GB774688A - Improvements relating to aircraft - Google Patents

Improvements relating to aircraft

Info

Publication number
GB774688A
GB774688A GB443554A GB443554A GB774688A GB 774688 A GB774688 A GB 774688A GB 443554 A GB443554 A GB 443554A GB 443554 A GB443554 A GB 443554A GB 774688 A GB774688 A GB 774688A
Authority
GB
United Kingdom
Prior art keywords
aircraft
wing
spars
frame
sections
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
GB443554A
Inventor
Herbert Eugene Chaplin
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.)
Fairey Aviation Co Ltd
Original Assignee
Fairey Aviation Co 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 Fairey Aviation Co Ltd filed Critical Fairey Aviation Co Ltd
Priority to GB443554A priority Critical patent/GB774688A/en
Publication of GB774688A publication Critical patent/GB774688A/en
Expired legal-status Critical Current

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C39/00—Aircraft not otherwise provided for
    • B64C39/10—All-wing aircraft

Landscapes

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

Abstract

774,688. Aircraft framework. FAIREY AVIATION CO., Ltd. May 13, 1955 [Feb. 15, 1954], No. 4435/54. Addition to 734,532. Class 4. In delta-wing aircraft having an unbraced fuselage each main load-carrying spar 3 of the wings extends in a plane at right angles to the fore-and-aft axis of the aircraft and is connected to the corresponding spar of the other wing through a frame in the form of a ring or other closed figure extending across both the top and the bottom of the fuselage, characterized in that the frame is formed in two or three sections 1, 2 or 8, 9, 10, Fig. 4, the two wing spars being secured to different frame sections, 1 and 2 or 8 and 9. The wing spars may be integral with their respective frame sections and port and starboard spars may be identical.
GB443554A 1954-02-15 1954-02-15 Improvements relating to aircraft Expired GB774688A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB443554A GB774688A (en) 1954-02-15 1954-02-15 Improvements relating to aircraft

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB443554A GB774688A (en) 1954-02-15 1954-02-15 Improvements relating to aircraft

Publications (1)

Publication Number Publication Date
GB774688A true GB774688A (en) 1957-05-15

Family

ID=9777122

Family Applications (1)

Application Number Title Priority Date Filing Date
GB443554A Expired GB774688A (en) 1954-02-15 1954-02-15 Improvements relating to aircraft

Country Status (1)

Country Link
GB (1) GB774688A (en)

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