GB431767A - Airplane wings - Google Patents

Airplane wings

Info

Publication number
GB431767A
GB431767A GB28103/33A GB2810333A GB431767A GB 431767 A GB431767 A GB 431767A GB 28103/33 A GB28103/33 A GB 28103/33A GB 2810333 A GB2810333 A GB 2810333A GB 431767 A GB431767 A GB 431767A
Authority
GB
United Kingdom
Prior art keywords
link
airplane wings
abridged
void
wing
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
GB28103/33A
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.)
L P R Co
Original Assignee
L P R Co
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 L P R Co filed Critical L P R Co
Priority to GB28103/33A priority Critical patent/GB431767A/en
Publication of GB431767A publication Critical patent/GB431767A/en
Expired legal-status Critical Current

Links

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C13/00Control 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)
  • Toys (AREA)

Abstract

431,767. Controlling aircraft. L.P.R. CO., 277, Park Avenue, New York, U.S.A. Oct. 11, 1933, No. 28103. Void [Abridged as open to inspection under Sect. 91 of the Acts, April 12, 1934]. Drawings to Specification. [Class 4] An auxiliary aerofoil of high-aspect ratio is mounted in front of and above the leading edge of a wing and by means of a link is connected to a manual-adjustable aileron. In a modification, the link is replaced by crossed cables.
GB28103/33A 1933-10-11 1933-10-11 Airplane wings Expired GB431767A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB28103/33A GB431767A (en) 1933-10-11 1933-10-11 Airplane wings

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB28103/33A GB431767A (en) 1933-10-11 1933-10-11 Airplane wings

Publications (1)

Publication Number Publication Date
GB431767A true GB431767A (en) 1935-07-15

Family

ID=10270314

Family Applications (1)

Application Number Title Priority Date Filing Date
GB28103/33A Expired GB431767A (en) 1933-10-11 1933-10-11 Airplane wings

Country Status (1)

Country Link
GB (1) GB431767A (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3223356A (en) * 1963-03-06 1965-12-14 Alvarez-Calderon Alberto Deflected slipstream system for aircraft

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3223356A (en) * 1963-03-06 1965-12-14 Alvarez-Calderon Alberto Deflected slipstream system for aircraft

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