GB124482A - Improvements in or relating to the Control Members of Aircraft. - Google Patents

Improvements in or relating to the Control Members of Aircraft.

Info

Publication number
GB124482A
GB124482A GB1122/16A GB112216A GB124482A GB 124482 A GB124482 A GB 124482A GB 1122/16 A GB1122/16 A GB 1122/16A GB 112216 A GB112216 A GB 112216A GB 124482 A GB124482 A GB 124482A
Authority
GB
United Kingdom
Prior art keywords
planes
control
balancing
lever
fuselage
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
GB1122/16A
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.)
Vickers Ltd
Original Assignee
Vickers 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 Vickers Ltd filed Critical Vickers Ltd
Priority to GB1122/16A priority Critical patent/GB124482A/en
Publication of GB124482A publication Critical patent/GB124482A/en
Expired legal-status Critical Current

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C1/00—Fuselages; Constructional features common to fuselages, wings, stabilising surfaces or the like
    • 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

124,482. Vickers, Ltd., and Pierson, R. K. Jan. 24, 1916. Steering and balancing.-The control planes of aeroplanes are connected to separate balancing-surfaces in such a manner that the pull on the controls due to air pressure on the balancing-surfaces counterbalances wholly or in part that due to the pressure on the control planes. Fig. 3 shows a machine having mounted at each side of the fuselage, on the ends of a shaft h which actuates the elevator, a lever d' carrying a plane c<1>. A similar plane c<2> carried by a lever d<2> is connected either to the rudder bar, as shown below the fuselage, or by means of a spindle k and lever m to the control wires l of the rudder as shown above the fuselage. Ailerons may be similarly balanced in a biplane by a plane carried on a lever pivoted to one of the struts and connected at its rear end to the control wire connecting the ailerons on the upper and lower planes. The balancing-planes may be weighted to balance the control planes statically as well as aerodynamically, and may be changed for others of different size or their leverage altered to effect adjustment. They may also be arranged in different planes to their corresponding control members. Reference has been directed by the Comptroller to Specification 14577/15.
GB1122/16A 1916-01-24 1916-01-24 Improvements in or relating to the Control Members of Aircraft. Expired GB124482A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB1122/16A GB124482A (en) 1916-01-24 1916-01-24 Improvements in or relating to the Control Members of Aircraft.

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB1122/16A GB124482A (en) 1916-01-24 1916-01-24 Improvements in or relating to the Control Members of Aircraft.

Publications (1)

Publication Number Publication Date
GB124482A true GB124482A (en) 1919-04-03

Family

ID=32340447

Family Applications (1)

Application Number Title Priority Date Filing Date
GB1122/16A Expired GB124482A (en) 1916-01-24 1916-01-24 Improvements in or relating to the Control Members of Aircraft.

Country Status (1)

Country Link
GB (1) GB124482A (en)

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