Aircraft turn coordinator

Measuring and testing – Navigation – Take-off and landing monitors

Patent

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G01C 2100

Patent

active

040066320

ABSTRACT:
An aircraft turn coordinator used in an aircraft to sense both yaw and roll rate along the longitudinal flight axis. The coordinator includes a gimbaled rate gyroscope which is connected to a turn indicator arm by a gear train. The rapid rotation or lashing of the gimbaled gyroscope due to air turbulence is reduced by dampening the movement of the gimbal.

REFERENCES:
patent: 1985148 (1934-12-01), Chappell et al.
patent: 3355943 (1967-12-01), Mills et al.

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