GB506714A - Means for shifting flaps on aircraft - Google Patents

Means for shifting flaps on aircraft

Info

Publication number
GB506714A
GB506714A GB35652/38A GB3565238A GB506714A GB 506714 A GB506714 A GB 506714A GB 35652/38 A GB35652/38 A GB 35652/38A GB 3565238 A GB3565238 A GB 3565238A GB 506714 A GB506714 A GB 506714A
Authority
GB
United Kingdom
Prior art keywords
lever
flap
rails
aircraft
rollers
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
GB35652/38A
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.)
Arado Flugzeugwerke GmbH
Original Assignee
Arado Flugzeugwerke 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 Arado Flugzeugwerke GmbH filed Critical Arado Flugzeugwerke GmbH
Publication of GB506714A publication Critical patent/GB506714A/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
    • 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
    • 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
    • B64C9/18—Adjustable control surfaces or members, e.g. rudders forming slots at the rear of the wing by single flaps

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Transmission Devices (AREA)

Abstract

506,714. Controlling aircraft. ARADO FLUGZEUGWERKE GES. Dec. 7, 1938, No. 35652. Convention date, Jan. 25. [Class 4] A flap 2 on an aircraft, adapted to be swung rearwardly and downwardly from the main wing, is connected to the ends of two levers 3, 4 connected by a pivot 15<1> at the central parts. The lever 3 is guided by rollers in rails 5 at its centre and is connected to screw-and-nut operating-gear 11, 12 at its forward end. The lever 4 is guided at the forward end by rollers in rails 7 and at its rear end is pivoted to a rod 17 slidable in the nose of the flap. When the flap is projected by the gear 11. 12 and the lever 3, the lever 4 is also moved and in consequence of the inclination of the rails 7 the lever 4 is rocked and the flap swung downwards. The guide rails may be curved and may be movable.
GB35652/38A 1938-01-25 1938-12-07 Means for shifting flaps on aircraft Expired GB506714A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DE506714X 1938-01-25

Publications (1)

Publication Number Publication Date
GB506714A true GB506714A (en) 1939-06-02

Family

ID=6546631

Family Applications (1)

Application Number Title Priority Date Filing Date
GB35652/38A Expired GB506714A (en) 1938-01-25 1938-12-07 Means for shifting flaps on aircraft

Country Status (1)

Country Link
GB (1) GB506714A (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2423984A (en) * 1943-07-12 1947-07-15 Lockheed Aircraft Corp Wing flap extending mechanism
US2932161A (en) * 1952-10-25 1960-04-12 United Aircraft Corp Variable area nozzle

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2423984A (en) * 1943-07-12 1947-07-15 Lockheed Aircraft Corp Wing flap extending mechanism
US2932161A (en) * 1952-10-25 1960-04-12 United Aircraft Corp Variable area nozzle

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