GB121741A - Airplane Rib Construction. - Google Patents

Airplane Rib Construction.

Info

Publication number
GB121741A
GB121741A GB21291/19A GB2129119A GB121741A GB 121741 A GB121741 A GB 121741A GB 21291/19 A GB21291/19 A GB 21291/19A GB 2129119 A GB2129119 A GB 2129119A GB 121741 A GB121741 A GB 121741A
Authority
GB
United Kingdom
Prior art keywords
longitudinals
rib construction
construction
airplane
airplane rib
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
GB21291/19A
Inventor
John William Rapp
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 GB121741A publication Critical patent/GB121741A/en
Expired legal-status Critical Current

Links

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C3/00Wings
    • B64C3/18Spars; Ribs; Stringers
    • B64C3/187Ribs

Abstract

121,741. Rapp, J. W., (Assignee of Vanorio, J.). Dec. 19, 1917, [Convention date]. Framework. planes, construction of.- Ribs or spars of aerofoils are composed of upper and lower longitudinals 2, 2<a> each formed of metal plate bent into T-section as shown in Fig. 5, the two longitudinals being connected together by diagonal braces 9 having the ends bevelled as shown at 9<b> and spot-welded between the inwardly-extending flanges 7 of the longitudinals. The longitudinals are perforated as shown at 10. Fig. 1 shows a complete rib having the ends of the longitudinals connected to members 3, 3<a>.
GB21291/19A 1917-12-19 1918-12-19 Airplane Rib Construction. Expired GB121741A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US121741XA 1917-12-19 1917-12-19

Publications (1)

Publication Number Publication Date
GB121741A true GB121741A (en) 1920-02-26

Family

ID=32680017

Family Applications (1)

Application Number Title Priority Date Filing Date
GB21291/19A Expired GB121741A (en) 1917-12-19 1918-12-19 Airplane Rib Construction.

Country Status (1)

Country Link
GB (1) GB121741A (en)

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