GB420146A - Improvements in and relating to aircraft - Google Patents

Improvements in and relating to aircraft

Info

Publication number
GB420146A
GB420146A GB5415/33A GB541533A GB420146A GB 420146 A GB420146 A GB 420146A GB 5415/33 A GB5415/33 A GB 5415/33A GB 541533 A GB541533 A GB 541533A GB 420146 A GB420146 A GB 420146A
Authority
GB
United Kingdom
Prior art keywords
aircraft
strengthening
secured
sections
flanges
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
GB5415/33A
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.)
GEOFFREY EMBLETON WALKER
Original Assignee
GEOFFREY EMBLETON WALKER
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 GEOFFREY EMBLETON WALKER filed Critical GEOFFREY EMBLETON WALKER
Priority to GB5415/33A priority Critical patent/GB420146A/en
Publication of GB420146A publication Critical patent/GB420146A/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

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Pressure Welding/Diffusion-Bonding (AREA)

Abstract

420,146. Aircraft fuselages. WALKER, G. E., 65, Rockley Road, Sheffield. Feb. 22, 1933, No. 5415. [Class 4] In an aircraft fuselage which is built up externally of flanged metal pressings or stampings 1 adapted to meet in horizontal and vertical planes and to be secured at their flanges by riveting, bolting, or welding with strengthening-members interposed between and secured to the sections, the strengthening-members at requisite parts of the aircraft are formed as diaphragms 3 bridging the space of the hollow structure to form deckings, floorings, roofings, or mountings for the engines, fuel tanks, or other fittings to be accommodated in the aircraft. The flanges facilitate the attachment of bracing wires &c. and are disposed in the direction of flight and the sections may be corrugated. As shown, a keel 10 is provided in the cockpit.
GB5415/33A 1933-02-22 1933-02-22 Improvements in and relating to aircraft Expired GB420146A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB5415/33A GB420146A (en) 1933-02-22 1933-02-22 Improvements in and relating to aircraft

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB5415/33A GB420146A (en) 1933-02-22 1933-02-22 Improvements in and relating to aircraft

Publications (1)

Publication Number Publication Date
GB420146A true GB420146A (en) 1934-11-22

Family

ID=9795741

Family Applications (1)

Application Number Title Priority Date Filing Date
GB5415/33A Expired GB420146A (en) 1933-02-22 1933-02-22 Improvements in and relating to aircraft

Country Status (1)

Country Link
GB (1) GB420146A (en)

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