GB270022A - Improvements in or relating to framed structures such as the fuselages of aeroplanes and the like - Google Patents

Improvements in or relating to framed structures such as the fuselages of aeroplanes and the like

Info

Publication number
GB270022A
GB270022A GB395026A GB395026A GB270022A GB 270022 A GB270022 A GB 270022A GB 395026 A GB395026 A GB 395026A GB 395026 A GB395026 A GB 395026A GB 270022 A GB270022 A GB 270022A
Authority
GB
United Kingdom
Prior art keywords
longerons
struts
fuselages
saddle pieces
longeron
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
GB395026A
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.)
Individual
Original Assignee
Individual
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 Individual filed Critical Individual
Priority to GB395026A priority Critical patent/GB270022A/en
Publication of GB270022A publication Critical patent/GB270022A/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)
  • Joining Of Building Structures In Genera (AREA)
  • Wire Processing (AREA)

Abstract

270,022. Fairey, C. R., and Lobelle, M. Feb. 11, 1926. Framework; fuselages.-In framed structures such as fuselages, the longerons a are united to the struts b by saddle pieces c riveted to the longerons and welded to the struts, lugs h, g for the attachment of bracing wires being received in slots in the struts and welded thereto and to the saddle pieces. The saddle pieces c extend rather more than halfway around the longerons to which they are secured by pairs of rivets d which pass through the interior of the longeron. The longerons a are formed of high tensile steel tubes whilst the struts, lugs, and saddle pieces are of low grade steel. Fig. 1 shows a fuselage built up from four longerons a and a plurality of rectangular frames b, which are preferably built up separately with saddle pieces c at their corners and afterwards secured to the longerons a in parallel planes and stayed by bracing wires m. A longeron may be easily replaced by removing the rivets d.
GB395026A 1926-02-11 1926-02-11 Improvements in or relating to framed structures such as the fuselages of aeroplanes and the like Expired GB270022A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB395026A GB270022A (en) 1926-02-11 1926-02-11 Improvements in or relating to framed structures such as the fuselages of aeroplanes and the like

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB395026A GB270022A (en) 1926-02-11 1926-02-11 Improvements in or relating to framed structures such as the fuselages of aeroplanes and the like

Publications (1)

Publication Number Publication Date
GB270022A true GB270022A (en) 1927-05-05

Family

ID=9767928

Family Applications (1)

Application Number Title Priority Date Filing Date
GB395026A Expired GB270022A (en) 1926-02-11 1926-02-11 Improvements in or relating to framed structures such as the fuselages of aeroplanes and the like

Country Status (1)

Country Link
GB (1) GB270022A (en)

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