GB150517A - Improvements in joint plates especially for use with aeroplanes and like structures - Google Patents

Improvements in joint plates especially for use with aeroplanes and like structures

Info

Publication number
GB150517A
GB150517A GB1980819A GB1980819A GB150517A GB 150517 A GB150517 A GB 150517A GB 1980819 A GB1980819 A GB 1980819A GB 1980819 A GB1980819 A GB 1980819A GB 150517 A GB150517 A GB 150517A
Authority
GB
United Kingdom
Prior art keywords
plate
sockets
lugs
aeroplanes
structures
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
GB1980819A
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 GB1980819A priority Critical patent/GB150517A/en
Publication of GB150517A publication Critical patent/GB150517A/en
Expired legal-status Critical Current

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C3/00—Wings
    • B64C3/18—Spars; Ribs; Stringers

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Joining Of Building Structures In Genera (AREA)

Abstract

150,517. Roe, A. V. Aug. 12, 1919 framework.-A joint plate for connecting struts to longerons, especially in aeroplane fuselages, comprises an angle plate 1 fitting on to a longeron 6 and formed with sockets 3 to receive the ends of the struts, and on each side of one or both sockets with lugs 4 for attaching bracing- wires 7. The plate is secured to the longeron by a diagonal bolt 10, the head of which may be formed with an eye to receive a transverse bracing-wire 8; or the wire 8 may be attached to lugs 11 bent up from a piece 12 secured under the head of the bolt, as shown. The sockets 3 may be attached to the plate 1 by lugs 16, which are passed through holes in the plate and then turned over.
GB1980819A 1919-08-12 1919-08-12 Improvements in joint plates especially for use with aeroplanes and like structures Expired GB150517A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB1980819A GB150517A (en) 1919-08-12 1919-08-12 Improvements in joint plates especially for use with aeroplanes and like structures

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB1980819A GB150517A (en) 1919-08-12 1919-08-12 Improvements in joint plates especially for use with aeroplanes and like structures

Publications (1)

Publication Number Publication Date
GB150517A true GB150517A (en) 1920-09-09

Family

ID=10135558

Family Applications (1)

Application Number Title Priority Date Filing Date
GB1980819A Expired GB150517A (en) 1919-08-12 1919-08-12 Improvements in joint plates especially for use with aeroplanes and like structures

Country Status (1)

Country Link
GB (1) GB150517A (en)

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