GB191012819A - Apparatus for Maintaining Equilibrium in Aeroplane Flying Machines. - Google Patents

Apparatus for Maintaining Equilibrium in Aeroplane Flying Machines.

Info

Publication number
GB191012819A
GB191012819A GB191012819DA GB191012819A GB 191012819 A GB191012819 A GB 191012819A GB 191012819D A GB191012819D A GB 191012819DA GB 191012819 A GB191012819 A GB 191012819A
Authority
GB
United Kingdom
Prior art keywords
planes
machine
pulley
shafts
shaft
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
Hans Lohmann
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 GB191012819A publication Critical patent/GB191012819A/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
    • B64C3/385Variable incidence wings

Abstract

12,819. Lohmann, H. May 26. Aerial machines without aerostats; planes, arrangement of; steering and balancing.-The supporting - planes of an aerial machine are divided at the middle and pivoted on a frame carrying the front elevator, rear rudder, and g r o u n d wheels. The planes on the two sides of the machine can be adjusted independently by hand, or they can be turned automatically in opposite directions for balancing. The handlevers controlling the planes on the two sides of the machine also serve to actuate the rudder and the elevator. The invention is shown applied to a biplane machine in which the upper and lower planes are connected by hinged struts 6 provided with toothed sectors 10, 11, which engage with pinions secured to shafts 16, 17 extending laterally. The shafts 16, 17 are carried on frames 22 secured to the frame 5 of the machine. A sprocket-wheel 30 connected by a chain to wheels on the inner ends of the shafts 16, 17 is mounted on a shaft 70 carrying a pulley 25. A similar sprocket-wheel 30 and pulley 26 are mounted on the shaft 71 for operating the planes 3, 4 on the opposite side of the machine. Separate operating - devices 33, 34 are provided for the planes at the two sides of the machine, each device comprising a hand - lever 42, Fig. 4, movable in two directions. The cord 35, passing around the pulley 25 or 26, is guided by pulleys 39, 40 around a pulley 38 mounted on an upright 37. The lever 42 is secured to the pivot of the pulley 38, and passes between a double locking-rack 43. The uprights 37 of the operating-devices 33, 34 are mounted to rotate in bearings, so that, by moving the hand-lever 42 horizontally, the pulley 45 is turned to actuate either the rudder or the elevator. The lever is locked against horizontal movement by a spring tooth 54, which engages with a rack 52 pivoted to the frame of the machine. The automatic mechanism for adjusting the lateral planes in opposite directions for balancing comprising a pendulum 60, Fig. 1, pivoted at 61 and controlling a relay mechanism. A shaft 64 is driven from the motor shaft and carries two bevel pinions 76, 77, one of which is adapted, when the shaft 64 is lowered or raised by an arm 63 attached to the pendulum, to gear with pinions 72, 73 on the shafts 70, 71. The shafts 70, 71 are connected by the sprocket-wheels 30 and chains with the shafts 16, 17 which adjust the inclination of the planes. A similar automatic device is used for actuating the front elevator, and comprises a rotating shaft 83 carrying pinions adapted to engage with a pinion 87 when the shaft is raised or lowered by the action of the pendulum 78. The pinion 87 is secured to a pulley 89 connected to the elevator.
GB191012819D 1910-05-26 1910-05-26 Apparatus for Maintaining Equilibrium in Aeroplane Flying Machines. Expired GB191012819A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB191012819T 1910-05-26

Publications (1)

Publication Number Publication Date
GB191012819A true GB191012819A (en) 1911-05-25

Family

ID=32638224

Family Applications (1)

Application Number Title Priority Date Filing Date
GB191012819D Expired GB191012819A (en) 1910-05-26 1910-05-26 Apparatus for Maintaining Equilibrium in Aeroplane Flying Machines.

Country Status (1)

Country Link
GB (1) GB191012819A (en)

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