FR2128855A1 - - Google Patents

Info

Publication number
FR2128855A1
FR2128855A1 FR7208512A FR7208512A FR2128855A1 FR 2128855 A1 FR2128855 A1 FR 2128855A1 FR 7208512 A FR7208512 A FR 7208512A FR 7208512 A FR7208512 A FR 7208512A FR 2128855 A1 FR2128855 A1 FR 2128855A1
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.)
Granted
Application number
FR7208512A
Other languages
French (fr)
Other versions
FR2128855B1 (enExample
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.)
British Aircraft Corp Ltd
Original Assignee
British Aircraft Corp Ltd
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 British Aircraft Corp Ltd filed Critical British Aircraft Corp Ltd
Publication of FR2128855A1 publication Critical patent/FR2128855A1/fr
Application granted granted Critical
Publication of FR2128855B1 publication Critical patent/FR2128855B1/fr
Expired legal-status Critical Current

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C9/00—Adjustable control surfaces or members, e.g. rudders
    • B64C9/14—Adjustable control surfaces or members, e.g. rudders forming slots
    • B64C9/16—Adjustable control surfaces or members, e.g. rudders forming slots at the rear of the wing
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C13/00—Control systems or transmitting systems for actuating flying-control surfaces, lift-increasing flaps, air brakes, or spoilers
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C9/00—Adjustable control surfaces or members, e.g. rudders
    • B64C9/14—Adjustable control surfaces or members, e.g. rudders forming slots
    • B64C9/16—Adjustable control surfaces or members, e.g. rudders forming slots at the rear of the wing
    • B64C9/20—Adjustable control surfaces or members, e.g. rudders forming slots at the rear of the wing by multiple flaps

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Automation & Control Theory (AREA)
  • Transmission Devices (AREA)
  • Perforating, Stamping-Out Or Severing By Means Other Than Cutting (AREA)
FR7208512A 1971-03-12 1972-03-10 Expired FR2128855B1 (enExample)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB672271 1971-03-12

Publications (2)

Publication Number Publication Date
FR2128855A1 true FR2128855A1 (enExample) 1972-10-20
FR2128855B1 FR2128855B1 (enExample) 1976-06-11

Family

ID=9819589

Family Applications (1)

Application Number Title Priority Date Filing Date
FR7208512A Expired FR2128855B1 (enExample) 1971-03-12 1972-03-10

Country Status (5)

Country Link
US (1) US3819133A (enExample)
DE (1) DE2211249A1 (enExample)
FR (1) FR2128855B1 (enExample)
GB (1) GB1339662A (enExample)
IT (1) IT952204B (enExample)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP0052240A1 (en) * 1980-11-13 1982-05-26 Rockwell International Corporation Actuation system for a control surface of an aircraft

Families Citing this family (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE10328540B4 (de) * 2003-06-24 2008-02-14 Eads Deutschland Gmbh Betätigungseinrichtung für eine an der Hinterkante des Tragflügels eines Flugzeugs angeordnete Ruderklappe
GB0921007D0 (en) * 2009-11-30 2010-01-13 Airbus Operations Ltd Trailing edge flap
US10017243B2 (en) * 2013-09-24 2018-07-10 The Boeing Company Adaptive trailing edge actuator system and method

Citations (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2451009A (en) * 1945-10-18 1948-10-12 Bell Aircraft Corp Aircraft control surface
US3486720A (en) * 1967-12-07 1969-12-30 Boeing Co Continuous slot forming leading edge slats for cranked wings

Family Cites Families (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2579534A (en) * 1948-05-12 1951-12-25 United Aircraft Corp Flap mechanism
US3568957A (en) * 1968-11-13 1971-03-09 Mc Donnell Douglas Corp Long structural column support

Patent Citations (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2451009A (en) * 1945-10-18 1948-10-12 Bell Aircraft Corp Aircraft control surface
US3486720A (en) * 1967-12-07 1969-12-30 Boeing Co Continuous slot forming leading edge slats for cranked wings

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP0052240A1 (en) * 1980-11-13 1982-05-26 Rockwell International Corporation Actuation system for a control surface of an aircraft

Also Published As

Publication number Publication date
US3819133A (en) 1974-06-25
GB1339662A (en) 1973-12-05
IT952204B (it) 1973-07-20
DE2211249A1 (de) 1972-09-14
FR2128855B1 (enExample) 1976-06-11

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Legal Events

Date Code Title Description
ST Notification of lapse