FR1213762A - Perfectionnement aux organes de contrôle de voilures tournantes - Google Patents

Perfectionnement aux organes de contrôle de voilures tournantes

Info

Publication number
FR1213762A
FR1213762A FR1213762DA FR1213762A FR 1213762 A FR1213762 A FR 1213762A FR 1213762D A FR1213762D A FR 1213762DA FR 1213762 A FR1213762 A FR 1213762A
Authority
FR
France
Prior art keywords
control units
rotary wing
wing control
advanced training
training
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
Application number
Other languages
English (en)
Inventor
Rene Dorand
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.)
Individual
Original Assignee
Individual
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 Individual filed Critical Individual
Application granted granted Critical
Publication of FR1213762A publication Critical patent/FR1213762A/fr
Expired 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)
FR1213762D 1958-10-27 1958-10-27 Perfectionnement aux organes de contrôle de voilures tournantes Expired FR1213762A (fr)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR1213762T 1958-10-27

Publications (1)

Publication Number Publication Date
FR1213762A true FR1213762A (fr) 1960-04-04

Family

ID=9676663

Family Applications (1)

Application Number Title Priority Date Filing Date
FR1213762D Expired FR1213762A (fr) 1958-10-27 1958-10-27 Perfectionnement aux organes de contrôle de voilures tournantes

Country Status (1)

Country Link
FR (1) FR1213762A (fr)

Cited By (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3129769A (en) * 1962-09-21 1964-04-21 Kaman Aircraft Corp Fail safe device for servo flap controlled rotor blades
US3144908A (en) * 1962-12-28 1964-08-18 Bell Aerospace Selective second harmonic control
US3217809A (en) * 1963-02-28 1965-11-16 Kaman Aircraft Corp Rotor blade pitch changing mechanism for rotary wing aircraft
US3412807A (en) * 1964-12-15 1968-11-26 Giravions Dorand Soc Device for ensuring the re-entry into the atmosphere and the recovery of space vehicles
US3494706A (en) * 1967-08-28 1970-02-10 Bell Aerospace Corp In-plane out-of-plane flapping proprotor frequency decoupling
CN113968336A (zh) * 2021-12-06 2022-01-25 中国商用飞机有限责任公司 带有密封结构的扭力管装置以及具有该扭力管装置的飞机

Cited By (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3129769A (en) * 1962-09-21 1964-04-21 Kaman Aircraft Corp Fail safe device for servo flap controlled rotor blades
US3144908A (en) * 1962-12-28 1964-08-18 Bell Aerospace Selective second harmonic control
US3217809A (en) * 1963-02-28 1965-11-16 Kaman Aircraft Corp Rotor blade pitch changing mechanism for rotary wing aircraft
US3412807A (en) * 1964-12-15 1968-11-26 Giravions Dorand Soc Device for ensuring the re-entry into the atmosphere and the recovery of space vehicles
US3494706A (en) * 1967-08-28 1970-02-10 Bell Aerospace Corp In-plane out-of-plane flapping proprotor frequency decoupling
CN113968336A (zh) * 2021-12-06 2022-01-25 中国商用飞机有限责任公司 带有密封结构的扭力管装置以及具有该扭力管装置的飞机

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