GB190930521A - Improvements in and relating to Aeroplanes, Airships and the like. - Google Patents

Improvements in and relating to Aeroplanes, Airships and the like.

Info

Publication number
GB190930521A
GB190930521A GB190930521DA GB190930521A GB 190930521 A GB190930521 A GB 190930521A GB 190930521D A GB190930521D A GB 190930521DA GB 190930521 A GB190930521 A GB 190930521A
Authority
GB
United Kingdom
Prior art keywords
regulator
piston
lever
pulley
machine
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
Donat Banki
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 GB190930521A publication Critical patent/GB190930521A/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)
  • Transmission Devices (AREA)

Abstract

30,521. Bßnki, D. Nov. 5, [Convention date]. Steering and balancing.- In an automatic control mechanism for flying-machines comprising a gravity-actuated regulator which operates on the slide valve of a fluid pressure motor actuating the balancing-planes, the motor and controlling mechanism are pivotally mounted on the flying-machine, and can be adjusted manually to vary the normal incidence of the machine. The regulator h, Fig. 1, is mounted on a lever 6 pivoted at k to a lever l connected to the piston-rod 1 ot the auxiliary motor a, and is linked by a rod 2 to the slide valves n. When the machine tilts, fluid under pressure is admitted by one of the valves to one side of the piston b which is moved to actuate the balancing-planes. At the same time, the point of support k of the regulator is moved in the same direction as the piston so that the valves n are moved back to a central position and the movement of the piston is stopped. A float contained in a cylindrical vessel may be used in place of the pendulum h; or, the regulator may consist of a pipe 4, Fig..3, containing liquid and provided at its ends with diaphragms 5 connected together and to the controlling-lever 6. The controlling-devices are pivoted at d, Fig. 1, to the frame of the machine, and are tilted by a hand-lever 7. The Specification in the original form, as open to inspection under Section 91 (3) (a), comprises also the following subject-matter. The regulator may be modified to prevent accelerations of the machine from affecting the controlling- apparatus. A ball or other valve m, Fig. 4<a>, (Cancelled), is inserted in the pipe 4, Fig. 3, between the diaphragms 5. When an acceleration takes place, the ball is forced against a seating on the pipe and closes it so that the inertia of the fluid in the regulator is prevented from acting on the diaphragm. In order to obtain a sufficient power for actuating the planes, and also a proper sensitiveness of the apparatus, two fluid-pressure motors arranged in series are employed. The first motor is provided with a distributor e', j<1>, Fig. 6<a> (Cancelled), of small diameter, and the piston b<1> is connected to the distributor e, f of large dimensions corresponding to the power required. The apparatus can be used for longitudinal or transverse stability. In an example shown in Fig. 6 (Cancelled), the apparatus is designed to actuate the lateral balancing-members which are connected to cords C<1>, C<2> passed around a pulley B. The shaft A of the pulley B is connected to the cross-head H of the piston of the actuating-motor a, which is controlled as previously described by a fluid regulator having diaphragms N<1>, N<2>. The link s t actuating the distributor e f is connected by a rod d to the pulley B so that movement of the pulley moves back the distributor to its central position. The motor and regulator are carried by a lever D which is adjusted by cords E<1>, E<2> to vary the normal incidence of the machine. The lever D is normally loose on the shaft A of the pulley B, but can be connected to the pulley by a spring bolt when it is desired to actuate the balancing- members manually. This subject-matter does not appear in the Specification as accepted.
GB190930521D 1909-11-05 1909-12-30 Improvements in and relating to Aeroplanes, Airships and the like. Expired GB190930521A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
HU190930521X 1909-11-05

Publications (1)

Publication Number Publication Date
GB190930521A true GB190930521A (en) 1910-12-30

Family

ID=32448795

Family Applications (1)

Application Number Title Priority Date Filing Date
GB190930521D Expired GB190930521A (en) 1909-11-05 1909-12-30 Improvements in and relating to Aeroplanes, Airships and the like.

Country Status (1)

Country Link
GB (1) GB190930521A (en)

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