GB2115883B - Turbomachine airfoil mounting assembly - Google Patents

Turbomachine airfoil mounting assembly

Info

Publication number
GB2115883B
GB2115883B GB08300213A GB8300213A GB2115883B GB 2115883 B GB2115883 B GB 2115883B GB 08300213 A GB08300213 A GB 08300213A GB 8300213 A GB8300213 A GB 8300213A GB 2115883 B GB2115883 B GB 2115883B
Authority
GB
United Kingdom
Prior art keywords
mounting assembly
turbomachine airfoil
airfoil mounting
turbomachine
assembly
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
Application number
GB08300213A
Other versions
GB8300213D0 (en
GB2115883A (en
Inventor
Robert Howard Roth
Bruno Gustav Lampsat
Jack Lee Readnour
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.)
General Electric Co
Original Assignee
General Electric Co
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 General Electric Co filed Critical General Electric Co
Publication of GB8300213D0 publication Critical patent/GB8300213D0/en
Publication of GB2115883A publication Critical patent/GB2115883A/en
Application granted granted Critical
Publication of GB2115883B publication Critical patent/GB2115883B/en
Expired legal-status Critical Current

Links

Classifications

    • 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
    • F01D9/00—Stators
    • F01D9/02—Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles
    • F01D9/04—Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles forming ring or sector
    • F01D9/042—Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles forming ring or sector fixing blades to stators
    • 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
    • F05D2230/60—Assembly 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
    • 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
GB08300213A 1982-02-26 1983-01-06 Turbomachine airfoil mounting assembly Expired GB2115883B (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US35311282A 1982-02-26 1982-02-26

Publications (3)

Publication Number Publication Date
GB8300213D0 GB8300213D0 (en) 1983-02-09
GB2115883A GB2115883A (en) 1983-09-14
GB2115883B true GB2115883B (en) 1986-04-30

Family

ID=23387807

Family Applications (1)

Application Number Title Priority Date Filing Date
GB08300213A Expired GB2115883B (en) 1982-02-26 1983-01-06 Turbomachine airfoil mounting assembly

Country Status (5)

Country Link
JP (1) JPS58165503A (en)
DE (1) DE3305880A1 (en)
FR (1) FR2522362B1 (en)
GB (1) GB2115883B (en)
IT (1) IT1171062B (en)

Families Citing this family (26)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2568953B1 (en) * 1984-08-08 1989-02-10 Ratier Figeac Soc FIXED BLADE FOR REACTORS
US4655682A (en) * 1985-09-30 1987-04-07 United Technologies Corporation Compressor stator assembly having a composite inner diameter shroud
FR2599081B1 (en) * 1986-05-23 1988-07-29 Snecma MULTIFLUX TURBOJET BLOWER RECTIFIER
FR2606071B1 (en) * 1986-10-29 1990-11-30 Snecma STATOR STAGE AND TURBOMACHINE COMPRESSOR COMPRISING THE SAME
FR2610673B1 (en) * 1987-02-05 1991-03-15 Snecma MULTIFLUX TURBOREACTOR WITH EXTERNAL CROWN OF FREQUENCY BLOWER RECTIFIER ON THE CRANKCASE
US4907946A (en) * 1988-08-10 1990-03-13 General Electric Company Resiliently mounted outlet guide vane
US4993918A (en) * 1989-05-19 1991-02-19 United Technologies Corporation Replaceable fairing for a turbine exhaust case
FR2685383B1 (en) * 1991-12-18 1994-02-11 Snecma STRUCTURAL ARM OF THE HOUSING OF A TURBOMACHINE.
US5292227A (en) * 1992-12-10 1994-03-08 General Electric Company Turbine frame
US5411370A (en) * 1994-08-01 1995-05-02 United Technologies Corporation Vibration damping shroud for a turbomachine vane
DE19547653C2 (en) * 1995-12-20 1999-08-19 Abb Patent Gmbh Guide device for a turbine with a guide vane carrier and method for producing this guide device
US5690469A (en) * 1996-06-06 1997-11-25 United Technologies Corporation Method and apparatus for replacing a vane assembly in a turbine engine
JP4502517B2 (en) * 1999-03-24 2010-07-14 シーメンス アクチエンゲゼルシヤフト Guide vanes and guide vane rings of fluid machinery
US6425736B1 (en) * 1999-08-09 2002-07-30 United Technologies Corporation Stator assembly for a rotary machine and method for making the stator assembly
US6619917B2 (en) * 2000-12-19 2003-09-16 United Technologies Corporation Machined fan exit guide vane attachment pockets for use in a gas turbine
US6773228B2 (en) * 2002-07-03 2004-08-10 General Electric Company Methods and apparatus for turbine nozzle locks
GB2418709B (en) * 2004-09-29 2007-10-10 Rolls Royce Plc Damped assembly
GB2427900B (en) 2005-07-02 2007-10-10 Rolls Royce Plc Vane support in a gas turbine engine
US7648336B2 (en) * 2006-01-03 2010-01-19 General Electric Company Apparatus and method for assembling a gas turbine stator
JP2007255224A (en) * 2006-03-20 2007-10-04 Mitsubishi Heavy Ind Ltd Turbine blade and gas turbine
US7614848B2 (en) * 2006-10-10 2009-11-10 United Technologies Corporation Fan exit guide vane repair method and apparatus
WO2009157817A1 (en) * 2008-06-26 2009-12-30 Volvo Aero Corporation Vane assembly and method of fabricating, and a turbo-machine with such vane assembly
EP2196629B1 (en) * 2008-12-11 2018-05-16 Safran Aero Boosters SA Segmented composite shroud ring of an axial compressor
US8206100B2 (en) * 2008-12-31 2012-06-26 General Electric Company Stator assembly for a gas turbine engine
GB201106050D0 (en) 2011-04-11 2011-05-25 Rolls Royce Plc A retention device for a composite blade of a gas turbine engine
GB202108717D0 (en) 2021-06-18 2021-08-04 Rolls Royce Plc Vane joint

Family Cites Families (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB660383A (en) * 1949-02-23 1951-11-07 Winnett Boyd Blade mounting for axial-flow compressors and the like
GB722458A (en) * 1952-07-14 1955-01-26 Bristol Aeroplane Co Ltd Improvements in or relating to the manufacture of blades for use in axial flow compressors or the like
GB753224A (en) * 1953-04-13 1956-07-18 Rolls Royce Improvements in or relating to blading for turbines or compressors
US3689174A (en) * 1971-01-11 1972-09-05 Westinghouse Electric Corp Axial flow turbine structure
US3836282A (en) * 1973-03-28 1974-09-17 United Aircraft Corp Stator vane support and construction thereof
US4378961A (en) * 1979-01-10 1983-04-05 United Technologies Corporation Case assembly for supporting stator vanes

Also Published As

Publication number Publication date
JPH0425408B2 (en) 1992-04-30
JPS58165503A (en) 1983-09-30
IT8319761A0 (en) 1983-02-25
IT8319761A1 (en) 1984-08-25
GB8300213D0 (en) 1983-02-09
IT1171062B (en) 1987-06-10
DE3305880C2 (en) 1993-04-29
GB2115883A (en) 1983-09-14
FR2522362A1 (en) 1983-09-02
FR2522362B1 (en) 1988-12-30
DE3305880A1 (en) 1983-09-15

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Legal Events

Date Code Title Description
PE20 Patent expired after termination of 20 years

Effective date: 20030105