GB211606A - Improvements in the construction of structural members for aircraft - Google Patents

Improvements in the construction of structural members for aircraft

Info

Publication number
GB211606A
GB211606A GB33058/22A GB3305822A GB211606A GB 211606 A GB211606 A GB 211606A GB 33058/22 A GB33058/22 A GB 33058/22A GB 3305822 A GB3305822 A GB 3305822A GB 211606 A GB211606 A GB 211606A
Authority
GB
United Kingdom
Prior art keywords
booms
strips
edges
corrugations
fit
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
GB33058/22A
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 GB33058/22A priority Critical patent/GB211606A/en
Publication of GB211606A publication Critical patent/GB211606A/en
Expired legal-status Critical Current

Links

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C1/00Fuselages; Constructional features common to fuselages, wings, stabilising surfaces or the like
    • B64C1/06Frames; Stringers; Longerons ; Fuselage sections
    • B64C1/064Stringers; Longerons
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C1/00Fuselages; Constructional features common to fuselages, wings, stabilising surfaces or the like
    • B64C1/06Frames; Stringers; Longerons ; Fuselage sections
    • B64C1/065Spars
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C1/00Fuselages; Constructional features common to fuselages, wings, stabilising surfaces or the like
    • B64C2001/0054Fuselage structures substantially made from particular materials
    • B64C2001/0081Fuselage structures substantially made from particular materials from metallic materials

Landscapes

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

Abstract

211,606. Mooney, D. J. Dec. 4, 1922. Framework.-A girder, spar, longeron, or the like comprises upper and lower channel-section booms a, b with longitudinally-corrugated webs and separate connecting strips c, of channel section with parallel plane sides, running diagonally from boom to boom, their ends butting together at d, fitting within the channels of the booms, and being fastened by their sides to the sides of the booms by rivets e passing through distance tubes f. The edges of the booms may be turned outwards as shown at g, Fig. 3. The end edges o, Fig. 6, of the strips c may be shaped to fit the corrugations of the booms, and the strips may be corrugated longitudinally, the edges n being turned over to prevent their cutting into the booms. Fig. 7 shows a modification in which a strip c, slightly wider than the booms, has its ends k narrowed together to fit the booms. Fig. 8 shows a longitudinally corrugated strip c with corrugations m stamped in the ends to fit the corrugations of the booms, the strips butting together vertically along the edges m<1>. Specifications 8522/12 and 26147/13 are referred to.
GB33058/22A 1922-12-04 1922-12-04 Improvements in the construction of structural members for aircraft Expired GB211606A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB33058/22A GB211606A (en) 1922-12-04 1922-12-04 Improvements in the construction of structural members for aircraft

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB33058/22A GB211606A (en) 1922-12-04 1922-12-04 Improvements in the construction of structural members for aircraft

Publications (1)

Publication Number Publication Date
GB211606A true GB211606A (en) 1924-02-28

Family

ID=10347968

Family Applications (1)

Application Number Title Priority Date Filing Date
GB33058/22A Expired GB211606A (en) 1922-12-04 1922-12-04 Improvements in the construction of structural members for aircraft

Country Status (1)

Country Link
GB (1) GB211606A (en)

Similar Documents

Publication Publication Date Title
GB125748A (en) Improvements in Construction of Metal Spars and Longerons for Aircraft.
GB211606A (en) Improvements in the construction of structural members for aircraft
GB220383A (en) Improvements in metal framework for aircraft
US2170458A (en) Light-weight girder, especially for aircraft
GB162108A (en) Improvements in or relating to the construction of metal spars longerons and the like for aircraft
GB361010A (en) Improvements in and relating to metal spars and the like for aircraft
GB308061A (en) Improvements in or connected with beams or spars for aircraft and other light structures
GB161063A (en) Improvements in metal construction of spars, longerons and the like for aircraft
GB202761A (en) Improvements in or relating to spars for aircraft
GB128262A (en) Improvements in Girders and similar Structures for Aircraft and other purposes.
GB247313A (en) Improvements in the construction of aircraft members
GB227482A (en) Improvements in ribs, cross members and the like for aircraft
GB430759A (en) Improvements in or relating to metal beams
GB223670A (en) Improvements in or relating to metal spars and the like for aviation
GB125209A (en) Improvements in or relating to Structural Units in the Form of Beams, Girders and the like.
GB234878A (en) Improvements in ribs, cross members and the like for aircraft
GB264626A (en) Improvements in or relating to light metal structures
GB293552A (en) Improvements in or connected with girders, spars and like members
GB128663A (en) Improvements in Metal Construction for Aircraft.
GB261492A (en) Improvements in the construction of spars, longerons and the like for aircraft
GB157311A (en) Improvement in spar beams or ribs for airplanes
GB230213A (en) Improvements in or relating to light metal spars or beams
GB154035A (en) Improvements in metal construction for aircraft
GB192966A (en) Improvements in the construction of wings and like members of aircraft
GB253651A (en) Improvements in and connected with girder structures particularly applicable to the construction of aircraft