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GB832762A - Improvements in aeroplanes - Google Patents

Improvements in aeroplanes

Info

Publication number
GB832762A
GB832762A GB976356A GB976356A GB832762A GB 832762 A GB832762 A GB 832762A GB 976356 A GB976356 A GB 976356A GB 976356 A GB976356 A GB 976356A GB 832762 A GB832762 A GB 832762A
Authority
GB
United Kingdom
Prior art keywords
aircraft
aeroplanes
armstrongs
vickers
bow
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
GB976356A
Inventor
Barnes Neville Wallis
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.)
Vickers Armstrongs Aircraft Ltd
Original Assignee
Vickers Armstrongs Aircraft 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 Vickers Armstrongs Aircraft Ltd filed Critical Vickers Armstrongs Aircraft Ltd
Priority to GB976356A priority Critical patent/GB832762A/en
Publication of GB832762A publication Critical patent/GB832762A/en
Expired legal-status Critical Current

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C3/00—Wings
    • B64C3/38—Adjustment of complete wings or parts thereof
    • B64C3/40—Varying angle of sweep

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Pressure Welding/Diffusion-Bonding (AREA)
  • Laminated Bodies (AREA)
  • Tires In General (AREA)

Abstract

832,762. Aircraft. VICKERS-ARMSTRONGS (AIRCRAFT) Ltd. March 28, 1956, No. 9763/56. Addition to 832,760. Class 4. The fore body of the aircraft described in the parent Specification is, in plan form, a finely pointed triangle A B B in which the leading edges D, D lie within the straight lines D 1 , D 1 joining the bow to the ends of the base, thereby obtaining a low thickness/chord ratio without increase in drag.
GB976356A 1956-03-28 1956-03-28 Improvements in aeroplanes Expired GB832762A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB976356A GB832762A (en) 1956-03-28 1956-03-28 Improvements in aeroplanes

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB976356A GB832762A (en) 1956-03-28 1956-03-28 Improvements in aeroplanes

Publications (1)

Publication Number Publication Date
GB832762A true GB832762A (en) 1960-04-13

Family

ID=9878318

Family Applications (1)

Application Number Title Priority Date Filing Date
GB976356A Expired GB832762A (en) 1956-03-28 1956-03-28 Improvements in aeroplanes

Country Status (1)

Country Link
GB (1) GB832762A (en)

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