GB207500A - An improved joint or connecting device for aircraft and other framework - Google Patents

An improved joint or connecting device for aircraft and other framework

Info

Publication number
GB207500A
GB207500A GB21476/23A GB2147623A GB207500A GB 207500 A GB207500 A GB 207500A GB 21476/23 A GB21476/23 A GB 21476/23A GB 2147623 A GB2147623 A GB 2147623A GB 207500 A GB207500 A GB 207500A
Authority
GB
United Kingdom
Prior art keywords
flanges
aircraft
tube
joint
members
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
GB21476/23A
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.)
EMBOUTISSAGE ET DE CONST MECAN
Original Assignee
EMBOUTISSAGE ET DE CONST MECAN
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 EMBOUTISSAGE ET DE CONST MECAN filed Critical EMBOUTISSAGE ET DE CONST MECAN
Publication of GB207500A publication Critical patent/GB207500A/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
    • 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)
  • Mutual Connection Of Rods And Tubes (AREA)

Abstract

207,500. Soc. d'Emboutissage et de Constructions MÚcaniques. Nov. 22, 1922, [Convention. date]. Rod couplings and connections.-A joint for aircraft and other framework comprises one or more stamped or pressed members adapted to be secured together to embrace the ends of the parts to be connected or extensions or projections thereon, one or more of the members having each one or more depressions or a channel adapted to engage corresponding portions on the parts to be connected to prevent endwise movement. The Figure shows a joint for an aircraft fuselage in which the ends of tubular members a, b, c, d, e are embraced by flanged metal plates f , g, h riveted together. For the attachment of stay wires a plate j may be inserted between the flanges as shown in the plane of the tube c, or holes g<10> may be formed in the flanges themselves and if necessary strengthened by an additional plate k as shown in the plane of the tube b. Strengthening-plates l may be placed on the outsides of the flanges. To prevent endwise movement of the tubes, projections b', e' may engage corresponding recesses in the tube ends or a channel or moulding d<1> may be provided.
GB21476/23A 1922-11-22 1923-08-24 An improved joint or connecting device for aircraft and other framework Expired GB207500A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
BE207500X 1922-11-22

Publications (1)

Publication Number Publication Date
GB207500A true GB207500A (en) 1924-11-24

Family

ID=3865876

Family Applications (1)

Application Number Title Priority Date Filing Date
GB21476/23A Expired GB207500A (en) 1922-11-22 1923-08-24 An improved joint or connecting device for aircraft and other framework

Country Status (1)

Country Link
GB (1) GB207500A (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2133108A (en) * 1983-01-05 1984-07-18 John Robinson Structural jointing members
US6056240A (en) * 1995-04-05 2000-05-02 Luftschiffbau Gmbh Support for an airship

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2133108A (en) * 1983-01-05 1984-07-18 John Robinson Structural jointing members
US6056240A (en) * 1995-04-05 2000-05-02 Luftschiffbau Gmbh Support for an airship

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