GB1339662A - Aircraft - Google Patents

Aircraft

Info

Publication number
GB1339662A
GB1339662A GB672271*[A GB1339662DA GB1339662A GB 1339662 A GB1339662 A GB 1339662A GB 1339662D A GB1339662D A GB 1339662DA GB 1339662 A GB1339662 A GB 1339662A
Authority
GB
United Kingdom
Prior art keywords
flap
ram
grooves
splines
nut
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
GB672271*[A
Other languages
English (en)
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 GB1339662A publication Critical patent/GB1339662A/en
Expired legal-status Critical Current

Links

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C9/00Adjustable control surfaces or members, e.g. rudders
    • B64C9/14Adjustable control surfaces or members, e.g. rudders forming slots
    • B64C9/16Adjustable control surfaces or members, e.g. rudders forming slots at the rear of the wing
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C13/00Control systems or transmitting systems for actuating flying-control surfaces, lift-increasing flaps, air brakes, or spoilers
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C9/00Adjustable control surfaces or members, e.g. rudders
    • B64C9/14Adjustable control surfaces or members, e.g. rudders forming slots
    • B64C9/16Adjustable control surfaces or members, e.g. rudders forming slots at the rear of the wing
    • B64C9/20Adjustable 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)
GB672271*[A 1971-03-12 1971-03-12 Aircraft Expired GB1339662A (en)

Applications Claiming Priority (1)

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

Publications (1)

Publication Number Publication Date
GB1339662A true GB1339662A (en) 1973-12-05

Family

ID=9819589

Family Applications (1)

Application Number Title Priority Date Filing Date
GB672271*[A Expired GB1339662A (en) 1971-03-12 1971-03-12 Aircraft

Country Status (5)

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

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
IT952204B (it) 1973-07-20
US3819133A (en) 1974-06-25
FR2128855A1 (https=) 1972-10-20
DE2211249A1 (de) 1972-09-14
FR2128855B1 (https=) 1976-06-11

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Legal Events

Date Code Title Description
PS Patent sealed [section 19, patents act 1949]
PCNP Patent ceased through non-payment of renewal fee