GB9104609D0 - Nozzle guide vane arrangement - Google Patents

Nozzle guide vane arrangement

Info

Publication number
GB9104609D0
GB9104609D0 GB919104609A GB9104609A GB9104609D0 GB 9104609 D0 GB9104609 D0 GB 9104609D0 GB 919104609 A GB919104609 A GB 919104609A GB 9104609 A GB9104609 A GB 9104609A GB 9104609 D0 GB9104609 D0 GB 9104609D0
Authority
GB
United Kingdom
Prior art keywords
guide vane
nozzle guide
vane arrangement
arrangement
nozzle
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.)
Withdrawn
Application number
GB919104609A
Other versions
GB2253443A (en
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
Priority to GB9104609A priority Critical patent/GB2253443A/en
Publication of GB9104609D0 publication Critical patent/GB9104609D0/en
Publication of GB2253443A publication Critical patent/GB2253443A/en
Withdrawn legal-status Critical Current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
    • F01D5/00—Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
    • F01D5/12—Blades
    • F01D5/14—Form or construction
    • F01D5/141—Shape, i.e. outer, aerodynamic form
    • F01D5/145—Means for influencing boundary layers or secondary circulations
    • 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
GB9104609A 1991-03-05 1991-03-05 Gas turbine nozzle guide vane arrangement Withdrawn GB2253443A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB9104609A GB2253443A (en) 1991-03-05 1991-03-05 Gas turbine nozzle guide vane arrangement

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB9104609A GB2253443A (en) 1991-03-05 1991-03-05 Gas turbine nozzle guide vane arrangement

Publications (2)

Publication Number Publication Date
GB9104609D0 true GB9104609D0 (en) 1991-04-17
GB2253443A GB2253443A (en) 1992-09-09

Family

ID=10691004

Family Applications (1)

Application Number Title Priority Date Filing Date
GB9104609A Withdrawn GB2253443A (en) 1991-03-05 1991-03-05 Gas turbine nozzle guide vane arrangement

Country Status (1)

Country Link
GB (1) GB2253443A (en)

Families Citing this family (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5382135A (en) * 1992-11-24 1995-01-17 United Technologies Corporation Rotor blade with cooled integral platform
GB9417406D0 (en) * 1994-08-30 1994-10-19 Gec Alsthom Ltd Turbine blade
US6354797B1 (en) * 2000-07-27 2002-03-12 General Electric Company Brazeless fillet turbine nozzle
US6830432B1 (en) * 2003-06-24 2004-12-14 Siemens Westinghouse Power Corporation Cooling of combustion turbine airfoil fillets
US7217096B2 (en) * 2004-12-13 2007-05-15 General Electric Company Fillet energized turbine stage
US7976274B2 (en) * 2005-12-08 2011-07-12 General Electric Company Methods and apparatus for assembling turbine engines
EP2918779A1 (en) 2014-03-11 2015-09-16 Siemens Aktiengesellschaft Turbine blade

Family Cites Families (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3610769A (en) * 1970-06-08 1971-10-05 Gen Motors Corp Porous facing attachment
GB1400285A (en) * 1972-08-02 1975-07-16 Rolls Royce Hollow cooled vane or blade for a gas turbine engine
US4153386A (en) * 1974-12-11 1979-05-08 United Technologies Corporation Air cooled turbine vanes
FR2313551A1 (en) * 1975-06-02 1976-12-31 United Technologies Corp COOLING A TURBINE BLADE
DE2643049A1 (en) * 1975-10-14 1977-04-21 United Technologies Corp SHOVEL WITH COOLED PLATFORM FOR A FLOW MACHINE
GB2107405B (en) * 1981-10-13 1985-08-14 Rolls Royce Nozzle guide vane for a gas turbine engine

Also Published As

Publication number Publication date
GB2253443A (en) 1992-09-09

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Legal Events

Date Code Title Description
WAP Application withdrawn, taken to be withdrawn or refused ** after publication under section 16(1)