AU2003298377A1 - Link between combustion chamber end wall and booster motor propeller nozzle - Google Patents

Link between combustion chamber end wall and booster motor propeller nozzle

Info

Publication number: AU2003298377A1
Authority: AU; Australia
Prior art keywords: link; combustion chamber; end wall; chamber end; booster motor
Prior art date: 2002-12-02
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.): Abandoned

Application number

AU2003298377A

Other versions

AU2003298377A8 (en

Inventor

Gilles Renoust

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.)

Safran Ceramics SA

Original Assignee

SNECMA Propulsion Solide 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.)

2002-12-02

Filing date

2003-12-01

Publication date

2004-06-30

2003-12-01 Application filed by SNECMA Propulsion Solide SA filed Critical SNECMA Propulsion Solide SA

2004-06-30 Publication of AU2003298377A8 publication Critical patent/AU2003298377A8/en

2004-06-30 Publication of AU2003298377A1 publication Critical patent/AU2003298377A1/en

Status Abandoned legal-status Critical Current

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)
Combustion Methods Of Internal-Combustion Engines (AREA)
Cylinder Crankcases Of Internal Combustion Engines (AREA)
Air Supply (AREA)

AU2003298377A 2002-12-02 2003-12-01 Link between combustion chamber end wall and booster motor propeller nozzle Abandoned AU2003298377A1 (en)

Applications Claiming Priority (3)

Application Number	Priority Date	Filing Date	Title
FR02/15158		2002-12-02
FR0215158A FR2847945B1 (en)	2002-12-02	2002-12-02	CONNECTION BETWEEN REAR BURNER OF COMBUSTION CHAMBER AND TUYERE OF FIRED ENGINE
PCT/FR2003/003538 WO2004053320A2 (en)	2002-12-02	2003-12-01	Link between combustion chamber end wall and booster motor propeller nozzle

Publications (2)

Publication Number	Publication Date
AU2003298377A8 AU2003298377A8 (en)	2004-06-30
AU2003298377A1 true AU2003298377A1 (en)	2004-06-30

Family

ID=32309920

Family Applications (1)

Application Number	Title	Priority Date	Filing Date
AU2003298377A Abandoned AU2003298377A1 (en)	2002-12-02	2003-12-01	Link between combustion chamber end wall and booster motor propeller nozzle

Country Status (9)

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

Families Citing this family (8)

* Cited by examiner, † Cited by third party
Publication number	Priority date	Publication date	Assignee	Title
RU2446307C1 (en) *	2010-10-21	2012-03-27	Открытое акционерное общество Научно-производственное объединение "Искра"	Adjustable solid-propellant rocket engine
RU2480611C1 (en) *	2012-01-11	2013-04-27	Открытое Акционерное Общество "Уральский научно-исследовательский институт композиционных материалов"	Manufacturing method of liquid-propellant engine chamber
RU2480610C1 (en) *	2012-01-11	2013-04-27	Открытое Акционерное Общество "Уральский научно-исследовательский институт композиционных материалов"	Liquid-propellant engine chamber
RU2496017C1 (en) *	2012-03-27	2013-10-20	Открытое акционерное общество Конструкторско-производственное предприятие "Авиамотор"	Seal of inner joint between gas turbine distributor and combustion chamber
CN104696104B (en) *	2013-12-10	2016-08-31	上海新力动力设备研究所	Solid propellant rocket baffle ring attachment structure
CN112594092A (en) *	2020-12-20	2021-04-02	西安航天化学动力有限公司	Connecting sleeve for solid rocket engine jet pipe and combustion chamber
CN114922741A (en) *	2022-04-28	2022-08-19	北京星际荣耀空间科技股份有限公司	Solid rocket motor snap ring connection structure, rocket motor and rocket
CN115523056B (en) *	2022-10-31	2024-06-04	北京中科宇航技术有限公司	Solid rocket engine connected by clamping ring

Family Cites Families (6)

* Cited by examiner, † Cited by third party
Publication number	Priority date	Publication date	Assignee	Title
DE1162637B (en) *	1961-03-15	1964-02-06	Thiokol Chemical Corp	Rocket engine
US5358262A (en) *	1992-10-09	1994-10-25	Rolls-Royce, Inc.	Multi-layer seal member
FR2722249B1 (en) *	1994-07-08	1996-10-04	Europ Propulsion	PROPELLER COMBUSTION CHAMBER WITH SEALED CONNECTION BETWEEN COMPOSITE TUBULAR STRUCTURE AND BOTTOM
US5657998A (en) *	1994-09-19	1997-08-19	General Electric Company	Gas-path leakage seal for a gas turbine
RU2084678C1 (en) *	1994-11-22	1997-07-20	Научно-производственное объединение "Искра"	Path member for high-temperature flow
RU2183762C1 (en) *	2000-12-07	2002-06-20	Государственное унитарное предприятие Машиностроительное конструкторское бюро "Факел" им. акад. П.Д. Грушина	Two-mode nozzle unit for rocket engine

2002
- 2002-12-02 FR FR0215158A patent/FR2847945B1/en not_active Expired - Fee Related
2003
- 2003-12-01 JP JP2004558142A patent/JP2006508296A/en not_active Withdrawn
- 2003-12-01 WO PCT/FR2003/003538 patent/WO2004053320A2/en not_active Ceased
- 2003-12-01 AU AU2003298377A patent/AU2003298377A1/en not_active Abandoned
- 2003-12-01 EP EP03796117A patent/EP1567761A2/en not_active Withdrawn
- 2003-12-01 UA UAA200505240A patent/UA81643C2/en unknown
- 2003-12-01 BR BR0316787-9A patent/BR0316787A/en not_active IP Right Cessation
- 2003-12-01 RU RU2005116972/06A patent/RU2330172C2/en not_active IP Right Cessation
2005
- 2005-05-30 IL IL168861A patent/IL168861A/en not_active IP Right Cessation

Also Published As

Publication number	Publication date
UA81643C2 (en)	2008-01-25
IL168861A (en)	2008-11-26
WO2004053320A3 (en)	2004-08-12
AU2003298377A8 (en)	2004-06-30
RU2005116972A (en)	2006-01-20
JP2006508296A (en)	2006-03-09
WO2004053320A2 (en)	2004-06-24
EP1567761A2 (en)	2005-08-31
FR2847945B1 (en)	2005-02-25
RU2330172C2 (en)	2008-07-27
FR2847945A1 (en)	2004-06-04
BR0316787A (en)	2005-11-01

Publication	Publication Date	Title
AU2001290510A1 (en)	2002-01-08	Extreme repetition rate gas discharge laser with improved blower motor
AU2003233159A1 (en)	2004-01-19	Orbiting combustion nozzle engine
AU2003266099A1 (en)	2004-03-29	Jet motor or turbine motor
AU2001292289A1 (en)	2002-04-08	Engine starter
AU2001292288A1 (en)	2002-04-08	Engine starter
AU2003271447A1 (en)	2004-04-23	Direct injection combustion chamber geometry
AU2002354155A1 (en)	2003-06-10	Engine controller
AUPR726801A0 (en)	2001-09-20	Engine
AU2002311751A1 (en)	2002-10-15	Fiber-reinforced rocket motor insulation
AU2003241691A1 (en)	2003-12-31	Ultrasonic jet burner
AU2003298377A1 (en)	2004-06-30	Link between combustion chamber end wall and booster motor propeller nozzle
AU2002212196A1 (en)	2002-03-22	Fire engine trailer
AU2003265299A1 (en)	2004-06-30	Hermetic motor and gas booster
AU2002350369A1 (en)	2003-07-30	Hot-air engine
AU2002213810A1 (en)	2002-04-08	Plasma jet ignition system
AU2002252206A1 (en)	2002-09-24	Air assist fuel nozzle
AU2002238050A1 (en)	2002-09-04	Air assist fuel injector
AU2002311144A1 (en)	2003-10-13	An air engine
AU2002339155A1 (en)	2003-06-10	Magnetic-powered engine
AUPR725801A0 (en)	2001-09-20	An efficient nozzle design
AU2002325555A1 (en)	2003-03-03	Jet engine using exhaust gas
AUPR741301A0 (en)	2001-09-20	An efficient nozzle
AUPQ985000A0 (en)	2000-09-28	Partial discharge injector
AU2001276283A1 (en)	2002-01-14	Axial piston engine
AUPR770501A0 (en)	2001-10-11	Axial engine

Legal Events

Date	Code	Title	Description
2005-09-15	MK6	Application lapsed section 142(2)(f)/reg. 8.3(3) - pct applic. not entering national phase