See how a vortex tube separates bleed air into hot and cold flows to boost thermoelectric power
See how multiple intercoolers and supercritical refrigerant compound cycles improve part load e
See how a vapour compression system raises ancillary waste heat temperature to enable transfer
See how a vortex tube separates bleed air into hot and cold flows to enhance thermoelectric gen
See how integrating an air-cycle machine into the generator housing enables compact, shaft-driv
See how a turbine-generator cooling assembly reduces ambient air from 1800°F to 100°F–300°F whi
See how phase change materials absorb heat from high-power directed energy systems in aircraft
See how an external pod gas turbine integrates power generation and phase-change thermal condit
See how a variable cross-sectional area adjustment device optimizes cooling air flow to aircraf
See how a pod-mounted gas turbine and phase change material thermal system enable independent p
A heat exchanger plus vortex cooler conditions compressor air for self-cleaning filters when warm climates limit air-to-air cooling.
A gas-turbine pod uses bleed air, refrigerant cooling, and phase-change storage to power and cool aircraft payloads across flight conditions.
Cooling inlet air below dew point and reheating it with energy recovery boosts turbine output while preventing filter caking and retrofit downtime.
Liquid coolant pipes and conductive potting move heat from stator windings to cut resistance and preserve electric machine life.
Dual airflow buffer cavities and pressurized cooling air protect an embedded gas turbine electrical machine from extreme heat while preserving service access.
Flowpath air is routed through internal machine passages to improve heat dissipation and avoid startup surge in turbine engine powerplants.