GB950492A - Improvements in aircraft adapted for vertical take-off and landing - Google Patents

Improvements in aircraft adapted for vertical take-off and landing

Info

Publication number
GB950492A
GB950492A GB768561A GB768561A GB950492A GB 950492 A GB950492 A GB 950492A GB 768561 A GB768561 A GB 768561A GB 768561 A GB768561 A GB 768561A GB 950492 A GB950492 A GB 950492A
Authority
GB
United Kingdom
Prior art keywords
landing
vertical take
aircraft
servomotor
nozzle
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
GB768561A
Inventor
Lawrence Reid
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.)
Short Brothers PLC
Original Assignee
Short Brothers and Harland Ltd
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 Short Brothers and Harland Ltd filed Critical Short Brothers and Harland Ltd
Priority to GB768561A priority Critical patent/GB950492A/en
Publication of GB950492A publication Critical patent/GB950492A/en
Expired legal-status Critical Current

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C29/00—Aircraft capable of landing or taking-off vertically, e.g. vertical take-off and landing [VTOL] aircraft
    • B64C29/0091—Accessories not provided for elsewhere

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Automatic Analysis And Handling Materials Therefor (AREA)

Abstract

950,492. Controlling aircraft. SHORT BROS. & HARLAND Ltd. Feb. 9, 1962 [March 2, 1961], No. 7685/61. Heading B7G. In a V.T.O.L. aircraft controlled and stabilized both by aerodynamic control surfaces D and jet nozzles E control mechanism is provided comprising a high-rate servomotor B and a low-rate servomotor A respectively coupled to opposite ends of a differential lever C, which is provided with further connections CD and CE to the surface D and nozzle E respectively. The arrangement is such that the nozzle E is subjected to direct control by motor B whereas surface D is subjected to the algebraic sum of the outputs of both servomotors.
GB768561A 1961-03-02 1961-03-02 Improvements in aircraft adapted for vertical take-off and landing Expired GB950492A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB768561A GB950492A (en) 1961-03-02 1961-03-02 Improvements in aircraft adapted for vertical take-off and landing

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB768561A GB950492A (en) 1961-03-02 1961-03-02 Improvements in aircraft adapted for vertical take-off and landing

Publications (1)

Publication Number Publication Date
GB950492A true GB950492A (en) 1964-02-26

Family

ID=9837831

Family Applications (1)

Application Number Title Priority Date Filing Date
GB768561A Expired GB950492A (en) 1961-03-02 1961-03-02 Improvements in aircraft adapted for vertical take-off and landing

Country Status (1)

Country Link
GB (1) GB950492A (en)

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