GB329657A - Improvements in or relating to aircraft structures - Google Patents

Improvements in or relating to aircraft structures

Info

Publication number
GB329657A
GB329657A GB5811/29A GB581129A GB329657A GB 329657 A GB329657 A GB 329657A GB 5811/29 A GB5811/29 A GB 5811/29A GB 581129 A GB581129 A GB 581129A GB 329657 A GB329657 A GB 329657A
Authority
GB
United Kingdom
Prior art keywords
wing
members
internal
strut
external
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
GB5811/29A
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.)
Bristol Aeroplane Co Ltd
Original Assignee
Bristol Aeroplane 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 Bristol Aeroplane Co Ltd filed Critical Bristol Aeroplane Co Ltd
Priority to GB5811/29A priority Critical patent/GB329657A/en
Publication of GB329657A publication Critical patent/GB329657A/en
Expired legal-status Critical Current

Links

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C3/00Wings

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Jib Cranes (AREA)

Abstract

329,657. Bristol Aeroplane Co., Ltd.. and Pollard, F. J. Feb. 21, 1929. Planes, construction of; planes connecting together and to machine.-A strut or tie for supporting an aircraft wing structure from without comprises an external part and a plurality of internal parts all engaging the external part (for example at a common point) within the structure, the free ends of the internal parts being connected to the interior of the structure at distributed points. In the example shown a, wing structure is built up of seven spars 10 each comprising an upper and lower boom spaced round the periphery of the wing. To each upper boom a member 11 is secured and these have their lower ends brought together in two groups as shown and connected to external strut members 12 and 13 which are anchored to the fuselage at 14, or, in the case of a biplane structure, to similar internal bracing members within the lower wing: the lower plane may, in turn, be similarly supported. Alternatively in a very light structure all the internal members may be grouped together and a single external strut used. Each of the internal members 11 may be secured to the wing structure at more, than one point. Specification 309,110 is referred to.
GB5811/29A 1929-02-21 1929-02-21 Improvements in or relating to aircraft structures Expired GB329657A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB5811/29A GB329657A (en) 1929-02-21 1929-02-21 Improvements in or relating to aircraft structures

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB5811/29A GB329657A (en) 1929-02-21 1929-02-21 Improvements in or relating to aircraft structures

Publications (1)

Publication Number Publication Date
GB329657A true GB329657A (en) 1930-05-21

Family

ID=9803041

Family Applications (1)

Application Number Title Priority Date Filing Date
GB5811/29A Expired GB329657A (en) 1929-02-21 1929-02-21 Improvements in or relating to aircraft structures

Country Status (1)

Country Link
GB (1) GB329657A (en)

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