GB514157A - Improvements in or relating to control surfaces on aircraft - Google Patents

Improvements in or relating to control surfaces on aircraft

Info

Publication number
GB514157A
GB514157A GB9318/38A GB931838A GB514157A GB 514157 A GB514157 A GB 514157A GB 9318/38 A GB9318/38 A GB 9318/38A GB 931838 A GB931838 A GB 931838A GB 514157 A GB514157 A GB 514157A
Authority
GB
United Kingdom
Prior art keywords
lever
rod
aircraft
control surfaces
similar
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
GB9318/38A
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.)
Individual
Original Assignee
Individual
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 Individual filed Critical Individual
Priority to GB9318/38A priority Critical patent/GB514157A/en
Publication of GB514157A publication Critical patent/GB514157A/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)
  • Mechanisms For Operating Contacts (AREA)

Abstract

514,157. Controlling aircraft. TAMPIER, R March 26, 1938, No. 9318. [Class 4] An aircraft includes a control surface comprising a relatively small area for use at high speeds and a relatively large area for use at slower speeds and means for actuating one of the areas only after the other has been actuated. In one form, the control surface 3 effective during high-speed flight is operated from a lever 32 through lever and link mechanism and a device 13 similar to that described in Specification 499,503. Extended movement of the lever 32 causes an abutment 31 on a rod 30 to contact one or other of abutments 25, 26 mounted on a rod 24 and connected to return springs 27, 29. The subsequent movement of the rod 24 moves the surface 2 through an irreversible device 4 similar to that described in Specification 496,875. The control surfaces 2, 3 may be hingeably connected in tandem.
GB9318/38A 1938-03-26 1938-03-26 Improvements in or relating to control surfaces on aircraft Expired GB514157A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB9318/38A GB514157A (en) 1938-03-26 1938-03-26 Improvements in or relating to control surfaces on aircraft

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB9318/38A GB514157A (en) 1938-03-26 1938-03-26 Improvements in or relating to control surfaces on aircraft

Publications (1)

Publication Number Publication Date
GB514157A true GB514157A (en) 1939-11-01

Family

ID=9869659

Family Applications (1)

Application Number Title Priority Date Filing Date
GB9318/38A Expired GB514157A (en) 1938-03-26 1938-03-26 Improvements in or relating to control surfaces on aircraft

Country Status (1)

Country Link
GB (1) GB514157A (en)

Cited By (1)

* 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

Cited By (1)

* 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

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