FR2375092B1 - - Google Patents

Info

Publication number
FR2375092B1
FR2375092B1 FR7738641A FR7738641A FR2375092B1 FR 2375092 B1 FR2375092 B1 FR 2375092B1 FR 7738641 A FR7738641 A FR 7738641A FR 7738641 A FR7738641 A FR 7738641A FR 2375092 B1 FR2375092 B1 FR 2375092B1
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
FR7738641A
Other languages
French (fr)
Other versions
FR2375092A1 (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.)
Airbus Defence and Space GmbH
Original Assignee
Messerschmitt Bolkow Blohm AG
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 Messerschmitt Bolkow Blohm AG filed Critical Messerschmitt Bolkow Blohm AG
Publication of FR2375092A1 publication Critical patent/FR2375092A1/en
Application granted granted Critical
Publication of FR2375092B1 publication Critical patent/FR2375092B1/fr
Granted legal-status Critical Current

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

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Transmission Devices (AREA)
  • Retarders (AREA)
  • Toys (AREA)
FR7738641A 1976-12-24 1977-12-21 CONTROL LINKAGE, ESPECIALLY FOR A SWIVEL PLATE FOR THE COLLECTIVE AND CYCLICAL PITCH CONTROL OF THE BLADES OF A ROTATING BLADE AIRCRAFT Granted FR2375092A1 (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DE19762658828 DE2658828C3 (en) 1976-12-24 1976-12-24 Rotor for a rotary wing aircraft

Publications (2)

Publication Number Publication Date
FR2375092A1 FR2375092A1 (en) 1978-07-21
FR2375092B1 true FR2375092B1 (en) 1983-10-28

Family

ID=5996625

Family Applications (1)

Application Number Title Priority Date Filing Date
FR7738641A Granted FR2375092A1 (en) 1976-12-24 1977-12-21 CONTROL LINKAGE, ESPECIALLY FOR A SWIVEL PLATE FOR THE COLLECTIVE AND CYCLICAL PITCH CONTROL OF THE BLADES OF A ROTATING BLADE AIRCRAFT

Country Status (3)

Country Link
DE (1) DE2658828C3 (en)
FR (1) FR2375092A1 (en)
GB (1) GB1595440A (en)

Families Citing this family (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
IT1164936B (en) * 1979-02-27 1987-04-15 Giovanni Agusta Costruzioni Ae INTERNAL CONTROL ROTOR SHAFT FOR HELICOPTERS
DE3036093C1 (en) * 1980-09-25 1982-07-29 Messerschmitt-Bölkow-Blohm GmbH, 8000 München Rotor especially for a rotary wing aircraft
DE3123082A1 (en) * 1981-06-11 1982-12-30 Messerschmitt-Bölkow-Blohm GmbH, 8000 München "ROTOR WITH JOINT AND BEARING-FREE BLADE CONNECTION"
DE3134603C1 (en) * 1981-09-01 1983-04-14 Messerschmitt-Bölkow-Blohm GmbH, 8000 München Rotor for a rotary wing aircraft
DE3146347A1 (en) * 1981-11-23 1983-06-01 Messerschmitt-Bölkow-Blohm GmbH, 8000 München Rotor, especially for a rotating-wing aircraft
US4545733A (en) * 1982-03-18 1985-10-08 Messerschmitt-Boelkow-Blohm Gesellschaft Mit Beschraenkter Haftung Apparatus for adjusting the tracking of the blades in a rotor, especially for a rotary wing aircraft

Family Cites Families (13)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE1164835B (en) * 1964-03-05 Boelkow Entwicklungen Kg Rotary wing aircraft
DE702159C (en) * 1938-01-19 1941-01-31 E H Henrich Focke Dr Ing Adjustment gear for screwdriver rotors
US2473331A (en) * 1944-10-20 1949-06-14 Vertiflite Inc Helicopter power and control mechanism
US2856788A (en) * 1953-10-26 1958-10-21 D K Jovanovich Helicopter control mechanism
US2978038A (en) * 1958-03-11 1961-04-04 Doman Helicopters Inc Swash plate operating mechanism and combination with swash plate
DE1096208B (en) * 1959-04-07 1960-12-29 Boelkow Entwicklungen Kg Control device for helicopters with a swash plate
FR1253738A (en) * 1960-04-07 1961-02-10 Bolkow Entwicklungen Kg Helicopter control device
US3095931A (en) * 1961-05-10 1963-07-02 Kaman Aircraft Corp Blade pitch control mechanism for a helicopter
FR1354956A (en) * 1963-01-29 1964-03-13 Device for controlling variations in the incidence of rotorcraft rotor blades
US3217809A (en) * 1963-02-28 1965-11-16 Kaman Aircraft Corp Rotor blade pitch changing mechanism for rotary wing aircraft
DE1270409B (en) * 1965-05-17 1968-06-12 Wagner Josef Device for direction control for helicopters with two coaxial load-bearing rotors running in opposite directions
US3572616A (en) * 1969-09-18 1971-03-30 United Aircraft Corp Pitch control mechanism for bladed rotor
JPS5614519B1 (en) * 1971-04-06 1981-04-04

Also Published As

Publication number Publication date
GB1595440A (en) 1981-08-12
FR2375092A1 (en) 1978-07-21
DE2658828B2 (en) 1981-06-25
DE2658828C3 (en) 1982-02-25
DE2658828A1 (en) 1978-06-29

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Legal Events

Date Code Title Description
ST Notification of lapse