GB123902A - Improvements in the Construction of Aeroplane Spars, Struts, Longerons, Bearers, and the like. - Google Patents

Improvements in the Construction of Aeroplane Spars, Struts, Longerons, Bearers, and the like.

Info

Publication number
GB123902A
GB123902A GB855318A GB855318A GB123902A GB 123902 A GB123902 A GB 123902A GB 855318 A GB855318 A GB 855318A GB 855318 A GB855318 A GB 855318A GB 123902 A GB123902 A GB 123902A
Authority
GB
United Kingdom
Prior art keywords
longerons
struts
spars
aeroplane
bearers
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
GB855318A
Inventor
Louis Massey
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 GB855318A priority Critical patent/GB123902A/en
Publication of GB123902A publication Critical patent/GB123902A/en
Expired legal-status Critical Current

Links

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C3/00Wings
    • B64C3/18Spars; Ribs; Stringers
    • B64C3/185Spars

Abstract

123,902. Massey, L. May 23, 1918. Framework. - Wooden spars, struts, longerons, &c. for aeroplanes are constructed of webs A, B arranged in cruciform manner and fitted with peripheral filling-in pieces C to give the external shape desired. The web B may comprise two pieces fitting into grooves at oppositesides of the web A. The hollow spaces D are filled in at the ends of the spar and at points where fittings are to be attached. A fairing F of veneer may be added as shown.
GB855318A 1918-05-23 1918-05-23 Improvements in the Construction of Aeroplane Spars, Struts, Longerons, Bearers, and the like. Expired GB123902A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB855318A GB123902A (en) 1918-05-23 1918-05-23 Improvements in the Construction of Aeroplane Spars, Struts, Longerons, Bearers, and the like.

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB855318A GB123902A (en) 1918-05-23 1918-05-23 Improvements in the Construction of Aeroplane Spars, Struts, Longerons, Bearers, and the like.

Publications (1)

Publication Number Publication Date
GB123902A true GB123902A (en) 1919-03-13

Family

ID=32343371

Family Applications (1)

Application Number Title Priority Date Filing Date
GB855318A Expired GB123902A (en) 1918-05-23 1918-05-23 Improvements in the Construction of Aeroplane Spars, Struts, Longerons, Bearers, and the like.

Country Status (1)

Country Link
GB (1) GB123902A (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2834073A (en) * 1953-09-28 1958-05-13 Macgillis & Gibbs Company Fabricated pole

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2834073A (en) * 1953-09-28 1958-05-13 Macgillis & Gibbs Company Fabricated pole

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