GB117926A - Improvements in or relating to Aircraft and other Light-weight Apparatus. - Google Patents

Improvements in or relating to Aircraft and other Light-weight Apparatus.

Info

Publication number
GB117926A
GB117926A GB1073617A GB1073617A GB117926A GB 117926 A GB117926 A GB 117926A GB 1073617 A GB1073617 A GB 1073617A GB 1073617 A GB1073617 A GB 1073617A GB 117926 A GB117926 A GB 117926A
Authority
GB
United Kingdom
Prior art keywords
members
tubes
tube
aircraft
shows
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
GB1073617A
Inventor
Sydney Crowe
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 GB1073617A priority Critical patent/GB117926A/en
Publication of GB117926A publication Critical patent/GB117926A/en
Expired legal-status Critical Current

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C3/00—Wings
    • B64C3/18—Spars; Ribs; Stringers
    • B64C3/185—Spars

Abstract

117,926. Crowe, S. July 26, 1917. Framework; planes, construction of.-Spars, girders, struts, &c. for aircraft and other light structures are composed of outer longitudinal members connected together and to one or more intermediate tubular members or cores by series of transverse members. Fig. 1 shows upper and lower channels a connected to a tube b bv transverse members c comprising tubes with splayed ends. The tubes c are passed through holes in the tube b and secured thereto; or the tube b may pass through the tubes c. Fig. 3 shows another form having two tubes b<1>, b<2> connected by short lengths of rectangular tubing g to the members a, which are composed of angle-members with their flanges f placed together. In another form, the transverse members comprise flanged plates set obliquely. Fig. 6 shows a method of jointing together a spar and web by means of plates j. The outer members a may be constituted by a tubular structure surrounding the core b, and the tubes b may be ribbed.
GB1073617A 1917-07-26 1917-07-26 Improvements in or relating to Aircraft and other Light-weight Apparatus. Expired GB117926A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB1073617A GB117926A (en) 1917-07-26 1917-07-26 Improvements in or relating to Aircraft and other Light-weight Apparatus.

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB1073617A GB117926A (en) 1917-07-26 1917-07-26 Improvements in or relating to Aircraft and other Light-weight Apparatus.

Publications (1)

Publication Number Publication Date
GB117926A true GB117926A (en) 1918-07-26

Family

ID=32671495

Family Applications (1)

Application Number Title Priority Date Filing Date
GB1073617A Expired GB117926A (en) 1917-07-26 1917-07-26 Improvements in or relating to Aircraft and other Light-weight Apparatus.

Country Status (1)

Country Link
GB (1) GB117926A (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US8186622B2 (en) 2006-03-27 2012-05-29 Airbus Operations Limited Aircraft component

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US8186622B2 (en) 2006-03-27 2012-05-29 Airbus Operations Limited Aircraft component

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