GB191022220A - Improvements in Aeroplanes. - Google Patents

Improvements in Aeroplanes.

Info

Publication number
GB191022220A
GB191022220A GB191022220DA GB191022220A GB 191022220 A GB191022220 A GB 191022220A GB 191022220D A GB191022220D A GB 191022220DA GB 191022220 A GB191022220 A GB 191022220A
Authority
GB
United Kingdom
Prior art keywords
ailerons
elevator
pinions
pinion
gear
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
Henry Farman
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 GB191022220A publication Critical patent/GB191022220A/en
Expired legal-status Critical Current

Links

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C13/00Control systems or transmitting systems for actuating flying-control surfaces, lift-increasing flaps, air brakes, or spoilers

Abstract

22,220. Farman, H. Jan. 8, [Convention date]. Steering.-Ailerons D, Fig. 1, are hinged to the tail C of a biplane or monoplane flying- machine, and are adapted to be adjusted simultaneously with or independently of the front elevator B. The hand-lever a carries a pinion c, Fig. 3, adapted to slide on a feather on the spindle b. The pinion c can thus be placed in gear with both pinions d, e to adjust the ailerons D and elevator B in opposite senses, or in gear with either of the pinions i, h to adjust the elevator or ailerons separately.
GB191022220D 1910-01-08 1910-09-24 Improvements in Aeroplanes. Expired GB191022220A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR191022220X 1910-01-08

Publications (1)

Publication Number Publication Date
GB191022220A true GB191022220A (en) 1910-11-24

Family

ID=32480773

Family Applications (1)

Application Number Title Priority Date Filing Date
GB191022220D Expired GB191022220A (en) 1910-01-08 1910-09-24 Improvements in Aeroplanes.

Country Status (1)

Country Link
GB (1) GB191022220A (en)

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