IT952204B - Perfezionamento nei dispositivi di ipersostentamento per - Google Patents

Perfezionamento nei dispositivi di ipersostentamento per

Info

Publication number
IT952204B
IT952204B IT48912/72A IT4891272A IT952204B IT 952204 B IT952204 B IT 952204B IT 48912/72 A IT48912/72 A IT 48912/72A IT 4891272 A IT4891272 A IT 4891272A IT 952204 B IT952204 B IT 952204B
Authority
IT
Italy
Prior art keywords
hypersostentation
improvement
devices
hypersostentation devices
Prior art date
Application number
IT48912/72A
Other languages
English (en)
Italian (it)
Inventor
Mobili
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
Application granted granted Critical
Publication of IT952204B publication Critical patent/IT952204B/it

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)
IT48912/72A 1971-03-12 1972-03-10 Perfezionamento nei dispositivi di ipersostentamento per IT952204B (it)

Applications Claiming Priority (1)

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

Publications (1)

Publication Number Publication Date
IT952204B true IT952204B (it) 1973-07-20

Family

ID=9819589

Family Applications (1)

Application Number Title Priority Date Filing Date
IT48912/72A IT952204B (it) 1971-03-12 1972-03-10 Perfezionamento nei dispositivi di ipersostentamento per

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)

Families Citing this family (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4395007A (en) * 1980-11-13 1983-07-26 Rockwell International Corporation Actuation system for a control surface of an aircraft
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

Family Cites Families (4)

* 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
US2579534A (en) * 1948-05-12 1951-12-25 United Aircraft Corp Flap mechanism
US3486720A (en) * 1967-12-07 1969-12-30 Boeing Co Continuous slot forming leading edge slats for cranked wings
US3568957A (en) * 1968-11-13 1971-03-09 Mc Donnell Douglas Corp Long structural column support

Also Published As

Publication number Publication date
US3819133A (en) 1974-06-25
GB1339662A (en) 1973-12-05
FR2128855A1 (enExample) 1972-10-20
DE2211249A1 (de) 1972-09-14
FR2128855B1 (enExample) 1976-06-11

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