GB247313A - Improvements in the construction of aircraft members - Google Patents

Improvements in the construction of aircraft members

Info

Publication number
GB247313A
GB247313A GB27786/24A GB2778624A GB247313A GB 247313 A GB247313 A GB 247313A GB 27786/24 A GB27786/24 A GB 27786/24A GB 2778624 A GB2778624 A GB 2778624A GB 247313 A GB247313 A GB 247313A
Authority
GB
United Kingdom
Prior art keywords
webs
booms
bolts
flanges
shaped
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
GB27786/24A
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 GB27786/24A priority Critical patent/GB247313A/en
Publication of GB247313A publication Critical patent/GB247313A/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
    • 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

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Tents Or Canopies (AREA)

Abstract

247,313. Mooney, D. J. Nov. 20, 1924. Framework.-Metal spars, longerons, girders &c. are composed of tubular booms a and strip webs c connected together by bolts passing through the interior of the tubular booms, which are shaped so as to resist the resultant pressure. In the construction shown in Fig. 1, the booms a are shaped at b to fit the overlapping portions of the webs c, and take the pressure when the connecting bolts d are screwed up. The booms and webs may be varied in form to suit requirements, and distance pieces may be threaded upon the bolts. According to the modification shown n Fig. 4, the flanges l may be bent inwardly and the webs secured by bolts d passing through the sides of the tubes a, and through the flanges l. According to the Provisional Specification the webs may be placed at intervals or perforated for lightness.
GB27786/24A 1924-11-20 1924-11-20 Improvements in the construction of aircraft members Expired GB247313A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB27786/24A GB247313A (en) 1924-11-20 1924-11-20 Improvements in the construction of aircraft members

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB27786/24A GB247313A (en) 1924-11-20 1924-11-20 Improvements in the construction of aircraft members

Publications (1)

Publication Number Publication Date
GB247313A true GB247313A (en) 1926-02-18

Family

ID=10265282

Family Applications (1)

Application Number Title Priority Date Filing Date
GB27786/24A Expired GB247313A (en) 1924-11-20 1924-11-20 Improvements in the construction of aircraft members

Country Status (1)

Country Link
GB (1) GB247313A (en)

Similar Documents

Publication Publication Date Title
GB125748A (en) Improvements in Construction of Metal Spars and Longerons for Aircraft.
GB531357A (en) Improvements in or relating to aircraft fusilages
GB247313A (en) Improvements in the construction of aircraft members
GB151352A (en) Improvements in metal framework for aircraft
GB220383A (en) Improvements in metal framework for aircraft
GB161063A (en) Improvements in metal construction of spars, longerons and the like for aircraft
GB162108A (en) Improvements in or relating to the construction of metal spars longerons and the like for aircraft
GB234881A (en) Improvements in structural members for aircraft
GB211606A (en) Improvements in the construction of structural members for aircraft
GB608911A (en) Improvements relating to anchor nut structures
GB261492A (en) Improvements in the construction of spars, longerons and the like for aircraft
GB252755A (en) Improvements in the construction of framework members for aircraft
GB263264A (en) Improvements in the construction of framework members for aircraft
GB223670A (en) Improvements in or relating to metal spars and the like for aviation
GB128262A (en) Improvements in Girders and similar Structures for Aircraft and other purposes.
GB263602A (en) Improvements in construction of framework members for aircraft
GB224298A (en) Improvements in metal girders of light construction for aircraft and the like
GB227482A (en) Improvements in ribs, cross members and the like for aircraft
GB137197A (en) Improvements in or relating to metal spars or built-up girders
GB218074A (en) Improvements in or relating to metal spars and the like for aircraft
GB261489A (en) Improvements in or relating to aeroplane-wings having metal frames
GB264626A (en) Improvements in or relating to light metal structures
GB194114A (en) Improvements in or relating to metal spars and the like for aviation
GB225307A (en) Improvements in the construction of metal framework members for aircraft
GB308061A (en) Improvements in or connected with beams or spars for aircraft and other light structures