GB191020125A - Improvements in Aeroplanes. - Google Patents

Improvements in Aeroplanes.

Info

Publication number
GB191020125A
GB191020125A GB191020125DA GB191020125A GB 191020125 A GB191020125 A GB 191020125A GB 191020125D A GB191020125D A GB 191020125DA GB 191020125 A GB191020125 A GB 191020125A
Authority
GB
United Kingdom
Prior art keywords
tail
planes
rudder
steering
hinged
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 - Lifetime
Application number
Inventor
Waldemar Schaef Arthur
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 of GB191020125A publication Critical patent/GB191020125A/en
Application filed by Individual filed Critical Individual
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C23/00—Influencing air flow over aircraft surfaces, not otherwise provided for
    • B64C23/005—Influencing air flow over aircraft surfaces, not otherwise provided for by other means not covered by groups B64C23/02 - B64C23/08, e.g. by electric charges, magnetic panels, piezoelectric elements, static charges or ultrasounds

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Motorcycle And Bicycle Frame (AREA)

Abstract

20,125. Schaef, A. W. Aug. 30, 1909, [Convention date]. Void. [Published under Section 91 of the Act.] Aerial machines without aerostats ; planes, arrangement of.-The aerial machine is provided with main and tail planes 2, 23 mounted on a longitudinal frame 1, which may be covered with canvas. The tail is arranged below the level of the main plane. A screw propeller 3 is arranged at the front of the machine. Steering.-Elevating-planes 5, hinged at the forward end, are arranged at each side of the frame 1 below the main plane 2, and are moved together by cords passing around a hand-wheel 7. The rudder 24 is hinged at its rear end 25 above the fixed tail 23, and is controlled by cords attached to the front end and passing around a hand-wheel 26. The side of the tail plane to which the rudder is turned is depressed and the other raised in order to assist the steering.
GB191020125D 1909-08-30 1910-08-29 Improvements in Aeroplanes. Expired - Lifetime GB191020125A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
NZ191020125X 1909-08-30

Publications (1)

Publication Number Publication Date
GB191020125A true GB191020125A (en)

Family

ID=32501641

Family Applications (1)

Application Number Title Priority Date Filing Date
GB191020125D Expired - Lifetime GB191020125A (en) 1909-08-30 1910-08-29 Improvements in Aeroplanes.

Country Status (1)

Country Link
GB (1) GB191020125A (en)

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