GB191019759A - Improved Means for Automatically Balancing Aeroplanes against the Action of Side Winds or Gusts. - Google Patents

Improved Means for Automatically Balancing Aeroplanes against the Action of Side Winds or Gusts.

Info

Publication number
GB191019759A
GB191019759A GB191019759DA GB191019759A GB 191019759 A GB191019759 A GB 191019759A GB 191019759D A GB191019759D A GB 191019759DA GB 191019759 A GB191019759 A GB 191019759A
Authority
GB
United Kingdom
Prior art keywords
pendulum
valves
aeroplanes
gusts
action
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
Samuel Mcclelland
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 GB191019759A publication Critical patent/GB191019759A/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

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Operation Control Of Excavators (AREA)

Abstract

19,759. McClelland, S. Aug. 24. Balancing; planes, construction of. -In an aeroplane of the type in which the frame is rigidly attached to the supporting - plane, two sets of hit-or-miss valves are provided in the planes, each set being actuated by a pendulum. Preferably, holes b are made in the plane, and a sliding frame c, having corresponding holes e, is moved in a direction parallel to itself by a pendulum h. If the aeroplane is tilted to a dangerous angle, the valves at the higher side are opened, and the support on this side reduced. The rod i extends to the operator's seat, and it has a slide j within which the rod of the pendulum is free to move. The spring l holds the slide in such a position that it does not limit the motion of the rod, but permits the operator to open the valves at pleasure.
GB191019759D 1910-08-24 1910-08-24 Improved Means for Automatically Balancing Aeroplanes against the Action of Side Winds or Gusts. Expired GB191019759A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB191019759T 1910-08-24

Publications (1)

Publication Number Publication Date
GB191019759A true GB191019759A (en) 1911-07-20

Family

ID=32564035

Family Applications (1)

Application Number Title Priority Date Filing Date
GB191019759D Expired GB191019759A (en) 1910-08-24 1910-08-24 Improved Means for Automatically Balancing Aeroplanes against the Action of Side Winds or Gusts.

Country Status (1)

Country Link
GB (1) GB191019759A (en)

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