GB226871A - Improvements in or connected with the control mechanism of aircraft - Google Patents

Improvements in or connected with the control mechanism of aircraft

Info

Publication number
GB226871A
GB226871A GB24063/23A GB2406323A GB226871A GB 226871 A GB226871 A GB 226871A GB 24063/23 A GB24063/23 A GB 24063/23A GB 2406323 A GB2406323 A GB 2406323A GB 226871 A GB226871 A GB 226871A
Authority
GB
United Kingdom
Prior art keywords
spindle
ailerons
wing flaps
lever
aircraft
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
GB24063/23A
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 GB24063/23A priority Critical patent/GB226871A/en
Publication of GB226871A publication Critical patent/GB226871A/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)
  • Toys (AREA)

Abstract

226,871. Bolas, H., and Parnall, G. G. Sept. 27, 1923. Steering and balancing. - In aircraft having ailerons to control lateral balance and wing flaps which may be additional to or identified with the ailerons for varying the camber of the main planes, the aileron control cables or rods are connected to levers 14<a> on the ends of hollow transverse shafts 14 substantially wholly enclosed within a hollow casing 15 which can be rotated about bearings at its ends by means of a lever 19 to actuate the wing flaps. The ailerons in the apparatus shown act also as wing flaps and are movable in the same or opposite directions on the two sides of the machine. The inner ends of the shafts 14 have bevel wheels 12, 13 geared to a bevel wheel 11 on a spindle 10 in a central housing 6. The spindle carries a plate 9 engaged by rollers on a two armed lever mounted on a second spindle supported by brackets on the central housing 6, the pilot's control lever being mounted on the end of this second spindle.
GB24063/23A 1923-09-27 1923-09-27 Improvements in or connected with the control mechanism of aircraft Expired GB226871A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB24063/23A GB226871A (en) 1923-09-27 1923-09-27 Improvements in or connected with the control mechanism of aircraft

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB24063/23A GB226871A (en) 1923-09-27 1923-09-27 Improvements in or connected with the control mechanism of aircraft

Publications (1)

Publication Number Publication Date
GB226871A true GB226871A (en) 1924-12-29

Family

ID=10205768

Family Applications (1)

Application Number Title Priority Date Filing Date
GB24063/23A Expired GB226871A (en) 1923-09-27 1923-09-27 Improvements in or connected with the control mechanism of aircraft

Country Status (1)

Country Link
GB (1) GB226871A (en)

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