SE523633C2 - Dysförlängning - Google Patents

Dysförlängning

Info

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
Application number
SE0203504A
Other languages
English (en)
Swedish (sv)
Other versions
SE0203504D0 (sv
SE0203504L (sv
Inventor
Josef Groeber
Peter Hampl
Herbert Linner
Karl Brey
Bernhard Stahn
Original Assignee
Astrium Gmbh
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 Astrium Gmbh filed Critical Astrium Gmbh
Publication of SE0203504D0 publication Critical patent/SE0203504D0/xx
Publication of SE0203504L publication Critical patent/SE0203504L/
Publication of SE523633C2 publication Critical patent/SE523633C2/sv

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)
SE0203504A 2001-11-27 2002-11-26 Dysförlängning SE523633C2 (sv)

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)

* Cited by examiner, † Cited by third party
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)

* Cited by examiner, † Cited by third party
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

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