AU2003298377A1 - Link between combustion chamber end wall and booster motor propeller nozzle - Google Patents
Link between combustion chamber end wall and booster motor propeller nozzleInfo
- Publication number
- AU2003298377A1 AU2003298377A1 AU2003298377A AU2003298377A AU2003298377A1 AU 2003298377 A1 AU2003298377 A1 AU 2003298377A1 AU 2003298377 A AU2003298377 A AU 2003298377A AU 2003298377 A AU2003298377 A AU 2003298377A AU 2003298377 A1 AU2003298377 A1 AU 2003298377A1
- Authority
- AU
- Australia
- Prior art keywords
- link
- combustion chamber
- end wall
- chamber end
- booster motor
- Prior art date
- 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
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)
- Combustion Methods Of Internal-Combustion Engines (AREA)
- Air Supply (AREA)
- Cylinder Crankcases Of Internal Combustion Engines (AREA)
Applications Claiming Priority (3)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR0215158A FR2847945B1 (en) | 2002-12-02 | 2002-12-02 | CONNECTION BETWEEN REAR BURNER OF COMBUSTION CHAMBER AND TUYERE OF FIRED ENGINE |
FR02/15158 | 2002-12-02 | ||
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 (6)
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 |
Family Cites Families (4)
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 |
-
2002
- 2002-12-02 FR FR0215158A patent/FR2847945B1/en not_active Expired - Fee Related
-
2003
- 2003-12-01 BR BR0316787-9A patent/BR0316787A/en not_active IP Right Cessation
- 2003-12-01 UA UAA200505240A patent/UA81643C2/en unknown
- 2003-12-01 RU RU2005116972/06A patent/RU2330172C2/en not_active IP Right Cessation
- 2003-12-01 JP JP2004558142A patent/JP2006508296A/en not_active Withdrawn
- 2003-12-01 WO PCT/FR2003/003538 patent/WO2004053320A2/en active Application Filing
- 2003-12-01 AU AU2003298377A patent/AU2003298377A1/en not_active Abandoned
- 2003-12-01 EP EP03796117A patent/EP1567761A2/en not_active Withdrawn
-
2005
- 2005-05-30 IL IL168861A patent/IL168861A/en not_active IP Right Cessation
Also Published As
Publication number | Publication date |
---|---|
IL168861A (en) | 2008-11-26 |
AU2003298377A8 (en) | 2004-06-30 |
BR0316787A (en) | 2005-11-01 |
FR2847945A1 (en) | 2004-06-04 |
UA81643C2 (en) | 2008-01-25 |
RU2005116972A (en) | 2006-01-20 |
WO2004053320A3 (en) | 2004-08-12 |
FR2847945B1 (en) | 2005-02-25 |
RU2330172C2 (en) | 2008-07-27 |
JP2006508296A (en) | 2006-03-09 |
WO2004053320A2 (en) | 2004-06-24 |
EP1567761A2 (en) | 2005-08-31 |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
AU2001290510A1 (en) | Extreme repetition rate gas discharge laser with improved blower motor | |
AU2002340071A1 (en) | Fuel injecton nozzle adapter | |
AU2003233159A1 (en) | Orbiting combustion nozzle engine | |
AU2001233160A1 (en) | Small engine driven generator | |
AU2002360877A1 (en) | Fire engine | |
AUPR726801A0 (en) | Engine | |
EP1331116A3 (en) | Air nozzle | |
AU2002311751A1 (en) | Fiber-reinforced rocket motor insulation | |
AU2003298377A1 (en) | Link between combustion chamber end wall and booster motor propeller nozzle | |
AU2003267323A1 (en) | Turbo-jet pump and water jet engine | |
AU2001279521A1 (en) | Piezoelectric motor | |
AU2002232208A1 (en) | Water jet propulsion outboard engine | |
AU4364600A (en) | Fuel pressure delay cylinder | |
AU2002350369A1 (en) | Hot-air engine | |
AU2003207347A1 (en) | Jet pump | |
AU2001230931A1 (en) | Jet pump | |
AU2002213810A1 (en) | Plasma jet ignition system | |
AU2002252206A1 (en) | Air assist fuel nozzle | |
AU2002238050A1 (en) | Air assist fuel injector | |
AU2002339155A1 (en) | Magnetic-powered engine | |
AU2002951477A0 (en) | Air injected engine | |
AU2001213411A1 (en) | Gas displaced chamber lift system having gas lift assist | |
AUPR725801A0 (en) | An efficient nozzle design | |
AU2002325555A1 (en) | Jet engine using exhaust gas | |
AU1323501A (en) | Nozzleless rocket motor |
Legal Events
Date | Code | Title | Description |
---|---|---|---|
MK6 | Application lapsed section 142(2)(f)/reg. 8.3(3) - pct applic. not entering national phase |