SE8406320D0 - GAS TURBINE ENGINE BLADE - Google Patents

GAS TURBINE ENGINE BLADE

Info

Publication number
SE8406320D0
SE8406320D0 SE8406320A SE8406320A SE8406320D0 SE 8406320 D0 SE8406320 D0 SE 8406320D0 SE 8406320 A SE8406320 A SE 8406320A SE 8406320 A SE8406320 A SE 8406320A SE 8406320 D0 SE8406320 D0 SE 8406320D0
Authority
SE
Sweden
Prior art keywords
gas turbine
turbine engine
engine blade
portions
slopes
Prior art date
Application number
SE8406320A
Other languages
Swedish (sv)
Other versions
SE8406320L (en
Inventor
J G Nourse
J J Bourneuf
D R Abbott
J R Martin
Original Assignee
Gen Electric
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
Priority claimed from US06/560,718 external-priority patent/US4682935A/en
Priority claimed from US06/560,656 external-priority patent/US4585395A/en
Application filed by Gen Electric filed Critical Gen Electric
Publication of SE8406320D0 publication Critical patent/SE8406320D0/en
Publication of SE8406320L publication Critical patent/SE8406320L/en

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

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)

Abstract

A blade 10 for a gas turbine engine has a non-linear stacking axis 30 with portions 40, 42 of differing slopes. The slopes of the portions 40, 42 are of opposite signs. The arrangement provides a compressive component of bending stress on the trailing and leading edges due to centrifugal forces when in use. <IMAGE>
SE8406320A 1983-12-12 1984-12-12 GAS FOR GAS TURBINE ENGINE SE8406320L (en)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US06/560,718 US4682935A (en) 1983-12-12 1983-12-12 Bowed turbine blade
US06/560,656 US4585395A (en) 1983-12-12 1983-12-12 Gas turbine engine blade

Publications (2)

Publication Number Publication Date
SE8406320D0 true SE8406320D0 (en) 1984-12-12
SE8406320L SE8406320L (en) 1985-06-13

Family

ID=27072428

Family Applications (1)

Application Number Title Priority Date Filing Date
SE8406320A SE8406320L (en) 1983-12-12 1984-12-12 GAS FOR GAS TURBINE ENGINE

Country Status (5)

Country Link
DE (1) DE3444810C2 (en)
FR (1) FR2556409B1 (en)
GB (1) GB2151310B (en)
IT (1) IT1178658B (en)
SE (1) SE8406320L (en)

Families Citing this family (22)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2603953B1 (en) * 1986-09-12 1991-02-22 Peugeot Aciers Et Outillage PROPELLER BLADE AND ITS APPLICATION TO MOTOR FANS
FR2643940B1 (en) * 1989-03-01 1991-05-17 Snecma MOBILE VANE OF TURBOMACHINE WITH MOMENT OF COMPENSATED FOOT
JP2665005B2 (en) * 1989-10-24 1997-10-22 三菱重工業株式会社 Blades of axial flow machines
WO1994012390A2 (en) * 1992-11-24 1994-06-09 United Technologies Corporation Coolable rotor blade structure
DE4344189C1 (en) * 1993-12-23 1995-08-03 Mtu Muenchen Gmbh Axial vane grille with swept front edges
GB9417406D0 (en) * 1994-08-30 1994-10-19 Gec Alsthom Ltd Turbine blade
US5525038A (en) * 1994-11-04 1996-06-11 United Technologies Corporation Rotor airfoils to control tip leakage flows
GB0003676D0 (en) * 2000-02-17 2000-04-05 Abb Alstom Power Nv Aerofoils
FR2861128B1 (en) * 2003-10-16 2007-06-08 Snecma Moteurs DEVICE FOR ATTACHING A MOBILE DARK TO A TURBINE ROTOR DISK IN A TURBOMACHINE
CH698109B1 (en) 2005-07-01 2009-05-29 Alstom Technology Ltd Turbomachinery blade.
US7549846B2 (en) 2005-08-03 2009-06-23 United Technologies Corporation Turbine blades
US8087884B2 (en) 2006-11-30 2012-01-03 General Electric Company Advanced booster stator vane
US7967571B2 (en) * 2006-11-30 2011-06-28 General Electric Company Advanced booster rotor blade
US8292574B2 (en) 2006-11-30 2012-10-23 General Electric Company Advanced booster system
US8480372B2 (en) 2008-11-06 2013-07-09 General Electric Company System and method for reducing bucket tip losses
DE102010009615B4 (en) * 2010-02-27 2016-11-17 MTU Aero Engines AG Airfoil with threaded profile cuts
EP2568114A1 (en) 2011-09-09 2013-03-13 Siemens Aktiengesellschaft Method for profiling a replacement blade as a replacement part for an old blade on an axial flow machine
US8894376B2 (en) * 2011-10-28 2014-11-25 General Electric Company Turbomachine blade with tip flare
ITCO20120059A1 (en) * 2012-12-13 2014-06-14 Nuovo Pignone Srl METHODS FOR MANUFACTURING SHAPED SHAPED LOAFERS IN 3D OF TURBOMACCHINE BY ADDITIVE PRODUCTION, TURBOMACCHINA CAVE BLOCK AND TURBOMACCHINE
FR3040071B1 (en) 2015-08-11 2020-03-27 Safran Aircraft Engines TURBOMACHINE ROTOR DAWN
JP6959589B2 (en) * 2018-11-05 2021-11-02 株式会社Ihi Blades of axial fluid machinery
DE102019210880A1 (en) * 2019-07-23 2021-01-28 MTU Aero Engines AG ROTATING BLADE FOR A FLOW MACHINE

Family Cites Families (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DD34133A (en) *
US2110679A (en) * 1936-04-22 1938-03-08 Gen Electric Elastic fluid turbine
US2663493A (en) * 1949-04-26 1953-12-22 A V Roe Canada Ltd Blading for compressors, turbines, and the like
SU411214A1 (en) * 1968-05-12 1974-01-15
GB1231424A (en) * 1968-11-15 1971-05-12
DE1903642A1 (en) * 1969-01-20 1970-08-06 Bbc Sulzer Turbomaschinen Blading for rotors of axial compressors
DE2144600A1 (en) * 1971-09-07 1973-03-15 Maschf Augsburg Nuernberg Ag TWISTED AND TAPERED BLADE FOR AXIAL TURBO MACHINERY
US3989406A (en) * 1974-11-26 1976-11-02 Bolt Beranek And Newman, Inc. Method of and apparatus for preventing leading edge shocks and shock-related noise in transonic and supersonic rotor blades and the like
US4012172A (en) * 1975-09-10 1977-03-15 Avco Corporation Low noise blades for axial flow compressors
JPS5447907A (en) * 1977-09-26 1979-04-16 Hitachi Ltd Blading structure for axial-flow fluid machine
US4621979A (en) * 1979-11-30 1986-11-11 United Technologies Corporation Fan rotor blades of turbofan engines

Also Published As

Publication number Publication date
FR2556409A1 (en) 1985-06-14
GB8430785D0 (en) 1985-01-16
IT8423829A1 (en) 1986-05-30
FR2556409B1 (en) 1991-07-12
IT8423829A0 (en) 1984-11-30
GB2151310A (en) 1985-07-17
DE3444810C2 (en) 1997-09-11
SE8406320L (en) 1985-06-13
GB2151310B (en) 1988-10-19
DE3444810A1 (en) 1985-06-20
IT1178658B (en) 1987-09-16

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Ref document number: 8406320-5

Effective date: 19880809