GB191011894A - Improvements in Automatic Balancing Apparatus for Aerial Machines and Vessels, and the like. - Google Patents

Improvements in Automatic Balancing Apparatus for Aerial Machines and Vessels, and the like.

Info

Publication number
GB191011894A
GB191011894A GB191011894DA GB191011894A GB 191011894 A GB191011894 A GB 191011894A GB 191011894D A GB191011894D A GB 191011894DA GB 191011894 A GB191011894 A GB 191011894A
Authority
GB
United Kingdom
Prior art keywords
pendulum
planes
spindle
solenoid
plane
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
John Galea
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 GB191011894A publication Critical patent/GB191011894A/en
Expired legal-status Critical Current

Links

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C17/00Aircraft stabilisation not otherwise provided for

Abstract

11,894. Galea, J. May 13. [Addition to 9805/09.] Planes, construction of; balancing. - In a device for balancing automatically an aerial machine as described in the parent Specification, the efficiency of the balancing-planes is increased by forming them with the upper surface corrugated or providing them with louvres which are opened when the plane is inclined. The devices for operating the planes are also modified. A series of planes 2, Fig. 2, are hinged to the frame 1 as described in the parent Specification referred to, and are formed with corrugations on the upper surface, or the plane is formed of louvres 2<a>, Fig. 4, connected by a cord 35 which passes around a pulley 36 on a shaft 38 geared to the shaft 4 carrying the plane 2 and the operating-pulley 5. The plane is inclined by a cord 6 actuated by an electromagnet 10 and passing around the pulley 5. The controlling-device comprises a wind vane 20, Fig. 7, which sets itself in the direction of the air current and is provided with means for automatically determining the selection of the circuits independently of the pendulum 19. The spindle 21 of the vane carries a pair of insulated spring fingers arranged parallel to the vane 20 and moving over a series of pairs of contacts 18 on the bottom of the switch-box 16. Each pair of contacts is connected with a solenoid for actuating one of the planes, and the circuit to be closed is selected by the windvane. Two rings 25 are arranged around the box 16, and, when the pendulum 19 swings in the guide 22 attached to the upper end of the spindle 21, the electric circuit of the solenoid b for actuating one of the controlling-planes is closed. In another form, a short pendulum 19, Fig. 1, is carried by the spindle of the upper of two gear-wheels 27 mounted in a frame carried by the spindle 21. The lower wheel is provided with an arm 28, adapted to be moved by the swing of the pendulum 19 against the ring 25, to close the circuit of the solenoid b. The arm may be dispensed with, and the pinions 27, Figs. 11 and 12, formed of insulating-material with a sector 27<a> of conducting-material. The pendulum 19 is secured to a spindle 19<a> carrying a sector 19<b>, which gears with a pinion 26<a> on the shaft of the upper wheel 27. The conducting sectors 27<a> of the wheels 27 are normally out of contact, but the movement of the pendulum in one direction brings the sectors into gear and completes the circuit of the operating-solenoid b. In another form, the method of mounting the pendulum and gearwheels, shown in Fig. 12, may be combined with an arm 28 and contact circle 25 as shown in Fig. 9, the gear wheels being made of metal. The vane may be formed of two blades set at an angle of 30 degrees to one another.
GB191011894D 1909-04-26 1910-05-13 Improvements in Automatic Balancing Apparatus for Aerial Machines and Vessels, and the like. Expired GB191011894A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB190909805T 1909-04-26

Publications (1)

Publication Number Publication Date
GB191011894A true GB191011894A (en) 1910-11-03

Family

ID=32444130

Family Applications (2)

Application Number Title Priority Date Filing Date
GB190909805D Expired GB190909805A (en) 1909-04-26 1909-04-26 Improvements in and relating to Automatic Balancing Apparatus for Aerial Machines and Vessels and the like.
GB191011894D Expired GB191011894A (en) 1909-04-26 1910-05-13 Improvements in Automatic Balancing Apparatus for Aerial Machines and Vessels, and the like.

Family Applications Before (1)

Application Number Title Priority Date Filing Date
GB190909805D Expired GB190909805A (en) 1909-04-26 1909-04-26 Improvements in and relating to Automatic Balancing Apparatus for Aerial Machines and Vessels and the like.

Country Status (1)

Country Link
GB (2) GB190909805A (en)

Also Published As

Publication number Publication date
GB190909805A (en) 1910-01-27

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