FR2491865B1 - - Google Patents

Info

Publication number
FR2491865B1
FR2491865B1 FR8119141A FR8119141A FR2491865B1 FR 2491865 B1 FR2491865 B1 FR 2491865B1 FR 8119141 A FR8119141 A FR 8119141A FR 8119141 A FR8119141 A FR 8119141A FR 2491865 B1 FR2491865 B1 FR 2491865B1
Authority
FR
France
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
Application number
FR8119141A
Other languages
French (fr)
Other versions
FR2491865A1 (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.)
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
Priority claimed from US06/195,808 external-priority patent/US4354234A/en
Priority claimed from US06/195,723 external-priority patent/US4376979A/en
Application filed by United Technologies Corp filed Critical United Technologies Corp
Publication of FR2491865A1 publication Critical patent/FR2491865A1/en
Application granted granted Critical
Publication of FR2491865B1 publication Critical patent/FR2491865B1/fr
Granted legal-status Critical Current

Links

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C27/00Rotorcraft; Rotors peculiar thereto
    • B64C27/54Mechanisms for controlling blade adjustment or movement relative to rotor head, e.g. lag-lead movement
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C27/00Rotorcraft; Rotors peculiar thereto
    • B64C27/32Rotors
    • B64C27/46Blades
    • B64C27/473Constructional features
    • B64C27/50Blades foldable to facilitate stowage of aircraft

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Toys (AREA)
  • Transmission Devices (AREA)
FR8119141A 1980-10-10 1981-10-12 POSITIONING OF AUTOMATIC LOCKING OF FOLDING BLADES OF HELICOPTER Granted FR2491865A1 (en)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US06/195,808 US4354234A (en) 1980-10-10 1980-10-10 Automatic lock-positioning of foldable helicopter blades
US06/195,723 US4376979A (en) 1980-10-10 1980-10-10 Updated lock-positioning of foldable helicopter blades

Publications (2)

Publication Number Publication Date
FR2491865A1 FR2491865A1 (en) 1982-04-16
FR2491865B1 true FR2491865B1 (en) 1983-12-23

Family

ID=26891271

Family Applications (1)

Application Number Title Priority Date Filing Date
FR8119141A Granted FR2491865A1 (en) 1980-10-10 1981-10-12 POSITIONING OF AUTOMATIC LOCKING OF FOLDING BLADES OF HELICOPTER

Country Status (8)

Country Link
AU (1) AU540743B2 (en)
CA (1) CA1161413A (en)
CH (1) CH652673A5 (en)
DE (1) DE3139720C2 (en)
ES (1) ES506143A0 (en)
FR (1) FR2491865A1 (en)
GB (1) GB2085194B (en)
IT (1) IT1138938B (en)

Families Citing this family (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4696445A (en) * 1986-09-18 1987-09-29 United Technologies Corporation Collective control system for a helicopter
AU587363B1 (en) * 1988-07-27 1989-08-10 Richard Henry Tollervey Improvements to helicopter rotor blades
FR2754779B1 (en) * 1996-10-22 1998-12-31 Eurocopter France METHOD FOR FOLDING THE BLADES OF A MAIN ROTOR OF A GIRAVION AND DEVICE FOR IMPLEMENTING SAME
FR2931132B1 (en) 2008-05-19 2010-04-23 Eurocopter France ASSISTED CONTROL SYSTEM OF A GIRAVON
US9682771B2 (en) * 2013-08-14 2017-06-20 Sikorsky Aircraft Corporation Controlling rotor blades of a swashplateless rotor
CN114465065B (en) * 2022-01-06 2023-11-03 广东汇天航空航天科技有限公司 Aircraft main shaft slip ring device, aircraft rotor system and aircraft
CN114802739B (en) * 2022-06-09 2023-04-07 广东汇天航空航天科技有限公司 Rotor positioning method for aircraft, aircraft and storage medium

Family Cites Families (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3698662A (en) * 1970-10-12 1972-10-17 Lockheed Aircraft Corp Apparatus and method for sequencing the folding and unfolding of rotor blades in a compound vehicle
US4103848A (en) * 1977-03-08 1978-08-01 United Technologies Corporation Variable incidence helicopter stabilator and fail safe actuator
US4284387A (en) * 1979-05-02 1981-08-18 United Technologies Corp. Blade fold restraint system

Also Published As

Publication number Publication date
AU7622781A (en) 1982-04-22
FR2491865A1 (en) 1982-04-16
GB2085194A (en) 1982-04-21
CH652673A5 (en) 1985-11-29
DE3139720C2 (en) 1994-02-10
IT1138938B (en) 1986-09-17
GB2085194B (en) 1984-03-07
DE3139720A1 (en) 1982-05-19
ES8206331A1 (en) 1982-08-16
ES506143A0 (en) 1982-08-16
IT8124415A0 (en) 1981-10-09
CA1161413A (en) 1984-01-31
AU540743B2 (en) 1984-11-29

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Legal Events

Date Code Title Description
ST Notification of lapse