Rate sensor

Claim 2

A rate sensor for sensing applied rate on at least two axes, including a vibrating structure, means for vibrating the structure in a Cos 2θ carrier mode at a Cos 2θ carrier mode frequency such that rotation about one or other of said at least two axes in the plane of the vibrating structure will generate a Coriolis force sufficient to cause a rocking motion and rocking mode vibration of the vibrating structure about the same axis out of the plane of the vibrating structure at the Cos 2θ carrier mode frequency, with the vibrating structure having a substantially planar substantially ring or hoop-like form shaped and dimensioned to match the frequencies of the Cos 2θ carrier mode and the rocking mode vibration in the vibrating structure to give a resonant amplification of the rocking motion, which rocking mode vibration is proportional to the applied rate, and means for detecting the rocking mode vibration and thereby the applied rate.

Claim 3

A sensor according to claim 1, wherein the vibrating structure is made of metal or of silicon.

Claim 4

A sensor according to claim 2, wherein the vibrating structure is ring like in form having an outer rim supported by a plurality of legs extending substantially radially from a central boss.

Claim 5

A sensor according to claim 3, for sensing applied rate on two axes, having a substantially planar ring-like vibrating structure made from metal, wherein the means for vibrating the vibrating structure in a Cos 2θ carrier mode includes an electromagnetic carrier mode drive element and a capacitive carrier mode pick off element arranged at 0° and 270° respectively with respect to the outer rim of the vibrating structure and located in the plane of the outer rim radially externally thereof adjacent points of maximum radial motion of said rim when vibrating in the Cos 2θ carrier mode, and wherein the means for detecting the rocking mode vibration includes an x axis electromagnetic drive element, an x axis capacitive pick off element, a y axis electromagnetic drive element and a y axis capacitive pick off element, located adjacent to the outer rim in superimposed relationship therewith at a perpendicular spacing therefrom, with the y axis pick off element, x axis drive element, y axis drive element and x axis pick off element being arranged at 0°, 90°, 180° and 270° respectively around the outer rim.

Claim 6

A sensor according to claim 4, for sensing applied rate on three axes, wherein the means for vibrating the vibrating structure additionally includes an electromagnetic response mode drive element and a capacitive response mode pick off element located in the plane of the outer rim of the vibrating structure adjacent to the points of maximum radial movement for the outer rim when vibrating in a response mode, with the response mode drive element and the pick off element being arranged at 135° and 225° respectively with respect to the outer rim of the vibrating structure and located in the plane of the outer rim radially externally thereof, to sense rotation about an axis normal to the plane of the vibrating structure.

Claim 7

A sensor to claim 3, wherein the outer rim is substantially circular in plan view or is substantially rectangular in plan view.

Claim 8

A sensor according to claim 5, wherein the vibrating structure is made of a nickel-iron alloy.

Claim 9

A sensor according to claim 3, for sensing applied rate on two axes, having a substantially planar, substantially ring-like vibrating structure made from silicon, wherein the means for vibrating the vibrating structure in a Cos 2θ carrier mode includes two electrostatic carrier mode drive elements and two electrostatic carrier mode pick off elements arranged with the drive elements at 0° and 180° and the pick off elements at 90° and 270° respectively with respect to the outer rim of the vibrating structure and located radially externally of the outer rim adjacent points of maximum radial motion of the outer rim when vibrating in the Cos 2θ carrier mode, and wherein the means for detecting the rocking mode vibration includes an x axis electrostatic drive element, an x axis electrostatic pick off element, a y axis electrostatic drive element and a y axis electrostatic pick off element located adjacent the outer rim in superimposed relationship therewith at a perpendicular spacing therefrom, with the y axis drive element, the x axis pick off element, the y axis pick off element and the x axis drive element being arranged at 0°, 90°, 180° and 270°, respectively around the outer rim.

Claim 10

A sensor according to claim 8, for sensing applied rate on three axes, wherein the means for vibrating the vibrating structure additionally includes two electrostatic z axis response mode drive elements and two electrostatic z axis response mode pick off elements located in the plane of the outer rim of the vibrating structure radially externally thereof adjacent points of maximum radial movement for the outer rim when vibrating in a response mode, with the first z axis response mode drive element, the first z axis response mode pick off element, the second z axis response mode drive element and the second z axis response mode pick off element being arranged at 45°, 135°, 225° and 315° respectively around the outer rim of the vibrating structure.

Claim 11

A sensor according to claim 9, wherein the outer rim is substantially circular in plan view with the outer rim and the legs being suspended above an insulated substrate layer by means of the central boss which is mounted thereon.

Claim 12

A sensor according to claim 3, wherein the vibrating structure is dimensioned to match the frequencies of the Cos 2θ carrier mode and the rocking mode vibration by controlled removal of material from the edge of the outer rim to modify the mass thereof or by controlled removal of material from a neutral axis of the outer rim to modify the stiffness of the outer rim.

Claim 13

A sensor according to claim 4, wherein the vibrating structure is dimensioned to match the frequencies of the Cos 2θ carrier mode and the rocking mode vibration by controlled removal of material from the edge of the outer rim to modify the mass thereof or by controlled removal of material from a neutral axis of the outer rim to modify the stiffness of the outer rim.

Claim 14

A sensor according to claim 5, wherein the vibrating structure is dimensioned to match the frequencies of the Cos 2θ carrier mode and the rocking mode vibration by controlled removal of material from the edge of the outer rim to modify the mass thereof or by controlled removal of material from a neutral axis of the outer rim to modify the stiffness of the outer rim.

Claim 15

A sensor according to claim 6, wherein the vibrating structure is dimensioned to match the frequencies of the Cos 2θ carrier mode and the rocking mode vibration by controlled removal of material from the edge of the outer rim to modify the mass thereof or by controlled removal of material from a neutral axis of the outer rim to modify the stiffness of the outer rim.

Claim 16

A sensor according to claim 7, wherein the vibrating structure is dimensioned to match the frequencies of the Cos 2θ carrier mode and the rocking mode vibration by controlled removal of material from the edge of the outer rim to modify the mass thereof or by controlled removal of material from a neutral axis of the outer rim to modify the stiffness of the outer rim.

Claim 17

A sensor according to claim 8, wherein the vibrating structure is dimensioned to match the frequencies of the Cos 2θ carrier mode and the rocking mode vibration by controlled removal of material from the edge of the outer rim to modify the mass thereof or by controlled removal of material from a neutral axis of the outer rim to modify the stiffness of the outer rim.

Claim 18

A sensor according to claim 9, wherein the vibrating structure is dimensioned to match the frequencies of the Cos 2θ carrier mode and the rocking mode vibration by controlled removal of material from the edge of the outer rim to modify the mass thereof or by controlled removal of material from a neutral axis of the outer rim to modify the stiffness of the outer rim.

Claim 19

A sensor according to claim 10, wherein the vibrating structure is dimensioned to match the frequencies of the Cos 2θ carrier mode and the rocking mode vibration by controlled removal of material from the edge of the outer rim to modify the mass thereof or by controlled removal of material from a neutral axis of the outer rim to modify the stiffness of the outer rim.