GB408936A - A combined magnetic compass and inclinometer - Google Patents

A combined magnetic compass and inclinometer

Info

Publication number
GB408936A
GB408936A GB2870332A GB2870332A GB408936A GB 408936 A GB408936 A GB 408936A GB 2870332 A GB2870332 A GB 2870332A GB 2870332 A GB2870332 A GB 2870332A GB 408936 A GB408936 A GB 408936A
Authority
GB
United Kingdom
Prior art keywords
sphere
rod
ring
magnets
fixed
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
GB2870332A
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.)
MARGARET ALICE COOKE
Original Assignee
MARGARET ALICE COOKE
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 MARGARET ALICE COOKE filed Critical MARGARET ALICE COOKE
Priority to GB2870332A priority Critical patent/GB408936A/en
Publication of GB408936A publication Critical patent/GB408936A/en
Expired legal-status Critical Current

Links

Classifications

    • GPHYSICS
    • G01MEASURING; TESTING
    • G01CMEASURING DISTANCES, LEVELS OR BEARINGS; SURVEYING; NAVIGATION; GYROSCOPIC INSTRUMENTS; PHOTOGRAMMETRY OR VIDEOGRAMMETRY
    • G01C17/00Compasses; Devices for ascertaining true or magnetic north for navigation or surveying purposes

Abstract

408,936. Magnetic compasses; inclinometers. COOKE, M. A., Elysium, Shillong, Assam, India. Oct. 14, 1932, No. 28703. [Class 97 (ii).] A combined magnetic compass and inclinometer comprises a uni versally rotatable indicating mem ber, having a magnetic axis and a gravity axis, tending to align respectively with the earth's magnetic fielc and the gravity field, the gravity bias being re ducible to avoid inertia effects due to turning of the supporting air craft &c. In the form shown, the indicating element comprises a hollow sphere 2, having one hemispherical part fixed to a ring 11 and the other hemispherical part adapted to be screwed thereto. Two groups of magnets 1 are mounted by brackets 7 on an externally threaded tubular rod 8, which is diametrically supported by bearings 10 in the ring 11. Screws 32 enable the magnets 1 to be fixed so that they make an angle with the axis of the ring 11 corresponding to the angle of dip. A ring 12 fixed to the ring 11 at right angles thereto, carries a rod 26 terminating in a sleeve 27, which loosely surrounds the rod 8 and is held in position by a threaded rod 28, fixed in the ring 12 at right angles to the rod 8. A bracket 14, carrying adjustable weights 15 for applying gravity bias, is arranged to slide on the rod 26 and is attached to the bottom of the ring 12 by a series of spring walled capsules 16 which communicate with each other and with an aperture in the sphere 2 by a pipe 20. Increase of pressure in the capsules 16 causes them to spring into the distended position and lift the bracket 14, thus rendering the bias weights inoperative. Adjustable balance weights 29 are provided on the rods 8 and 28 and balancing screws 31, arranged at right angles are threaded through the rod 8. The sphere 2 is suspended in a liquid, e.g. alcohol, of the same density and contained in an outer sphere 3 with a window 5. The sphere 2 is centralised in the sphere 3 by jets from four nozzles 4 arranged at the four corners of a tetrahedron. Each nozzle, Fig. 2, has a central bore 4<b>, to which alcohol under pressure is supplied from pump 6 by pipes 48, and a concave spherical surface 4<a>, between which and the sphere 2 the alcohol passes to an annular passage 4c and from thence through pipes 49 back to the pump. Before accelerating or turning of the supporting craft, the pressure in the sphere 3 is increased either by the manually operated pump 21, 22 or automatically in response to movement of the controls of the craft, so that the capsules 16 are distended and the gravity bias eliminated. In a modified form the clamping screws 32 are dispensed with and the rod 8 provided with two friction discs. The latter are normally engaged by brake pads on the ends of two spring-urged levers, the free ends of which are arranged adjacent a flexible part in the wall of the sphere 2. When it is desired to reset the magnets 1, a plunger 41, Fig. 1, is pressed against the flexible part and causes the levers to rock and withdraw the brake pads. The magnets 1 then settle in accordance with the angle of dip and may be clamped again by withdrawing the plunger 41. The sphere 2 may be marked with lines of latitude and longitude and the window 5 with cross wires. According to the Provisional Specification a fixed bias weight may be mounted at the bottom of the sphere 2 and its effect counteracted when desired by forcing the alcohol up a normally vertical passage to a chamber above the centre of the sphere 2. Specification 408,973 is referred to.
GB2870332A 1932-10-14 1932-10-14 A combined magnetic compass and inclinometer Expired GB408936A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB2870332A GB408936A (en) 1932-10-14 1932-10-14 A combined magnetic compass and inclinometer

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB2870332A GB408936A (en) 1932-10-14 1932-10-14 A combined magnetic compass and inclinometer

Publications (1)

Publication Number Publication Date
GB408936A true GB408936A (en) 1934-04-16

Family

ID=10279748

Family Applications (1)

Application Number Title Priority Date Filing Date
GB2870332A Expired GB408936A (en) 1932-10-14 1932-10-14 A combined magnetic compass and inclinometer

Country Status (1)

Country Link
GB (1) GB408936A (en)

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE1169147B (en) * 1957-10-30 1964-04-30 Pedro Pere Parera Magnetic compass with a spherical hollow body that accommodates the magnet
US3365942A (en) * 1964-04-03 1968-01-30 Sperry Rand Corp Inertial altimeter
GB2256272A (en) * 1991-05-31 1992-12-02 3D Instr Ltd Attitude sensor

Cited By (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE1169147B (en) * 1957-10-30 1964-04-30 Pedro Pere Parera Magnetic compass with a spherical hollow body that accommodates the magnet
US3365942A (en) * 1964-04-03 1968-01-30 Sperry Rand Corp Inertial altimeter
GB2256272A (en) * 1991-05-31 1992-12-02 3D Instr Ltd Attitude sensor
WO1992021936A1 (en) * 1991-05-31 1992-12-10 3D Instruments Limited Attitude sensor
GB2256272B (en) * 1991-05-31 1994-10-26 3D Instr Ltd Attitude sensor
AU658886B2 (en) * 1991-05-31 1995-05-04 3D Instruments Limited Attitude sensor
US5452519A (en) * 1991-05-31 1995-09-26 3D Instruments Limited Attitude sensor

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