GB207329A - Improvements in structural members for aircraft - Google Patents

Improvements in structural members for aircraft

Info

Publication number
GB207329A
GB207329A GB2754922A GB2754922A GB207329A GB 207329 A GB207329 A GB 207329A GB 2754922 A GB2754922 A GB 2754922A GB 2754922 A GB2754922 A GB 2754922A GB 207329 A GB207329 A GB 207329A
Authority
GB
United Kingdom
Prior art keywords
aircraft
strip
structural members
edges
tubular
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
GB2754922A
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 GB2754922A priority Critical patent/GB207329A/en
Publication of GB207329A publication Critical patent/GB207329A/en
Expired legal-status Critical Current

Links

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C3/00Wings
    • B64C3/18Spars; Ribs; Stringers
    • B64C3/185Spars

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Rigid Pipes And Flexible Pipes (AREA)

Abstract

207,329. North, J. D. Oct. 11, 1922. Metal pipes and tubes. - A tubular strut for use in aircraft framework is formed by bending a strip 1 of sheet metal to approximately circular section, providing it with inwardly turned beaded edges 2. 3 passing over it rings 4 of such a diameter as to press these edges tightly together, and fitting the ends into tubular sockets 5. The strip 1 may be formed with one or more longitudinal grooves 6 as shown in Fig. 6. Each socket 5 is formed with a shoulder bearing on the end of the tube as shown in Fig. 4.
GB2754922A 1922-10-11 1922-10-11 Improvements in structural members for aircraft Expired GB207329A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB2754922A GB207329A (en) 1922-10-11 1922-10-11 Improvements in structural members for aircraft

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB2754922A GB207329A (en) 1922-10-11 1922-10-11 Improvements in structural members for aircraft

Publications (1)

Publication Number Publication Date
GB207329A true GB207329A (en) 1923-11-29

Family

ID=10261397

Family Applications (1)

Application Number Title Priority Date Filing Date
GB2754922A Expired GB207329A (en) 1922-10-11 1922-10-11 Improvements in structural members for aircraft

Country Status (1)

Country Link
GB (1) GB207329A (en)

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