DE351439C - Balanced twist flap for aircraft - Google Patents

Balanced twist flap for aircraft

Info

Publication number
DE351439C
DE351439C DED37876D DED0037876D DE351439C DE 351439 C DE351439 C DE 351439C DE D37876 D DED37876 D DE D37876D DE D0037876 D DED0037876 D DE D0037876D DE 351439 C DE351439 C DE 351439C
Authority
DE
Germany
Prior art keywords
flap
aircraft
twist
balanced twist
balanced
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
DED37876D
Other languages
German (de)
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.)
RUDOLF DANNENBERG
Original Assignee
RUDOLF DANNENBERG
Publication date
Priority to DED37876D priority Critical patent/DE351439C/en
Application granted granted Critical
Publication of DE351439C publication Critical patent/DE351439C/en
Expired legal-status Critical Current

Links

Classifications

    • 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

Landscapes

  • Engineering & Computer Science (AREA)
  • Automation & Control Theory (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Tires In General (AREA)
  • Aerials With Secondary Devices (AREA)

Description

Hierzu 1 Blatt Zeichnungen.1 sheet of drawings.

Claims (1)

Patent-Anspruch:Patent claim: Ausgeglichene Verwindungsklappe für Flugzeuge, dadurch gekennzeichnet, daß zum Ausgleich der hinteren Verwindungsklappe (b) ein nicht vorragender Teil (a) der Tragfläche benutzt wird, der um eine zur Achse der Verwindungsklappe parallele Achse drehbar und mit der Verwindungsklappe zwangläufig verbunden ist.Balanced twist flap for aircraft, characterized in that a non-protruding part (a) of the wing is used to compensate for the rear twist flap (b) , which is rotatable about an axis parallel to the axis of the twist flap and is positively connected to the twist flap.
DED37876D Balanced twist flap for aircraft Expired DE351439C (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
DED37876D DE351439C (en) Balanced twist flap for aircraft

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DED37876D DE351439C (en) Balanced twist flap for aircraft

Publications (1)

Publication Number Publication Date
DE351439C true DE351439C (en) 1922-08-18

Family

ID=7043821

Family Applications (1)

Application Number Title Priority Date Filing Date
DED37876D Expired DE351439C (en) Balanced twist flap for aircraft

Country Status (1)

Country Link
DE (1) DE351439C (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2433649A (en) * 1944-03-14 1947-12-30 Cloyd P Clevenger Aircraft control surfaces for yaw control
DE1237439B (en) * 1962-03-12 1967-03-23 British Aircraft Corp Ltd Flap device for aircraft

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2433649A (en) * 1944-03-14 1947-12-30 Cloyd P Clevenger Aircraft control surfaces for yaw control
DE1237439B (en) * 1962-03-12 1967-03-23 British Aircraft Corp Ltd Flap device for aircraft

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