SE0702896L - En komponent avsedd att utsättas för hög termisk last vid drift - Google Patents
En komponent avsedd att utsättas för hög termisk last vid driftInfo
- Publication number
- SE0702896L SE0702896L SE0702896A SE0702896A SE0702896L SE 0702896 L SE0702896 L SE 0702896L SE 0702896 A SE0702896 A SE 0702896A SE 0702896 A SE0702896 A SE 0702896A SE 0702896 L SE0702896 L SE 0702896L
- Authority
- SE
- Sweden
- Prior art keywords
- wall structure
- during operation
- high thermal
- thermal load
- load during
- Prior art date
Links
- 238000001816 cooling Methods 0.000 abstract 3
- 239000002826 coolant Substances 0.000 abstract 2
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
- F02K9/42—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof using liquid or gaseous propellants
- F02K9/60—Constructional parts; Details not otherwise provided for
- F02K9/62—Combustion or thrust chambers
- F02K9/64—Combustion or thrust chambers having cooling arrangements
-
- 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
- F02K9/972—Fluid cooling arrangements for 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
- F02K9/42—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof using liquid or gaseous propellants
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Heat-Exchange Devices With Radiators And Conduit Assemblies (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
Priority Applications (4)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
SE0702896A SE531857C2 (sv) | 2007-12-21 | 2007-12-21 | En komponent avsedd att utsättas för hög termisk last vid drift |
PCT/SE2008/000481 WO2009082315A1 (en) | 2007-12-21 | 2008-08-27 | A component configured for being subjected to high thermal load during operation |
EP08794107A EP2250363A4 (en) | 2007-12-21 | 2008-08-27 | COMPONENT DESIGNED TO SUPPORT THERMAL LOADS DURING THE MARKET |
US12/809,609 US20100300067A1 (en) | 2007-12-21 | 2008-08-27 | Component configured for being subjected to high thermal load during operation |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
SE0702896A SE531857C2 (sv) | 2007-12-21 | 2007-12-21 | En komponent avsedd att utsättas för hög termisk last vid drift |
Publications (2)
Publication Number | Publication Date |
---|---|
SE0702896L true SE0702896L (sv) | 2009-06-22 |
SE531857C2 SE531857C2 (sv) | 2009-08-25 |
Family
ID=40801443
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
SE0702896A SE531857C2 (sv) | 2007-12-21 | 2007-12-21 | En komponent avsedd att utsättas för hög termisk last vid drift |
Country Status (4)
Country | Link |
---|---|
US (1) | US20100300067A1 (sv) |
EP (1) | EP2250363A4 (sv) |
SE (1) | SE531857C2 (sv) |
WO (1) | WO2009082315A1 (sv) |
Families Citing this family (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB201110796D0 (en) * | 2011-06-27 | 2011-08-10 | Rolls Royce Plc | Heat exchanger |
US9194335B2 (en) * | 2012-03-09 | 2015-11-24 | Aerojet Rocketdyne Of De, Inc. | Rocket engine coolant system including an exit manifold having at least one flow guide within the manifold |
CN109733634B (zh) * | 2019-01-08 | 2020-11-24 | 厦门大学 | 三维内转四通道高超声速组合进气道的设计方法 |
CN115653789B (zh) * | 2022-10-31 | 2024-08-13 | 上海空间推进研究所 | 液体火箭发动机再生冷却身部结构、制造方法及发动机 |
Family Cites Families (19)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3190070A (en) * | 1950-04-05 | 1965-06-22 | Thiokol Chemical Corp | Reaction motor construction |
GB794660A (en) * | 1954-08-30 | 1958-05-07 | Havilland Engine Co Ltd | Heat exchangers |
US3105522A (en) * | 1956-12-10 | 1963-10-01 | Robert C Veit | Tube of uniform depth and variable width |
US2977754A (en) | 1958-01-29 | 1961-04-04 | Thiokol Chemical Corp | Rocket chamber with multi-pass axial flow coolant passageways |
US3086358A (en) * | 1959-05-25 | 1963-04-23 | United Aircraft Corp | Rocket nozzle construction |
US3066702A (en) * | 1959-05-28 | 1962-12-04 | United Aircraft Corp | Cooled nozzle structure |
US3004386A (en) * | 1959-06-23 | 1961-10-17 | United Aircraft Corp | Rocket nozzle tube construction |
DE1941296B2 (de) * | 1969-08-14 | 1971-09-30 | Messerschmitt Bolkow Blohm GmbH, 8000 München | Durch ein fluessiges medium regenerativ gekuehlte brenn kammer mit schubduese |
US3780533A (en) * | 1972-05-17 | 1973-12-25 | Us Air Force | Composite wall for a regeneratively cooled thrust chamber of a liquid propellant rocket engine |
US4107919A (en) * | 1975-03-19 | 1978-08-22 | The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration | Heat exchanger |
US4245469A (en) * | 1979-04-23 | 1981-01-20 | The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration | Heat exchanger and method of making |
US5221045A (en) | 1991-09-23 | 1993-06-22 | The Babcock & Wilcox Company | Bulge formed cooling channels with a variable lead helix on a hollow body of revolution |
SE512942C2 (sv) * | 1998-10-02 | 2000-06-12 | Volvo Aero Corp | Förfarande för tillverkning av utloppsmunstycken för raketmotorer |
ATE395508T1 (de) * | 2001-01-11 | 2008-05-15 | Volvo Aero Corp | Verfahren zur herstellung von austrittsdüsen für raketentriebwerke |
AU2002347745A1 (en) * | 2001-12-18 | 2003-06-30 | Volvo Aero Corporation | A component for being subjected to high thermal load during operation and a method for manufacturing such a component |
US6890148B2 (en) | 2003-08-28 | 2005-05-10 | Siemens Westinghouse Power Corporation | Transition duct cooling system |
US7740161B2 (en) * | 2005-09-06 | 2010-06-22 | Volvo Aero Corporation | Engine wall structure and a method of producing an engine wall structure |
WO2008010748A1 (en) | 2006-07-19 | 2008-01-24 | Volvo Aero Corporation | Method for manufacturing a wall structure |
WO2008100186A1 (en) * | 2007-02-13 | 2008-08-21 | Volvo Aero Corporation | A component configured for being subjected to high thermal load during operation |
-
2007
- 2007-12-21 SE SE0702896A patent/SE531857C2/sv not_active IP Right Cessation
-
2008
- 2008-08-27 WO PCT/SE2008/000481 patent/WO2009082315A1/en active Application Filing
- 2008-08-27 EP EP08794107A patent/EP2250363A4/en not_active Withdrawn
- 2008-08-27 US US12/809,609 patent/US20100300067A1/en not_active Abandoned
Also Published As
Publication number | Publication date |
---|---|
EP2250363A4 (en) | 2011-03-16 |
WO2009082315A1 (en) | 2009-07-02 |
EP2250363A1 (en) | 2010-11-17 |
SE531857C2 (sv) | 2009-08-25 |
US20100300067A1 (en) | 2010-12-02 |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
ATE540280T1 (de) | Einbauelement einer einbaupackung | |
EP2381070A3 (en) | Hot gas path component cooling system | |
DE602008005026D1 (de) | uBIPOLARPLATTE FÜR EINE BRENNSTOFFZELLE MIT EINEM UMGANGENEN SERPENTINEN-STRÖMUNGSWEG FÜR OXIDATIONSGAS; KÜHLPLATTE FÜR EINE BRENNSTOFFZELLE MIT EINEM UMGANGENEN SERPENTINEN-STRÖMUNGSWEG FÜR KÜHLFLUID; BRENNSTOFFZELLE MIT SOLCHEN PLATTEN UND VERWENDUNGEN DAFÜR | |
EP3266056A4 (en) | Battery module with thermal runaway and gas exhaust management system | |
ATE528807T1 (de) | Modulares batteriesystem | |
GB201100985D0 (en) | Scoring balloon with offset scoring elements | |
WO2015039022A3 (en) | Enhanced heat transport systems for cooling chambers and surfaces | |
WO2010007375A3 (en) | X-ray tube anodes | |
ES2620482T3 (es) | Impermeabilización del canal de flujo de una turbomáquina | |
ATE538300T1 (de) | System zum mischen von gasströmen in einem gasturbinentriebwerk, zugehöriges gasturbinentriebwerk und flugzeugtriebwerk | |
CL2012003252A1 (es) | Canalon de descarga para manejo de material para direccionar el flujo de material en donde el canalon de descarga para manejo de material comprende una estructura soporte y al menos un modulo de revestimiento del canalon de descarga, al menos un modulo de revestimiento del canalon de descarga comprende un material compuesto que incluye metal y material de ceramica; un modulo y revestimiento. | |
IN2014MN02201A (sv) | ||
EP2846097A3 (en) | A gas turbine combustion chamber with tiles having film cooling apertures | |
SE0702896L (sv) | En komponent avsedd att utsättas för hög termisk last vid drift | |
WO2013016127A3 (en) | Heat exchanger comprising one or more plate assemblies with a plurality of interconnected channels and related method | |
BR112016002648A2 (pt) | pá de estator de turbomáquina | |
EA201370065A1 (ru) | Уплотнительная гильза для запорного вентиля | |
JP2016503224A5 (sv) | ||
MY170389A (en) | Cross-flow fan | |
MX2013002500A (es) | Absorbedor de energia que tiene la capacidad de prevenir el aumento de temperatura de funcionamiento. | |
WO2012080039A3 (fr) | Echangeur de chaleur a plaques empilees | |
JP2014114810A5 (sv) | ||
WO2011127416A3 (en) | Improved mechanical support for a thin-film thermoelectric cooling device | |
DK3640577T3 (da) | Varmeveksler omfattende plader med forstærket diagonal område | |
SG194734A1 (en) | Solar energy converter |
Legal Events
Date | Code | Title | Description |
---|---|---|---|
NUG | Patent has lapsed |