FR2482666B1 - Liaison mecanique et isolante entre une tuyere et l'enveloppe bobinee de la chambre de combustion d'un propulseur - Google Patents

Liaison mecanique et isolante entre une tuyere et l'enveloppe bobinee de la chambre de combustion d'un propulseur

Info

Publication number
FR2482666B1
FR2482666B1 FR8011127A FR8011127A FR2482666B1 FR 2482666 B1 FR2482666 B1 FR 2482666B1 FR 8011127 A FR8011127 A FR 8011127A FR 8011127 A FR8011127 A FR 8011127A FR 2482666 B1 FR2482666 B1 FR 2482666B1
Authority
FR
France
Prior art keywords
propeller
nozzle
mechanical
combustion chamber
insulating connection
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
Application number
FR8011127A
Other languages
English (en)
Other versions
FR2482666A1 (fr
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.)
Societe Europeenne de Propulsion SEP SA
Original Assignee
Societe Europeenne de Propulsion SEP SA
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 Societe Europeenne de Propulsion SEP SA filed Critical Societe Europeenne de Propulsion SEP SA
Priority to FR8011127A priority Critical patent/FR2482666B1/fr
Priority to IT21782/81A priority patent/IT1135847B/it
Priority to DE19813119712 priority patent/DE3119712A1/de
Priority to GB8115197A priority patent/GB2076061B/en
Priority to CA000377798A priority patent/CA1175241A/fr
Priority to JP7434381A priority patent/JPS5716239A/ja
Publication of FR2482666A1 publication Critical patent/FR2482666A1/fr
Priority to US06/576,127 priority patent/US4967599A/en
Application granted granted Critical
Publication of FR2482666B1 publication Critical patent/FR2482666B1/fr
Expired 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
    • F02K9/08—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof using solid propellants
    • F02K9/32—Constructional parts; Details not otherwise provided for
    • 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
    • F02K9/08—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof using solid propellants
    • F02K9/32—Constructional parts; Details not otherwise provided for
    • F02K9/34—Casings; Combustion chambers; Liners thereof
    • F02K9/343—Joints, connections, seals therefor
    • 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

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Thermal Insulation (AREA)
  • Ceramic Products (AREA)
FR8011127A 1980-05-19 1980-05-19 Liaison mecanique et isolante entre une tuyere et l'enveloppe bobinee de la chambre de combustion d'un propulseur Expired FR2482666B1 (fr)

Priority Applications (7)

Application Number Priority Date Filing Date Title
FR8011127A FR2482666B1 (fr) 1980-05-19 1980-05-19 Liaison mecanique et isolante entre une tuyere et l'enveloppe bobinee de la chambre de combustion d'un propulseur
IT21782/81A IT1135847B (it) 1980-05-19 1981-05-18 Dispositivo di collegamento meccanico e isolante fra un ugello e l'involucro avvolto della camera di combustione di un propulsore
DE19813119712 DE3119712A1 (de) 1980-05-19 1981-05-18 Duesentriebwerk, insbesondere raketentriebwerk mit einer duese, die mit dem mantel der brennkammer mechanisch und waermeisoliert verbunden ist
GB8115197A GB2076061B (en) 1980-05-19 1981-05-18 Mechanical and insulating connection between a nozzle and the filament-wound casing of the combustion chamber of a propeller
CA000377798A CA1175241A (fr) 1980-05-19 1981-05-19 Raccord mecanique et isolant entre la decharge et l'enveloppe bobinee de la chambre de combustion d'un reacteur
JP7434381A JPS5716239A (en) 1980-05-19 1981-05-19 Casing nozzle combination structure
US06/576,127 US4967599A (en) 1980-05-19 1984-02-02 Mechanical and insulating connection between a nozzle and the filament-wound casing of the combustion chamber of a solid propellant rocket motor

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR8011127A FR2482666B1 (fr) 1980-05-19 1980-05-19 Liaison mecanique et isolante entre une tuyere et l'enveloppe bobinee de la chambre de combustion d'un propulseur

Publications (2)

Publication Number Publication Date
FR2482666A1 FR2482666A1 (fr) 1981-11-20
FR2482666B1 true FR2482666B1 (fr) 1985-06-21

Family

ID=9242102

Family Applications (1)

Application Number Title Priority Date Filing Date
FR8011127A Expired FR2482666B1 (fr) 1980-05-19 1980-05-19 Liaison mecanique et isolante entre une tuyere et l'enveloppe bobinee de la chambre de combustion d'un propulseur

Country Status (6)

Country Link
JP (1) JPS5716239A (fr)
CA (1) CA1175241A (fr)
DE (1) DE3119712A1 (fr)
FR (1) FR2482666B1 (fr)
GB (1) GB2076061B (fr)
IT (1) IT1135847B (fr)

Families Citing this family (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2706183B1 (fr) * 1993-06-07 1995-09-01 Europ Propulsion Dispositif de purge de résidus de combustion.
DE19915082C1 (de) * 1999-04-01 2000-07-13 Daimler Chrysler Ag Verfahren zur Herstellung einer gekühlten Düse für ein Raketentriebwerk
US11028802B2 (en) * 2016-11-14 2021-06-08 Northrop Grumman Systems Corporation Liquid rocket engine assemblies and related methods
RU2746081C1 (ru) * 2020-02-11 2021-04-06 Акционерное общество "Опытное конструкторское бюро "Новатор" Вкладыш соплового блока ракетного двигателя твердого топлива из углерод-кремнеземного композиционного материала
CN113250858A (zh) * 2021-04-21 2021-08-13 西安英利科电气科技有限公司 一种大开口固体火箭燃烧室的缠绕结构及方法

Family Cites Families (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3228186A (en) * 1962-08-27 1966-01-11 Thiokol Chemical Corp Combination self-restraining nozzle and exit cone for solid propellant rocket motors
US3212257A (en) * 1964-10-23 1965-10-19 Hercules Powder Co Ltd Rocket motor
US3648461A (en) * 1970-05-13 1972-03-14 Nasa Solid propellent rocket motor nozzle
US4063684A (en) * 1975-11-25 1977-12-20 The United States Of America As Represented By The Secretary Of The Air Force Composite rocket nozzle structure

Also Published As

Publication number Publication date
IT8121782A0 (it) 1981-05-18
DE3119712C2 (fr) 1992-02-06
GB2076061A (en) 1981-11-25
CA1175241A (fr) 1984-10-02
JPS64586B2 (fr) 1989-01-06
FR2482666A1 (fr) 1981-11-20
IT1135847B (it) 1986-08-27
JPS5716239A (en) 1982-01-27
GB2076061B (en) 1983-09-07
DE3119712A1 (de) 1982-03-04

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Legal Events

Date Code Title Description
TP Transmission of property