Turn rate indicator of aircraft using gyroscope

Details Turn rate indicator of aircraft using gyroscope Turn rate indicator of aircraft using gyroscope

1978-04-06

1979-07-24

Gill, James J.

Measuring and testing

Speed, velocity, or acceleration

Angular rate using gyroscopic or coriolis effect

74 547, G01P 902

Patent

active

041618840

ABSTRACT:
A turn rate indicator of an aircraft wherein the outer rotor of a Hall motor is used as a gyro rotor. A driving circuit for the gyro stator circuit is provided integrally with the gyro gimbal. The driving circuit is coupled to a connector affixed to the case of the turn rate indicator with fine connecting lines keeping a slack section between the driving circuit and the connector.

REFERENCES:
patent: 2737815 (1956-03-01), Wikkenhauser
patent: 2963912 (1960-12-01), Kawarada
patent: 3240076 (1966-03-01), Li
patent: 3753374 (1973-08-01), Strassburg

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