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GB1527836A - Auxiliary device for controlling and manoeuvring an aircraft - Google Patents

Auxiliary device for controlling and manoeuvring an aircraft

Info

Publication number
GB1527836A
GB1527836A GB1362877A GB1362877A GB1527836A GB 1527836 A GB1527836 A GB 1527836A GB 1362877 A GB1362877 A GB 1362877A GB 1362877 A GB1362877 A GB 1362877A GB 1527836 A GB1527836 A GB 1527836A
Authority
GB
United Kingdom
Prior art keywords
aircraft
manoeuvring
controlling
auxiliary device
jettisonable
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
GB1362877A
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 GmbH
Original Assignee
Dornier 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 GmbH filed Critical Dornier GmbH
Publication of GB1527836A publication Critical patent/GB1527836A/en
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

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Cooling, Air Intake And Gas Exhaust, And Fuel Tank Arrangements In Propulsion Units (AREA)
  • Motorcycle And Bicycle Frame (AREA)
  • Auxiliary Drives, Propulsion Controls, And Safety Devices (AREA)

Abstract

1527836 Aircraft control surfaces DORNIER GmbH 31 March 1977 [24 June 1976] 13628/77 Heading B7G A structural member 4 for supporting an external load 6, such as an engine, fuel tank or jettisonable pod on a wing has the form of an aerofoil and is provided with a pivotable trailing edge flap 9, 10 which may be operable by the rudder pedals.
GB1362877A 1976-06-24 1977-03-31 Auxiliary device for controlling and manoeuvring an aircraft Expired GB1527836A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DE19762628391 DE2628391A1 (en) 1976-06-24 1976-06-24 ADDITIONAL CONTROL AND MANEUVERING DEVICE FOR AIRCRAFT

Publications (1)

Publication Number Publication Date
GB1527836A true GB1527836A (en) 1978-10-11

Family

ID=5981348

Family Applications (1)

Application Number Title Priority Date Filing Date
GB1362877A Expired GB1527836A (en) 1976-06-24 1977-03-31 Auxiliary device for controlling and manoeuvring an aircraft

Country Status (3)

Country Link
DE (1) DE2628391A1 (en)
FR (1) FR2355714A1 (en)
GB (1) GB1527836A (en)

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4682746A (en) * 1984-12-05 1987-07-28 Lockheed Corporation Control force generator

Family Cites Families (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE2355979B2 (en) * 1973-11-09 1976-12-02 Dornier Gmbh, 7990 Friedrichshafen ADDITIONAL CONTROL DEVICE FOR AIRCRAFT

Also Published As

Publication number Publication date
FR2355714A1 (en) 1978-01-20
DE2628391A1 (en) 1977-12-29
FR2355714B1 (en) 1983-08-12

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Legal Events

Date Code Title Description
PS Patent sealed
PCNP Patent ceased through non-payment of renewal fee