SE523633C2 - Dysförlängning - Google Patents
DysförlängningInfo
- Publication number
- SE523633C2 SE523633C2 SE0203504A SE0203504A SE523633C2 SE 523633 C2 SE523633 C2 SE 523633C2 SE 0203504 A SE0203504 A SE 0203504A SE 0203504 A SE0203504 A SE 0203504A SE 523633 C2 SE523633 C2 SE 523633C2
- Authority
- SE
- Sweden
- Prior art keywords
- nozzle
- flange
- extension
- exhaust pipe
- section
- Prior art date
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
- F02K9/97—Rocket nozzles
- F02K9/976—Deployable nozzles
-
- 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)
- Inorganic Fibers (AREA)
- Ceramic Products (AREA)
- Nozzles (AREA)
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DE10157752A DE10157752B4 (de) | 2001-11-27 | 2001-11-27 | Düsenverlängerung |
Publications (3)
Publication Number | Publication Date |
---|---|
SE0203504D0 SE0203504D0 (sv) | 2002-11-26 |
SE0203504L SE0203504L (sv) | 2003-05-28 |
SE523633C2 true SE523633C2 (sv) | 2004-05-04 |
Family
ID=7706890
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
SE0203504A SE523633C2 (sv) | 2001-11-27 | 2002-11-26 | Dysförlängning |
Country Status (5)
Country | Link |
---|---|
US (1) | US6817184B2 (de) |
DE (1) | DE10157752B4 (de) |
FR (1) | FR2832762B1 (de) |
IT (1) | ITMI20022423A1 (de) |
SE (1) | SE523633C2 (de) |
Families Citing this family (17)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2840030B1 (fr) * | 2002-05-21 | 2005-03-04 | Eads Launch Vehicles | Moteur a tuyere a noyau central pour lanceur spatial |
FR2916018B1 (fr) * | 2007-05-10 | 2009-08-21 | Snecma Propulsion Solide Sa | Systeme d'echappement pour turbine a gaz |
DE102008020198B8 (de) * | 2008-04-15 | 2015-05-13 | Astrium Gmbh | Düsenerweiterung für ein Triebwerk und Verfahren zur Herstellung und Kühlung einer Düsenerweiterung |
FR2934014B1 (fr) * | 2008-07-17 | 2011-05-13 | Snecma Propulsion Solide | Procede de realisation d'une tuyere ou d'un divergent de tuyere en materiau composite. |
US8281603B2 (en) * | 2008-08-11 | 2012-10-09 | United Technologies Corporation | Fastener assembly for connecting rocket engine nozzles |
FR2949821B1 (fr) * | 2009-09-10 | 2011-09-30 | Snecma | Moteur fusee a divergent deployable |
DE102011011220A1 (de) * | 2011-02-15 | 2012-08-16 | Astrium Gmbh | Raketentriebwerk mit einer ausfahrbaren Düsenerweiterung |
FR3008139B1 (fr) * | 2013-07-04 | 2015-07-24 | Snecma | Dispositif et procede de liaison |
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 |
WO2017222908A1 (en) * | 2016-06-21 | 2017-12-28 | Aerojet Rocketdyne, Inc. | Liquid propellant rocket engine with passive condensate cooling |
FR3053403B1 (fr) * | 2016-06-29 | 2018-07-27 | Arianegroup Sas | Moteur-fusee a divergent composite |
FR3056256B1 (fr) * | 2016-09-20 | 2020-11-06 | Airbus Safran Launchers | Moteur-fusee a divergent segmente |
US11028802B2 (en) | 2016-11-14 | 2021-06-08 | Northrop Grumman Systems Corporation | Liquid rocket engine assemblies and related methods |
US10471542B1 (en) * | 2017-06-27 | 2019-11-12 | United States Of America As Represented By The Administrator Of Nasa | Cladding and freeform deposition for coolant channel closeout |
FR3094414B1 (fr) * | 2019-03-27 | 2021-04-09 | Arianegroup Sas | Tuyère équipée d’une couronne thermo-régulée |
CN112523902A (zh) * | 2020-11-30 | 2021-03-19 | 内蒙动力机械研究所 | 一种基于3d打印的喷管用复合材料固定壳体 |
CN115182828B (zh) * | 2022-06-27 | 2024-09-10 | 西安鑫垚陶瓷复合材料股份有限公司 | 一种陶瓷基复合材料喷管法兰及其制备方法 |
Family Cites Families (15)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3596465A (en) * | 1970-03-12 | 1971-08-03 | Nasa | Inflatable transpiration cooled nozzle |
US3648461A (en) * | 1970-05-13 | 1972-03-14 | Nasa | Solid propellent rocket motor nozzle |
US3866792A (en) * | 1973-03-02 | 1975-02-18 | Hercules Inc | Integral filament reinforced composite-rocket chamber/adapter |
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 |
US4182495A (en) * | 1978-12-04 | 1980-01-08 | The United States Of America As Represented By The Secretary Of The Navy | Graphite or carbon fiber composite structure, low temperature cure |
US4967599A (en) * | 1980-05-19 | 1990-11-06 | Societe Europeenne De Propulsion | Mechanical and insulating connection between a nozzle and the filament-wound casing of the combustion chamber of a solid propellant rocket motor |
US4383407A (en) * | 1981-02-02 | 1983-05-17 | Thiokol Corporation | Extendible thrust nozzle for rockets |
US4477024A (en) * | 1983-04-05 | 1984-10-16 | The United States Of America As Represented By The Secretary Of The Air Force | Carbon/carbon rocket motor exit cone reinforcement |
US5540949A (en) * | 1986-04-24 | 1996-07-30 | The United States Of America As Represented By The Secretary Of The Air Force | Method for cutting threads in a carbon-carbon structure |
FR2652615B1 (fr) * | 1989-10-04 | 1992-02-07 | Europ Propulsion | Chambre de combustion de propulseur. |
US6324833B1 (en) * | 1990-04-24 | 2001-12-04 | Cordant Technologies, Inc. | Reinforced composite articles and method of making same |
US5113540A (en) * | 1991-07-03 | 1992-05-19 | Sereboff Joel L | Fluid cushion with passages for ischial spines |
DE19632893C2 (de) * | 1996-08-16 | 2001-02-08 | Industrieanlagen Betr Sgmbh Ia | Verfahren zur Herstellung von Flugkörperkomponenten aus faserverstärkter Keramik |
DE19730674A1 (de) * | 1997-07-17 | 1999-01-21 | Deutsch Zentr Luft & Raumfahrt | Brennkammer und Verfahren zur Herstellung einer Brennkammer |
DE19858197B4 (de) * | 1998-12-17 | 2005-05-04 | Eads Space Transportation Gmbh | Triebwerk |
-
2001
- 2001-11-27 DE DE10157752A patent/DE10157752B4/de not_active Expired - Fee Related
-
2002
- 2002-11-15 IT IT002423A patent/ITMI20022423A1/it unknown
- 2002-11-26 US US10/306,147 patent/US6817184B2/en not_active Expired - Lifetime
- 2002-11-26 SE SE0203504A patent/SE523633C2/sv not_active IP Right Cessation
- 2002-11-27 FR FR0214852A patent/FR2832762B1/fr not_active Expired - Fee Related
Also Published As
Publication number | Publication date |
---|---|
FR2832762A1 (fr) | 2003-05-30 |
DE10157752B4 (de) | 2006-04-06 |
DE10157752A1 (de) | 2003-06-18 |
SE0203504D0 (sv) | 2002-11-26 |
US20030136128A1 (en) | 2003-07-24 |
US6817184B2 (en) | 2004-11-16 |
SE0203504L (sv) | 2003-05-28 |
ITMI20022423A1 (it) | 2003-05-28 |
FR2832762B1 (fr) | 2007-11-02 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
NUG | Patent has lapsed |