GB126514A - Improvements in Bodies or Fuselages for Aeroplanes and other Aircraft. - Google Patents

Improvements in Bodies or Fuselages for Aeroplanes and other Aircraft.

Info

Publication number
GB126514A
GB126514A GB9814/18A GB981418A GB126514A GB 126514 A GB126514 A GB 126514A GB 9814/18 A GB9814/18 A GB 9814/18A GB 981418 A GB981418 A GB 981418A GB 126514 A GB126514 A GB 126514A
Authority
GB
United Kingdom
Prior art keywords
aircraft
fitted
braces
diagonal
aeroplanes
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
GB9814/18A
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.)
HENRY PHILLIP FOLLAND
Nieuport & General Aircraft Co
Original Assignee
HENRY PHILLIP FOLLAND
Nieuport & General Aircraft Co
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 HENRY PHILLIP FOLLAND, Nieuport & General Aircraft Co filed Critical HENRY PHILLIP FOLLAND
Priority to GB9814/18A priority Critical patent/GB126514A/en
Publication of GB126514A publication Critical patent/GB126514A/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
    • B64C1/061—Frames
    • 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
    • B64C2001/0063—Fuselage structures substantially made from particular materials from wood

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Rod-Shaped Construction Members (AREA)

Abstract

126,514. Nieuport & General Aircraft Co., and Folland, H. P. June 14,1918. Cars and cabins; framework.-The fuselage of an aircraft is constructed with longitudinal members a arranged one at each corner of the crosssection, connected together by braces a<1>, a<2>, jointed to them by the use of gusset-pieces b pegged and glued in place, and stiffened by chocks d, d'. Diagonal braces e may also be fitted. Between the main frames, light bars may be fitted to support the wooden sheathing, which is formed by longitudinal or diagonal planking, nailed or wired on. The whole may then be covered with fabric fixed on with the threads running obliquely.
GB9814/18A 1918-06-14 1918-06-14 Improvements in Bodies or Fuselages for Aeroplanes and other Aircraft. Expired GB126514A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB9814/18A GB126514A (en) 1918-06-14 1918-06-14 Improvements in Bodies or Fuselages for Aeroplanes and other Aircraft.

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB9814/18A GB126514A (en) 1918-06-14 1918-06-14 Improvements in Bodies or Fuselages for Aeroplanes and other Aircraft.

Publications (1)

Publication Number Publication Date
GB126514A true GB126514A (en) 1919-05-15

Family

ID=32670943

Family Applications (1)

Application Number Title Priority Date Filing Date
GB9814/18A Expired GB126514A (en) 1918-06-14 1918-06-14 Improvements in Bodies or Fuselages for Aeroplanes and other Aircraft.

Country Status (1)

Country Link
GB (1) GB126514A (en)

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