GB128040A - Improvements in or relating to Stabilisers for Aeroplanes. - Google Patents

Improvements in or relating to Stabilisers for Aeroplanes.

Info

Publication number
GB128040A
GB128040A GB11403/18A GB1140318A GB128040A GB 128040 A GB128040 A GB 128040A GB 11403/18 A GB11403/18 A GB 11403/18A GB 1140318 A GB1140318 A GB 1140318A GB 128040 A GB128040 A GB 128040A
Authority
GB
United Kingdom
Prior art keywords
lever
control
cables
taplin
vanes
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
GB11403/18A
Inventor
Thomas James Taplin
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 GB11403/18A priority Critical patent/GB128040A/en
Publication of GB128040A publication Critical patent/GB128040A/en
Expired legal-status Critical Current

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C17/00—Aircraft stabilisation not otherwise provided for

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Toys (AREA)

Abstract

128,040. Taplin, T. J., and Taplin, T. J. July 11, 1918. Balancing automatically. The elevator and ailerons of an aeroplane are controlled by a universally mounted lever having crossed wind-vanes at its upper end and adjustable springs at its lower end so that the lever is kept normally vertical. The Figure shows a lever A having vanes at its upper end in longitudinal and transverse vertical planes. The lower end of the lever below the universal joint B is connected to springs E, E<1>, F, F<1>, the tension of which can be adjusted by turning drums E<3>, F<2>, F<3>. The spring E<1> may be dispensed with and a stop provided to limit the longitudinal swing of the lever. The control cables may be connected to the pilot's control lever, or separate connexions may be provided in which case the control cables from the lever A may be passed around movable jockey pulleys so that these cables can be slackened, when the pilot desires to resume hand control.
GB11403/18A 1918-07-11 1918-07-11 Improvements in or relating to Stabilisers for Aeroplanes. Expired GB128040A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB11403/18A GB128040A (en) 1918-07-11 1918-07-11 Improvements in or relating to Stabilisers for Aeroplanes.

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB11403/18A GB128040A (en) 1918-07-11 1918-07-11 Improvements in or relating to Stabilisers for Aeroplanes.

Publications (1)

Publication Number Publication Date
GB128040A true GB128040A (en) 1919-06-19

Family

ID=32344992

Family Applications (1)

Application Number Title Priority Date Filing Date
GB11403/18A Expired GB128040A (en) 1918-07-11 1918-07-11 Improvements in or relating to Stabilisers for Aeroplanes.

Country Status (1)

Country Link
GB (1) GB128040A (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN108109465A (en) * 2017-12-29 2018-06-01 天津华翼蓝天科技股份有限公司 A kind of emulation rudder trim knob assembly of flight simulator

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN108109465A (en) * 2017-12-29 2018-06-01 天津华翼蓝天科技股份有限公司 A kind of emulation rudder trim knob assembly of flight simulator

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