IL75447A - Process for fabricating multi-alloy components - Google Patents
Process for fabricating multi-alloy componentsInfo
- Publication number
- IL75447A IL75447A IL75447A IL7544785A IL75447A IL 75447 A IL75447 A IL 75447A IL 75447 A IL75447 A IL 75447A IL 7544785 A IL7544785 A IL 7544785A IL 75447 A IL75447 A IL 75447A
- Authority
- IL
- Israel
- Prior art keywords
- alloy components
- fabricating multi
- fabricating
- alloy
- components
- Prior art date
Links
Classifications
-
- 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
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B21—MECHANICAL METAL-WORKING WITHOUT ESSENTIALLY REMOVING MATERIAL; PUNCHING METAL
- B21K—MAKING FORGED OR PRESSED METAL PRODUCTS, e.g. HORSE-SHOES, RIVETS, BOLTS OR WHEELS
- B21K1/00—Making machine elements
- B21K1/28—Making machine elements wheels; discs
- B21K1/36—Making machine elements wheels; discs with blades
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B21—MECHANICAL METAL-WORKING WITHOUT ESSENTIALLY REMOVING MATERIAL; PUNCHING METAL
- B21K—MAKING FORGED OR PRESSED METAL PRODUCTS, e.g. HORSE-SHOES, RIVETS, BOLTS OR WHEELS
- B21K1/00—Making machine elements
- B21K1/76—Making machine elements elements not mentioned in one of the preceding groups
- B21K1/761—Making machine elements elements not mentioned in one of the preceding groups rings
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B22—CASTING; POWDER METALLURGY
- B22F—WORKING METALLIC POWDER; MANUFACTURE OF ARTICLES FROM METALLIC POWDER; MAKING METALLIC POWDER; APPARATUS OR DEVICES SPECIALLY ADAPTED FOR METALLIC POWDER
- B22F5/00—Manufacture of workpieces or articles from metallic powder characterised by the special shape of the product
- B22F5/04—Manufacture of workpieces or articles from metallic powder characterised by the special shape of the product of turbine blades
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B22—CASTING; POWDER METALLURGY
- B22F—WORKING METALLIC POWDER; MANUFACTURE OF ARTICLES FROM METALLIC POWDER; MAKING METALLIC POWDER; APPARATUS OR DEVICES SPECIALLY ADAPTED FOR METALLIC POWDER
- B22F7/00—Manufacture of composite layers, workpieces, or articles, comprising metallic powder, by sintering the powder, with or without compacting wherein at least one part is obtained by sintering or compression
- B22F7/06—Manufacture of composite layers, workpieces, or articles, comprising metallic powder, by sintering the powder, with or without compacting wherein at least one part is obtained by sintering or compression of composite workpieces or articles from parts, e.g. to form tipped tools
- B22F7/062—Manufacture of composite layers, workpieces, or articles, comprising metallic powder, by sintering the powder, with or without compacting wherein at least one part is obtained by sintering or compression of composite workpieces or articles from parts, e.g. to form tipped tools involving the connection or repairing of preformed parts
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B23—MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
- B23K—SOLDERING OR UNSOLDERING; WELDING; CLADDING OR PLATING BY SOLDERING OR WELDING; CUTTING BY APPLYING HEAT LOCALLY, e.g. FLAME CUTTING; WORKING BY LASER BEAM
- B23K20/00—Non-electric welding by applying impact or other pressure, with or without the application of heat, e.g. cladding or plating
- B23K20/02—Non-electric welding by applying impact or other pressure, with or without the application of heat, e.g. cladding or plating by means of a press ; Diffusion bonding
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B23—MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
- B23K—SOLDERING OR UNSOLDERING; WELDING; CLADDING OR PLATING BY SOLDERING OR WELDING; CUTTING BY APPLYING HEAT LOCALLY, e.g. FLAME CUTTING; WORKING BY LASER BEAM
- B23K20/00—Non-electric welding by applying impact or other pressure, with or without the application of heat, e.g. cladding or plating
- B23K20/22—Non-electric welding by applying impact or other pressure, with or without the application of heat, e.g. cladding or plating taking account of the properties of the materials to be welded
- B23K20/227—Non-electric welding by applying impact or other pressure, with or without the application of heat, e.g. cladding or plating taking account of the properties of the materials to be welded with ferrous layer
-
- 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
- B23P15/006—Making specific metal objects by operations not covered by a single other subclass or a group in this subclass turbine wheels
-
- 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
- F01D5/00—Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
- F01D5/12—Blades
- F01D5/28—Selecting particular materials; Particular measures relating thereto; Measures against erosion or corrosion
-
- 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
- F01D5/00—Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
- F01D5/34—Rotor-blade aggregates of unitary construction, e.g. formed of sheet laminae
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B23—MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
- B23K—SOLDERING OR UNSOLDERING; WELDING; CLADDING OR PLATING BY SOLDERING OR WELDING; CUTTING BY APPLYING HEAT LOCALLY, e.g. FLAME CUTTING; WORKING BY LASER BEAM
- B23K2101/00—Articles made by soldering, welding or cutting
- B23K2101/001—Turbines
-
- 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
-
- 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
- Y10S—TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10S29/00—Metal working
- Y10S29/031—Pressing powder with other step
-
- 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
- Y10S—TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10S420/00—Alloys or metallic compositions
- Y10S420/902—Superplastic
-
- 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
- Y10T29/49316—Impeller making
- Y10T29/4932—Turbomachine making
- Y10T29/49321—Assembling individual fluid flow interacting members, e.g., blades, vanes, buckets, on rotary support member
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Manufacturing & Machinery (AREA)
- Chemical & Material Sciences (AREA)
- Materials Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Composite Materials (AREA)
- Ceramic Engineering (AREA)
- Pressure Welding/Diffusion-Bonding (AREA)
- Forging (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
- Rotary Pumps (AREA)
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US06/635,782 US4529452A (en) | 1984-07-30 | 1984-07-30 | Process for fabricating multi-alloy components |
Publications (2)
Publication Number | Publication Date |
---|---|
IL75447A0 IL75447A0 (en) | 1985-10-31 |
IL75447A true IL75447A (en) | 1987-08-31 |
Family
ID=24549101
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
IL75447A IL75447A (en) | 1984-07-30 | 1985-06-07 | Process for fabricating multi-alloy components |
Country Status (6)
Country | Link |
---|---|
US (1) | US4529452A (no) |
EP (1) | EP0171344B1 (no) |
JP (1) | JPH0818146B2 (no) |
DE (2) | DE3568148D1 (no) |
IL (1) | IL75447A (no) |
NO (1) | NO162896C (no) |
Families Citing this family (87)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4659288A (en) * | 1984-12-10 | 1987-04-21 | The Garrett Corporation | Dual alloy radial turbine rotor with hub material exposed in saddle regions of blade ring |
US4680160A (en) * | 1985-12-11 | 1987-07-14 | Trw Inc. | Method of forming a rotor |
US4907736A (en) * | 1986-06-27 | 1990-03-13 | Airfoil Textron Inc. | Method of forming articles |
US5573609A (en) * | 1987-03-30 | 1996-11-12 | Rockwell International Corporation | Hot isostatic pressing of single crystal superalloy articles |
US4820358A (en) * | 1987-04-01 | 1989-04-11 | General Electric Company | Method of making high strength superalloy components with graded properties |
US4864706A (en) * | 1987-08-12 | 1989-09-12 | United Technologies Corporation | Fabrication of dual alloy integrally bladed rotors |
US5312650A (en) * | 1988-01-12 | 1994-05-17 | Howmet Corporation | Method of forming a composite article by metal spraying |
US5106012A (en) * | 1989-07-10 | 1992-04-21 | Wyman-Gordon Company | Dual-alloy disk system |
DE68916432T2 (de) * | 1988-07-29 | 1995-01-19 | Wyman Gordon Co | Plattensystem mit doppelter legierung. |
US4907947A (en) * | 1988-07-29 | 1990-03-13 | Allied-Signal Inc. | Heat treatment for dual alloy turbine wheels |
US5161950A (en) * | 1989-10-04 | 1992-11-10 | General Electric Company | Dual alloy turbine disk |
US5100050A (en) * | 1989-10-04 | 1992-03-31 | General Electric Company | Method of manufacturing dual alloy turbine disks |
GB2237758B (en) * | 1989-11-07 | 1992-10-21 | Rolls Royce Plc | Rotor assembly and method of manufacture |
US5061154A (en) * | 1989-12-11 | 1991-10-29 | Allied-Signal Inc. | Radial turbine rotor with improved saddle life |
CA2030427A1 (en) * | 1989-12-19 | 1991-06-20 | Jonathan S. Stinson | Method of enhancing bond joint structural integrity of spray cast articles |
US5074925A (en) * | 1990-06-25 | 1991-12-24 | The United States Of America As Represented By The Secretary Of The Air Force | Thermomechanical fabrication of net shape single crystal airfoils |
US5113583A (en) * | 1990-09-14 | 1992-05-19 | United Technologies Corporation | Integrally bladed rotor fabrication |
US5292385A (en) * | 1991-12-18 | 1994-03-08 | Alliedsignal Inc. | Turbine rotor having improved rim durability |
DE4219470A1 (de) * | 1992-06-13 | 1993-12-16 | Asea Brown Boveri | Bauteil für hohe Temperaturen, insbesondere Turbinenschaufel, und Verfahren zur Herstellung dieses Bauteils |
DE4219469A1 (de) * | 1992-06-13 | 1993-12-16 | Asea Brown Boveri | Hohen Temperaturen aussetzbares Bauteil, insbesondere Turbinenschaufel, und Verfahren zur Herstellung dieses Bauteils |
US5273708A (en) * | 1992-06-23 | 1993-12-28 | Howmet Corporation | Method of making a dual alloy article |
GB2269555B (en) * | 1992-08-14 | 1995-01-04 | Rolls Royce Plc | A method of manufacturing an article by superplastic forming and diffusion bonding |
US5457884A (en) * | 1992-08-14 | 1995-10-17 | Rolls-Royce Plc | Method of manufacturing an article by superplastic forming and diffusion bonding |
US5820700A (en) * | 1993-06-10 | 1998-10-13 | United Technologies Corporation | Nickel base superalloy columnar grain and equiaxed materials with improved performance in hydrogen and air |
US5581882A (en) * | 1994-06-07 | 1996-12-10 | Rolls-Royce Plc | Method of manufacturing an article by superplastic forming and diffusion bonding |
FR2723868B1 (fr) * | 1994-08-24 | 1996-09-20 | Snecma | Procede d'obtention d'une piece circulaire metallique a aubes |
US5665180A (en) * | 1995-06-07 | 1997-09-09 | The United States Of America As Represented By The Secretary Of The Air Force | Method for hot rolling single crystal nickel base superalloys |
US5688108A (en) * | 1995-08-01 | 1997-11-18 | Allison Engine Company, Inc. | High temperature rotor blade attachment |
US5609471A (en) * | 1995-12-07 | 1997-03-11 | Allison Advanced Development Company, Inc. | Multiproperty rotor disk and method of manufacture |
US6325871B1 (en) | 1997-10-27 | 2001-12-04 | Siemens Westinghouse Power Corporation | Method of bonding cast superalloys |
AU3447799A (en) | 1997-10-27 | 1999-07-19 | Siemens Westinghouse Power Corporation | Turbine components comprising thin skins bonded to superalloy substrates |
FR2784616B1 (fr) * | 1998-10-15 | 2000-11-17 | Snecma | Procede d'obtention de pieces metalliques minces, legeres et rigides |
US6331361B1 (en) * | 1998-11-19 | 2001-12-18 | Hickham Industries, Inc. | Methods for manufacture and repair and resulting components with directionally solidified or single crystal materials |
US6780497B1 (en) * | 1999-08-05 | 2004-08-24 | Gore Enterprise Holdings, Inc. | Surface modified expanded polytetrafluoroethylene devices and methods of producing the same |
US6596685B2 (en) | 2000-01-19 | 2003-07-22 | Kao Corporation | Softener composition |
US6499953B1 (en) | 2000-09-29 | 2002-12-31 | Pratt & Whitney Canada Corp. | Dual flow impeller |
US6838427B2 (en) | 2001-06-08 | 2005-01-04 | Kao Corporation | Softener composition |
US6902096B2 (en) * | 2001-10-29 | 2005-06-07 | United Technologies Corporation | Method of joining material |
US6709771B2 (en) | 2002-05-24 | 2004-03-23 | Siemens Westinghouse Power Corporation | Hybrid single crystal-powder metallurgy turbine component |
US6935840B2 (en) * | 2002-07-15 | 2005-08-30 | Pratt & Whitney Canada Corp. | Low cycle fatigue life (LCF) impeller design concept |
US7392927B2 (en) * | 2003-04-17 | 2008-07-01 | General Electric Company | Combinatorial production of material compositions from a single sample |
US7338259B2 (en) * | 2004-03-02 | 2008-03-04 | United Technologies Corporation | High modulus metallic component for high vibratory operation |
FR2873940B1 (fr) * | 2004-08-03 | 2008-01-04 | Snecma Moteurs Sa | Procede de fabrication de pieces constitutives d'une aube creuse par laminage |
US7560065B2 (en) * | 2004-10-08 | 2009-07-14 | Igor Troitski | Method and system for manufacturing of multi-component complex shape parts consisting of monolithic and powder materials working at different performance conditions |
US7316057B2 (en) * | 2004-10-08 | 2008-01-08 | Siemens Power Generation, Inc. | Method of manufacturing a rotating apparatus disk |
DE102005006047A1 (de) * | 2005-02-10 | 2006-09-07 | Mtu Aero Engines Gmbh | Verfahren zur Herstellung und/oder Reparatur eines integral beschaufelten Rotors |
US9322089B2 (en) * | 2006-06-02 | 2016-04-26 | Alstom Technology Ltd | Nickel-base alloy for gas turbine applications |
GB0718026D0 (en) * | 2007-09-15 | 2007-10-24 | Rolls Royce Plc | Joining method and a resultant article |
US8206117B2 (en) * | 2007-12-19 | 2012-06-26 | Honeywell International Inc. | Turbine components and methods of manufacturing turbine components |
US8187724B2 (en) * | 2009-02-24 | 2012-05-29 | Honeywell International Inc. | Method of manufacture of a dual alloy impeller |
US9399258B2 (en) * | 2009-09-10 | 2016-07-26 | Aerojet Rocketdyne Of De, Inc. | Method of processing a bimetallic part |
GB0920697D0 (en) * | 2009-11-26 | 2010-01-13 | Rolls Royce Plc | Method of manufacturing a multiple composition component |
US8480368B2 (en) * | 2010-02-05 | 2013-07-09 | General Electric Company | Welding process and component produced therefrom |
GB201005270D0 (en) * | 2010-03-30 | 2010-05-12 | Rolls Royce Plc | A method and apparatus for manufacturing a rotor disc |
IT1399883B1 (it) | 2010-05-18 | 2013-05-09 | Nuova Pignone S R L | Girante incamiciata con materiale funzionale graduato e metodo |
US8727203B2 (en) | 2010-09-16 | 2014-05-20 | Howmedica Osteonics Corp. | Methods for manufacturing porous orthopaedic implants |
US8992168B2 (en) | 2011-10-28 | 2015-03-31 | United Technologies Corporation | Rotating vane seal with cooling air passages |
US8944762B2 (en) | 2011-10-28 | 2015-02-03 | United Technologies Corporation | Spoked spacer for a gas turbine engine |
US9938831B2 (en) | 2011-10-28 | 2018-04-10 | United Technologies Corporation | Spoked rotor for a gas turbine engine |
GB201200360D0 (en) * | 2012-01-11 | 2012-02-22 | Rolls Royce Plc | Component production method |
US8408446B1 (en) | 2012-02-13 | 2013-04-02 | Honeywell International Inc. | Methods and tooling assemblies for the manufacture of metallurgically-consolidated turbine engine components |
US10309232B2 (en) * | 2012-02-29 | 2019-06-04 | United Technologies Corporation | Gas turbine engine with stage dependent material selection for blades and disk |
US9033670B2 (en) | 2012-04-11 | 2015-05-19 | Honeywell International Inc. | Axially-split radial turbines and methods for the manufacture thereof |
US9115586B2 (en) | 2012-04-19 | 2015-08-25 | Honeywell International Inc. | Axially-split radial turbine |
US20140140859A1 (en) * | 2012-09-28 | 2014-05-22 | United Technologies Corporation | Uber-cooled multi-alloy integrally bladed rotor |
US9574573B2 (en) * | 2012-11-06 | 2017-02-21 | Syncrude Canada Ltd. In Trust For The Owners Of The Syncrude Project As Such Owners Exist Now And In The Future | Wear resistant slurry pump parts produced using hot isostatic pressing |
US20150298247A1 (en) * | 2012-11-30 | 2015-10-22 | European Space Agency | Method of manufacturing a metallic component from individual units arranged in a space filling arrangement |
US9702252B2 (en) * | 2012-12-19 | 2017-07-11 | Honeywell International Inc. | Turbine nozzles with slip joints and methods for the production thereof |
US9726044B2 (en) | 2013-02-12 | 2017-08-08 | United Technologies Corporation | Consumable assembly mistake proofing tool for a gas turbine engine |
US9476305B2 (en) | 2013-05-13 | 2016-10-25 | Honeywell International Inc. | Impingement-cooled turbine rotor |
US9163322B2 (en) | 2013-07-01 | 2015-10-20 | General Electric Company | Method and apparatus for refurbishing turbine components |
US10370984B2 (en) | 2013-12-06 | 2019-08-06 | United Technologies Corporation | Aluminum alloy airfoil with designed crystallographic texture |
US9567554B2 (en) | 2014-01-10 | 2017-02-14 | General Electric Company | Apparatus, method, and solvent for cleaning turbine components |
US20220097139A1 (en) * | 2014-04-29 | 2022-03-31 | Saint Jean Industries | Method for the production of parts made from metal or metal matrix composite and resulting from additive manufacturing followed by an operation involving the forging of said parts |
US20160146024A1 (en) * | 2014-11-24 | 2016-05-26 | Honeywell International Inc. | Hybrid bonded turbine rotors and methods for manufacturing the same |
US10030517B2 (en) * | 2015-01-20 | 2018-07-24 | United Technologies Corporation | Rotor disk boss |
US9938834B2 (en) | 2015-04-30 | 2018-04-10 | Honeywell International Inc. | Bladed gas turbine engine rotors having deposited transition rings and methods for the manufacture thereof |
DE102015111746A1 (de) * | 2015-07-20 | 2017-01-26 | Rolls-Royce Deutschland Ltd & Co Kg | Gekühltes Turbinenlaufrad, insbesondere für ein Flugtriebwerk |
US9951632B2 (en) | 2015-07-23 | 2018-04-24 | Honeywell International Inc. | Hybrid bonded turbine rotors and methods for manufacturing the same |
US10294804B2 (en) | 2015-08-11 | 2019-05-21 | Honeywell International Inc. | Dual alloy gas turbine engine rotors and methods for the manufacture thereof |
US10036254B2 (en) | 2015-11-12 | 2018-07-31 | Honeywell International Inc. | Dual alloy bladed rotors suitable for usage in gas turbine engines and methods for the manufacture thereof |
US11313673B2 (en) * | 2017-01-24 | 2022-04-26 | General Electric Company | Methods of making a component with an integral strain indicator |
FR3076750B1 (fr) * | 2018-01-18 | 2020-06-05 | Safran Power Units | Procede de fabrication d'une roue pour une turbomachine |
US11130174B2 (en) * | 2018-08-03 | 2021-09-28 | General Electric Company | Support structure and methods for additively manufacturing impellers |
CN110125629B (zh) * | 2019-06-27 | 2020-04-07 | 马鞍山市恒利达机械刀片有限公司 | 一种高平面度的滚剪刀片加工工艺 |
CN114310161B (zh) * | 2021-12-13 | 2022-11-22 | 哈尔滨工业大学 | 一种基于高表面质量轻质合金三维点阵夹层结构制备方法 |
CN115488342B (zh) * | 2022-08-31 | 2024-04-02 | 中国机械总院集团北京机电研究所有限公司 | 异种金属整体叶盘增等材短流程制备方法 |
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US4477955A (en) * | 1980-04-10 | 1984-10-23 | Cameron Iron Works, Inc. | Method of producing a lined structure |
JPS5728690A (en) * | 1980-07-25 | 1982-02-16 | Hitachi Ltd | Method for joining titanium alloy |
SE446606B (sv) * | 1981-08-27 | 1986-09-29 | Stal Laval Turbin Ab | Sett att framstella skovelringar och skivor med skovlar for roterande maskiner sasom kompressorer eller turbiner |
GB2107225A (en) * | 1981-10-16 | 1983-04-27 | Rolls Royce | Method of providing location means for gas turbine engine components |
US4605452A (en) * | 1981-12-14 | 1986-08-12 | United Technologies Corporation | Single crystal articles having controlled secondary crystallographic orientation |
JPS5919037A (ja) * | 1982-07-22 | 1984-01-31 | Mitsubishi Keikinzoku Kogyo Kk | 超塑性金属板から中空物品を製造する方法 |
US4481047A (en) * | 1982-09-22 | 1984-11-06 | United Technologies Corporation | High modulus shafts |
US4402767A (en) * | 1982-12-27 | 1983-09-06 | Owens-Corning Fiberglas Corporation | Fabrication of alloys |
-
1984
- 1984-07-30 US US06/635,782 patent/US4529452A/en not_active Expired - Lifetime
-
1985
- 1985-06-06 DE DE8585630085T patent/DE3568148D1/de not_active Expired
- 1985-06-06 EP EP85630085A patent/EP0171344B1/en not_active Expired
- 1985-06-06 DE DE198585630085T patent/DE171344T1/de active Pending
- 1985-06-07 IL IL75447A patent/IL75447A/xx not_active IP Right Cessation
- 1985-06-25 NO NO852546A patent/NO162896C/no unknown
- 1985-06-27 JP JP60141410A patent/JPH0818146B2/ja not_active Expired - Lifetime
Also Published As
Publication number | Publication date |
---|---|
JPH0818146B2 (ja) | 1996-02-28 |
EP0171344B1 (en) | 1989-02-08 |
NO162896C (no) | 1990-03-07 |
US4529452A (en) | 1985-07-16 |
NO162896B (no) | 1989-11-27 |
JPS6137387A (ja) | 1986-02-22 |
DE171344T1 (de) | 1986-07-24 |
NO852546L (no) | 1986-01-31 |
DE3568148D1 (en) | 1989-03-16 |
IL75447A0 (en) | 1985-10-31 |
EP0171344A1 (en) | 1986-02-12 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
KB | Patent renewed | ||
KB | Patent renewed | ||
EXP | Patent expired |