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GB225307A - Improvements in the construction of metal framework members for aircraft - Google Patents

Improvements in the construction of metal framework members for aircraft

Info

Publication number
GB225307A
GB225307A GB22540/23A GB2254023A GB225307A GB 225307 A GB225307 A GB 225307A GB 22540/23 A GB22540/23 A GB 22540/23A GB 2254023 A GB2254023 A GB 2254023A GB 225307 A GB225307 A GB 225307A
Authority
GB
United Kingdom
Prior art keywords
booms
aircraft
strips
construction
metal framework
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
GB22540/23A
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.)
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 GB22540/23A priority Critical patent/GB225307A/en
Publication of GB225307A publication Critical patent/GB225307A/en
Expired legal-status Critical Current

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C1/00—Fuselages; Constructional features common to fuselages, wings, stabilising surfaces or the like
    • B64C1/06—Frames; Stringers; Longerons ; Fuselage sections
    • B64C1/065—Spars
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C1/00—Fuselages; Constructional features common to fuselages, wings, stabilising surfaces or the like
    • B64C2001/0054—Fuselage structures substantially made from particular materials
    • B64C2001/0081—Fuselage structures substantially made from particular materials from metallic materials
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00—Aeronautics or air transport
    • Y02T50/40—Weight reduction

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Moulding By Coating Moulds (AREA)

Abstract

225,307. Mooney, D. J. Sept. 7,1923. Framework. - Aircraft spars or ribs, comprising booms and webs formed of separate metal strips, have those booms which are in compression made of thicker material or of a stiffer shape than those parts that are in tension ; or both means may be employed together. Alternatively the same gauge material may be used throughout and those parts that are in compression may be strengthened by additional strips of the same shape so as to form double-thickness booms, or strips c, g, or i, Figs. 6, 12 or 14, may be employed. Cylindrical booms may be reinforced by sliding on to them tubes of slightly greater diameter. Specifications 131,969 and 195,825 are referred to.
GB22540/23A 1923-09-07 1923-09-07 Improvements in the construction of metal framework members for aircraft Expired GB225307A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB22540/23A GB225307A (en) 1923-09-07 1923-09-07 Improvements in the construction of metal framework members for aircraft

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB22540/23A GB225307A (en) 1923-09-07 1923-09-07 Improvements in the construction of metal framework members for aircraft

Publications (1)

Publication Number Publication Date
GB225307A true GB225307A (en) 1924-12-04

Family

ID=10181055

Family Applications (1)

Application Number Title Priority Date Filing Date
GB22540/23A Expired GB225307A (en) 1923-09-07 1923-09-07 Improvements in the construction of metal framework members for aircraft

Country Status (1)

Country Link
GB (1) GB225307A (en)

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