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GB206998A - Improvements in the construction of wings and like members of aeroplane flying machines - Google Patents

Improvements in the construction of wings and like members of aeroplane flying machines

Info

Publication number
GB206998A
GB206998A GB28196/22A GB2819622A GB206998A GB 206998 A GB206998 A GB 206998A GB 28196/22 A GB28196/22 A GB 28196/22A GB 2819622 A GB2819622 A GB 2819622A GB 206998 A GB206998 A GB 206998A
Authority
GB
United Kingdom
Prior art keywords
sections
members
flight
wing
transverse
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
GB28196/22A
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 GB28196/22A priority Critical patent/GB206998A/en
Publication of GB206998A publication Critical patent/GB206998A/en
Expired legal-status Critical Current

Links

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C3/00Wings

Landscapes

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

Abstract

206,998. Short, H. O. Oct. 17, 1922. Planes and the like, construction of.-A metal wing is built up of tubular sections the divisions between which extend parallel to the direction of flight, the edges of adjacent sections being overlapped and riveted together. Stiffening members extending in or transverse to the direction of flight, or in both directions, may be fixed to the internal surfaces of the wing sections. Figs. 2 and 3 show respectively crosssections of a wing section 4 taken in the direction of flight and transverse to the direction of flight. The sections are built up of overlapping sheet metal plates 6 of suitable shape, continuous stiffening members 8 of right angle section being positioned externally at the junctions of the wing sections. Strengthening members 7 of channel section are also fixed at intervals to the internal surfaces of the sections and extend transverse to the direction of flight between the members 8, the ends of the flanges of these members 7 being bent downwards so that the edge of the plating 6 of the next wing section 5 and a flange of the angle strip 8 can be inserted between the plating 6 and the bent-down flanges of the members 8, and the whole riveted together. Plates 10 may also be riveted at the nose and trailing edge. The Provisional Specification states that the sections may be fitted with internal structures, which permit them to be threaded on to spars, or if all internal supports are dispensed with the metal covering may be corrugated.
GB28196/22A 1922-10-17 1922-10-17 Improvements in the construction of wings and like members of aeroplane flying machines Expired GB206998A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB28196/22A GB206998A (en) 1922-10-17 1922-10-17 Improvements in the construction of wings and like members of aeroplane flying machines

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB28196/22A GB206998A (en) 1922-10-17 1922-10-17 Improvements in the construction of wings and like members of aeroplane flying machines

Publications (1)

Publication Number Publication Date
GB206998A true GB206998A (en) 1923-11-22

Family

ID=10271807

Family Applications (1)

Application Number Title Priority Date Filing Date
GB28196/22A Expired GB206998A (en) 1922-10-17 1922-10-17 Improvements in the construction of wings and like members of aeroplane flying machines

Country Status (1)

Country Link
GB (1) GB206998A (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US7677496B2 (en) 2006-11-03 2010-03-16 Airbus Operations Limited Stringer for an aircraft wing and a method of reinforcing thereof

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US7677496B2 (en) 2006-11-03 2010-03-16 Airbus Operations Limited Stringer for an aircraft wing and a method of reinforcing thereof

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