FR1446212A - Device for controlling the pitch of the blades of rotary-wing aircraft - Google Patents

Device for controlling the pitch of the blades of rotary-wing aircraft

Info

Publication number
FR1446212A
FR1446212A FR8404A FR67008404A FR1446212A FR 1446212 A FR1446212 A FR 1446212A FR 8404 A FR8404 A FR 8404A FR 67008404 A FR67008404 A FR 67008404A FR 1446212 A FR1446212 A FR 1446212A
Authority
FR
France
Prior art keywords
blades
pitch
rotary
controlling
wing aircraft
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
FR8404A
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.)
Dornier Werke GmbH
Original Assignee
Dornier Werke GmbH
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 Dornier Werke GmbH filed Critical Dornier Werke GmbH
Application granted granted Critical
Publication of FR1446212A publication Critical patent/FR1446212A/en
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)
  • Structures Of Non-Positive Displacement Pumps (AREA)
FR8404A 1964-09-04 1965-09-03 Device for controlling the pitch of the blades of rotary-wing aircraft Expired FR1446212A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DE1964D0045348 DE1431153A1 (en) 1964-09-04 1964-09-04 Device for blade angle adjustment in rotary wing aircraft

Publications (1)

Publication Number Publication Date
FR1446212A true FR1446212A (en) 1966-07-15

Family

ID=7048943

Family Applications (1)

Application Number Title Priority Date Filing Date
FR8404A Expired FR1446212A (en) 1964-09-04 1965-09-03 Device for controlling the pitch of the blades of rotary-wing aircraft

Country Status (2)

Country Link
DE (1) DE1431153A1 (en)
FR (1) FR1446212A (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4242044A (en) * 1979-07-11 1980-12-30 The United States Of America As Represented By The Secretary Of The Navy Compensating structure for circulation control rotor pneumatic valve
US6131849A (en) * 1998-12-02 2000-10-17 Mcdonnell Douglas Helicopter Company Articulating/telescoping duct for reaction drive helicopters

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4242044A (en) * 1979-07-11 1980-12-30 The United States Of America As Represented By The Secretary Of The Navy Compensating structure for circulation control rotor pneumatic valve
US6131849A (en) * 1998-12-02 2000-10-17 Mcdonnell Douglas Helicopter Company Articulating/telescoping duct for reaction drive helicopters

Also Published As

Publication number Publication date
DE1431153A1 (en) 1968-11-14

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