FR2584136B1 - Piece a profil d'ailette pour moteur a turbine a gaz - Google Patents

Piece a profil d'ailette pour moteur a turbine a gaz

Info

Publication number
FR2584136B1
FR2584136B1 FR8606302A FR8606302A FR2584136B1 FR 2584136 B1 FR2584136 B1 FR 2584136B1 FR 8606302 A FR8606302 A FR 8606302A FR 8606302 A FR8606302 A FR 8606302A FR 2584136 B1 FR2584136 B1 FR 2584136B1
Authority
FR
France
Prior art keywords
gas turbine
turbine engine
profile part
blade profile
blade
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 - Fee Related
Application number
FR8606302A
Other languages
English (en)
Other versions
FR2584136A1 (fr
Inventor
Hamblett Et Duncan John Livsey Martin
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
Publication of FR2584136A1 publication Critical patent/FR2584136A1/fr
Application granted granted Critical
Publication of FR2584136B1 publication Critical patent/FR2584136B1/fr
Anticipated expiration legal-status Critical
Expired - Fee Related 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
    • 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
    • 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
    • F05D2250/00—Geometry
    • F05D2250/10—Two-dimensional
    • F05D2250/16—Two-dimensional parabolic
    • 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
    • Y10S415/00—Rotary kinetic fluid motors or pumps
    • Y10S415/914—Device to control boundary layer

Landscapes

  • Engineering & Computer Science (AREA)
  • Physics & Mathematics (AREA)
  • Fluid Mechanics (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
FR8606302A 1985-06-28 1986-04-30 Piece a profil d'ailette pour moteur a turbine a gaz Expired - Fee Related FR2584136B1 (fr)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB08516436A GB2177163B (en) 1985-06-28 1985-06-28 Improvements in or relating to aerofoil section members for gas turbine engines

Publications (2)

Publication Number Publication Date
FR2584136A1 FR2584136A1 (fr) 1987-01-02
FR2584136B1 true FR2584136B1 (fr) 1993-11-12

Family

ID=10581493

Family Applications (1)

Application Number Title Priority Date Filing Date
FR8606302A Expired - Fee Related FR2584136B1 (fr) 1985-06-28 1986-04-30 Piece a profil d'ailette pour moteur a turbine a gaz

Country Status (5)

Country Link
US (1) US4696621A (fr)
JP (1) JPS623103A (fr)
DE (1) DE3614467C2 (fr)
FR (1) FR2584136B1 (fr)
GB (1) GB2177163B (fr)

Families Citing this family (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE4228879A1 (de) * 1992-08-29 1994-03-03 Asea Brown Boveri Axialdurchströmte Turbine
US5480285A (en) * 1993-08-23 1996-01-02 Westinghouse Electric Corporation Steam turbine blade
US5326221A (en) * 1993-08-27 1994-07-05 General Electric Company Over-cambered stage design for steam turbines
GB9417406D0 (en) * 1994-08-30 1994-10-19 Gec Alsthom Ltd Turbine blade
EP0798447B1 (fr) * 1996-03-28 2001-09-05 MTU Aero Engines GmbH Aube pour une turbomachine
JPH10103002A (ja) * 1996-09-30 1998-04-21 Toshiba Corp 軸流流体機械用翼
EP1468974A3 (fr) 2003-04-17 2004-12-01 Hoya Corporation Verre optique, préforme à moulage et méthode de sa production et élément optique et méthode de sa production
US11661850B2 (en) * 2018-11-09 2023-05-30 Raytheon Technologies Corporation Airfoil with convex sides and multi-piece baffle
US11421702B2 (en) 2019-08-21 2022-08-23 Pratt & Whitney Canada Corp. Impeller with chordwise vane thickness variation

Family Cites Families (13)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB712523A (en) * 1950-03-03 1954-07-28 Rolls Royce Improvements in or relating to guide vane assemblies in annular fluid ducts
US2801790A (en) * 1950-06-21 1957-08-06 United Aircraft Corp Compressor blading
US2746672A (en) * 1950-07-27 1956-05-22 United Aircraft Corp Compressor blading
US2920864A (en) * 1956-05-14 1960-01-12 United Aircraft Corp Secondary flow reducer
GB891090A (en) * 1959-08-24 1962-03-07 Power Jets Res & Dev Ltd Improvements in and relating to turbine and compressor blades
BE638547A (fr) * 1962-10-29 1900-01-01
GB995685A (en) * 1963-05-31 1965-06-23 Frederick John Lardner Improvements in and relating to propeller blades
US3572962A (en) * 1969-06-02 1971-03-30 Canadian Patents Dev Stator blading for noise reduction in turbomachinery
US3745629A (en) * 1972-04-12 1973-07-17 Secr Defence Method of determining optimal shapes for stator blades
US4131387A (en) * 1976-02-27 1978-12-26 General Electric Company Curved blade turbomachinery noise reduction
JPS5447907A (en) * 1977-09-26 1979-04-16 Hitachi Ltd Blading structure for axial-flow fluid machine
JPS56162206A (en) * 1980-05-16 1981-12-14 Toshiba Corp Turbine blade
GB2129882B (en) * 1982-11-10 1986-04-16 Rolls Royce Gas turbine stator vane

Also Published As

Publication number Publication date
GB2177163A (en) 1987-01-14
GB2177163B (en) 1988-12-07
JPS623103A (ja) 1987-01-09
DE3614467C2 (de) 1993-10-14
US4696621A (en) 1987-09-29
DE3614467A1 (de) 1987-01-08
FR2584136A1 (fr) 1987-01-02

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Legal Events

Date Code Title Description
ST Notification of lapse