GB2076061B - Mechanical and insulating connection between a nozzle and the filament-wound casing of the combustion chamber of a propeller - Google Patents

Mechanical and insulating connection between a nozzle and the filament-wound casing of the combustion chamber of a propeller

Info

Publication number
GB2076061B
GB2076061B GB8115197A GB8115197A GB2076061B GB 2076061 B GB2076061 B GB 2076061B GB 8115197 A GB8115197 A GB 8115197A GB 8115197 A GB8115197 A GB 8115197A GB 2076061 B GB2076061 B GB 2076061B
Authority
GB
United Kingdom
Prior art keywords
propeller
filament
nozzle
mechanical
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
Application number
GB8115197A
Other languages
English (en)
Other versions
GB2076061A (en
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
Publication of GB2076061A publication Critical patent/GB2076061A/en
Application granted granted Critical
Publication of GB2076061B publication Critical patent/GB2076061B/en
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)
GB8115197A 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 Expired GB2076061B (en)

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
GB2076061A GB2076061A (en) 1981-11-25
GB2076061B true GB2076061B (en) 1983-09-07

Family

ID=9242102

Family Applications (1)

Application Number Title Priority Date Filing Date
GB8115197A Expired 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

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
FR2482666B1 (fr) 1985-06-21
DE3119712A1 (de) 1982-03-04

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Legal Events

Date Code Title Description
PCNP Patent ceased through non-payment of renewal fee

Effective date: 19990518