GB309205A - Improvements in and relating to the control of aeroplanes - Google Patents

Improvements in and relating to the control of aeroplanes

Info

Publication number
GB309205A
GB309205A GB26477/27A GB2647727A GB309205A GB 309205 A GB309205 A GB 309205A GB 26477/27 A GB26477/27 A GB 26477/27A GB 2647727 A GB2647727 A GB 2647727A GB 309205 A GB309205 A GB 309205A
Authority
GB
United Kingdom
Prior art keywords
lever
raised
control
ailerons
elevator
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
GB26477/27A
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.)
EDWARD GAY
HUBER WILLIAM BEEDLE
Original Assignee
EDWARD GAY
HUBER WILLIAM BEEDLE
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 EDWARD GAY, HUBER WILLIAM BEEDLE filed Critical EDWARD GAY
Priority to GB26477/27A priority Critical patent/GB309205A/en
Publication of GB309205A publication Critical patent/GB309205A/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)
  • Catching Or Destruction (AREA)
  • Toys (AREA)
  • Special Chairs (AREA)

Abstract

309,205. Beedle, H. W., Rackett, P. E., and Gay, E. Oct. 6, 1927. Steering and balancing ; planes, construction of.-An aeroplane provided with a pendulous mass, such as the pilot's chair, so as to control the lateral and longitudinal balance automatically, through the usual universally mounted hand lever, has means for freeing the hand lever from the automatic control to enable the controls to be actuated manually. Upwardly opening valves may be provided near the leading edge of the plane adapted to be raised together or separately bv manual means which, when both valves are raised, can be coupled to the automatic means for controlling the elevator and ailerons. A chair 16 suspended from a universal joint 17 has a downwardly projecting rod 28 normally connected by a bar 30 to the lower end of a control lever 18 which actuates the ailerons and elevator through cables 5<a>, 7<a>. The rod 28 is connected by three normally slack cables 17<a> passing through holes in a fixed ring 19 to an outer ring 20. When the ring 20 is rotated about the ring 19 by a cable 22 actuated by a handlever 26, the cables 17a are drawn taut to centre the rod 28, and simultaneously a cable 29 passing through the control lever 18 is slackened to lower the bar 30 out of engagement with the lever 18. Fig. 12 shows a modification in which the ailerons and elevator are controlled by nods 5, 7 connected to a lever 4a universally jointed at the same point as the chair frame 16. When automatic operation is desired a bolt 34 is raised into engagement with a recess 37 in the lever 4a. Fig. 7 shows a valve flap 12 adapted to be raised against the pull of a spring 14 to open a passage through the plane near each tip and adjacent to the leading edge.
GB26477/27A 1927-10-06 1927-10-06 Improvements in and relating to the control of aeroplanes Expired GB309205A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB26477/27A GB309205A (en) 1927-10-06 1927-10-06 Improvements in and relating to the control of aeroplanes

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB26477/27A GB309205A (en) 1927-10-06 1927-10-06 Improvements in and relating to the control of aeroplanes

Publications (1)

Publication Number Publication Date
GB309205A true GB309205A (en) 1929-04-08

Family

ID=10244257

Family Applications (1)

Application Number Title Priority Date Filing Date
GB26477/27A Expired GB309205A (en) 1927-10-06 1927-10-06 Improvements in and relating to the control of aeroplanes

Country Status (1)

Country Link
GB (1) GB309205A (en)

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