Hybrid pneumatic and electric secondary power integrated cabin energy system for a pressurized vehicle
A system for providing compressed air to pneumatic loads in a vehicle such as an aircraft, the system includes a gas turbine engine having; a) an engine compressor with an air inlet coupled to an interior of a cabin of the vehicle; and b) a load compressor coupled to the gas turbine engine having a compressed air outlet coupled to one or more pneumatic loads of the vehicle. One or more electrically driven cabin air compressors (CAC) have compressed air outlets coupled to the one or more pneumatic loads.
1. A system for providing compressed air to pneumatic loads of a vehicle, the system comprising:
a gas turbine engine that is an auxiliary power unit (APU) and has an engine compressor that receives air from an interior of a cabin of the vehicle;
a load compressor driven by the gas turbine engine, wherein an output of the load compressor supplies compressed air to one or more pneumatic loads;
an electrical generator driven by the gas turbine engine, wherein an output of the electrical generator is coupled to an electrical power system of the vehicle; and
one or more electrically driven cabin air compressors (CACs) supplying compressed air to the one or more pneumatic loads, wherein at least one CAC receives electrical power from a main engine of the vehicle;
wherein, at least one CAC provides compressed air to start another main engine of the vehicle;
wherein, in a first mode of operation of the vehicle, the APU provides all requisite compressed air and pressure for the one or more pneumatic loads;
wherein, in a second mode of operation of the vehicle, one of the CACs augments compressed air flow still being delivered by the APU to the one or more pneumatic loads;
wherein, in a third mode of operation of the vehicle, when the APU is inoperable due to a failure, a respective CAC provides compressed air to each of the one or more pneumatic loads, and main engine generators of the vehicle provide all electric power required to drive the CACs.
2. The system of claim 1 :
wherein the vehicle is an aircraft; and
wherein the APU is positioned so that APU exhaust provides forward thrust to the aircraft.
3. The system of claim 1 , wherein a main-engine generator of the vehicle is coupled to the one or more CACs to selectively provide electrical power to the one or more CACs when there is inoperability of the APU or the electrical generator, or failure of electrical load management.
4. The system of claim 3 , wherein each main engine of the vehicle is configured to drive only one main-engine generator.