Measuring and testing – Speed – velocity – or acceleration – Angular rate using gyroscopic or coriolis effect
Patent
1997-10-08
1999-06-22
Williams, Hezron
Measuring and testing
Speed, velocity, or acceleration
Angular rate using gyroscopic or coriolis effect
7350402, G01P 904
Patent
active
059152761
ABSTRACT:
A rate sensor for sensing applied rate on at least two axes is provided. A vibrating structure is vibrated in a Cos 2.theta. carrier mode at a Cos 2.theta. carrier mode frequency such that rotation about one or the other of the two axes 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 2.theta. carrier mode frequency. The vibrating structure has a substantially planar, substantially ring or hoop-like form that is shaped and dimensioned to match the frequencies of the Cos 2.theta. carrier mode and the rocking mode vibration in the vibrating structure to give a resonant amplification of the rocking motion. The rocking mode vibration is proportional to the applied rate. The rocking mode vibration is detected to determine the applied rate.
REFERENCES:
patent: 5226321 (1993-07-01), Varnham et al.
patent: 5471875 (1995-12-01), Sato et al.
patent: 5540094 (1996-07-01), Varnham et al.
patent: 5587529 (1996-12-01), Iguchi et al.
patent: 5621171 (1997-04-01), Fell
British Aerospace Public Limited Company
Kwok Helen C.
Williams Hezron
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