A centrifugal pump impeller vane features a recessed step surface on its rotational rear end to develop swirling flows.
Local quality variation in sloped blades increases surface area to improve cooling efficiency while minimizing acoustic emissions from tip turbulence.
Segmented blade hub design releases torque during static conditions to protect the motor from damage caused by foreign material deposition or freezing.
Joule-Thomson expansion of compressed gas cools bearings, eliminating complex auxiliary systems and extending operational life.
Annular groove disperses pressure into a casing chamber, suppressing surge and extending the stable operation range.
Centrifugal compressor diverts compression air through a double skin casing to cool the shaft, eliminating separate ventilation power consumption.
A gas turbine air inlet manifold uses a compressed polyurethane anti-vibration pad to isolate compressor vibrations.
Movable hub alignment reduces resonance noise and power consumption while maintaining thin device profiles.
A composite fan frame structure disperses resonance zones through material damping.
Segmented compartments with a single rotating valve minimize leakage between pressure streams while maintaining continuous flow at high rotational speeds.