GB191100255A - Improvements in and relating to Flying Machines. - Google Patents

Improvements in and relating to Flying Machines.

Info

Publication number
GB191100255A
GB191100255A GB191100255DA GB191100255A GB 191100255 A GB191100255 A GB 191100255A GB 191100255D A GB191100255D A GB 191100255DA GB 191100255 A GB191100255 A GB 191100255A
Authority
GB
United Kingdom
Prior art keywords
planes
lateral
rudder
plane
hand
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 Elmer Dennis
Harry Say Bretton
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 GB191100255A publication Critical patent/GB191100255A/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
    • B64C3/42Adjusting about chordwise axes

Abstract

255. Dennis, W. E., and Bretton, H. S. Jan. 4. Aerial machines without aerostats; planes, arrangement and construction of.-The flying-machine is arranged with the load suspended below the main supporting - planes so that it keeps the machine stable. The aeroplane may be of any type and is shown on the drawings as a biplane. The main planes 12, 13 are supported on a framework c o mprising longitudinal and transverse members connected by vertical struts. The frame extends fore-and-aft and supports a double elevator 31 at the front and a single elevator 32 and rudder 55 at the rear. The supporting - planes 12, 13 and the elevators are concave downwards for the greater portion of their surface and at the forward end are inclined upwards to present a convex surface downwards. At the rear of the lower main plane 12 are arranged tapered resilient tips 74, Fig. 6, which are connected to the plane by a spring hinge. The tips move upwards under an excessive air pressure, and allow the air to escape easily at the rear of the plane. Hinged to the lateral extremities of the upper plane 13 are outwardlytapering planes 68, which are concave in both transverse and longitudinal directions, similar to a bird's wing. Below the lateral planes 68 are similar planes 68<a> hinged to the frame members 18 and connected by links 68<b> to the planes 68. Steering is effected (1) by front and rear elevators connected to move similarly, (2) by lateral planes 68, 68<a> movable upwards and downwards together about axes arranged in the line of flight, (3) by a rear rudder 55. The steering-planes are controlled by hand-wheels arranged close together. (1) The elevators 31, 32, Fig. 4, are provided with arms 33, 34 connected to a longitudinal rack 36 which is moved by a pinion 37 actuated through intermediate gear by a hollow shaft 41, Fig. 7, mounted on an inclined support 42 and provided with a hand-wheel 45. On the inclined support 42 are mounted on concentric sleeves 46, 47 the hand-wheels 49, 50 for actuating the rudder and lateral planes respectively. (2) The lateral planes 68 are hinged to the main plane 13, and the outer end 69 of the planes is guided by a curved slotted member 65. The actuating-cords are attached to the tips 69 of the planes, and are passed around guide-pulleys and drums carried by the sleeve 47 and rotated by the hand-wheel 50. The auxiliary planes 68<a> are connected to move with the planes 68. The planes at the two sides move upwards or downwards together. (3) The rear rudder 55 is actuated by cords conected to a tiller secured to the sleeve 46 and controlled by the handwheel 49.
GB191100255D 1911-01-04 1911-01-04 Improvements in and relating to Flying Machines. Expired GB191100255A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB191100255T 1911-01-04

Publications (1)

Publication Number Publication Date
GB191100255A true GB191100255A (en) 1911-12-30

Family

ID=32365040

Family Applications (1)

Application Number Title Priority Date Filing Date
GB191100255D Expired GB191100255A (en) 1911-01-04 1911-01-04 Improvements in and relating to Flying Machines.

Country Status (1)

Country Link
GB (1) GB191100255A (en)

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