Geometrical instruments – Indicator of direction of force traversing natural media – Gyroscopically controlled or stabilized
Patent
1977-11-09
1980-04-15
Martin, Jr., William D.
Geometrical instruments
Indicator of direction of force traversing natural media
Gyroscopically controlled or stabilized
33352, 33361, 74 547, G01C 1900, G01C 1938
Patent
active
041976550
ABSTRACT:
A gyroscopic device of the type having a short-circuited rotor winding or conductor so shaped so as to produce axial and radial flux components when rotated in the earth's magnetic field is coupled to a coaxial sensing coil coaxial which gyroscopically stabilized thereby, signals induced in the sensing coil due to the axial flux component of the rotor is used to derive magnetic heading information and there is provided at least one further coil on the supporting body and inductively linked to the sensing coil and rotor such that when the sensing coil is gyroscopically stabilized by the rotor, the coil supported on the supporting body in relation to the gyroscopically stabilized sensing coil is such that any changes in angular orientation of the supporting body relative to the gyroscopically stabilized sensing coil introduces changes in the signal voltages induced in the coils. The further coil on the supporting body may be excited with one or more excitation signals of a frequency different than the angular speed of the rotor and constituted by pairs of orthogonally related coils on all three axes, namely, the roll, pitch and yaw axes. The coil located on the yaw axis is coaxial with the gyroscopically stabilized sensing coil in the rest position and is used for eliminating ambiguities.
REFERENCES:
patent: 2049232 (1936-07-01), Sydnes
patent: 2201559 (1940-05-01), Moseley
patent: 2315216 (1943-03-01), Moller et al.
patent: 2603767 (1952-07-01), Ferrill
patent: 2737054 (1956-03-01), Wendt
patent: 3858328 (1975-01-01), La Rose
patent: 4013946 (1977-03-01), Lewis
Cessna Aircraft Company
Martin, Jr. William D.
Zegeer Jim
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