plates (AREA)
FR7611709A 1975-05-02 1976-04-21 Anneau collecteur de refrigerant pour propulseur-fusee Granted FR2309729A1 (fr)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DE19752519538 DE2519538C2 (de) 1975-05-02 1975-05-02 Verbindung zwischen dem Kühlmittel-Zulaufring und der Brennkammer-oder Schubdüsenwand eines Raketentriebwerks

Publications (2)

Publication Number Publication Date
FR2309729A1 true FR2309729A1 (fr) 1976-11-26
FR2309729B1 FR2309729B1 (enExample) 1980-04-18

Family

ID=5945560

Family Applications (1)

Application Number Title Priority Date Filing Date
FR7611709A Granted FR2309729A1 (fr) 1975-05-02 1976-04-21 Anneau collecteur de refrigerant pour propulseur-fusee

Country Status (3)

Country Link
JP (1) JPS51133613A (enExample)
DE (1) DE2519538C2 (enExample)
FR (1) FR2309729A1 (enExample)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
RU2519003C1 (ru) * 2013-04-09 2014-06-10 Открытое акционерное общество "Конструкторское бюро химавтоматики" Способ изготовления сопла камеры сгорания жидкостного ракетного двигателя

Families Citing this family (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE10237381B4 (de) * 2002-08-12 2005-06-23 Eads Space Transportation Gmbh Brennkammerstruktur und Verfahren zu deren Herstellung
RU2465483C1 (ru) * 2011-03-31 2012-10-27 Федеральное государственное унитарное предприятие "Государственный космический научно-производственный центр имени М.В. Хруничева" (ФГУП "ГКНПЦ им. М.В. Хруничева") Способ изготовления сопла камеры сгорания жидкостного ракетного двигателя (жрд)
CN107940157B (zh) * 2017-11-20 2020-07-24 西安航天动力研究所 一种再生冷却燃气导管及其加工方法
CN108979900A (zh) * 2018-08-29 2018-12-11 北京航天动力研究所 一种液体火箭发动机推力室身部的集液环
CN118188222B (zh) * 2024-04-25 2024-10-11 陕西天回航天技术有限公司 双夹层再生冷却与液膜冷却的复合方法、系统及发动机推力室

Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR1187946A (fr) * 1956-11-09 1959-09-17 Armstrong Siddeley Motors Ltd Chambre de combustion
FR1232288A (fr) * 1957-06-21 1960-10-06 Bristol Siddeley Engines Ltd Perfectionnements aux chambres de combustion
US3001726A (en) * 1959-06-23 1961-09-26 United Aircraft Corp Manifold attachment
US3062566A (en) * 1959-06-25 1962-11-06 United Aircraft Corp Manifold attachment to tubular wall
FR2058274A1 (enExample) * 1969-08-14 1971-05-28 Messerschmitt Boelkow Blohm
FR2250899A1 (enExample) * 1973-11-13 1975-06-06 Messerschmitt Boelkow Blohm

Family Cites Families (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE1751180A1 (de) * 1968-04-18 1971-04-29 Messerschmitt Boelkow Blohm Ausbildung und Anordnung eines Zulaufringes oder Ablaufsammelringes fuer Schubduesen oder Brennkammern von Raketentriebwerken,insbesondere Fluessigkeitsraketentriebwerken
DE6901525U (de) * 1969-01-16 1970-07-09 Messerschmitt Boelkow Blohm Vorrichtung zur verbindung des kuehlmitteleinlaufringes mit der wand einer raketenbrennkammer oder schubduese

Patent Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR1187946A (fr) * 1956-11-09 1959-09-17 Armstrong Siddeley Motors Ltd Chambre de combustion
FR1232288A (fr) * 1957-06-21 1960-10-06 Bristol Siddeley Engines Ltd Perfectionnements aux chambres de combustion
US3001726A (en) * 1959-06-23 1961-09-26 United Aircraft Corp Manifold attachment
US3062566A (en) * 1959-06-25 1962-11-06 United Aircraft Corp Manifold attachment to tubular wall
FR2058274A1 (enExample) * 1969-08-14 1971-05-28 Messerschmitt Boelkow Blohm
FR2250899A1 (enExample) * 1973-11-13 1975-06-06 Messerschmitt Boelkow Blohm

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
RU2519003C1 (ru) * 2013-04-09 2014-06-10 Открытое акционерное общество "Конструкторское бюро химавтоматики" Способ изготовления сопла камеры сгорания жидкостного ракетного двигателя

Also Published As

Publication number Publication date
FR2309729B1 (enExample) 1980-04-18
JPS51133613A (en) 1976-11-19
DE2519538C2 (de) 1982-12-30
DE2519538A1 (de) 1976-11-18

Similar Documents

Publication Publication Date Title
FR2333964A1 (fr) Tuyere de propulsion pour moteur a turbine a gaz
FR2309729A1 (fr) Anneau collecteur de refrigerant pour propulseur-fusee
GB1517418A (en) Sealed flange joint
GB1329497A (en) Internal combustion engine gas seal
ES426222A1 (es) Perfeccionamientos en los aparatos para soldar bridas a tu-bos.
GB1418739A (en) Method for making a branch connection to a pipe under pressure
ES444960A1 (es) Perfeccionamientos en dispositivos para el prensado de tu- bos.
GB1071382A (en) Exhaust silencer
FR2395401A1 (fr) Chambre de combustion pour une turbine a gaz
GB1454888A (en) Centre housing for a rotary piston internal combustion engine
GB1341280A (enExample)
FR2456217A1 (fr) Moteur-fusee
ES306254A1 (es) Perfeccionamientos en la construcciën de juntas tubulares para unir tubos de distintos diametros
GB1286925A (en) Method of assembling a junction piece to a planetary cooler tube on a rotary kiln
BE790710A (fr) Generateur pyrotechnique de gaz sous pression a charge de refroidissement solide
GB1142235A (en) Improvements in conduit flanges
GB1164725A (en) A Telescopic Conduit Connected Between the Exhaust of an Internal Combustion Engine and an Exhaust Gas Turbine
FR2320808A1 (fr) Machine pour le soudage de tubes bout a bout par resistance
GB1288680A (enExample)
GB1305516A (enExample)
FR2311246A1 (fr) Bride pour circuit de fluide a serrage auto-equilibre
FR2227784A5 (en) Jointing seal for large dia. concrete undersea piping - has compensation for misalignment of pipe ends
GB1297708A (enExample)
FR2411351A1 (fr) Accouplement pour conduites
GB1491391A (en) Engine having an oil cooled seal

Legal Events

Date Code Title Description
ST Notification of lapse