GB191102215A - Improvements in Aeroplane Flying Machines. - Google Patents

Improvements in Aeroplane Flying Machines.

Info

Publication number
GB191102215A
GB191102215A GB191102215DA GB191102215A GB 191102215 A GB191102215 A GB 191102215A GB 191102215D A GB191102215D A GB 191102215DA GB 191102215 A GB191102215 A GB 191102215A
Authority
GB
United Kingdom
Prior art keywords
plane
adjusted
transverse axis
uniform width
width
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 Theinert
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 GB191102215A publication Critical patent/GB191102215A/en
Expired legal-status Critical Current

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C3/00—Wings
    • B64C3/38—Adjustment of complete wings or parts thereof
    • B64C3/385—Variable incidence wings

Landscapes

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

Abstract

2215. Theinert, W. Jan. 28. No Patent granted (Sealing fee not paid). Aerial machines without aerostats; planes, arrangement and construction of. - A flying- machine comprises an upper main plane a having the front part of snbstantially uniform width and the rear part tapering in width, as shown in Fig. 2; a lower supporting-plane e of uniform width; and the usual elevators t, rudder r, and propeller s. The underside of the plane a may be formed with a series of concavities d extending transversely, for preventing the formation of eddies. The front edge of the plane a may be curved as shown in Fig. 2. Steering.-The main plane a can be adjusted about a transverse axis k by means of links l, connected to the plane and to nuts m engaging right and left handed screws on a rod n rotated bv a hand-wheel o. The lower plane e may also be adjusted about a transverse axis. p.
GB191102215D 1911-01-28 1911-01-28 Improvements in Aeroplane Flying Machines. Expired GB191102215A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB191102215T 1911-01-28

Publications (1)

Publication Number Publication Date
GB191102215A true GB191102215A (en) 1911-08-17

Family

ID=32495945

Family Applications (1)

Application Number Title Priority Date Filing Date
GB191102215D Expired GB191102215A (en) 1911-01-28 1911-01-28 Improvements in Aeroplane Flying Machines.

Country Status (1)

Country Link
GB (1) GB191102215A (en)

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