FR2935625B1 - Procede de fabrication d'une piece thermamecanique de revolution circulaire comportant un substrat porteur a base de titane revetu d'acier ou superalliage, carter de compresseur de turbomachine resistant au feu de titane - Google Patents
Procede de fabrication d'une piece thermamecanique de revolution circulaire comportant un substrat porteur a base de titane revetu d'acier ou superalliage, carter de compresseur de turbomachine resistant au feu de titaneInfo
- Publication number
- FR2935625B1 FR2935625B1 FR0855963A FR0855963A FR2935625B1 FR 2935625 B1 FR2935625 B1 FR 2935625B1 FR 0855963 A FR0855963 A FR 0855963A FR 0855963 A FR0855963 A FR 0855963A FR 2935625 B1 FR2935625 B1 FR 2935625B1
- Authority
- FR
- France
- Prior art keywords
- titanium
- thermamechanical
- superalliation
- coated
- steel
- 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
Links
Classifications
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B23—MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
- B23P—METAL-WORKING NOT OTHERWISE PROVIDED FOR; COMBINED OPERATIONS; UNIVERSAL MACHINE TOOLS
- B23P15/00—Making specific metal objects by operations not covered by a single other subclass or a group in this subclass
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B21—MECHANICAL METAL-WORKING WITHOUT ESSENTIALLY REMOVING MATERIAL; PUNCHING METAL
- B21D—WORKING OR PROCESSING OF SHEET METAL OR METAL TUBES, RODS OR PROFILES WITHOUT ESSENTIALLY REMOVING MATERIAL; PUNCHING METAL
- B21D39/00—Application of procedures in order to connect objects or parts, e.g. coating with sheet metal otherwise than by plating; Tube expanders
- B21D39/04—Application of procedures in order to connect objects or parts, e.g. coating with sheet metal otherwise than by plating; Tube expanders of tubes with tubes; of tubes with rods
- B21D39/042—Application of procedures in order to connect objects or parts, e.g. coating with sheet metal otherwise than by plating; Tube expanders of tubes with tubes; of tubes with rods using explosives
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B21—MECHANICAL METAL-WORKING WITHOUT ESSENTIALLY REMOVING MATERIAL; PUNCHING METAL
- B21J—FORGING; HAMMERING; PRESSING METAL; RIVETING; FORGE FURNACES
- B21J1/00—Preparing metal stock or similar ancillary operations prior, during or post forging, e.g. heating or cooling
- B21J1/04—Shaping in the rough solely by forging or pressing
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B15/00—Layered products comprising a layer of metal
- B32B15/01—Layered products comprising a layer of metal all layers being exclusively metallic
- B32B15/013—Layered products comprising a layer of metal all layers being exclusively metallic one layer being formed of an iron alloy or steel, another layer being formed of a metal other than iron or aluminium
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
- F01D25/00—Component parts, details, or accessories, not provided for in, or of interest apart from, other groups
- F01D25/08—Cooling; Heating; Heat-insulation
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
- F01D25/00—Component parts, details, or accessories, not provided for in, or of interest apart from, other groups
- F01D25/24—Casings; Casing parts, e.g. diaphragms, casing fastenings
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
- F02C7/00—Features, components parts, details or accessories, not provided for in, or of interest apart form groups F02C1/00 - F02C6/00; Air intakes for jet-propulsion plants
- F02C7/24—Heat or noise insulation
- F02C7/25—Fire protection or prevention
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
- F04D—NON-POSITIVE-DISPLACEMENT PUMPS
- F04D29/00—Details, component parts, or accessories
- F04D29/02—Selection of particular materials
- F04D29/023—Selection of particular materials especially adapted for elastic fluid pumps
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
- F04D—NON-POSITIVE-DISPLACEMENT PUMPS
- F04D29/00—Details, component parts, or accessories
- F04D29/40—Casings; Connections of working fluid
- F04D29/52—Casings; Connections of working fluid for axial pumps
- F04D29/54—Fluid-guiding means, e.g. diffusers
- F04D29/541—Specially adapted for elastic fluid pumps
- F04D29/542—Bladed diffusers
-
- 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
- F05D2230/20—Manufacture essentially without removing material
- F05D2230/23—Manufacture essentially without removing material by permanently joining parts together
- F05D2230/232—Manufacture essentially without removing material by permanently joining parts together by welding
-
- 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
- F05D2230/20—Manufacture essentially without removing material
- F05D2230/25—Manufacture essentially without removing material by forging
-
- 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
- F05D2230/20—Manufacture essentially without removing material
- F05D2230/26—Manufacture essentially without removing material by rolling
-
- 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
- F05D2300/10—Metals, alloys or intermetallic compounds
- F05D2300/13—Refractory metals, i.e. Ti, V, Cr, Zr, Nb, Mo, Hf, Ta, W
- F05D2300/133—Titanium
-
- 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
- F05D2300/10—Metals, alloys or intermetallic compounds
- F05D2300/17—Alloys
- F05D2300/171—Steel alloys
-
- 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
- F05D2300/10—Metals, alloys or intermetallic compounds
- F05D2300/17—Alloys
- F05D2300/174—Titanium alloys, e.g. TiAl
-
- 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
- F05D2300/10—Metals, alloys or intermetallic compounds
- F05D2300/17—Alloys
- F05D2300/175—Superalloys
-
- 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
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T50/00—Aeronautics or air transport
- Y02T50/60—Efficient propulsion technologies, e.g. for aircraft
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
Priority Applications (3)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR0855963A FR2935625B1 (fr) | 2008-09-05 | 2008-09-05 | Procede de fabrication d'une piece thermamecanique de revolution circulaire comportant un substrat porteur a base de titane revetu d'acier ou superalliage, carter de compresseur de turbomachine resistant au feu de titane |
US13/060,719 US20110211945A1 (en) | 2008-09-05 | 2009-09-03 | Method for the manufacture of a circular revolution thermomechanical part including a titanium-based load-bearing substrate lined with steel or superalloy, a turbomachine compressor housing which is resistant to titanium fire obtained according to this method |
PCT/EP2009/061381 WO2010026179A1 (fr) | 2008-09-05 | 2009-09-03 | Procede de fabrication d'une piece thermomecanique de revolution circulaire comportant un substrat porteur a base de titane revetu d'acier ou superalliage, carter de compresseur de turbomachine resistant au feu de titane obtenu selon ce procede |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR0855963A FR2935625B1 (fr) | 2008-09-05 | 2008-09-05 | Procede de fabrication d'une piece thermamecanique de revolution circulaire comportant un substrat porteur a base de titane revetu d'acier ou superalliage, carter de compresseur de turbomachine resistant au feu de titane |
Publications (2)
Publication Number | Publication Date |
---|---|
FR2935625A1 FR2935625A1 (fr) | 2010-03-12 |
FR2935625B1 true FR2935625B1 (fr) | 2011-09-09 |
Family
ID=40551056
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
FR0855963A Active FR2935625B1 (fr) | 2008-09-05 | 2008-09-05 | Procede de fabrication d'une piece thermamecanique de revolution circulaire comportant un substrat porteur a base de titane revetu d'acier ou superalliage, carter de compresseur de turbomachine resistant au feu de titane |
Country Status (3)
Country | Link |
---|---|
US (1) | US20110211945A1 (fr) |
FR (1) | FR2935625B1 (fr) |
WO (1) | WO2010026179A1 (fr) |
Families Citing this family (9)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2951197B1 (fr) | 2009-10-12 | 2011-11-25 | Snecma | Homogeneisation d'aciers martensitiques inoxydables apres refusion sous laitier |
FR2951196B1 (fr) | 2009-10-12 | 2011-11-25 | Snecma | Degazage d'aciers martensitiques inoxydables avant refusion sous laitier |
FR2951198B1 (fr) | 2009-10-12 | 2013-05-10 | Snecma | Traitements thermiques d'aciers martensitiques inoxydables apres refusion sous laitier |
FR2978075B1 (fr) * | 2011-07-22 | 2013-08-16 | Snecma | Assemblage d'une coque titane et d'une coque alliage resistant au feu titane par deformation superplastique |
GB2507430A (en) * | 2011-07-22 | 2014-04-30 | Snecma | Method for assembling a titanium shell and a titanium fire-resistant alloy shell |
FR2978077B1 (fr) * | 2011-07-22 | 2013-08-16 | Snecma | Assemblage d'une coque titane et d'une coque alliage resistant au feu titane par compression isostatique a chaud |
CN106078112B (zh) * | 2016-07-21 | 2018-07-20 | 滁州南钢盛达实业有限公司 | 一种h型钢的生产工艺 |
US11982236B2 (en) | 2017-12-22 | 2024-05-14 | General Electric Company | Titanium alloy compressor case |
US11033992B2 (en) * | 2018-10-05 | 2021-06-15 | Pratt & Whitney Canada Corp. | Double row compressor stators |
Family Cites Families (29)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3137937A (en) * | 1960-10-26 | 1964-06-23 | Du Pont | Explosive bonding |
US3434197A (en) * | 1964-08-03 | 1969-03-25 | Singer General Precision | Explosive welding |
US3403889A (en) * | 1966-04-07 | 1968-10-01 | Gen Electric | Frame assembly having low thermal stresses |
US3360848A (en) * | 1966-10-17 | 1968-01-02 | Du Pont | Process for explosion-bonding metals |
US3798011A (en) * | 1969-01-31 | 1974-03-19 | Du Pont | Multilayered metal composite |
US3728780A (en) * | 1970-01-24 | 1973-04-24 | Inst Science And Technology | Explosive cladding on geometrically non-uniform metal material |
US3854891A (en) * | 1972-09-25 | 1974-12-17 | Allegheny Ludlum Ind Inc | Titanium composite |
US4155680A (en) * | 1977-02-14 | 1979-05-22 | General Electric Company | Compressor protection means |
EP0003078A1 (fr) * | 1978-01-17 | 1979-07-25 | Imperial Chemical Industries Plc | Perfectionnements au plaquage par explosion |
US4612259A (en) * | 1981-03-05 | 1986-09-16 | Asahi Kasei Kogyo Kabushiki Kaisha | Titanium clad steel plate |
DE3407945A1 (de) * | 1984-03-03 | 1985-09-05 | MTU Motoren- und Turbinen-Union München GmbH, 8000 München | Verfahren und mittel zur vermeidung der entstehung von titanfeuer |
DE3407946A1 (de) * | 1984-03-03 | 1985-09-05 | MTU Motoren- und Turbinen-Union München GmbH, 8000 München | Einrichtung zur verhinderung der ausbreitung von titanfeuer bei turbomaschinen, insbesondere gasturbinen- bzw. gasturbinenstrahltriebwerken |
GB8720248D0 (en) * | 1987-08-27 | 1987-10-07 | Imi Titanium Ltd | Turbines |
DE3926151C1 (fr) * | 1989-02-28 | 1990-05-10 | Mtu Muenchen Gmbh | |
US5074970A (en) * | 1989-07-03 | 1991-12-24 | Kostas Routsis | Method for applying an abrasive layer to titanium alloy compressor airfoils |
US5210945A (en) * | 1991-05-22 | 1993-05-18 | Ngk Spark Plug Co., Ltd. | Method of assembly of a rotary shaft in a ball-bearing type turbocharger |
GB9121147D0 (en) * | 1991-10-04 | 1991-11-13 | Ici Plc | Method for producing clad metal plate |
AU1875595A (en) * | 1994-02-16 | 1995-09-04 | Sohl, Charles E. | Coating scheme to contain molten material during gas turbine engine fires |
GB9823267D0 (en) * | 1998-10-24 | 1998-12-16 | Hardwick Roy | Method of producing a metal composites which can be processed at high temperatures |
GB9824611D0 (en) * | 1998-11-11 | 1999-01-06 | Rolls Royce Plc | A beta titanium alloy |
FR2794816B1 (fr) * | 1999-06-10 | 2001-07-06 | Snecma | Stator de compresseur a haute pression |
GB0116988D0 (en) * | 2000-08-11 | 2001-09-05 | Rolls Royce Plc | A gas turbine engine blade containment assembly |
GB0300014D0 (en) * | 2003-01-02 | 2003-02-05 | Hardwick Roy | Method of producing explosively bonded interfaces which are waveless when using explosives of higher detonation velocity which normally produce waves |
CA2420117A1 (fr) * | 2003-02-17 | 2004-08-17 | Sigmabond Technologies Corporation | Methode de production de composites metalliques comprenant des metaux incompatibles |
WO2005068845A1 (fr) * | 2004-01-14 | 2005-07-28 | Ishikawajima-Harima Heavy Industries Co., Ltd. | Compresseur, ailette de rotor fabriquee en titane, procede de fabrication de moteur a reaction et d'ailette de rotor en titane |
US7575418B2 (en) * | 2004-09-30 | 2009-08-18 | General Electric Company | Erosion and wear resistant protective structures for turbine components |
US7530485B1 (en) * | 2006-02-07 | 2009-05-12 | High Energy Metals, Inc. | Method for explosive bonding of tubular metal liners |
US8950069B2 (en) * | 2006-12-29 | 2015-02-10 | Rolls-Royce North American Technologies, Inc. | Integrated compressor vane casing |
DE102008019296A1 (de) * | 2008-04-16 | 2009-10-22 | Rolls-Royce Deutschland Ltd & Co Kg | Verfahren zur Herstellung eines Feuerschutzes für aus Titan bestehende Bauteilkörper einer Fluggasturbine und Bauteilkörper aus Titan für eine Fluggasturbine |
-
2008
- 2008-09-05 FR FR0855963A patent/FR2935625B1/fr active Active
-
2009
- 2009-09-03 WO PCT/EP2009/061381 patent/WO2010026179A1/fr active Application Filing
- 2009-09-03 US US13/060,719 patent/US20110211945A1/en not_active Abandoned
Also Published As
Publication number | Publication date |
---|---|
FR2935625A1 (fr) | 2010-03-12 |
US20110211945A1 (en) | 2011-09-01 |
WO2010026179A1 (fr) | 2010-03-11 |
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