GB125284A - Improvements in Struts for Aircraft. - Google Patents

Improvements in Struts for Aircraft.

Info

Publication number
GB125284A
GB125284A GB1044218A GB1044218A GB125284A GB 125284 A GB125284 A GB 125284A GB 1044218 A GB1044218 A GB 1044218A GB 1044218 A GB1044218 A GB 1044218A GB 125284 A GB125284 A GB 125284A
Authority
GB
United Kingdom
Prior art keywords
flanges
struts
plate
members
aircraft
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
GB1044218A
Inventor
Edward Eugene Brown
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 GB1044218A priority Critical patent/GB125284A/en
Publication of GB125284A publication Critical patent/GB125284A/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)
  • Laminated Bodies (AREA)

Abstract

125,284. Brown, E. E., and Mooney, D. J. June 25, 1918. Framework.-Struts for aeroplanes are formed by two longitudinally corrugated channel members a, Fig. 4, with .side flanges c riveted together and shaped to receive end fittings, the members a being covered to an approximate stream-like section by material h such as sheet-metal, veneer, doped fabric, or three-ply wood. The front flanges may be bent at p and may be secured to a plate d, Fig. 7. Corrugations e may also be formed on the plate d, or on the rear flanges as shown. The end fitting may have a single or double eye or a socket, and may be formed upon a split tube. Two plates d may be used, and may form the bends p and the rear extension from the cover h.
GB1044218A 1918-06-25 1918-06-25 Improvements in Struts for Aircraft. Expired GB125284A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB1044218A GB125284A (en) 1918-06-25 1918-06-25 Improvements in Struts for Aircraft.

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB1044218A GB125284A (en) 1918-06-25 1918-06-25 Improvements in Struts for Aircraft.

Publications (1)

Publication Number Publication Date
GB125284A true GB125284A (en) 1919-04-17

Family

ID=32344581

Family Applications (1)

Application Number Title Priority Date Filing Date
GB1044218A Expired GB125284A (en) 1918-06-25 1918-06-25 Improvements in Struts for Aircraft.

Country Status (1)

Country Link
GB (1) GB125284A (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN108248814A (en) * 2018-01-10 2018-07-06 中国商用飞机有限责任公司 Aircraft bird strike resistant front edge and support for aircraft bird strike resistant front edge

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN108248814A (en) * 2018-01-10 2018-07-06 中国商用飞机有限责任公司 Aircraft bird strike resistant front edge and support for aircraft bird strike resistant front edge

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