DE394183T1 - Einrichtung zur veraenderung der propellersteigung. - Google Patents

Einrichtung zur veraenderung der propellersteigung.

Info

Publication number
DE394183T1
DE394183T1 DE199090630090T DE90630090T DE394183T1 DE 394183 T1 DE394183 T1 DE 394183T1 DE 199090630090 T DE199090630090 T DE 199090630090T DE 90630090 T DE90630090 T DE 90630090T DE 394183 T1 DE394183 T1 DE 394183T1
Authority
DE
Germany
Prior art keywords
incline
propeller
changing
propeller incline
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.)
Pending
Application number
DE199090630090T
Other languages
English (en)
Other versions
DE69030090D1 (de
DE69030090T2 (de
Inventor
Jerome G. Andover Connecticut 06232 Us Duchesneau
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
Publication of DE394183T1 publication Critical patent/DE394183T1/de
Pending 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
    • F01D7/00—Rotors with blades adjustable in operation; Control thereof
    • 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
    • B64C11/32—Blade pitch-changing mechanisms mechanical
    • 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
DE199090630090T 1989-04-21 1990-04-12 Einrichtung zur veraenderung der propellersteigung. Pending DE394183T1 (de)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US07/342,002 US4934901A (en) 1989-04-21 1989-04-21 Pitch change actuation system

Publications (1)

Publication Number Publication Date
DE394183T1 true DE394183T1 (de) 1991-06-13

Family

ID=23339920

Family Applications (2)

Application Number Title Priority Date Filing Date
DE90630090T Expired - Fee Related DE69002523T2 (de) 1989-04-21 1990-04-12 Einrichtung zur Veränderung der Propellersteigung.
DE199090630090T Pending DE394183T1 (de) 1989-04-21 1990-04-12 Einrichtung zur veraenderung der propellersteigung.

Family Applications Before (1)

Application Number Title Priority Date Filing Date
DE90630090T Expired - Fee Related DE69002523T2 (de) 1989-04-21 1990-04-12 Einrichtung zur Veränderung der Propellersteigung.

Country Status (7)

Country Link
US (1) US4934901A (de)
EP (1) EP0394183B1 (de)
JP (1) JPH0365494A (de)
BR (1) BR9001830A (de)
CA (1) CA2013856C (de)
DE (2) DE69002523T2 (de)
ES (1) ES2019846T3 (de)

Families Citing this family (33)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5213471A (en) * 1990-09-04 1993-05-25 General Electric Company Propeller pitch control
CA2243151C (en) * 1998-07-15 2008-06-17 Flexxaire Manufacturing Inc. Variable pitch fan
US6439850B1 (en) 1998-07-15 2002-08-27 Flexxaire Manufacturing Inc. Variable pitch fan
GB2367595A (en) * 2000-08-08 2002-04-10 Rolls Royce Plc Actuator mechanism for variable angle vanes having a unison ring directly connected to a vane spindle
US7331761B2 (en) * 2005-11-10 2008-02-19 Kaydon Corporation Wind turbine pitch bearing and method
FR2937678B1 (fr) * 2008-10-23 2013-11-22 Snecma Dispositif de commande de l'orientation des pales de soufflante d'un turbopropulseur
DE102009007013A1 (de) * 2009-01-31 2010-08-12 Deutsches Zentrum für Luft- und Raumfahrt e.V. Triebwerk, insbesondere CROR-Antrieb, für ein Flugzeug
US20120023899A1 (en) * 2009-02-06 2012-02-02 Shoji Yasuda Turbofan engine
US8172530B2 (en) * 2009-06-09 2012-05-08 Hamilton Sundstrand Corporation Pitch change actuation system for a counter-rotating propeller
US8167553B2 (en) * 2009-06-09 2012-05-01 Hamilton Sundstrand Corporation Electrical system for driving a propeller pitch change mechanism
US8277182B2 (en) * 2009-07-02 2012-10-02 Hamilton Sundstrand Corporation Remote pitch controller for a variable pitch propeller
GB201000054D0 (en) * 2010-01-05 2010-02-17 Rolls Royce Plc Propeller assembly pitch change apparatus
GB201000103D0 (en) * 2010-01-06 2010-02-17 Rolls Royce Plc Back-Up Feathers
GB201000144D0 (en) * 2010-01-07 2010-02-24 Rolls Royce Plc Pitch Change Apparatus
DE102010039394A1 (de) * 2010-08-17 2012-02-23 Siemens Aktiengesellschaft Verstellpropeller oder -repeller
US9963981B2 (en) * 2015-06-10 2018-05-08 General Electric Company Pitch change mechanism for shrouded fan with low fan pressure ratio
US10533436B2 (en) 2015-11-04 2020-01-14 General Electric Company Centerline-mounted hydraulic pitch change mechanism actuator
US10221706B2 (en) 2015-11-17 2019-03-05 General Electric Company Variable pitch fan actuator
GB201601862D0 (en) * 2016-02-02 2016-03-16 Rolls Royce Plc Actuation system for varying blade pitch
US10889367B2 (en) 2017-04-24 2021-01-12 Pratt & Whitney Canada Corp. Feedback system for pitch-adjustable blades of aircraft bladed rotor
US11046422B2 (en) 2018-07-16 2021-06-29 Pratt & Whitney Canada Corp. Propeller blade angle feedback arrangement and method
US11279465B2 (en) 2018-07-16 2022-03-22 Pratt & Whitney Canada Corp. Propeller blade angle feedback arrangement and method
US10174763B1 (en) 2018-08-02 2019-01-08 Florida Turbine Technologies, Inc Variable pitch fan for gas turbine engine
EP3666639B1 (de) * 2018-12-11 2022-04-06 Berg Propulsion Production AB Antriebssystem für ein wasserfahrzeug
US10829201B2 (en) * 2019-03-20 2020-11-10 Pratt & Whitney Canada Corp. Blade angle position feedback system with extended markers
US11554850B2 (en) 2019-04-25 2023-01-17 Pratt & Whitney Canada Corp. Blade angle position feedback system with offset sensors
US11046423B2 (en) 2019-07-18 2021-06-29 Pratt & Whitney Canada Corp. Blade angle position feedback system with magnetic shield
US11286038B2 (en) 2019-09-03 2022-03-29 Pratt & Whitney Canada Corp. Pitch control assembly for an aircraft-bladed rotor
US11597502B2 (en) 2019-09-05 2023-03-07 Pratt & Whitney Canada Corp. Signal amplification in blade angle position feedback system
US11365691B2 (en) 2019-09-05 2022-06-21 Pratt & Whitney Canada Corp. Blade angle position feedback system with embedded markers
US11505307B2 (en) 2019-10-21 2022-11-22 Pratt & Whitney Canada Corp. Phonic wheel and related system and method
US11428116B2 (en) 2019-11-29 2022-08-30 Pratt & Whitney Canada Corp. System and method for measuring an axial position of a rotating component of an engine
US11420772B2 (en) 2019-12-17 2022-08-23 Pratt & Whitney Canada Corp. System and method for determining an axial position of a feedback device

Family Cites Families (14)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CA491923A (en) * 1953-04-07 United Aircraft Corporation Pitch lock and actuating valve therefor
US2666490A (en) * 1950-05-03 1954-01-19 United Aircraft Corp Auxiliary drive for propeller pitch control
GB1196588A (en) * 1966-11-09 1970-07-01 British Aircraft Corp Ltd Form Improvements relating to Turbo-fan Aircraft Engines
GB1196589A (en) * 1966-11-21 1970-07-01 British Aircraft Corp Ltd Form Improvements relating to Turbo-fan Aircraft Engines
US3467198A (en) * 1966-12-05 1969-09-16 Rolls Royce Gear transmission
US3687569A (en) * 1971-03-19 1972-08-29 Gen Electric Rotor with variable angle blades
US3866415A (en) * 1974-02-25 1975-02-18 Gen Electric Fan blade actuator using pressurized air
US4533295A (en) * 1982-12-20 1985-08-06 United Technologies Corporation Pitch control system for variable pitch propeller
US4523891A (en) * 1983-06-15 1985-06-18 United Technologies Corporation Propeller pitch change actuation system
US4738590A (en) * 1986-09-09 1988-04-19 General Electric Company Blade pitch varying mechanism
US4738591A (en) * 1986-09-09 1988-04-19 General Electric Company Blade pitch varying mechanism
US4753572A (en) * 1986-10-02 1988-06-28 United Technologies Corporation Propeller pitch change actuation system
US4750862A (en) * 1986-11-28 1988-06-14 United Technologies Corporation Modular propeller blade pitch actuation system
GB2199378B (en) * 1986-12-24 1991-02-13 Rolls Royce Plc Pitch change arrangement for a variable pitch fan

Also Published As

Publication number Publication date
JPH0365494A (ja) 1991-03-20
BR9001830A (pt) 1991-06-18
US4934901A (en) 1990-06-19
CA2013856C (en) 1995-07-18
DE69002523T2 (de) 1993-12-09
EP0394183B1 (de) 1993-08-04
ES2019846A4 (es) 1991-07-16
ES2019846T3 (es) 1993-12-16
CA2013856A1 (en) 1990-10-21
DE69002523D1 (de) 1993-09-09
EP0394183A1 (de) 1990-10-24

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