GB191314233A - Improvements in Aeroplanes of the Biplane Type. - Google Patents

Improvements in Aeroplanes of the Biplane Type.

Info

Publication number
GB191314233A
GB191314233A GB191314233DA GB191314233A GB 191314233 A GB191314233 A GB 191314233A GB 191314233D A GB191314233D A GB 191314233DA GB 191314233 A GB191314233 A GB 191314233A
Authority
GB
United Kingdom
Prior art keywords
plane
tail
fuselage
extensions
pair
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
George Holt Thomas
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 GB191314233A publication Critical patent/GB191314233A/en
Expired legal-status Critical Current

Links

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C39/00Aircraft not otherwise provided for
    • B64C39/08Aircraft not otherwise provided for having multiple wings

Abstract

14,233. Thomas, G. H. June 19. Aerial machines without aerostats ;planes, arrangement and construction of; cars; propelling.-In an aeroplane of the biplane type, the upper plane a extends laterally beyond the lower plane, and the extensions are arranged so that they may be swung forwards and folded down in order to lessen the width of the machine for transport. The rear tail plane s is carried by a s t r u c t u r e comprising upper and lower V-shaped frames u<1>, v<1>, secured together by uprights y and braces. The fusilage k is mounted directly on the lower plane b and provided at its forward end with seats m, n. The enginep and propeller r are mounted at the rear of the fuselage. Steering.-The extensions of the main plane a and the tail plane s are provided with pivoted flaps controlled by the aviator for balancing the machine laterally. A rudder z<1> is mounted at the rear of the tail frame. Aerial machines adapted to travel also on land.- The landing chassis consists of a pair of skids d', each attached to the lower plane by struts d<2>, and provided with a pair of resiliently mounted wheels d<3>. A tail skid z<4> is provided. Wind-deflecting screens, arrangement of.-A windscreen c<1> is placed at the forward extremity of the fuselage k.
GB191314233D 1913-06-19 1913-06-19 Improvements in Aeroplanes of the Biplane Type. Expired GB191314233A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB191314233T 1913-06-19

Publications (1)

Publication Number Publication Date
GB191314233A true GB191314233A (en) 1913-12-18

Family

ID=32645172

Family Applications (1)

Application Number Title Priority Date Filing Date
GB191314233D Expired GB191314233A (en) 1913-06-19 1913-06-19 Improvements in Aeroplanes of the Biplane Type.

Country Status (1)

Country Link
GB (1) GB191314233A (en)

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