Aeroload torque simulator

Measuring and testing – Blower – pump – and hydraulic equipment

Patent

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Details

73432SD, G01M 1706, G01M 900

Patent

active

042351030

ABSTRACT:
The aeroload torque simulator provides torques for either statically or dmically loading the output shaft of a power servo system such as a missile fin control system. It simulates the aerodynamic torque load developed at the missile fin which varies dynamically in flight.

REFERENCES:
patent: 3098382 (1963-07-01), Hoffman et al.
patent: 3727456 (1973-04-01), Gruneberg
patent: 4131010 (1978-12-01), Eyres

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