This invention discloses a rotating disk cavity
test platform, comprising a main air intake
system, a
cold air intake
system, an exhaust
system, a
power transmission system, a
lubrication system, and a cooling water system. The main air intake system is connected to the test piece and provides the test piece with the required flow rate, temperature, and pressure of the main
airflow. The
cold air intake system is connected to the test piece and provides the test piece with the required flow rate, temperature, and pressure of the secondary
airflow. The exhaust system is used to
exhaust gas from the test piece, and the main air intake system and the
cold air intake system are respectively connected to the exhaust system. The
power transmission system is used to drive the rotation of the test piece. The
lubrication system is used to lubricate the test piece and the
power transmission system. The cooling water system is connected to the
lubrication system and is used to dissipate heat from the lubricating oil in the lubrication system. This
test platform introduces modeled main and secondary flows under high-speed rotation conditions to conduct rotating disk cavity flow and
heat transfer tests, studying the effects of different engine speeds and variations in secondary flow rate / temperature / pressure parameters on disk cavity flow and
heat transfer.