GB191218675A - Improvements in Automatic Stabilising Apparatus for Aeroplanes. - Google Patents

Improvements in Automatic Stabilising Apparatus for Aeroplanes.

Info

Publication number
GB191218675A
GB191218675A GB191218675DA GB191218675A GB 191218675 A GB191218675 A GB 191218675A GB 191218675D A GB191218675D A GB 191218675DA GB 191218675 A GB191218675 A GB 191218675A
Authority
GB
United Kingdom
Prior art keywords
lever
servomotor
machine
pivoted
slide valve
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
Louis Adolphe Hayot
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 GB191218675A publication Critical patent/GB191218675A/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

Abstract

18,675. Hayot, L. A. Sept. 18, 1911, [Convention date]. Balancing automatically. The longitudinal balance of an aeroplane is maintained by a steering-plane controlled through a servomotor by a weighted bell-crank lever L<1>, L<2> pivoted about a transverse axis a to the frame of the machine, The lever is connected to the slide valve of the servomotor by the rod b. Springs R, r maintain the lever in or return it to the normal position in which the arm L<1> is vertical. Owing to its inertia, the lever lags during accelerations and angular oscillations about a transverse axis of the machine and operates the slide valve of the servomotor. For lateral balance, the controlling-device comprises a vertical weighted lever such as the lever L<1> pivoted about an axis longitudinal of the machine.
GB191218675D 1911-09-18 1912-08-14 Improvements in Automatic Stabilising Apparatus for Aeroplanes. Expired GB191218675A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR191218675X 1911-09-18

Publications (1)

Publication Number Publication Date
GB191218675A true GB191218675A (en) 1912-11-28

Family

ID=32606777

Family Applications (1)

Application Number Title Priority Date Filing Date
GB191218675D Expired GB191218675A (en) 1911-09-18 1912-08-14 Improvements in Automatic Stabilising Apparatus for Aeroplanes.

Country Status (1)

Country Link
GB (1) GB191218675A (en)

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