ATE479017T1 - Verfahren zur herstellung einer motorwandstruktur - Google Patents
Verfahren zur herstellung einer motorwandstrukturInfo
- Publication number
- ATE479017T1 ATE479017T1 AT05782623T AT05782623T ATE479017T1 AT E479017 T1 ATE479017 T1 AT E479017T1 AT 05782623 T AT05782623 T AT 05782623T AT 05782623 T AT05782623 T AT 05782623T AT E479017 T1 ATE479017 T1 AT E479017T1
- Authority
- AT
- Austria
- Prior art keywords
- wall
- wall structure
- producing
- engine
- engine wall
- 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
- F02K9/42—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
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B23—MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
- B23H—WORKING OF METAL BY THE ACTION OF A HIGH CONCENTRATION OF ELECTRIC CURRENT ON A WORKPIECE USING AN ELECTRODE WHICH TAKES THE PLACE OF A TOOL; SUCH WORKING COMBINED WITH OTHER FORMS OF WORKING OF METAL
- B23H9/00—Machining specially adapted for treating particular metal objects or for obtaining special effects or results on metal objects
- B23H9/10—Working turbine blades or 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
- F02K9/972—Fluid cooling arrangements for nozzles
-
- 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
- F05D2230/00—Manufacture
- F05D2230/10—Manufacture by removing material
-
- 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
- F05D2230/00—Manufacture
- F05D2230/10—Manufacture by removing material
- F05D2230/12—Manufacture by removing material by spark erosion methods
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
- Y10T29/00—Metal working
- Y10T29/49—Method of mechanical manufacture
- Y10T29/49229—Prime mover or fluid pump making
- Y10T29/49231—I.C. [internal combustion] engine making
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- General Engineering & Computer Science (AREA)
- Physics & Mathematics (AREA)
- Thermal Sciences (AREA)
- Electrical Discharge Machining, Electrochemical Machining, And Combined Machining (AREA)
- Exhaust Silencers (AREA)
- Iron Core Of Rotating Electric Machines (AREA)
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
PCT/SE2005/001294 WO2007030039A1 (en) | 2005-09-06 | 2005-09-06 | A method of producing an engine wall structure |
Publications (1)
Publication Number | Publication Date |
---|---|
ATE479017T1 true ATE479017T1 (de) | 2010-09-15 |
Family
ID=37836089
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
AT05782623T ATE479017T1 (de) | 2005-09-06 | 2005-09-06 | Verfahren zur herstellung einer motorwandstruktur |
Country Status (6)
Country | Link |
---|---|
US (1) | US8002168B2 (de) |
EP (1) | EP1929147B1 (de) |
AT (1) | ATE479017T1 (de) |
DE (1) | DE602005023223D1 (de) |
ES (1) | ES2350847T3 (de) |
WO (1) | WO2007030039A1 (de) |
Families Citing this family (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE10343049B3 (de) * | 2003-09-16 | 2005-04-14 | Eads Space Transportation Gmbh | Brennkammer mit Kühleinrichtung und Verfahren zur Herstellung der Brennkammer |
WO2007030038A1 (en) * | 2005-09-06 | 2007-03-15 | Volvo Aero Corporation | An engine wall structure and a method of producing an engine wall structure |
CN100570147C (zh) * | 2008-01-17 | 2009-12-16 | 清华大学 | 一种利用强吸热反应的层板发汗冷却结构 |
US9238284B2 (en) * | 2011-12-20 | 2016-01-19 | Unison Industries, Llc | Methods for forming a heat exchanger and portions thereof |
Family Cites Families (39)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2669835A (en) * | 1949-03-04 | 1954-02-23 | Kellogg M W Co | Wall structure for regeneratively cooled rocket motors |
US2968918A (en) * | 1949-08-22 | 1961-01-24 | California Inst Res Found | Rocket motor shell construction |
US3246469A (en) * | 1963-08-22 | 1966-04-19 | Bristol Siddelcy Engines Ltd | Cooling of aerofoil members |
GB1192637A (en) * | 1966-09-24 | 1970-05-20 | Bolkow Ges Mil Beschrankter Ha | Cooling Tubes for the Walls of Combustion Chambers |
FR2012723A1 (de) * | 1968-07-11 | 1970-03-20 | Messerschmitt Boelkow Blohm | |
US3692637A (en) * | 1969-11-24 | 1972-09-19 | Carl Helmut Dederra | Method of fabricating a hollow structure having cooling channels |
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 |
US3910039A (en) * | 1972-09-14 | 1975-10-07 | Nasa | Rocket chamber and method of making |
DE2406976A1 (de) * | 1974-02-14 | 1975-09-04 | Messerschmitt Boelkow Blohm | Verfahren zur herstellung von brennkammern und/oder schubduesen fuer fluessigkeitsraketentriebwerke |
DE2657474A1 (de) * | 1976-12-18 | 1978-06-22 | Messerschmitt Boelkow Blohm | Verfahren zum herstellen von regenerativ gekuehlten raketenbrennkammern und/oder schubduesen |
JPS6082602A (ja) * | 1983-10-07 | 1985-05-10 | Natl Aerospace Lab | ロケツト燃焼器外筒製作法 |
US4591534A (en) * | 1984-08-23 | 1986-05-27 | Rockwell International Corporation | Wall structure for rocket nozzle extension |
US5051559A (en) * | 1988-04-01 | 1991-09-24 | The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration | Nozzle fabrication technique |
US4852232A (en) * | 1988-04-01 | 1989-08-01 | The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration | Nozzle fabrication technique |
DE4015204C1 (de) * | 1990-05-11 | 1991-10-17 | Mtu Muenchen Gmbh | |
US5075966A (en) * | 1990-09-04 | 1991-12-31 | General Electric Company | Method for fabricating a hollow component for a rocket engine |
FR2669966B1 (fr) * | 1990-11-30 | 1993-03-26 | Europ Propulsion | Procede de fabrication de paroi de chambre de combustion, notamment pour moteur-fusee, et chambre de combustion obtenue par ce procede. |
US5501011A (en) * | 1992-05-18 | 1996-03-26 | Societe Europeenne De Propulsion | Method of manufacture of an enclosure containing hot gases cooled by transportation, in particular the thrust chamber of a rocket engine |
US5864949A (en) * | 1992-10-27 | 1999-02-02 | United Technologies Corporation | Tip seal and anti-contamination for turbine blades |
US5249357A (en) * | 1993-01-27 | 1993-10-05 | The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration | Method of fabricating a rocket engine combustion chamber |
US5688104A (en) * | 1993-11-24 | 1997-11-18 | United Technologies Corporation | Airfoil having expanded wall portions to accommodate film cooling holes |
US5418345A (en) * | 1994-02-28 | 1995-05-23 | United Technologies Corporation | Method for forming shaped passages |
DE19602731C1 (de) * | 1996-01-26 | 1997-07-10 | Daimler Benz Aerospace Ag | Wandstruktur für treibstoffgekühlte Triebwerkswände |
US5957657A (en) * | 1996-02-26 | 1999-09-28 | Mitisubishi Heavy Industries, Ltd. | Method of forming a cooling air passage in a gas turbine stationary blade shroud |
FR2776215B1 (fr) * | 1998-03-20 | 2000-06-16 | Snecma | Procede de fabrication d'un circuit regeneratif a fort flux thermique, notamment pour chambre de combustion de moteur-fusee |
US6850874B1 (en) * | 1998-04-17 | 2005-02-01 | United Technologies Corporation | Method and apparatus for predicting a characteristic of a product attribute formed by a machining process using a model of the process |
US6138451A (en) * | 1998-05-11 | 2000-10-31 | Hughes Electronics Corporation | Rocket engine with combustion chamber step structure insert, and its fabrication |
SE512942C2 (sv) * | 1998-10-02 | 2000-06-12 | Volvo Aero Corp | Förfarande för tillverkning av utloppsmunstycken för raketmotorer |
RU2278292C2 (ru) * | 2001-01-11 | 2006-06-20 | Вольво Аэро Корпорейшн | Элемент ракетного двигателя и способ изготовления такого элемента ракетного двигателя |
US6783824B2 (en) * | 2001-01-25 | 2004-08-31 | Hyper-Therm High-Temperature Composites, Inc. | Actively-cooled fiber-reinforced ceramic matrix composite rocket propulsion thrust chamber and method of producing the same |
US6612808B2 (en) * | 2001-11-29 | 2003-09-02 | General Electric Company | Article wall with interrupted ribbed heat transfer surface |
EP1458968B1 (de) * | 2001-12-18 | 2007-07-18 | Volvo Aero Corporation | Bauteil zur beaufschlagung mit hoher thermischer belastung beim betrieb und verfahren zur herstellung eines solchen bauteils |
US7124574B2 (en) * | 2002-12-04 | 2006-10-24 | United Technologies Corporation | Method and apparatus for a substantially coaxial injector element |
DE10343049B3 (de) * | 2003-09-16 | 2005-04-14 | Eads Space Transportation Gmbh | Brennkammer mit Kühleinrichtung und Verfahren zur Herstellung der Brennkammer |
US20050135923A1 (en) * | 2003-12-22 | 2005-06-23 | Todd Coons | Cooled vane cluster |
US7328580B2 (en) * | 2004-06-23 | 2008-02-12 | General Electric Company | Chevron film cooled wall |
US7694656B2 (en) * | 2004-09-01 | 2010-04-13 | Bishop Innovation Limited | Cylinder head for rotary valve internal combustion engine |
US20070012370A1 (en) * | 2005-07-18 | 2007-01-18 | Honeywell International, Inc. | Facetted high temperature thruster design |
GB2428749B (en) * | 2005-08-02 | 2007-11-28 | Rolls Royce Plc | A component comprising a multiplicity of cooling passages |
-
2005
- 2005-09-06 DE DE602005023223T patent/DE602005023223D1/de active Active
- 2005-09-06 US US12/063,827 patent/US8002168B2/en not_active Expired - Fee Related
- 2005-09-06 AT AT05782623T patent/ATE479017T1/de not_active IP Right Cessation
- 2005-09-06 WO PCT/SE2005/001294 patent/WO2007030039A1/en active Application Filing
- 2005-09-06 EP EP05782623A patent/EP1929147B1/de not_active Not-in-force
- 2005-09-06 ES ES05782623T patent/ES2350847T3/es active Active
Also Published As
Publication number | Publication date |
---|---|
ES2350847T3 (es) | 2011-01-27 |
EP1929147A1 (de) | 2008-06-11 |
WO2007030039A1 (en) | 2007-03-15 |
US8002168B2 (en) | 2011-08-23 |
DE602005023223D1 (de) | 2010-10-07 |
EP1929147B1 (de) | 2010-08-25 |
US20080216315A1 (en) | 2008-09-11 |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
WO2008133758A3 (en) | Airfoil for a gas turbine with impingement holes | |
ATE497087T1 (de) | Spaltkühlung zwischen brennkammerwand und turbinenwand einer gasturbinenanlage | |
UA84281C2 (ru) | Направляющая лопатка газотурбинного двигателя и турбина газотурбинного двигателя | |
TW200626787A (en) | Airfoil with large fillet and micro-circuit cooling | |
DE502007003266D1 (de) | Strukturiertes Wärmeaustauscherrohr und Verfahren zu dessen Herstellung | |
WO2014081492A3 (en) | Cooling for combustor liners with accelerating channels | |
RU2017111373A (ru) | Усовершенствованная панель теплообмена и уменьшения шума для газотурбинного двигателя | |
NZ600293A (en) | Method of manufacturing a mechanically lined pipe more than 500 m long | |
ATE527465T1 (de) | Verbesserte luftfederanordnung und -verfahren | |
WO2015108584A3 (en) | Passage geometry for gas turbine engine combustor | |
RU2014117394A (ru) | Способ изготовления звукопоглощающей панели | |
EP1930545A3 (de) | Schaufel mit Plasma-Generator zum Schutz einer Grenzschicht stromabwärts einer Filmkühlungsbohrung und entsprechendes Betriebsverfahren | |
FR2935356B1 (fr) | Procede de fabrication d'un panneau acoustique d'une levre d'entree d'air d'une nacelle | |
DE602004006732D1 (de) | Verfahren zur herstellung einer statorkomponente | |
EP2014386A8 (de) | Verfahren zur Herstellung einer hohlen Schaufel | |
PL1893932T3 (pl) | Zespół przegród i uszczelnień oraz sposób składania wymiennika ciepła | |
MY148395A (en) | Controlled metal foil production | |
EP2144003A3 (de) | Brennkammerwand für einen Gasturbinenmotor | |
EP3556999B8 (de) | Doppelwandige schaufelkühlkonfiguration für gasturbinenmotoren | |
MY162384A (en) | Turbine Vane | |
ATE479017T1 (de) | Verfahren zur herstellung einer motorwandstruktur | |
WO2014189572A3 (en) | Acoustic treatment to mitigate fan noise | |
PL2155979T3 (pl) | Izolacja cieplna elementów obejmujących kanały wentylacyjne | |
ATE467038T1 (de) | Luftspaltkrümmer | |
WO2015130380A3 (en) | Blade outer air seal cooling passage |
Legal Events
Date | Code | Title | Description |
---|---|---|---|
RER | Ceased as to paragraph 5 lit. 3 law introducing patent treaties |