GB121006A - Improvements in Metal Spars for Aircraft. - Google Patents

Improvements in Metal Spars for Aircraft.

Info

Publication number
GB121006A
GB121006A GB1892117A GB1892117A GB121006A GB 121006 A GB121006 A GB 121006A GB 1892117 A GB1892117 A GB 1892117A GB 1892117 A GB1892117 A GB 1892117A GB 121006 A GB121006 A GB 121006A
Authority
GB
United Kingdom
Prior art keywords
riveted
flanges
tongues
webs
section
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
GB1892117A
Inventor
Cedric William Taverner
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 GB1892117A priority Critical patent/GB121006A/en
Publication of GB121006A publication Critical patent/GB121006A/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
    • B64C3/185—Spars

Landscapes

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

Abstract

121,006. Taverner, C. W., and Mooney, D. J. Dec. 21, 1917. Framework.-A metal spar for wings, ailerons. &c., has thin metal flanges united by webs in the form of vertical rectangular tubes. Fig. 1 shows channel-section flanges a adapted to be riveted to web-sections b formed by bending thin metal to form three closed sides, from two of which tongues d are cut and are either bent over and secured together or riveted to the next section. Projections c, left when the tongues d are cut, overlap and are riveted to the adjacent section. Flanged holes and embossed parts are formed in the sides of the webs for lightness and strength. Fig. 5 shows a modification in which the web sections have flanges i riveted to flanges a of the form shown.
GB1892117A 1917-12-21 1917-12-21 Improvements in Metal Spars for Aircraft. Expired GB121006A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB1892117A GB121006A (en) 1917-12-21 1917-12-21 Improvements in Metal Spars for Aircraft.

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB1892117A GB121006A (en) 1917-12-21 1917-12-21 Improvements in Metal Spars for Aircraft.

Publications (1)

Publication Number Publication Date
GB121006A true GB121006A (en) 1918-12-05

Family

ID=32348165

Family Applications (1)

Application Number Title Priority Date Filing Date
GB1892117A Expired GB121006A (en) 1917-12-21 1917-12-21 Improvements in Metal Spars for Aircraft.

Country Status (1)

Country Link
GB (1) GB121006A (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN109733589A (en) * 2018-12-14 2019-05-10 南京航空航天大学 Novel jointing applied to wing module

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN109733589A (en) * 2018-12-14 2019-05-10 南京航空航天大学 Novel jointing applied to wing module

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