WO2004053320A3 - Liaison entre fond arriere de chambre de combustion et tuyere de moteur fusee - Google Patents
Liaison entre fond arriere de chambre de combustion et tuyere de moteur fusee Download PDFInfo
- Publication number
- WO2004053320A3 WO2004053320A3 PCT/FR2003/003538 FR0303538W WO2004053320A3 WO 2004053320 A3 WO2004053320 A3 WO 2004053320A3 FR 0303538 W FR0303538 W FR 0303538W WO 2004053320 A3 WO2004053320 A3 WO 2004053320A3
- Authority
- WO
- WIPO (PCT)
- Prior art keywords
- end wall
- link
- combustion chamber
- nozzle
- booster motor
- Prior art date
Links
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)
- Cylinder Crankcases Of Internal Combustion Engines (AREA)
- Air Supply (AREA)
- Combustion Methods Of Internal-Combustion Engines (AREA)
Abstract
Priority Applications (6)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
UAA200505240A UA81643C2 (ru) | 2002-12-02 | 2003-12-01 | Соединение между задней стенкой камеры сгорания и соплом ракетного двигателя |
EP03796117A EP1567761A2 (fr) | 2002-12-02 | 2003-12-01 | Liaison entre fond arriere de chambre de combustion et tuyere de moteur fusee |
BR0316787-9A BR0316787A (pt) | 2002-12-02 | 2003-12-01 | Ligação entre o fundo posterior da câmara de combustão e injetor de motor de propulsão |
AU2003298377A AU2003298377A1 (en) | 2002-12-02 | 2003-12-01 | Link between combustion chamber end wall and booster motor propeller nozzle |
JP2004558142A JP2006508296A (ja) | 2002-12-02 | 2003-12-01 | 燃焼室の後方端壁とロケットエンジンのノズルとの間の接続体 |
IL168861A IL168861A (en) | 2002-12-02 | 2005-05-30 | Connection between the rear end wall of a combustion chamber and the nozzle of a rocket engine |
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR02/15158 | 2002-12-02 | ||
FR0215158A FR2847945B1 (fr) | 2002-12-02 | 2002-12-02 | Liaison entre fond arriere de chambre de combustion et tuyere de moteur fusee |
Publications (2)
Publication Number | Publication Date |
---|---|
WO2004053320A2 WO2004053320A2 (fr) | 2004-06-24 |
WO2004053320A3 true WO2004053320A3 (fr) | 2004-08-12 |
Family
ID=32309920
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
PCT/FR2003/003538 WO2004053320A2 (fr) | 2002-12-02 | 2003-12-01 | Liaison entre fond arriere de chambre de combustion et tuyere de moteur fusee |
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) |
Families Citing this family (7)
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 |
RU2480610C1 (ru) * | 2012-01-11 | 2013-04-27 | Открытое Акционерное Общество "Уральский научно-исследовательский институт композиционных материалов" | Камера жидкостного ракетного двигателя |
RU2480611C1 (ru) * | 2012-01-11 | 2013-04-27 | Открытое Акционерное Общество "Уральский научно-исследовательский институт композиционных материалов" | Способ изготовления камеры жидкостного ракетного двигателя |
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 |
Citations (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR1283721A (fr) * | 1961-03-15 | 1962-02-02 | Thiokol Chemical Corp | Système de raccord séparable résistant à la pression |
US5358262A (en) * | 1992-10-09 | 1994-10-25 | Rolls-Royce, Inc. | Multi-layer seal member |
US5570573A (en) * | 1994-07-08 | 1996-11-05 | Societe Europeene De Propulsion | Combustion chamber for a thruster with a sealed connection between an end wall and a composite tubular structure |
US5657998A (en) * | 1994-09-19 | 1997-08-19 | General Electric Company | Gas-path leakage seal for a gas turbine |
-
2002
- 2002-12-02 FR FR0215158A patent/FR2847945B1/fr not_active Expired - Fee Related
-
2003
- 2003-12-01 RU RU2005116972/06A patent/RU2330172C2/ru not_active IP Right Cessation
- 2003-12-01 UA UAA200505240A patent/UA81643C2/ru unknown
- 2003-12-01 EP EP03796117A patent/EP1567761A2/fr not_active Withdrawn
- 2003-12-01 BR BR0316787-9A patent/BR0316787A/pt not_active IP Right Cessation
- 2003-12-01 AU AU2003298377A patent/AU2003298377A1/en not_active Abandoned
- 2003-12-01 WO PCT/FR2003/003538 patent/WO2004053320A2/fr active Application Filing
- 2003-12-01 JP JP2004558142A patent/JP2006508296A/ja not_active Withdrawn
-
2005
- 2005-05-30 IL IL168861A patent/IL168861A/en not_active IP Right Cessation
Patent Citations (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR1283721A (fr) * | 1961-03-15 | 1962-02-02 | Thiokol Chemical Corp | Système de raccord séparable résistant à la pression |
US5358262A (en) * | 1992-10-09 | 1994-10-25 | Rolls-Royce, Inc. | Multi-layer seal member |
US5570573A (en) * | 1994-07-08 | 1996-11-05 | Societe Europeene De Propulsion | Combustion chamber for a thruster with a sealed connection between an end wall and a composite tubular structure |
US5657998A (en) * | 1994-09-19 | 1997-08-19 | General Electric Company | Gas-path leakage seal for a gas turbine |
Also Published As
Publication number | Publication date |
---|---|
IL168861A (en) | 2008-11-26 |
EP1567761A2 (fr) | 2005-08-31 |
AU2003298377A1 (en) | 2004-06-30 |
FR2847945A1 (fr) | 2004-06-04 |
JP2006508296A (ja) | 2006-03-09 |
RU2005116972A (ru) | 2006-01-20 |
UA81643C2 (ru) | 2008-01-25 |
WO2004053320A2 (fr) | 2004-06-24 |
AU2003298377A8 (en) | 2004-06-30 |
RU2330172C2 (ru) | 2008-07-27 |
BR0316787A (pt) | 2005-11-01 |
FR2847945B1 (fr) | 2005-02-25 |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
EP0845634A3 (fr) | Chambre de combustion pour turbine à gaz et son procédé de fonctionnement | |
GB2317005B (en) | Gas turbine engine combustion chamber with thermal protective lining | |
GB2338086B (en) | Method of changing the operating mode of a direct-injection spark-ignition internal combustion engine | |
DE60013936D1 (de) | Abdichtung für das Endstück einer Gasturbinenbrennkammer | |
EP0648922B1 (fr) | Conduit d'échappement à motif isolé par une couche d'air pour moteurs à combustion interne | |
WO2002035072A3 (fr) | Turbine a gaz a coeur emboite | |
WO2004053320A3 (fr) | Liaison entre fond arriere de chambre de combustion et tuyere de moteur fusee | |
GB9410233D0 (en) | A gas turbine engine combustion chamber | |
GB0005772D0 (en) | Ducted fan gas turbine engine | |
WO2007038255A3 (fr) | Generateur de vapeur avec prechauffage et methode d'utilisation | |
DE602004000522D1 (de) | Rohrbündelraketentriebwerksbrennkammer mit einstückiger Ummantelung | |
DE69502984D1 (de) | Gasturbinenbrennkammer | |
CN212114628U (zh) | 一种具有防火性能的电缆保护套 | |
CN209747157U (zh) | 一种高柔性电缆 | |
CA2254099A1 (fr) | Procede de fabrication d'un isolant composite et d'un element de garnissage associe | |
CA2198442A1 (fr) | Lance thermique auto-extinguible | |
IT1285043B1 (it) | Candela riscaldante ad incandescenza, particolarmente per motori a ciclo diesel | |
CA2279615A1 (fr) | Systeme de demarrage pour moteur a essence | |
CN216871645U (zh) | 一种无卤低烟环保电缆 | |
ITTO980051A1 (it) | Stantuffo di motore a combustione interna. | |
KR200211087Y1 (ko) | 자동차의 배기 소음 방지용 구조 | |
KR20000016489U (ko) | 보일러용 연통구조 | |
KR200192436Y1 (ko) | 가스렌지의 버어너구조 | |
JPS6218957Y2 (fr) | ||
GB2293415B (en) | High thermal efficiency gas turbine engine |
Legal Events
Date | Code | Title | Description |
---|---|---|---|
AK | Designated states |
Kind code of ref document: A2 Designated state(s): AE AG AL AM AT AU AZ BA BB BG BR BW BY BZ CA CH CN CO CR CU CZ DE DK DM DZ EC EE EG ES FI GB GD GE GH GM HR HU ID IL IN IS JP KE KG KP KR KZ LC LK LR LS LT LU LV MA MD MG MK MN MW MX MZ NI NO NZ OM PG PH PL PT RO RU SC SD SE SG SK SL SY TJ TM TN TR TT TZ UA UG US UZ VC VN YU ZA ZM ZW |
|
AL | Designated countries for regional patents |
Kind code of ref document: A2 Designated state(s): BW GH GM KE LS MW MZ SD SL SZ TZ UG ZM ZW AM AZ BY KG KZ MD RU TJ TM AT BE BG CH CY CZ DE DK EE ES FI FR GB GR HU IE IT LU MC NL PT RO SE SI SK TR BF BJ CF CG CI CM GA GN GQ GW ML MR NE SN TD TG |
|
121 | Ep: the epo has been informed by wipo that ep was designated in this application | ||
WWE | Wipo information: entry into national phase |
Ref document number: 2003796117 Country of ref document: EP |
|
WWE | Wipo information: entry into national phase |
Ref document number: 168861 Country of ref document: IL |
|
WWE | Wipo information: entry into national phase |
Ref document number: 2004558142 Country of ref document: JP |
|
ENP | Entry into the national phase |
Ref document number: 2005116972 Country of ref document: RU Kind code of ref document: A |
|
WWP | Wipo information: published in national office |
Ref document number: 2003796117 Country of ref document: EP |
|
ENP | Entry into the national phase |
Ref document number: PI0316787 Country of ref document: BR |