GB130428A - Improvements in or relating to the Wings of Aeroplane Flying Machines. - Google Patents

Improvements in or relating to the Wings of Aeroplane Flying Machines.

Info

Publication number
GB130428A
GB130428A GB317518A GB317518A GB130428A GB 130428 A GB130428 A GB 130428A GB 317518 A GB317518 A GB 317518A GB 317518 A GB317518 A GB 317518A GB 130428 A GB130428 A GB 130428A
Authority
GB
United Kingdom
Prior art keywords
wires
cross
wings
spars
relating
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
GB317518A
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.)
Boulton and Paul Ltd
Original Assignee
Boulton and Paul Ltd
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 Boulton and Paul Ltd filed Critical Boulton and Paul Ltd
Priority to GB317518A priority Critical patent/GB130428A/en
Publication of GB130428A publication Critical patent/GB130428A/en
Expired legal-status Critical Current

Links

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C3/00Wings
    • B64C3/18Spars; Ribs; Stringers

Abstract

130,428. Boulton & Paul, and North, J. D. Feb. 22, 1918. Planes, construction of, and connecting together. -The internal and external bracing-wires and struts of the wings of aeroplanes are connected to a cross-member extending between the spars, whereby the spars are not materially weakened by the connexions, and these connexions are located within the aerofoil section so as to reduce the headresistance. The cross-member 1 passes through the front and rear wing spars 2 and may be secured by collars 4. Lugs 7. 13 for the attachment of the external bracing-wires 6, the incidence wires 15, and the interplane struts 12 are provided on collars 8, 14, which may be secured to the cross-member 1 by pins. A plate 9 bolted at 10 to the spar has lugs for the internal bracing-wires. This plate may be formed as a flange of the collar 8. The cross-member 1 may also serve as a drift strut.
GB317518A 1918-02-22 1918-02-22 Improvements in or relating to the Wings of Aeroplane Flying Machines. Expired GB130428A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB317518A GB130428A (en) 1918-02-22 1918-02-22 Improvements in or relating to the Wings of Aeroplane Flying Machines.

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB317518A GB130428A (en) 1918-02-22 1918-02-22 Improvements in or relating to the Wings of Aeroplane Flying Machines.

Publications (1)

Publication Number Publication Date
GB130428A true GB130428A (en) 1919-08-07

Family

ID=32341287

Family Applications (1)

Application Number Title Priority Date Filing Date
GB317518A Expired GB130428A (en) 1918-02-22 1918-02-22 Improvements in or relating to the Wings of Aeroplane Flying Machines.

Country Status (1)

Country Link
GB (1) GB130428A (en)

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