DE3862652D1 - Geblaeseblattsteigungsverstellvorrichtung. - Google Patents

Geblaeseblattsteigungsverstellvorrichtung.

Info

Publication number
DE3862652D1
DE3862652D1 DE8888630027T DE3862652T DE3862652D1 DE 3862652 D1 DE3862652 D1 DE 3862652D1 DE 8888630027 T DE8888630027 T DE 8888630027T DE 3862652 T DE3862652 T DE 3862652T DE 3862652 D1 DE3862652 D1 DE 3862652D1
Authority
DE
Germany
Prior art keywords
fan blade
increase adjustment
blade increase
adjustment
fan
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
DE8888630027T
Other languages
English (en)
Inventor
William T Dennison
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.)
Raytheon Technologies Corp
Original Assignee
United Technologies Corp
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 United Technologies Corp filed Critical United Technologies Corp
Application granted granted Critical
Publication of DE3862652D1 publication Critical patent/DE3862652D1/de
Anticipated expiration legal-status Critical
Expired - Fee Related legal-status Critical Current

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C11/00—Propellers, e.g. of ducted type; Features common to propellers and rotors for rotorcraft
    • B64C11/30—Blade pitch-changing mechanisms
    • B64C11/38—Blade pitch-changing mechanisms fluid, e.g. hydraulic
    • 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
    • F01D7/00—Rotors with blades adjustable in operation; Control thereof
    • 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
    • F05D2220/00—Application
    • F05D2220/30—Application in turbines
    • F05D2220/36—Application in turbines specially adapted for the fan of turbofan engines
    • 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
    • F05D2260/00—Function
    • F05D2260/70—Adjusting of angle of incidence or attack of rotating blades
    • F05D2260/74—Adjusting of angle of incidence or attack of rotating blades by turning around an axis perpendicular the rotor centre line
    • 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
    • F05D2260/00—Function
    • F05D2260/70—Adjusting of angle of incidence or attack of rotating blades
    • F05D2260/76—Adjusting of angle of incidence or attack of rotating blades the adjusting mechanism using auxiliary power sources

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Control Of Electric Motors In General (AREA)
  • Control Of Positive-Displacement Air Blowers (AREA)
  • Threshing Machine Elements (AREA)
DE8888630027T 1987-02-24 1988-02-18 Geblaeseblattsteigungsverstellvorrichtung. Expired - Fee Related DE3862652D1 (de)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US07/018,117 US4718823A (en) 1987-02-24 1987-02-24 Pitch changing mechanism for fan blades

Publications (1)

Publication Number Publication Date
DE3862652D1 true DE3862652D1 (de) 1991-06-13

Family

ID=21786335

Family Applications (1)

Application Number Title Priority Date Filing Date
DE8888630027T Expired - Fee Related DE3862652D1 (de) 1987-02-24 1988-02-18 Geblaeseblattsteigungsverstellvorrichtung.

Country Status (4)

Country Link
US (1) US4718823A (de)
EP (1) EP0280639B1 (de)
JP (1) JP2739581B2 (de)
DE (1) DE3862652D1 (de)

Families Citing this family (17)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2206381B (en) * 1987-06-30 1991-10-09 Rolls Royce Plc A variable stator vane arrangement for a compressor
DE4231815C1 (de) * 1992-09-23 1994-01-05 Landolt Alexander Dr Regelung für einen Bootsantrieb mit einem Motor und einem Verstellpropeller
US5431539A (en) * 1993-10-28 1995-07-11 United Technologies Corporation Propeller pitch change mechanism
US8753085B2 (en) * 2008-01-25 2014-06-17 Aktiebolaget Skf Device for changing a pitch of a blade of an impeller/propeller and a fan comprising the device
FR2945512B1 (fr) * 2009-05-15 2012-08-24 Snecma Helice non carenee a pales a calage variable pour une turbomachine
GB0911459D0 (en) * 2009-07-02 2009-08-12 Rolls Royce Plc An assembly providing contaminant removal
FR2956378B1 (fr) * 2010-02-15 2012-05-11 Snecma Turbopropulseur muni d'un dispositif d'orientation de pales
FR2956854B1 (fr) * 2010-03-01 2012-08-17 Snecma Dispositif de commande de l'orientation des pales de soufflante d'un turbopropulseur par contrepoids.
FR2980770B1 (fr) * 2011-10-03 2014-06-27 Snecma Turbomachine a helice(s) pour aeronef avec systeme pour changer le pas de l'helice.
FR2997138B1 (fr) * 2012-10-18 2014-11-14 Snecma Dispositif et procede de commande du calage des pales
US10221706B2 (en) * 2015-11-17 2019-03-05 General Electric Company Variable pitch fan actuator
FR3046433B1 (fr) * 2016-01-05 2019-05-24 Safran Aircraft Engines Module de soufflante a aubes a calage variable pour une turbomachine
FR3046407B1 (fr) * 2016-01-05 2022-03-25 Snecma Dispositif a verin fixe pour systeme de commande de l'orientation des pales de soufflante d'une turbomachine
EP3502438A1 (de) 2017-12-19 2019-06-26 Siemens Aktiengesellschaft Kompressorsteuerung
FR3118942B1 (fr) 2021-01-18 2022-12-09 Safran Aircraft Engines Soufflante a calage variable
FR3125505B1 (fr) * 2021-07-22 2023-07-21 Safran Aircraft Engines Systeme de changement de pas des pales d’une helice d’une turbomachine
EP4282764A1 (de) 2022-05-26 2023-11-29 RTX Corporation Flugzeugantriebssystem mit einstellbarem schubantrieb

Family Cites Families (16)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
BE558073A (de) *
US2440046A (en) * 1936-11-26 1948-04-20 Hautier Camille Reversible propeller with variable pitch
FR1177322A (fr) * 1957-06-18 1959-04-23 Creusot Forges Ateliers Dispositif de retournement des pales d'une turbine kaplan, en particulier pour turbine marémotrice
US3056457A (en) * 1961-03-03 1962-10-02 Macfarland Robin Adair Variable pitch propeller
US3487880A (en) * 1966-04-12 1970-01-06 Dowty Rotol Ltd Variable pitch fans
US3687569A (en) * 1971-03-19 1972-08-29 Gen Electric Rotor with variable angle blades
DE2218874C3 (de) * 1972-04-19 1979-05-17 Motoren- Und Turbinen-Union Muenchen Gmbh, 8000 Muenchen Vorrichtung zur Verstellung der Gebläseschaufeln eines Turbinenstrahltriebwerks
DE2307656C3 (de) * 1973-02-16 1979-01-04 Motoren- Und Turbinen-Union Muenchen Gmbh, 8000 Muenchen Vorrichtung zur Verstellung der Gebläselaufschaufeln eines Laufrades für Turbinenstrahltriebwerke
US3873235A (en) * 1973-10-01 1975-03-25 Gen Electric Variable pitch turbofan engine
US3922852A (en) * 1973-10-17 1975-12-02 Gen Electric Variable pitch fan for gas turbine engine
US3873236A (en) * 1973-12-26 1975-03-25 Gen Electric Fan with variable pitch blades and translating bearing actuation system
US4090812A (en) * 1976-11-19 1978-05-23 The United States Of America As Represented By The Secretary Of The Navy Axial fan with automatically controlled variable pitch blades
US4534705A (en) * 1983-01-21 1985-08-13 Selestam Rune K Horizontal-shaft wind turbine with few blades
GB2145777B (en) * 1983-08-29 1987-07-22 Gen Electric Aircraft propeller system
US4657484A (en) * 1984-09-04 1987-04-14 General Electric Company Blade pitch varying means
US4704862A (en) * 1985-05-29 1987-11-10 United Technologies Corporation Ducted prop engine

Also Published As

Publication number Publication date
EP0280639B1 (de) 1991-05-08
EP0280639A1 (de) 1988-08-31
JPS63227907A (ja) 1988-09-22
US4718823A (en) 1988-01-12
JP2739581B2 (ja) 1998-04-15

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Legal Events

Date Code Title Description
8364 No opposition during term of opposition
8339 Ceased/non-payment of the annual fee