Matches 1 - 9 out of 9
Match Document Document Title
7266946 Gas fuel compression by liquification  
An apparatus for supplying inlet gas 29 and fuel 17 to a gas turbine engine 10 , the apparatus comprising: a heat exchanger 28 for transferring thermal energy from the inlet gas 29 to a...
7260926 Thermal management system for an aircraft  
A fuel based thermal management system includes a fuel stabilization system which permits the fuel to exceed the traditional coking temperatures. High temperature components are arranged along the...
7222499 Closed loop air conditioning system  
A closed loop air conditioning system for an aircraft includes a compressor stage including at least one power driven compressor, for compressing working fluid, a first expansion turbine over which...
7171819 Indirect regenerative air cycle for integrated power and cooling machines  
An integrated power and cooling machine having an indirect regenerative air cooling feature may be useful for providing power and environmental control to both ground vehicles, such as tanks, and...
6939392 System and method for thermal management  
A system for the management of thermal transfer in a gas turbine engine includes a heat generating sub-system in operable communication with the engine, a fuel source to supply a fuel, a fuel...
6817575 Integrated system for providing aircraft environmental control  
The present invention relates to an integrated enviromental control system for an aircraft. The system uses bleed air from a propulsion engine to drive an air turbine which provides power to at...
6796527 Integrated air turbine driven system for providing aircraft environmental control  
The present invention relates to an integrated air turbine driving system for providing aircraft environmental control. The system has at least one air driven turbine for providing power to an...
EP1445449A2 Auxiliary power unit supplied with bypass air from fan  
A gas turbine engine assembly (10) is provided for use with an aircraft. The gas turbine engine assembly comprises a propelling gas turbine engine and an auxiliary power unit (12). The propelling...
6682016 Thermal management valve with drop-tight shutoff of return to tank  
A thermal management system for an aircraft fuel system includes a plurality of fuel pressure sources. A spool valve is fluidly connected to the pressure sources and is movable between a plurality...
Matches 1 - 9 out of 9