Measuring and testing – Speed – velocity – or acceleration – Angular rate using gyroscopic or coriolis effect
Patent
1984-05-07
1986-06-03
Levy, Stewart J.
Measuring and testing
Speed, velocity, or acceleration
Angular rate using gyroscopic or coriolis effect
73516LM, G01P 326
Patent
active
045922322
ABSTRACT:
The present invention relates to a sensor for sensing orthogonal components of angular velocity of rotation of the sensor about any axis in a plane perpendicular to a reference jet axis within the sensor, wherein a fluid jet is deflected relative to two pairs of electrically resistive, temperature sensitive elements in response to rotation of the sensor, wherein each pair of elements forms the sensing branch of a bridge circuit, the jet deflection causing differential cooling and bridge unbalance which is an indication of the deflection of the fluid jet from the reference jet axis which is in turn an indication of the rate and direction of angular rotation, wherein each pair of elements is disposed in a plane perpendicular to the reference jet axis, each pair sensing an orthogonal component of angular velocity of rotation.
REFERENCES:
patent: 3110185 (1963-11-01), Hughes
patent: 3205715 (1965-09-01), Meek
patent: 3500691 (1970-03-01), Moore
patent: 4020700 (1977-05-01), Lopiccolo et al.
patent: 4026159 (1977-05-01), Isakson et al.
Heated Sensor Finds Wide Applications in Fluid Flow Measurements, a publication of CGS/Datametrics, Bulletin 600, pp. 13-19.
Moffatt E. Marston
Swarts Richard E.
Chapman, Jr. John E.
Levy Stewart J.
Maguire, Jr. Francis J.
United Technologies Corporation
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