RU2330172C2 - Соединение между задней стенкой камеры сгорания и соплом ракетного двигателя - Google Patents

Соединение между задней стенкой камеры сгорания и соплом ракетного двигателя Download PDF

Info

Publication number
RU2330172C2
RU2330172C2 RU2005116972/06A RU2005116972A RU2330172C2 RU 2330172 C2 RU2330172 C2 RU 2330172C2 RU 2005116972/06 A RU2005116972/06 A RU 2005116972/06A RU 2005116972 A RU2005116972 A RU 2005116972A RU 2330172 C2 RU2330172 C2 RU 2330172C2
Authority
RU
Russia
Prior art keywords
cord
rear wall
thermal barrier
nozzle
compound according
Prior art date
Application number
RU2005116972/06A
Other languages
English (en)
Russian (ru)
Other versions
RU2005116972A (ru
Inventor
Жилль РЕНУ (FR)
Жилль РЕНУ
Original Assignee
Снекма Пропюльсьон Солид
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 Снекма Пропюльсьон Солид filed Critical Снекма Пропюльсьон Солид
Publication of RU2005116972A publication Critical patent/RU2005116972A/ru
Application granted granted Critical
Publication of RU2330172C2 publication Critical patent/RU2330172C2/ru

Links

Images

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16J—PISTONS; CYLINDERS; SEALINGS
    • F16J15/00—Sealings
    • F16J15/02—Sealings between relatively-stationary surfaces
    • F16J15/06—Sealings between relatively-stationary surfaces with solid packing compressed between sealing surfaces
    • F16J15/08—Sealings between relatively-stationary surfaces with solid packing compressed between sealing surfaces with exclusively metal packing
    • F16J15/0806—Sealings between relatively-stationary surfaces with solid packing compressed between sealing surfaces with exclusively metal packing characterised by material or surface treatment
    • F16J15/0812—Sealings between relatively-stationary surfaces with solid packing compressed between sealing surfaces with exclusively metal packing characterised by material or surface treatment with a braided or knitted body
    • 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
    • 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
    • F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16J—PISTONS; CYLINDERS; SEALINGS
    • F16J15/00—Sealings
    • F16J15/02—Sealings between relatively-stationary surfaces
    • F16J15/06—Sealings between relatively-stationary surfaces with solid packing compressed between sealing surfaces
    • F16J15/064—Sealings between relatively-stationary surfaces with solid packing compressed between sealing surfaces the packing combining the sealing function with other functions
    • F16J15/065—Sealings between relatively-stationary surfaces with solid packing compressed between sealing surfaces the packing combining the sealing function with other functions fire resistant
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2300/00—Materials; Properties thereof
    • F05D2300/60—Properties or characteristics given to material by treatment or manufacturing
    • F05D2300/614—Fibres or filaments

Landscapes

  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Gasket Seals (AREA)
  • Air Supply (AREA)
  • Cylinder Crankcases Of Internal Combustion Engines (AREA)
  • Combustion Methods Of Internal-Combustion Engines (AREA)
RU2005116972/06A 2002-12-02 2003-12-01 Соединение между задней стенкой камеры сгорания и соплом ракетного двигателя RU2330172C2 (ru)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR0215158A FR2847945B1 (fr) 2002-12-02 2002-12-02 Liaison entre fond arriere de chambre de combustion et tuyere de moteur fusee
FR02/15158 2002-12-02

Publications (2)

Publication Number Publication Date
RU2005116972A RU2005116972A (ru) 2006-01-20
RU2330172C2 true RU2330172C2 (ru) 2008-07-27

Family

ID=32309920

Family Applications (1)

Application Number Title Priority Date Filing Date
RU2005116972/06A RU2330172C2 (ru) 2002-12-02 2003-12-01 Соединение между задней стенкой камеры сгорания и соплом ракетного двигателя

Country Status (9)

Country Link
EP (1) EP1567761A2 (fr)
JP (1) JP2006508296A (fr)
AU (1) AU2003298377A1 (fr)
BR (1) BR0316787A (fr)
FR (1) FR2847945B1 (fr)
IL (1) IL168861A (fr)
RU (1) RU2330172C2 (fr)
UA (1) UA81643C2 (fr)
WO (1) WO2004053320A2 (fr)

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
RU2446307C1 (ru) * 2010-10-21 2012-03-27 Открытое акционерное общество Научно-производственное объединение "Искра" Ракетный двигатель твердого топлива
RU2480611C1 (ru) * 2012-01-11 2013-04-27 Открытое Акционерное Общество "Уральский научно-исследовательский институт композиционных материалов" Способ изготовления камеры жидкостного ракетного двигателя
RU2480610C1 (ru) * 2012-01-11 2013-04-27 Открытое Акционерное Общество "Уральский научно-исследовательский институт композиционных материалов" Камера жидкостного ракетного двигателя

Families Citing this family (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
RU2496017C1 (ru) * 2012-03-27 2013-10-20 Открытое акционерное общество Конструкторско-производственное предприятие "Авиамотор" Уплотнение внутреннего стыка камеры сгорания и соплового аппарата турбины газотурбинного двигателя
CN104696104B (zh) * 2013-12-10 2016-08-31 上海新力动力设备研究所 固体火箭发动机挡环连接结构
CN112594092A (zh) * 2020-12-20 2021-04-02 西安航天化学动力有限公司 固体火箭发动机喷管与燃烧室的连接套筒
CN115523056B (zh) * 2022-10-31 2024-06-04 北京中科宇航技术有限公司 一种卡环连接的固体火箭发动机

Family Cites Families (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE1162637B (de) * 1961-03-15 1964-02-06 Thiokol Chemical Corp Raketentriebwerk
US5358262A (en) * 1992-10-09 1994-10-25 Rolls-Royce, Inc. Multi-layer seal member
FR2722249B1 (fr) * 1994-07-08 1996-10-04 Europ Propulsion Chambre de combustion de propulseur avec liaison etanche entre structure tubulaire composite et fond
US5657998A (en) * 1994-09-19 1997-08-19 General Electric Company Gas-path leakage seal for a gas turbine

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
RU2446307C1 (ru) * 2010-10-21 2012-03-27 Открытое акционерное общество Научно-производственное объединение "Искра" Ракетный двигатель твердого топлива
RU2480611C1 (ru) * 2012-01-11 2013-04-27 Открытое Акционерное Общество "Уральский научно-исследовательский институт композиционных материалов" Способ изготовления камеры жидкостного ракетного двигателя
RU2480610C1 (ru) * 2012-01-11 2013-04-27 Открытое Акционерное Общество "Уральский научно-исследовательский институт композиционных материалов" Камера жидкостного ракетного двигателя

Also Published As

Publication number Publication date
JP2006508296A (ja) 2006-03-09
AU2003298377A1 (en) 2004-06-30
UA81643C2 (ru) 2008-01-25
WO2004053320A2 (fr) 2004-06-24
FR2847945B1 (fr) 2005-02-25
FR2847945A1 (fr) 2004-06-04
RU2005116972A (ru) 2006-01-20
IL168861A (en) 2008-11-26
AU2003298377A8 (en) 2004-06-30
EP1567761A2 (fr) 2005-08-31
BR0316787A (pt) 2005-11-01
WO2004053320A3 (fr) 2004-08-12

Similar Documents

Publication Publication Date Title
RU2224155C2 (ru) Вложенное уплотнение моста
US5705777A (en) Refrigeration compressor muffler
US5358262A (en) Multi-layer seal member
US20060272321A1 (en) Slip joint exhaust manifolds
RU2330172C2 (ru) Соединение между задней стенкой камеры сгорания и соплом ракетного двигателя
US7858879B2 (en) Insulated article and method of making same
US8714558B2 (en) Welded bellows seal assembly
US5570573A (en) Combustion chamber for a thruster with a sealed connection between an end wall and a composite tubular structure
RU2380546C2 (ru) Газотурбинный двигатель, содержащий два узла, соединенных под осевым усилием
WO2014158732A1 (fr) Petit élément d'étanchéité élastique à l'intérieur d'un bosselage d'étanchéité de combustion principal
CA1216608A (fr) Raccords de dilatation pour ambiances dangereuses
KR19990066831A (ko) 감쇄장치용 통합 플랜지-메쉬 링 조립체
US20040201180A1 (en) Exhaust pipe flange ring gasket
US6708983B2 (en) Spiral wound cylinder head gasket
US10995650B2 (en) Heat shield for bellows
US9284889B2 (en) Flexible seal system for a gas turbine engine
US20150020912A1 (en) Duct
EP3483505B1 (fr) Chambre de combustion de turbine à gaz
US6394140B1 (en) Gasket
US9657840B2 (en) Multi-layer gasket assembly
RU2721395C1 (ru) Экранно-вакуумная теплоизоляция ракетного двигателя малой тяги
SU1588965A1 (ru) Уплотнение фланцевого соединени
RU2208695C2 (ru) Заряд твёрдого топлива
KR200313052Y1 (ko) 엔진 배기가스 충격흡수용 튜브
RU2191939C1 (ru) Фланцевый разъем

Legal Events

Date Code Title Description
MM4A The patent is invalid due to non-payment of fees

Effective date: 20091202