GB220394A - Improvements in aircraft - Google Patents

Improvements in aircraft

Info

Publication number
GB220394A
GB220394A GB1351523A GB1351523A GB220394A GB 220394 A GB220394 A GB 220394A GB 1351523 A GB1351523 A GB 1351523A GB 1351523 A GB1351523 A GB 1351523A GB 220394 A GB220394 A GB 220394A
Authority
GB
United Kingdom
Prior art keywords
stays
frames
longitudinals
fuselage
longitudinal
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
GB1351523A
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 GB1351523A priority Critical patent/GB220394A/en
Publication of GB220394A publication Critical patent/GB220394A/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
    • B64C1/08Geodetic or other open-frame structures

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Mutual Connection Of Rods And Tubes (AREA)
  • Jib Cranes (AREA)

Abstract

220,394. McKelvey, A. L. May 22, 1923. Fuselages; framework; planes, connecting to machine. -A fuselage comprising a plurality of converging longitudinal menbers spaced apart at intervals along their length by rigid vertical frames, has connected to it wing- supporting truss frames, which surround the fuselage and are strengthened by cross bracing struts. In the construction shown, the fuselage is formed of three triangularly-arranged longitudinal members 7, 8, 9, each consisting of two concentric tubes spaced apart and bound together by V-shaped ribs 11, Fig. 3. The longitudinals converge towards their ends and are rigidly fixed together thereat. Spaced at intervals along their length are vertical frames each comprising two bent angle strips 12 placed back-to-back, secured at their ends 13 to the lower longitudinals 8, 9, and bent over the upper longitudinal 7. Two inner bracing stays 14, form a V-shaped inner wall for the lower longitudinals 8, 9, and are carried upwards face-to-face to support the top longitudinal 7. The converging parts of the stays 14 are braced by yokes 15, 16, which are connected together at their contiguous faces and are connected to the stays 14 at their ends. Struts 17 arranged in rhomboid form extend between the strips 12 and the stays 14. The frames are tied together by diagonal bracing wires 18, Fig. 1, provided with turnbuckles 19. The cabin or hull 10 consists of a double-walled shell the upper edges of which are connected to the longitudinals 8, 9. The hull is also supported by curved brackets 20, the ends of which are connected to the inner wall of the shell and to the lower ends of the stays 14. The wings are mounted upon frames 5, Figs. 1 and 2, strengthened by cross-bracing rods 6 and connected to the fuselage by masts 21, which extend through the upper longitudinal 7 and are connected to the lower longitudinals by interlaced frames 22. Steering, balancing, and regulating altitude.- The rudder 23, Fig. 1, is supported on a shaft 24 mounted on the upper longitudinal 7.
GB1351523A 1923-05-22 1923-05-22 Improvements in aircraft Expired GB220394A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB1351523A GB220394A (en) 1923-05-22 1923-05-22 Improvements in aircraft

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB1351523A GB220394A (en) 1923-05-22 1923-05-22 Improvements in aircraft

Publications (1)

Publication Number Publication Date
GB220394A true GB220394A (en) 1924-08-21

Family

ID=10024365

Family Applications (1)

Application Number Title Priority Date Filing Date
GB1351523A Expired GB220394A (en) 1923-05-22 1923-05-22 Improvements in aircraft

Country Status (1)

Country Link
GB (1) GB220394A (en)

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