FR1054268A - Device for mounting and cyclic control of the pitch of rotating wings of devices such as helicopters - Google Patents

Device for mounting and cyclic control of the pitch of rotating wings of devices such as helicopters

Info

Publication number
FR1054268A
FR1054268A FR1054268DA FR1054268A FR 1054268 A FR1054268 A FR 1054268A FR 1054268D A FR1054268D A FR 1054268DA FR 1054268 A FR1054268 A FR 1054268A
Authority
FR
France
Prior art keywords
helicopters
pitch
mounting
devices
cyclic control
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
French (fr)
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.)
HILLER HELICOPTERS
Original Assignee
HILLER HELICOPTERS
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 HILLER HELICOPTERS filed Critical HILLER HELICOPTERS
Application granted granted Critical
Publication of FR1054268A publication Critical patent/FR1054268A/en
Expired 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
    • B64C27/58Transmitting means, e.g. interrelated with initiating means or means acting on blades
    • B64C27/59Transmitting means, e.g. interrelated with initiating means or means acting on blades mechanical
    • B64C27/605Transmitting means, e.g. interrelated with initiating means or means acting on blades mechanical including swash plate, spider or cam mechanisms

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Aviation & Aerospace Engineering (AREA)
FR1054268D 1950-12-26 1951-12-22 Device for mounting and cyclic control of the pitch of rotating wings of devices such as helicopters Expired FR1054268A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US1054268XA 1950-12-26 1950-12-26

Publications (1)

Publication Number Publication Date
FR1054268A true FR1054268A (en) 1954-02-09

Family

ID=22305785

Family Applications (1)

Application Number Title Priority Date Filing Date
FR1054268D Expired FR1054268A (en) 1950-12-26 1951-12-22 Device for mounting and cyclic control of the pitch of rotating wings of devices such as helicopters

Country Status (1)

Country Link
FR (1) FR1054268A (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2564057A1 (en) * 1984-05-14 1985-11-15 Aerospatiale CYCLIC TRAY DEVICE MOUNTED TO LAMINATED JOINTS FOR CONTROLLING ROTOR BLADE PITCH
FR2569387A1 (en) * 1984-08-23 1986-02-28 United Technologies Corp FLEXIBLE ORGAN FOR CENTERING OSCILLATING PLATE FOR STEAM CONTROL OF HELICOPTER ROTOR BLADES

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2564057A1 (en) * 1984-05-14 1985-11-15 Aerospatiale CYCLIC TRAY DEVICE MOUNTED TO LAMINATED JOINTS FOR CONTROLLING ROTOR BLADE PITCH
EP0162773A1 (en) * 1984-05-14 1985-11-27 AEROSPATIALE Société Nationale Industrielle Swash-plate device supported by a laminated elastomeric bearing for the pitch control of rotor blades
US4630998A (en) * 1984-05-14 1986-12-23 Aerospatiale Societe Nationale Industrielle Apparatus for control of collective and cyclic pitch of the blades of a rotor
FR2569387A1 (en) * 1984-08-23 1986-02-28 United Technologies Corp FLEXIBLE ORGAN FOR CENTERING OSCILLATING PLATE FOR STEAM CONTROL OF HELICOPTER ROTOR BLADES

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