GB602911A - Wing structure for aeroplanes - Google Patents

Wing structure for aeroplanes

Info

Publication number
GB602911A
GB602911A GB32594/45A GB3259445A GB602911A GB 602911 A GB602911 A GB 602911A GB 32594/45 A GB32594/45 A GB 32594/45A GB 3259445 A GB3259445 A GB 3259445A GB 602911 A GB602911 A GB 602911A
Authority
GB
United Kingdom
Prior art keywords
skin
wing
aeroplanes
curved
wing structure
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
GB32594/45A
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 GB32594/45A priority Critical patent/GB602911A/en
Publication of GB602911A publication Critical patent/GB602911A/en
Expired legal-status Critical Current

Links

Classifications

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

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Toys (AREA)

Abstract

602,911. Aircraft wing structures. REID, W. T. Dec. 3, 1945, No. 32594. [Class 4] The framing between the upper and lower skins of a wing comprises channel-shaped members A, B, and C, of inverted U-form and extended span-wise of the wing to provide arch-shaped spaces to which access for storage &c. is had through apertures in the lower skin. The main member B has its curved top connected to the upper skin and the lower edges of its sides to the lower skin. End members A and D have curved edges secured to the nose 18 and the top skin respectively. Distance pieces such as 25 are employed between the lower wall-ends.
GB32594/45A 1945-12-03 1945-12-03 Wing structure for aeroplanes Expired GB602911A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB32594/45A GB602911A (en) 1945-12-03 1945-12-03 Wing structure for aeroplanes

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB32594/45A GB602911A (en) 1945-12-03 1945-12-03 Wing structure for aeroplanes

Publications (1)

Publication Number Publication Date
GB602911A true GB602911A (en) 1948-06-04

Family

ID=10341061

Family Applications (1)

Application Number Title Priority Date Filing Date
GB32594/45A Expired GB602911A (en) 1945-12-03 1945-12-03 Wing structure for aeroplanes

Country Status (1)

Country Link
GB (1) GB602911A (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN111924086A (en) * 2020-07-07 2020-11-13 北京机电工程研究所 Deformable mechanism driven by memory alloy

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN111924086A (en) * 2020-07-07 2020-11-13 北京机电工程研究所 Deformable mechanism driven by memory alloy

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