GB136293A - Improvements in Fittings for Aeronautical Machines. - Google Patents

Improvements in Fittings for Aeronautical Machines.

Info

Publication number
GB136293A
GB136293A GB21260/18A GB2126018A GB136293A GB 136293 A GB136293 A GB 136293A GB 21260/18 A GB21260/18 A GB 21260/18A GB 2126018 A GB2126018 A GB 2126018A GB 136293 A GB136293 A GB 136293A
Authority
GB
United Kingdom
Prior art keywords
plates
flanges
riveted
distance
stiffened
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
GB21260/18A
Inventor
Dermot Joseph Mooney
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 GB21260/18A priority Critical patent/GB136293A/en
Publication of GB136293A publication Critical patent/GB136293A/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
    • B64C1/065—Spars

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Connection Of Plates (AREA)

Abstract

136,293. Mooney, D. J. Dec. 19, 1918. Framework.-In built-up metal spars, the webs and flanges are stiffened by internal tubular distancepieces and external plates at the positions where bolts pass through for fixing wiring-plates or struts. A bolt b for securing a wiring- plate h passes through the web walls d of a built-up spar a, the walls being stiffened by an inner tubular distance-piece e and external riveted plates c. The plates c may be continued and flanged so as to be riveted to the top and bottom flanges. Where a vertical and an horizontal bolt cross, the two distance-tubes e may be connected bv a plate; or two half-tubes or channel distance-pieces with flanges may be used, the flanges being riveted together at the centre.
GB21260/18A 1918-12-19 1918-12-19 Improvements in Fittings for Aeronautical Machines. Expired GB136293A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB21260/18A GB136293A (en) 1918-12-19 1918-12-19 Improvements in Fittings for Aeronautical Machines.

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB21260/18A GB136293A (en) 1918-12-19 1918-12-19 Improvements in Fittings for Aeronautical Machines.

Publications (1)

Publication Number Publication Date
GB136293A true GB136293A (en) 1919-12-18

Family

ID=32672649

Family Applications (1)

Application Number Title Priority Date Filing Date
GB21260/18A Expired GB136293A (en) 1918-12-19 1918-12-19 Improvements in Fittings for Aeronautical Machines.

Country Status (1)

Country Link
GB (1) GB136293A (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2941604A (en) * 1956-11-05 1960-06-21 Ira J Marriage Blade structure for airplane propellers

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2941604A (en) * 1956-11-05 1960-06-21 Ira J Marriage Blade structure for airplane propellers

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