GB191020951A - Improvements in Flying Machines. - Google Patents

Improvements in Flying Machines.

Info

Publication number
GB191020951A
GB191020951A GB191020951DA GB191020951A GB 191020951 A GB191020951 A GB 191020951A GB 191020951D A GB191020951D A GB 191020951DA GB 191020951 A GB191020951 A GB 191020951A
Authority
GB
United Kingdom
Prior art keywords
panels
edge
cords
plane
balancing
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
Arthur Herbert Baily
Frederick John Cleveland
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 GB191020951A publication Critical patent/GB191020951A/en
Expired legal-status Critical Current

Links

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C3/00Wings
    • B64C3/38Adjustment of complete wings or parts thereof
    • B64C3/52Warping

Abstract

20,951. Baily, A. H., and Cleveland, F. J. Sept. 8. Steering and balancing.-An aeroplane is provided at each side with inclined curtains or panels, which can be twisted or skewed independently or simultaneously for balancing and steering. The upper plane a of a biplane extends beyond the lower one a<1>, and the inclined panels b, c are arranged between the extremities of the planes a, a<1>. One edge of the panels, shown as the bottom edge e, is secured at several points by cords d to the plane a', the other edge e<1> being secured only at its middle point to the plane a. The ends of the edge e are connected by cords f to the operating - mechanism. The panels may be variously shaped, and may taper towards the fixed edge to reduce the resistance. The cords f may be actuated by chains p, q, Fig. 16, passed around sprockets on a pair of handwheels n, o, mounted on a pillar r, which may be tilted to actuate the elevator or longitudinal stability members. When applied to a monoplane, the panels are stretched between the tips and the body. The upwardly and outwardly inclined position of the panels b, c tends to preserve the stability of the machine.
GB191020951D 1910-09-08 1910-09-08 Improvements in Flying Machines. Expired GB191020951A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB191020951T 1910-09-08

Publications (1)

Publication Number Publication Date
GB191020951A true GB191020951A (en) 1911-02-23

Family

ID=32492821

Family Applications (1)

Application Number Title Priority Date Filing Date
GB191020951D Expired GB191020951A (en) 1910-09-08 1910-09-08 Improvements in Flying Machines.

Country Status (1)

Country Link
GB (1) GB191020951A (en)

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