GB106485A - Improvements in or relating to the Construction of Aeroplane Fuselages. - Google Patents

Improvements in or relating to the Construction of Aeroplane Fuselages.

Info

Publication number
GB106485A
GB106485A GB5994/17A GB599417A GB106485A GB 106485 A GB106485 A GB 106485A GB 5994/17 A GB5994/17 A GB 5994/17A GB 599417 A GB599417 A GB 599417A GB 106485 A GB106485 A GB 106485A
Authority
GB
United Kingdom
Prior art keywords
frames
secured
plywood
members
bent
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
GB5994/17A
Inventor
Jules Vedrines
Louis Leon Astoux
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
Publication of GB106485A publication Critical patent/GB106485A/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
    • B64C1/06—Frames; Stringers; Longerons ; Fuselage sections
    • B64C1/08—Geodetic or other open-frame structures
    • 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)
  • Tents Or Canopies (AREA)

Abstract

106,485. Vedrines, J., and Astoux, L. L. May 16, 1916, [Convention date]. Framework.-An aeroplane fuselage has a rear part built around two plywood frames crossed at a right-angle or other angle, and a front part formed of four longitudinal members braced together, bent, and secured to the vertical frame of the rear part. Fig. 1 shows two open frames 1 and 2 each slotted longitudinally to enable a crossed joint to be formed which is strengthened by brackets 7. Frames 8, Fig. 4, also of plywood and conforming to the outer shape of the fuselage, are secured to the frames 1, 2 and are notched at 0 to receive flexible longitudinal battens to support the fabric covering. The frames 2, 1 are integral with the fixed stabilizing- plane and vertical fin respectively. The front part consists of four members 10 bent at their rear ends and secured to the frame 1. Plywood frames 11 similar to the frames 8 are secured to the members 10. Fabric may be used between adjacent layers of wood in the various frames.
GB5994/17A 1916-05-01 1917-04-27 Improvements in or relating to the Construction of Aeroplane Fuselages. Expired GB106485A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR106485X 1916-05-01

Publications (1)

Publication Number Publication Date
GB106485A true GB106485A (en) 1918-01-24

Family

ID=32241902

Family Applications (1)

Application Number Title Priority Date Filing Date
GB5994/17A Expired GB106485A (en) 1916-05-01 1917-04-27 Improvements in or relating to the Construction of Aeroplane Fuselages.

Country Status (1)

Country Link
GB (1) GB106485A (en)

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