GB130141A - Improvements in or relating to Controls for Aeroplanes and the like. - Google Patents

Improvements in or relating to Controls for Aeroplanes and the like.

Info

Publication number
GB130141A
GB130141A GB12017/18A GB1201718A GB130141A GB 130141 A GB130141 A GB 130141A GB 12017/18 A GB12017/18 A GB 12017/18A GB 1201718 A GB1201718 A GB 1201718A GB 130141 A GB130141 A GB 130141A
Authority
GB
United Kingdom
Prior art keywords
shaft
quadrants
control
ailerons
stick
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
GB12017/18A
Inventor
Wilfrid Thomas Reid
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 GB12017/18A priority Critical patent/GB130141A/en
Publication of GB130141A publication Critical patent/GB130141A/en
Expired legal-status Critical Current

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C13/00—Control systems or transmitting systems for actuating flying-control surfaces, lift-increasing flaps, air brakes, or spoilers

Abstract

130,141. Reid, W. T. July 23, 1918. Steering and balancing.-A control-stick D, which swings fore and aft to operate the elevators and has a hand-wheel D<1> for operating the ailerons of an aeroplane, has the hand-wheel connected by cords E, E<1> to grooved quadrants A<1>, A<2> mounted upon a transverse shaft A which operates the ailerons, the peripheries of the quadrants intersecting the pivotal axis of the controlstick D. One of the quadrants is fixed to the shaft A and the other is loose, and a second cord E<3> passing around an idle pulley E<4> connects the two together. A second control may be similarly mounted and connected to the shaft A. The control-stick is connected to a shaft B which operates the elevator preferably by the means described in Specification 130,142.
GB12017/18A 1918-07-23 1918-07-23 Improvements in or relating to Controls for Aeroplanes and the like. Expired GB130141A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB12017/18A GB130141A (en) 1918-07-23 1918-07-23 Improvements in or relating to Controls for Aeroplanes and the like.

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB12017/18A GB130141A (en) 1918-07-23 1918-07-23 Improvements in or relating to Controls for Aeroplanes and the like.

Publications (1)

Publication Number Publication Date
GB130141A true GB130141A (en) 1919-07-23

Family

ID=32345287

Family Applications (1)

Application Number Title Priority Date Filing Date
GB12017/18A Expired GB130141A (en) 1918-07-23 1918-07-23 Improvements in or relating to Controls for Aeroplanes and the like.

Country Status (1)

Country Link
GB (1) GB130141A (en)

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