GB191024697A - Improvements in or relating to Apparatus for Controlling Aeronautical Machines. - Google Patents

Improvements in or relating to Apparatus for Controlling Aeronautical Machines.

Info

Publication number
GB191024697A
GB191024697A GB191024697DA GB191024697A GB 191024697 A GB191024697 A GB 191024697A GB 191024697D A GB191024697D A GB 191024697DA GB 191024697 A GB191024697 A GB 191024697A
Authority
GB
United Kingdom
Prior art keywords
rudder
balancing
pinion
planes
turned
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
Inventor
Thomas Arthur Hughes
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
Application granted granted Critical
Publication of GB191024697A publication Critical patent/GB191024697A/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

Landscapes

  • Engineering & Computer Science (AREA)
  • Automation & Control Theory (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Cage And Drive Apparatuses For Elevators (AREA)

Abstract

24,697. Hughes, T. A. Oct. 24. Steering and balancing.-A differential gear is used in the transmission mechanism for operating lateral balancing-planes and a rudder so that the rudder is actuated whenever the balancing-planes are operated, and the rudder can be operated independently. The outer ring k of the differential gear is connected by a cord m to the rudder. The bevel-wheel a is provided with a pulley around which is passed a cord f connected to the means for operating the balancing - planes. When the pinion a is turned, the outer ring k also rotates and operates the rudder simultaneously with the actuation of the balancing- planes. When the pinion b is turned while the pinion a is fixed, the ring k is turned to actuate the rudder independently of the balancing- planes. In a modified form, the pinion b, Fig. 2, and sleeve d are loosely mounted on a hollow sleeve n, to which the pinion a is secured. A shaft p is connected by a key and keyway to the sleeve n, so that the shaft can slide therethrough to operate an elevator.
GB191024697D 1910-10-24 1910-10-24 Improvements in or relating to Apparatus for Controlling Aeronautical Machines. Expired GB191024697A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB191024697T 1910-10-24

Publications (1)

Publication Number Publication Date
GB191024697A true GB191024697A (en) 1911-08-24

Family

ID=32494151

Family Applications (1)

Application Number Title Priority Date Filing Date
GB191024697D Expired GB191024697A (en) 1910-10-24 1910-10-24 Improvements in or relating to Apparatus for Controlling Aeronautical Machines.

Country Status (1)

Country Link
GB (1) GB191024697A (en)

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