DE602005023223D1 - Verfahren zur herstellung einer motorwandstruktur - Google Patents

Verfahren zur herstellung einer motorwandstruktur

Info

Publication number
DE602005023223D1
DE602005023223D1 DE602005023223T DE602005023223T DE602005023223D1 DE 602005023223 D1 DE602005023223 D1 DE 602005023223D1 DE 602005023223 T DE602005023223 T DE 602005023223T DE 602005023223 T DE602005023223 T DE 602005023223T DE 602005023223 D1 DE602005023223 D1 DE 602005023223D1
Authority
DE
Germany
Prior art keywords
wall
wall structure
producing
engine
webs
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.)
Active
Application number
DE602005023223T
Other languages
English (en)
Inventor
Arne Boman
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.)
GKN Aerospace Sweden AB
Original Assignee
Volvo Aero AB
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 Volvo Aero AB filed Critical Volvo Aero AB
Publication of DE602005023223D1 publication Critical patent/DE602005023223D1/de
Active legal-status Critical Current
Anticipated expiration legal-status Critical

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)
DE602005023223T 2005-09-06 2005-09-06 Verfahren zur herstellung einer motorwandstruktur Active DE602005023223D1 (de)

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
DE602005023223D1 true DE602005023223D1 (de) 2010-10-07

Family

ID=37836089

Family Applications (1)

Application Number Title Priority Date Filing Date
DE602005023223T Active DE602005023223D1 (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)

* Cited by examiner, † Cited by third party
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
US7740161B2 (en) * 2005-09-06 2010-06-22 Volvo Aero Corporation 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)

* Cited by examiner, † Cited by third party
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
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
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
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
DE60212069T2 (de) * 2001-01-11 2006-12-21 Volvo Aero Corp. Raketentriebwerksglied und ein verfahren zur herstellung eines raketentriebwerksglieds
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
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
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
WO2006024087A1 (en) * 2004-09-01 2006-03-09 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

Also Published As

Publication number Publication date
US8002168B2 (en) 2011-08-23
ATE479017T1 (de) 2010-09-15
EP1929147A1 (de) 2008-06-11
ES2350847T3 (es) 2011-01-27
US20080216315A1 (en) 2008-09-11
EP1929147B1 (de) 2010-08-25
WO2007030039A1 (en) 2007-03-15

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