DE69409498D1 - Integrale Schaufel-Rotoreinheit - Google Patents

Integrale Schaufel-Rotoreinheit

Info

Publication number
DE69409498D1
DE69409498D1 DE69409498T DE69409498T DE69409498D1 DE 69409498 D1 DE69409498 D1 DE 69409498D1 DE 69409498 T DE69409498 T DE 69409498T DE 69409498 T DE69409498 T DE 69409498T DE 69409498 D1 DE69409498 D1 DE 69409498D1
Authority
DE
Germany
Prior art keywords
rotor unit
blade rotor
integral blade
integral
unit
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.)
Expired - Lifetime
Application number
DE69409498T
Other languages
English (en)
Other versions
DE69409498T2 (de
Inventor
Derek John Foster
Peter John Gillbanks
Keith Charles Moloney
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.)
Rolls Royce PLC
Original Assignee
Rolls Royce PLC
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 Rolls Royce PLC filed Critical Rolls Royce PLC
Application granted granted Critical
Publication of DE69409498D1 publication Critical patent/DE69409498D1/de
Publication of DE69409498T2 publication Critical patent/DE69409498T2/de
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B23MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
    • B23KSOLDERING OR UNSOLDERING; WELDING; CLADDING OR PLATING BY SOLDERING OR WELDING; CUTTING BY APPLYING HEAT LOCALLY, e.g. FLAME CUTTING; WORKING BY LASER BEAM
    • B23K20/00Non-electric welding by applying impact or other pressure, with or without the application of heat, e.g. cladding or plating
    • B23K20/12Non-electric welding by applying impact or other pressure, with or without the application of heat, e.g. cladding or plating the heat being generated by friction; Friction welding
    • B23K20/1215Non-electric welding by applying impact or other pressure, with or without the application of heat, e.g. cladding or plating the heat being generated by friction; Friction welding for other purposes than joining, e.g. built-up welding
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01DNON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D5/00Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
    • F01D5/12Blades
    • F01D5/14Form or construction
    • F01D5/20Specially-shaped blade tips to seal space between tips and stator
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01DNON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D5/00Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
    • F01D5/34Rotor-blade aggregates of unitary construction, e.g. formed of sheet laminae
    • YGENERAL 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
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10TTECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T29/00Metal working
    • Y10T29/49Method of mechanical manufacture
    • Y10T29/49316Impeller making
    • Y10T29/4932Turbomachine making
    • Y10T29/49325Shaping integrally bladed rotor

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Ceramic Engineering (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Forging (AREA)
DE69409498T 1993-12-08 1994-11-25 Integrale Schaufel-Rotoreinheit Expired - Lifetime DE69409498T2 (de)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB939325135A GB9325135D0 (en) 1993-12-08 1993-12-08 Manufacture of wear resistant components

Publications (2)

Publication Number Publication Date
DE69409498D1 true DE69409498D1 (de) 1998-05-14
DE69409498T2 DE69409498T2 (de) 1998-08-13

Family

ID=10746303

Family Applications (1)

Application Number Title Priority Date Filing Date
DE69409498T Expired - Lifetime DE69409498T2 (de) 1993-12-08 1994-11-25 Integrale Schaufel-Rotoreinheit

Country Status (4)

Country Link
US (1) US5556257A (de)
EP (1) EP0666407B1 (de)
DE (1) DE69409498T2 (de)
GB (1) GB9325135D0 (de)

Families Citing this family (19)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
AT2429U3 (de) * 1998-07-10 1999-01-25 Jakadofsky Peter Turbinenrad
DE10047307A1 (de) * 2000-09-25 2002-08-01 Alstom Switzerland Ltd Dichtungsanordnung
US6544003B1 (en) * 2000-11-08 2003-04-08 General Electric Co. Gas turbine blisk with ceramic foam blades and its preparation
FR2828824B1 (fr) 2001-08-23 2003-12-05 Snecma Moteurs Procede de fabrication d'un disque aubage monobloc de rotor et disque correspondant
US6926928B2 (en) * 2002-07-19 2005-08-09 General Electric Company Protection of a gas turbine component by a vapor-deposited oxide coating
US7334997B2 (en) * 2005-09-16 2008-02-26 General Electric Company Hybrid blisk
US7784182B2 (en) * 2006-11-08 2010-08-31 General Electric Company System for manufacturing a rotor having an MMC ring component and a unitary airfoil component
US8011892B2 (en) * 2007-06-28 2011-09-06 United Technologies Corporation Turbine blade nested seal and damper assembly
US20090028714A1 (en) * 2007-07-25 2009-01-29 Tahany Ibrahim El-Wardany Method of designing tool and tool path for forming a rotor blade including an airfoil portion
US8137075B2 (en) * 2007-08-31 2012-03-20 Honeywell International Inc. Compressor impellers, compressor sections including the compressor impellers, and methods of manufacturing
DE102008017494A1 (de) * 2008-04-04 2009-10-08 Rolls-Royce Deutschland Ltd & Co Kg Verfahren zur Fertigung integral beschaufelter Rotoren
DE102009010109A1 (de) 2009-02-21 2010-09-23 Mtu Aero Engines Gmbh Herstellung einer Turbinenblisk mit einer Oxikations- bzw. Korrosionsschutzschicht
US8925201B2 (en) * 2009-06-29 2015-01-06 Pratt & Whitney Canada Corp. Method and apparatus for providing rotor discs
JP5628307B2 (ja) * 2009-06-30 2014-11-19 ゼネラル・エレクトリック・カンパニイ 先端摩擦荷重を低減するためのロータブレード及び方法
US8657570B2 (en) 2009-06-30 2014-02-25 General Electric Company Rotor blade with reduced rub loading
US8662834B2 (en) 2009-06-30 2014-03-04 General Electric Company Method for reducing tip rub loading
US8403645B2 (en) 2009-09-16 2013-03-26 United Technologies Corporation Turbofan flow path trenches
EP2369136B1 (de) * 2010-03-12 2012-12-19 Techspace Aero S.A. Gewichtsreduzierte einteilige Mehrstufentrommel eines Axialverdichters
FR3116561B1 (fr) * 2020-11-25 2023-09-22 Safran Aircraft Engines Procédé et dispositif de fabrication d’un disque de turbomachine bi-matière et disque obtenu par ce procédé

Family Cites Families (22)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB363297A (en) * 1930-07-22 1931-12-17 Schmidt Sche Heissdampf Improvements in and relating to the blades of rotary fans
GB1302036A (de) * 1969-06-26 1973-01-04
US3885294A (en) * 1974-04-03 1975-05-27 Ford Motor Co Method of making a bonded silicon nitride article having portions of different density
SE7809198L (sv) * 1977-09-09 1979-03-10 United Technologies Corp Slipmaterial, anvendbart som dispersoid i metalliskt bindemedel, serskilt vid hoga temperaturer, samt forfarande for slipmaterialets framstellning
US4169020A (en) * 1977-12-21 1979-09-25 General Electric Company Method for making an improved gas seal
US4436485A (en) * 1978-04-17 1984-03-13 General Motors Corporation Turbine wheel with integral DS blades and equiaxed hub
US4581300A (en) * 1980-06-23 1986-04-08 The Garrett Corporation Dual alloy turbine wheels
US4479293A (en) * 1981-11-27 1984-10-30 United Technologies Corporation Process for fabricating integrally bladed bimetallic rotors
US4422648A (en) * 1982-06-17 1983-12-27 United Technologies Corporation Ceramic faced outer air seal for gas turbine engines
US4536932A (en) * 1982-11-22 1985-08-27 United Technologies Corporation Method for eliminating low cycle fatigue cracking in integrally bladed disks
DE3401742C2 (de) * 1984-01-19 1986-08-14 MTU Motoren- und Turbinen-Union München GmbH, 8000 München Rotor für einen Axialverdichter
US4610698A (en) * 1984-06-25 1986-09-09 United Technologies Corporation Abrasive surface coating process for superalloys
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
GB8603832D0 (en) * 1986-02-17 1986-03-26 Friction Technology Ltd Forming hard edges on materials
US4884820A (en) * 1987-05-19 1989-12-05 Union Carbide Corporation Wear resistant, abrasive laser-engraved ceramic or metallic carbide surfaces for rotary labyrinth seal members
US4851188A (en) * 1987-12-21 1989-07-25 United Technologies Corporation Method for making a turbine blade having a wear resistant layer sintered to the blade tip surface
US4881686A (en) * 1988-10-13 1989-11-21 Hunter-Melnor, Inc. Temperature recovery display device for an electronic programmable thermostat
US5059095A (en) * 1989-10-30 1991-10-22 The Perkin-Elmer Corporation Turbine rotor blade tip coated with alumina-zirconia ceramic
GB2242848A (en) * 1990-04-12 1991-10-16 Frictec Ltd Depositing coating on materials
AU8265291A (en) * 1990-09-04 1992-03-12 Welding Institute, The Friction surfacing
US5183390A (en) * 1991-07-10 1993-02-02 Westinghouse Electric Corp. Method of forming a trailing edge on a steam turbine blade and the blade made thereby
GB2268430B (en) * 1992-07-07 1996-02-07 Frictec Ltd Method of coating materials

Also Published As

Publication number Publication date
GB9325135D0 (en) 1994-02-09
EP0666407A2 (de) 1995-08-09
EP0666407B1 (de) 1998-04-08
DE69409498T2 (de) 1998-08-13
EP0666407A3 (de) 1996-09-11
US5556257A (en) 1996-09-17

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Legal Events

Date Code Title Description
8364 No opposition during term of opposition