Turn rate indicator of aircraft with improved zero seeking chara

Measuring and testing – Speed – velocity – or acceleration – Angular rate using gyroscopic or coriolis effect

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74 51, 74 542, G01P 902, G01C 1930

Patent

active

041494180

ABSTRACT:
A turn rate indicator for an aircraft includes magnetic substance pieces facing each other, one being rotatable integrally with a gimbal and the other being fixed to a body. Because of the attracting force generated between the magnetic substance pieces, a pointer of the indicator returns to its zero point smoothly and certainly.

REFERENCES:
patent: 1713930 (1929-05-01), Sperry
patent: 2924978 (1960-02-01), Barnes

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