GB191219502A - Improvements in and relating to Aeroplanes and like Machines. - Google Patents

Improvements in and relating to Aeroplanes and like Machines.

Info

Publication number
GB191219502A
GB191219502A GB191219502DA GB191219502A GB 191219502 A GB191219502 A GB 191219502A GB 191219502D A GB191219502D A GB 191219502DA GB 191219502 A GB191219502 A GB 191219502A
Authority
GB
United Kingdom
Prior art keywords
rod
sleeve
machine
aeroplanes
relating
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
William Samuel Laycock
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 GB191219502A publication Critical patent/GB191219502A/en
Expired legal-status Critical Current

Links

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C17/00Aircraft stabilisation not otherwise provided for

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Earth Drilling (AREA)
  • Door And Window Frames Mounted To Openings (AREA)
  • Jib Cranes (AREA)

Abstract

19,502. Laycock, W. S. Aug. 26. [Cognate Application, 20,231/12.] Balancing.-In a device for increasing the stability of an aeroplane comprising a depending rod having a weight attached to its lower end the rod is formed in two parts c, c<2> connected together by a chain c<1> or other universal joint and means are provided, comprising for example, an adjustable sleeve b<1>, for rigidly connecting the two parts together. The part c is secured to the frame a of the machine. The sleeve b<1> is raised vertically by the aviator so that the rod c<2> may swing freely in any direction to prevent injury thereto when the machine lands. In another form, the sleeve d<3>, Fig. 4, is provided with a bell-shaped end f for engaging the upper end of the part e' which carries the stabilizing- mass e<2> at its lower end.
GB191219502D 1912-08-26 1912-08-26 Improvements in and relating to Aeroplanes and like Machines. Expired GB191219502A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB191219502T 1912-08-26

Publications (1)

Publication Number Publication Date
GB191219502A true GB191219502A (en) 1913-05-22

Family

ID=32573351

Family Applications (1)

Application Number Title Priority Date Filing Date
GB191219502D Expired GB191219502A (en) 1912-08-26 1912-08-26 Improvements in and relating to Aeroplanes and like Machines.

Country Status (1)

Country Link
GB (1) GB191219502A (en)

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