GB129681A - Improvements in Controlling Gear for Aeroplanes. - Google Patents

Improvements in Controlling Gear for Aeroplanes.

Info

Publication number
GB129681A
GB129681A GB17326/17A GB1732617A GB129681A GB 129681 A GB129681 A GB 129681A GB 17326/17 A GB17326/17 A GB 17326/17A GB 1732617 A GB1732617 A GB 1732617A GB 129681 A GB129681 A GB 129681A
Authority
GB
United Kingdom
Prior art keywords
lever
aeroplanes
operating
turned down
controlling gear
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
GB17326/17A
Inventor
Emile Letord
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
Publication of GB129681A publication Critical patent/GB129681A/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
    • B64C13/24—Transmitting means

Abstract

129,681. Letord, E. Aug. 12, 1916, [Convention date]. Steering and balancing.-In a dual control gear for aeroplanes, the rear control lever is constructed so that it may be turned down out of the way when not in use, in order to allow free movement of the second pilot for operating a gun &c. Control levers 1, 2 are movable about pivots o, o<1> for operating the elevators, and are fit. ted with hand-wheels A, B controlling cables 7 leading to the ailerons. The rear lever 2 is jointed at 6 so that it may be turned down into a fixed spring .socket. When the lever 2 is required for use, the joint 6 is covered by a sleeve 9. The lever 2 is connected to its pivot o<1> by an arm a<1>.
GB17326/17A 1916-08-12 1917-11-23 Improvements in Controlling Gear for Aeroplanes. Expired GB129681A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR129681X 1916-08-12

Publications (1)

Publication Number Publication Date
GB129681A true GB129681A (en) 1919-07-24

Family

ID=32339464

Family Applications (1)

Application Number Title Priority Date Filing Date
GB17326/17A Expired GB129681A (en) 1916-08-12 1917-11-23 Improvements in Controlling Gear for Aeroplanes.

Country Status (1)

Country Link
GB (1) GB129681A (en)

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