GB511003A - Improvements in aerofoils for aircraft - Google Patents

Improvements in aerofoils for aircraft

Info

Publication number
GB511003A
GB511003A GB2877038A GB2877038A GB511003A GB 511003 A GB511003 A GB 511003A GB 2877038 A GB2877038 A GB 2877038A GB 2877038 A GB2877038 A GB 2877038A GB 511003 A GB511003 A GB 511003A
Authority
GB
United Kingdom
Prior art keywords
rod
flap
projected
aircraft
aileron
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
GB2877038A
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.)
ERNST HEINKEL PROF
SIEGFRIED GUENTER
Original Assignee
ERNST HEINKEL PROF
SIEGFRIED GUENTER
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 ERNST HEINKEL PROF, SIEGFRIED GUENTER filed Critical ERNST HEINKEL PROF
Priority to GB2877038A priority Critical patent/GB511003A/en
Publication of GB511003A publication Critical patent/GB511003A/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
    • B64C9/32—Air braking surfaces
    • B64C9/323—Air braking surfaces associated with wings
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C9/00—Adjustable control surfaces or members, e.g. rudders
    • B64C9/32—Air braking surfaces

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Toys (AREA)

Abstract

511,003. Controlling aircraft. HEINKEL, E., and GUNTER, S. Oct. 4, 1938, No. 28770. ,[Class 4] . An aerofoil for aircraft comprises a rearwardly projectable landing-flap arranged below a trailing edge, and is upwardly and downwardly pivotable for use also as an aileron both in retracted and any projected position. The flap c is adapted to be rearwardly projected by the device d operatedby'rack and pinion and is operated.as an aileron by a rod e connected to a bell-crank l mounted on the rod d and connected to the operating-mechanism by a rod o This arrangement produces downward deflection of the flap when it is projected by the device d.
GB2877038A 1938-10-04 1938-10-04 Improvements in aerofoils for aircraft Expired GB511003A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB2877038A GB511003A (en) 1938-10-04 1938-10-04 Improvements in aerofoils for aircraft

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB2877038A GB511003A (en) 1938-10-04 1938-10-04 Improvements in aerofoils for aircraft

Publications (1)

Publication Number Publication Date
GB511003A true GB511003A (en) 1939-08-11

Family

ID=10280866

Family Applications (1)

Application Number Title Priority Date Filing Date
GB2877038A Expired GB511003A (en) 1938-10-04 1938-10-04 Improvements in aerofoils for aircraft

Country Status (1)

Country Link
GB (1) GB511003A (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2620147A (en) * 1950-05-31 1952-12-02 Boeing Co Airplane flap control mechanism

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2620147A (en) * 1950-05-31 1952-12-02 Boeing Co Airplane flap control mechanism

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