IT1200718B - Organi di centraggio flessibile per il disco oscillante di un rotore di elicottero - Google Patents

Organi di centraggio flessibile per il disco oscillante di un rotore di elicottero

Info

Publication number
IT1200718B
IT1200718B IT21975/85A IT2197585A IT1200718B IT 1200718 B IT1200718 B IT 1200718B IT 21975/85 A IT21975/85 A IT 21975/85A IT 2197585 A IT2197585 A IT 2197585A IT 1200718 B IT1200718 B IT 1200718B
Authority
IT
Italy
Prior art keywords
helicopter rotor
centering devices
oscillating disc
flexible centering
flexible
Prior art date
Application number
IT21975/85A
Other languages
English (en)
Other versions
IT8521975A0 (it
Inventor
Donald L Ferris
Michael J Marchitto
Original Assignee
Inited Tecnologies 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 Inited Tecnologies Corp filed Critical Inited Tecnologies Corp
Publication of IT8521975A0 publication Critical patent/IT8521975A0/it
Application granted granted Critical
Publication of IT1200718B publication Critical patent/IT1200718B/it

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C27/00—Rotorcraft; Rotors peculiar thereto
    • B64C27/54—Mechanisms for controlling blade adjustment or movement relative to rotor head, e.g. lag-lead movement
    • B64C27/58—Transmitting means, e.g. interrelated with initiating means or means acting on blades
    • B64C27/59—Transmitting means, e.g. interrelated with initiating means or means acting on blades mechanical
    • B64C27/605—Transmitting means, e.g. interrelated with initiating means or means acting on blades mechanical including swash plate, spider or cam mechanisms
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C27/00—Rotorcraft; Rotors peculiar thereto
    • B64C27/54—Mechanisms for controlling blade adjustment or movement relative to rotor head, e.g. lag-lead movement
    • B64C27/58—Transmitting means, e.g. interrelated with initiating means or means acting on blades

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Support Of The Bearing (AREA)
  • Auxiliary Devices For And Details Of Packaging Control (AREA)
  • Holding Or Fastening Of Disk On Rotational Shaft (AREA)
  • Surgical Instruments (AREA)
IT21975/85A 1984-08-23 1985-08-23 Organi di centraggio flessibile per il disco oscillante di un rotore di elicottero IT1200718B (it)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US06/644,000 US4588355A (en) 1984-08-23 1984-08-23 Flexible swashplate centering member

Publications (2)

Publication Number Publication Date
IT8521975A0 IT8521975A0 (it) 1985-08-23
IT1200718B true IT1200718B (it) 1989-01-27

Family

ID=24583034

Family Applications (1)

Application Number Title Priority Date Filing Date
IT21975/85A IT1200718B (it) 1984-08-23 1985-08-23 Organi di centraggio flessibile per il disco oscillante di un rotore di elicottero

Country Status (6)

Country Link
US (1) US4588355A (it)
JP (1) JPH0829758B2 (it)
DE (1) DE3528219A1 (it)
FR (1) FR2569387B1 (it)
GB (1) GB2163395B (it)
IT (1) IT1200718B (it)

Families Citing this family (18)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2564057B1 (fr) * 1984-05-14 1986-10-31 Aerospatiale Dispositif a plateaux cycliques montes sur articulations lamifiees pour la commande du pas des pales d'un rotor
US4729753A (en) * 1985-11-04 1988-03-08 Bell Helicopter Textron Inc. Constant velocity elastomeric bearing joint
JPH0668504B2 (ja) * 1986-03-17 1994-08-31 日本碍子株式会社 電圧センサ
US4804315A (en) * 1987-07-30 1989-02-14 United Technologies Corporation Composite helicopter swashplate
US5071319A (en) * 1987-09-30 1991-12-10 The Boeing Company Low maintenance, advanced technology swashplate
US5067875A (en) * 1990-04-11 1991-11-26 United Technologies Corporation Composite scissors for a swashplate
JPH085437B2 (ja) * 1990-04-27 1996-01-24 防衛庁技術研究本部長 回転翼航空機用の無関節ハブ構造
FR2661886B1 (fr) * 1990-05-14 1992-08-28 Aerospatiale Dispositif a plateaux cycliques montes sur articulations decouplees en tangage et roulis, pour la commande du pas des pales d'un rotor de giravion.
US5074494A (en) * 1990-10-11 1991-12-24 United Technologies Corporation Elastomeric swashplate configuration for helicopters
US5083725A (en) * 1990-10-11 1992-01-28 United Technologies Corporation Elastomeric swashplate configuration for helicopters
US5628620A (en) * 1991-09-30 1997-05-13 Arlton; Paul E. Main rotor system for helicopters
DE19630665C2 (de) * 1996-07-30 1998-07-23 Eurocopter Deutschland Steuerungseinrichtung zur Rotorblattverstellung, insbesondere eines Drehflügelflugzeuges
JPH10104663A (ja) 1996-09-27 1998-04-24 Semiconductor Energy Lab Co Ltd 電気光学装置およびその作製方法
US5785497A (en) * 1997-03-11 1998-07-28 Sikorsky Aircraft Corporation Control rod mounting arrangement for helicopter swashplates
GB2457685B (en) * 2008-02-21 2012-06-27 David Hostettler Wain Vertically flexible swash plate
US10184511B2 (en) 2013-01-11 2019-01-22 United Technologies Corporation Linkage with spherical or journal bearing assembly
CA3024684A1 (en) * 2016-05-18 2017-11-23 Kyriacos Zachary Variable pitch propeller apparatus and variable thrust aircraft using same
US11780574B2 (en) * 2021-06-03 2023-10-10 Lockheed Martin Corporation Swashplate assembly for a rotor system

Family Cites Families (19)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2396038A (en) * 1942-05-28 1946-03-05 Bossi Enea Helicopter
FR888158A (fr) * 1942-07-18 1943-12-06 Fr Du Gyroplane Soc Perfectionnements aux voilures tournantes
US2410545A (en) * 1943-03-15 1946-11-05 David W Main Pitch control mechanism for rotors of rotary wing aircraft
FR1054268A (fr) * 1950-12-26 1954-02-09 Hiller Helicopters Dispositif de montage et de commande cyclique du pas des ailes tournantes d'appareils tels que les hélicoptères
US3451484A (en) * 1967-05-09 1969-06-24 Bell Aerospace Corp Focus rotor stabilization
US3554662A (en) * 1968-01-25 1971-01-12 Fairchild Hiller Corp Reverse velocity rotor and rotorcraft
US3729272A (en) * 1968-01-25 1973-04-24 Fairchild Industries Reverse velocity rotor and rotorcraft
US3558082A (en) * 1968-07-16 1971-01-26 Ralph F Bennie Rotary wing aircraft
US3924965A (en) * 1973-01-22 1975-12-09 Fairchild Industries Reverse velocity rotor and rotorcraft
US3933324A (en) * 1974-08-02 1976-01-20 Stanislaw Ostrowski Helicopter with opposite rotating torque cancelling horizontal propeller
US3952546A (en) * 1974-08-23 1976-04-27 Kawasaki Jukogyo Kabushiki Kaisha Elastic coupling
US3957227A (en) * 1975-02-10 1976-05-18 The Boeing Company Rotor pitch control mechanism
FR2328609A1 (fr) * 1975-10-23 1977-05-20 Owski Stanislaw Helicoptere a helices horizontales de neutralisation du couple de torsion
US4087203A (en) * 1977-01-07 1978-05-02 United Technologies Corporation Cross beam rotor
US4326834A (en) * 1979-06-05 1982-04-27 Stanislaw Ostrowski Helicopter rotor assembly and blade pitch control
US4297080A (en) * 1979-12-17 1981-10-27 United Technologies Corporation Rotor blade pitch control linkage
US4323332A (en) * 1979-12-21 1982-04-06 United Technologies Corporation Hingeless helicopter rotor with elastic gimbal hub
GB2077208A (en) * 1980-05-22 1981-12-16 Secr Defence Controlling Helicopter Rotors
FR2564057B1 (fr) * 1984-05-14 1986-10-31 Aerospatiale Dispositif a plateaux cycliques montes sur articulations lamifiees pour la commande du pas des pales d'un rotor

Also Published As

Publication number Publication date
US4588355A (en) 1986-05-13
FR2569387A1 (fr) 1986-02-28
JPS6160397A (ja) 1986-03-28
GB2163395A (en) 1986-02-26
JPH0829758B2 (ja) 1996-03-27
DE3528219A1 (de) 1986-03-06
IT8521975A0 (it) 1985-08-23
FR2569387B1 (fr) 1987-09-11
GB2163395B (en) 1987-11-04
GB8520686D0 (en) 1985-09-25

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