GB191322493A - Improvements in or relating to the Construction of Aeroplanes. - Google Patents

Improvements in or relating to the Construction of Aeroplanes.

Info

Publication number
GB191322493A
GB191322493A GB191322493DA GB191322493A GB 191322493 A GB191322493 A GB 191322493A GB 191322493D A GB191322493D A GB 191322493DA GB 191322493 A GB191322493 A GB 191322493A
Authority
GB
United Kingdom
Prior art keywords
case
construction
struts
wing
strut
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
Inventor
Frederick Michael Green
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
Application granted granted Critical
Publication of GB191322493A publication Critical patent/GB191322493A/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

Abstract

22,493. Green, r. M. Oct. 6. P l a n e s, arrangement and construction of.-The longitudinal spars D, E of the wing B of an aeroplane are connected by a single series of struts K to a lower wing C in the case of a biplane, and to a laterally-extending girder in the case of a monoplane. The struts are preferably I-shaped, and capable of bending fore-and-aft in order that the load on the lower wing may be transferred to the upper plane in case the centre of pressure of the lower plane is not coincident with the axis of the strut. A similar strut H connects the wings to the body A. Brace wires L, M, N are arranged as shown.
GB191322493D 1913-10-06 1913-10-06 Improvements in or relating to the Construction of Aeroplanes. Expired GB191322493A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB191322493T 1913-10-06

Publications (1)

Publication Number Publication Date
GB191322493A true GB191322493A (en) 1914-07-09

Family

ID=34360188

Family Applications (1)

Application Number Title Priority Date Filing Date
GB191322493D Expired GB191322493A (en) 1913-10-06 1913-10-06 Improvements in or relating to the Construction of Aeroplanes.

Country Status (1)

Country Link
GB (1) GB191322493A (en)

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