GB465131A - Trimming devices for aircraft flying controls - Google Patents

Trimming devices for aircraft flying controls

Info

Publication number
GB465131A
GB465131A GB30206/35A GB3020635A GB465131A GB 465131 A GB465131 A GB 465131A GB 30206/35 A GB30206/35 A GB 30206/35A GB 3020635 A GB3020635 A GB 3020635A GB 465131 A GB465131 A GB 465131A
Authority
GB
United Kingdom
Prior art keywords
drums
pinion
adjustment
spindle
lever
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
GB30206/35A
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.)
REGINALD ARTHUR N FA
GKN Aerospace Services Ltd
Original Assignee
REGINALD ARTHUR N FA
Vickers Aviation 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 REGINALD ARTHUR N FA, Vickers Aviation Ltd filed Critical REGINALD ARTHUR N FA
Priority to GB30206/35A priority Critical patent/GB465131A/en
Publication of GB465131A publication Critical patent/GB465131A/en
Expired legal-status Critical Current

Links

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C13/00Control systems or transmitting systems for actuating flying-control surfaces, lift-increasing flaps, air brakes, or spoilers

Landscapes

  • Engineering & Computer Science (AREA)
  • Automation & Control Theory (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Transmission Devices (AREA)

Abstract

465,131. Controlling aircraft. VICKERS (AVIATION), Ltd., PIERSON, R. K., and FIRMAN, R. A. Nov. 1, 1935, No. 30206. [Class 4] Means for adjusting trimming devices for aircraft flying controls in which small auxiliary surfaces are fitted to a main control surface, comprise a setting lever mounted for adjustment in two different directions, two separate mechanisms, one actuated by adjustment of the setting lever in one direction and the other by adjustment of the lever in the other direction and connections operatively connecting the mechanisms with the respective trimming devices. As shown, a spindle a provided with a knob a<1> is rotatable in a cross-head b integral with trunnions b<1>, b<2> mounted in plates c, c<1>. The crosshead b has arms b<3>, b<4> carrying drums d, d<1>, d<2>, d<3>. The drums d<2>, d<3> are adjusted in opposite directions upon rotation of the knob a' through bevel gearing e, e<1>, e<2>. The drums d, d<1> are adjusted in opposite directions upon fore- and-aft movement of the spindle a by a pinion g engaging a fixed arcuate rack f<1> and a pinion d<5> engaging teeth on the two drums. Each pair of drums d, d<1> and d<2>, d<3> are connected respectively to gear for adjusting the auxiliary surfaces on the rudder and elevator. This gear comprises a lever i<6> which receives at one end a projection on the auxiliary surface and at the other end comprises a nut i<5> which engages a screwed spindle i' connected to drum i<2>, i<3> operated from the drums d, d<1> and d<2>, d<3>. The pinion d<5> may be dispensed with in which case two fixed racks are provided. Movement of the various mechanisms may be limited by limitation of the number of teeth.
GB30206/35A 1935-11-01 1935-11-01 Trimming devices for aircraft flying controls Expired GB465131A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB30206/35A GB465131A (en) 1935-11-01 1935-11-01 Trimming devices for aircraft flying controls

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB30206/35A GB465131A (en) 1935-11-01 1935-11-01 Trimming devices for aircraft flying controls

Publications (1)

Publication Number Publication Date
GB465131A true GB465131A (en) 1937-05-03

Family

ID=10303958

Family Applications (1)

Application Number Title Priority Date Filing Date
GB30206/35A Expired GB465131A (en) 1935-11-01 1935-11-01 Trimming devices for aircraft flying controls

Country Status (1)

Country Link
GB (1) GB465131A (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4418633A (en) * 1980-04-09 1983-12-06 Schottel-Werft, Josef Becker Gmbh & Co. Kg Apparatus for controlling a watercraft

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4418633A (en) * 1980-04-09 1983-12-06 Schottel-Werft, Josef Becker Gmbh & Co. Kg Apparatus for controlling a watercraft

Similar Documents

Publication Publication Date Title
GB465131A (en) Trimming devices for aircraft flying controls
US2582348A (en) Control system for aircraft control surfaces
US2386709A (en) Airplane control mechanism
GB572417A (en) Improvements in helicopters
GB418540A (en) Improvements in or relating to the control surfaces of aircraft
GB519519A (en) Improvements relating to control systems for aeroplanes
DE749541C (en) Aircraft control with ailerons that can be operated independently of the rudder and a device to compensate for the yaw moments around the vertical axis when the ailerons deflect
GB263253A (en) Improvements in or relating to aircraft
DE572758C (en) Airplane for lift and plan flight with separate control surfaces for both types of flight
GB456144A (en) Improvements in and relating to motion transmitting mechanisms particularly for use in the actuation of control surfaces of aeroplanes
US2474813A (en) Gun aiming system
GB351914A (en) Improvements in engines, particularly for aircraft
GB381919A (en) Improvements in or relating to variable pitch propellers
DE668482C (en) Headlight control by listening device and telescope
GB130733A (en) Aeroplane Wing Incidence Control.
GB519532A (en) Improvements relating to operating gear for aircraft controls
DE732920C (en) Rudder balance weight for aircraft, especially for test aircraft
GB486682A (en) Improvements in or relating to control apparatus especially for aircraft
GB221352A (en) Improved means of actuating the control surfaces of aircraft
GB540041A (en) Improvements in transmitting mechanism for aircraft control surfaces
GB588147A (en) Improvements in seats
GB468602A (en) Improvements in and relating to variable pitch air-screws
GB291950A (en) Improvements in or connected with control mechanism for aircraft
GB419687A (en) Improvements in or relating to the controlling mechanism of aeroplanes
GB545449A (en) Improvements in irreversible gearing for controls