HYBRID PNEUMATIC AND ELECTRIC SECONDARY POWER INTEGRATED CABIN ENERGY SYSTEM FOR A PRESSURIZED VEHICLE

A system (100; 200) for providing compressed air to pneumatic loads in a vehicle (110) such as an aircraft, the system includes a gas turbine engine (102) having; a) an engine compressor (104) with an air inlet (106) coupled to an interior of a cabin (108) of the vehicle; and b) a load compressor (1...

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Bibliographische Detailangaben
Hauptverfasser:	BLUMER, Eric, ANGHEL, Cristian, JAN, David K
Format:	Patent
Sprache:	eng ; fre ; ger
Schlagworte:	AIR INTAKES FOR JET-PROPULSION PLANTS AIRCRAFT ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT AVIATION BLASTING COMBUSTION ENGINES CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS COSMONAUTICS ENGINE PLANTS IN GENERAL EQUIPMENT FOR FITTING IN OR TO AIRCRAFT FLYING SUITS GAS-TURBINE PLANTS HEATING HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS LIGHTING MACHINES OR ENGINES IN GENERAL MECHANICAL ENGINEERING NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAMTURBINES PARACHUTES PERFORMING OPERATIONS STEAM ENGINES TRANSPORTING WEAPONS
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Beschreibung
Zusammenfassung:	A system (100; 200) for providing compressed air to pneumatic loads in a vehicle (110) such as an aircraft, the system includes a gas turbine engine (102) having; a) an engine compressor (104) with an air inlet (106) coupled to an interior of a cabin (108) of the vehicle; and b) a load compressor (112) coupled to the gas turbine engine having a compressed air outlet coupled to one or more pneumatic loads (130) of the vehicle. One or more electrically driven cabin air compressors (CAC) (136, 138) have compressed air outlets coupled to the one or more pneumatic loads.