Engine component test apparatus

Measuring and testing – Simulating operating condition – Marine

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G01M 1900

Patent

active

051780038

ABSTRACT:
A component test apparatus is provided for measuring the torque of an aircraft engine inducer nozzle to characterize the efficiency of the nozzle prior to engine launch. A frictionless mount rotatably supports a forward inner nozzle support which combines with the support to form a pressurizable plenum for communicatively discharging air through the nozzle and imparting annular motion to the apparatus characteristic of the efficiency of the nozzle.

REFERENCES:
patent: 4774905 (1988-10-01), Nobis
patent: 4854569 (1989-08-01), Mizuta

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