GB217974A - Improvements in or relating to controlling devices for aeroplanes - Google Patents

Improvements in or relating to controlling devices for aeroplanes

Info

Publication number
GB217974A
GB217974A GB8091/23A GB809123A GB217974A GB 217974 A GB217974 A GB 217974A GB 8091/23 A GB8091/23 A GB 8091/23A GB 809123 A GB809123 A GB 809123A GB 217974 A GB217974 A GB 217974A
Authority
GB
United Kingdom
Prior art keywords
flaps
ailerons
hand
control cables
parts
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
GB8091/23A
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.)
Fairey Aviation Co Ltd
Original Assignee
Fairey Aviation Co Ltd
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 Fairey Aviation Co Ltd filed Critical Fairey Aviation Co Ltd
Priority to GB8091/23A priority Critical patent/GB217974A/en
Publication of GB217974A publication Critical patent/GB217974A/en
Expired legal-status Critical Current

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C3/00—Wings
    • B64C3/38—Adjustment of complete wings or parts thereof
    • B64C3/52—Warping

Abstract

217,974. Fairey Aviation Co., Ltd., and Fairey, C. R. March 21, 1923.. Balancing and regulating altitude.-In an aeroplane having the trailing marginal portions of each half plane divided into two parts, the inner parts or flaps are connected by control cables to elements which can be set at various distances apart by screw mechanisms to enable the flaps to be moved simultaneously in the same direction, and the control cables from the outer parts or ailerons are passed over stationary guide pulleys to a manually-operated drum to enable the ailerons to be moved in opposite directions, the two controls being independent of one another. The Figure shows an arrangement similar to that described in Specification 135,520 in which the upper plane of a biplane has two ailerons B', B<2> and two flaps C<1>, C<2>, the flaps being connected bv wires or struts to flaps E', E<2> on the lower plane. The control cables for the flaps are connected to nuts K<1>, K<2> on a shaft F having a right and left-hand screw adapted to be turned by a hand-wheel J. The cables from the ailerons B<1>, B<2> are passed over stationary pulleys l<3>, l<4>, l<3*>, l<4*>, to a drum L turned by a hand-wheel N.
GB8091/23A 1923-03-21 1923-03-21 Improvements in or relating to controlling devices for aeroplanes Expired GB217974A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB8091/23A GB217974A (en) 1923-03-21 1923-03-21 Improvements in or relating to controlling devices for aeroplanes

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB8091/23A GB217974A (en) 1923-03-21 1923-03-21 Improvements in or relating to controlling devices for aeroplanes

Publications (1)

Publication Number Publication Date
GB217974A true GB217974A (en) 1924-06-23

Family

ID=9845575

Family Applications (1)

Application Number Title Priority Date Filing Date
GB8091/23A Expired GB217974A (en) 1923-03-21 1923-03-21 Improvements in or relating to controlling devices for aeroplanes

Country Status (1)

Country Link
GB (1) GB217974A (en)

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