GB131080A - Improvements in the Construction of Metal Spars for Aircraft. - Google Patents

Improvements in the Construction of Metal Spars for Aircraft.

Info

Publication number
GB131080A
GB131080A GB6898/18A GB689818A GB131080A GB 131080 A GB131080 A GB 131080A GB 6898/18 A GB6898/18 A GB 6898/18A GB 689818 A GB689818 A GB 689818A GB 131080 A GB131080 A GB 131080A
Authority
GB
United Kingdom
Prior art keywords
aircraft
webs
construction
channel
flanges
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
GB6898/18A
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 GB6898/18A priority Critical patent/GB131080A/en
Publication of GB131080A publication Critical patent/GB131080A/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)
  • Moulding By Coating Moulds (AREA)
  • Laminated Bodies (AREA)

Abstract

131,080. Mooney, D. J. April 24, 1918. Framework. - A metal spar, longeron, &c. for aircraft is formed from channel members having parts stamped up from the webs to form vertical supports for the two flanges. Fig. 2 shows a channel member with a part c bent out from the web and riveted to the flanges f. The webs of two adjacent channel members may be united at intervals to form a girder by vertical channel-shaped members. Other lightening holes may be formed in the webs.
GB6898/18A 1918-04-24 1918-04-24 Improvements in the Construction of Metal Spars for Aircraft. Expired GB131080A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB6898/18A GB131080A (en) 1918-04-24 1918-04-24 Improvements in the Construction of Metal Spars for Aircraft.

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB6898/18A GB131080A (en) 1918-04-24 1918-04-24 Improvements in the Construction of Metal Spars for Aircraft.

Publications (1)

Publication Number Publication Date
GB131080A true GB131080A (en) 1919-08-21

Family

ID=32407854

Family Applications (1)

Application Number Title Priority Date Filing Date
GB6898/18A Expired GB131080A (en) 1918-04-24 1918-04-24 Improvements in the Construction of Metal Spars for Aircraft.

Country Status (1)

Country Link
GB (1) GB131080A (en)

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