GB190921384A - Improvements in Horizontal Rudders for Aeroplanes. - Google Patents

Improvements in Horizontal Rudders for Aeroplanes.

Info

Publication number
GB190921384A
GB190921384A GB190921384DA GB190921384A GB 190921384 A GB190921384 A GB 190921384A GB 190921384D A GB190921384D A GB 190921384DA GB 190921384 A GB190921384 A GB 190921384A
Authority
GB
United Kingdom
Prior art keywords
planes
frame
adjustable
rear end
aeroplanes
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
Wilhelm Pega
Karl Emich
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 GB190921384A publication Critical patent/GB190921384A/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

Abstract

21,384. Pega, W., and Emich, K. Sept. 18. Steering.-An elevator for an aeroplane machine comprises a series of superposed vanes a of upwardly increasing lengths, the forward end being pivoted at b to an inclined part of the frame, and the rear end being connected to a vertical rod c adjustable by a hand-lever d. When the rear end of the planes a is raised, each plane moves through a greater angle than the plane immediately below it, so that the perpendicular distance between the front of the planes becomes increased, whereby the planes are caused to converge towards the rear. In a modification, the rear of the planes is hinged to a fixed part of the frame, and the front of the planes is connected to an inclined adjustable rod. Planes, construction of.-The planes are constructed with a straight front edge, and an arched widened rear edge.
GB190921384D 1909-09-18 1909-09-18 Improvements in Horizontal Rudders for Aeroplanes. Expired GB190921384A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB190921384T 1909-09-18

Publications (1)

Publication Number Publication Date
GB190921384A true GB190921384A (en) 1910-03-31

Family

ID=32557533

Family Applications (1)

Application Number Title Priority Date Filing Date
GB190921384D Expired GB190921384A (en) 1909-09-18 1909-09-18 Improvements in Horizontal Rudders for Aeroplanes.

Country Status (1)

Country Link
GB (1) GB190921384A (en)

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