GB452726A - Improvements in the structure of fuselages, wings and other bodies of aircraft - Google Patents

Improvements in the structure of fuselages, wings and other bodies of aircraft

Info

Publication number
GB452726A
GB452726A GB625435A GB625435A GB452726A GB 452726 A GB452726 A GB 452726A GB 625435 A GB625435 A GB 625435A GB 625435 A GB625435 A GB 625435A GB 452726 A GB452726 A GB 452726A
Authority
GB
United Kingdom
Prior art keywords
members
flanges
aircraft
wings
bodies
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
GB625435A
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.)
GKN Aerospace Services Ltd
Original Assignee
Vickers Aviation 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 Aviation Ltd filed Critical Vickers Aviation Ltd
Priority to GB625435A priority Critical patent/GB452726A/en
Publication of GB452726A publication Critical patent/GB452726A/en
Expired legal-status Critical Current

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C1/00—Fuselages; Constructional features common to fuselages, wings, stabilising surfaces or the like
    • B64C1/06—Frames; Stringers; Longerons ; Fuselage sections
    • B64C1/08—Geodetic or other open-frame structures

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Body Structure For Vehicles (AREA)
  • Connection Of Plates (AREA)

Abstract

452,726. Aircraft structures. VICKERS (AVIATION), Ltd., and WALLIS, B. N., Byfleet Road, Weybridge, Surrey. Feb. 27, 1935, No. 6254. [Class 4] Aircraft fuselages, wings, or other bodies are constructed of longitudinal members a, a<1>, &c., and two series geodetic members b, c, continuous between the longitudinal members, shaped to the contour of the body, of greater depth than width, twisted about their neutral axes so that they are normal to the surface and recessed at their intersections with one another so that the two series can fit into each other. As shown, the members b, c are formed of channels having inturned flanges. Gusset plates d extend across the interrupted flanges C<SP>2> and are riveted to the flanges of the members whose webs are connected by angle plates e. The longitudinal members are built up of back-to-back channels a4, a<5> with stiffening strips a<6>, a<7>, a<8>. The geodetic members, at the ends of the structure are attached to a hoop. Specifications 388,438 and 412,232 arc referred to.
GB625435A 1935-02-27 1935-02-27 Improvements in the structure of fuselages, wings and other bodies of aircraft Expired GB452726A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB625435A GB452726A (en) 1935-02-27 1935-02-27 Improvements in the structure of fuselages, wings and other bodies of aircraft

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB625435A GB452726A (en) 1935-02-27 1935-02-27 Improvements in the structure of fuselages, wings and other bodies of aircraft

Publications (1)

Publication Number Publication Date
GB452726A true GB452726A (en) 1936-08-27

Family

ID=9811190

Family Applications (1)

Application Number Title Priority Date Filing Date
GB625435A Expired GB452726A (en) 1935-02-27 1935-02-27 Improvements in the structure of fuselages, wings and other bodies of aircraft

Country Status (1)

Country Link
GB (1) GB452726A (en)

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