Aerospace Nozzle Flow Test Bench

Aerospace Nozzle Flow Test Bench, have constant temperature refrigerated Liquid bath chiller with heater, whose size of inner chamber (500 x 400 x 400 mm//SS 304), with fluid capacity 80 Liter. This thermostatically controlled oil tank (temperature +5 to +95 degree Celsius with accuracy of +/-0.1 degree Celsius) will maintain temperature of working fluid (Turbonycoil 13 B) at 35 degree Celsius.

This thermostatically controlled oil tank (temperature +5 to +95 degree Celsius with accuracy of +/-0.1 degree Celsius) will maintain temperature of working fluid (Turbonycoil 13 B) at 35 degree Celsius.

This Bench will estimate flow rate (l.p.h) of nozzle at temperature 35 degree Celsius and working pressure (200 kpa ±10 kpa) by using Turbonycoil 13 B (oil).

This test will estimate Flow Rate and Flow Direction of oil jets/nozzle by using 3cst type oils at 98.9 degree Celsius meeting French specifications AIR 3514 or American specifications MIL-L-7808 G (TN 13 B for instance ),oil will use at a temperature 35 degree Celsius and at a pressure of 200kPa).