GB120777A - Improvements in or relating to Aeroplanes. - Google Patents

Improvements in or relating to Aeroplanes.

Info

Publication number
GB120777A
GB120777A GB17202/17A GB1720217A GB120777A GB 120777 A GB120777 A GB 120777A GB 17202/17 A GB17202/17 A GB 17202/17A GB 1720217 A GB1720217 A GB 1720217A GB 120777 A GB120777 A GB 120777A
Authority
GB
United Kingdom
Prior art keywords
planes
plane
sectors
engines
centre
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
GB17202/17A
Inventor
Edward Cragg
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 GB17202/17A priority Critical patent/GB120777A/en
Publication of GB120777A publication Critical patent/GB120777A/en
Expired legal-status Critical Current

Links

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C3/00Wings
    • B64C3/38Adjustment of complete wings or parts thereof
    • B64C3/54Varying in area

Abstract

120,777. Cragg, E. Nov. 22, 1917. Planes, construction of; propelling; steering and balancing.-An aeroplane has the centre portions of its planes adjustable in incidence and its tips variable in area, and has two propellers adapted to be coupled in various ways to either or both of two engines. Fig. 4 shows a cross section of a triplane wing in which main spars a, b of tubular metal extend the whole length of the planes and are horizontal for one-third their length in the centre. The central sections k of the planes are pivoted about the front spar a and are linked together by struts l which are connected to arms j on a shaft f pivoted in bearings on the rear inter-plane struts of the fixed portions of the plane. The shaft f has an arm g connected to a screwed spindle h adapted to be moved by turning a hand-wheel i provided with a nut. The spars b act as stops for the centre sections k. Mounted at the ends of each plane are curved rails m, Fig. 6, engaged by eye pieces o on plane sectors n adapted to slide into the sections adjacent to the main planes. Cords q passed over guidepulleys and over a drum r, Fig. 4, enable the seetors n to be expanded and collapsed simultaneously by turning a hand-wheel s. Spring tongues t on the outer edges of the sectors engage holes in the adjacent sectors as they are successively drawn out. The movable plane ends may each be formed in one piece instead of in sectors. Propellers mounted on the planes are driven by gearing from two engines in the fuselage, clutches being arranged between the two engines and adjacent gearing and a clutch being placed between the driving shafts on the two sides of the machine.
GB17202/17A 1917-11-22 1917-11-22 Improvements in or relating to Aeroplanes. Expired GB120777A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB17202/17A GB120777A (en) 1917-11-22 1917-11-22 Improvements in or relating to Aeroplanes.

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB17202/17A GB120777A (en) 1917-11-22 1917-11-22 Improvements in or relating to Aeroplanes.

Publications (1)

Publication Number Publication Date
GB120777A true GB120777A (en) 1918-11-22

Family

ID=32347472

Family Applications (1)

Application Number Title Priority Date Filing Date
GB17202/17A Expired GB120777A (en) 1917-11-22 1917-11-22 Improvements in or relating to Aeroplanes.

Country Status (1)

Country Link
GB (1) GB120777A (en)

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