Environmental control system utilizing a motor assist and an enhanced compressor
A system includes a first inlet providing a medium from a source and a compressing device arranged in communication with the first inlet. The compressing device includes a compressor configured to receive the medium and a turbine located downstream from the compressor. The system additionally includes at least one heat exchanger and an electric motor operably coupled to the compressor. The system is powered by mechanical power from the medium and by electrical power from the electric motor. The input power of the electric motor is less than or equal to 0.5 kilowatts per pounds per minute of medium compressed.
1. A system, comprising:
a first inlet for providing a medium from a source;
a compressing device in communication with the first inlet, wherein the compressing device comprises:
a compressor configured to receive the medium, and
a turbine downstream of the compressor;
at least one heat exchanger, and
an electric motor connected to the compressor via a shaft, the electric motor being operable to drive the compressor;
wherein the system is configured to be powered by mechanical power from the medium and by electrical power from the electric motor, and
wherein the electric motor has a motor input power of less than 0.5 kilowatts per pound per minute of medium compressed by the compressor.
2. The system of claim 1 , comprising:
an electric system having at least one engine driven generator.
3. The system of claim 2 , comprising:
an auxiliary power unit having a load compressor to start an engine or to drive the system.
4. The system of claim 1 , wherein the compressor has a rotor backsweep between 0° and 90° with a shroud bleed and a low solidity diffuser.
5. The system of claim 1 , wherein the compressing device comprises a diffuser on an exit path of a rotor of the compressor.
6. The system of claim 5 , wherein the diffuser is a low solidity diffuser.
7. The system of claim 5 , wherein the diffuser is a variable vaned diffuser.
8. The system of claim 5 , wherein the diffuser is a curved channel diffuser.
9. The system of claim 1 , wherein the compressor is a mixed flow compressor.
10. The system of claim 1 , wherein the medium output from the system is configured to be delivered to a chamber and has a pressure equal to a pressure of the chamber.
11. The system of claim 1 , wherein the system is a hybrid electric and bleed system.
12. The system of claim 1 , wherein the at least one heat exchanger comprises a first heat exchanger and a second heat exchanger, and
wherein the second heat exchanger is down-stream of the compressor.
13. The system of claim 1 , wherein the medium includes bleed air received by the system from an engine or an auxiliary power unit.
14. The system of claim 1 , wherein the system is part of an environmental control system of an airplane.
15. A system, comprising:
a first inlet for providing a medium from a source;
a compressing device in communication with the first inlet, wherein the compressing device comprises:
a compressor configured to receive the medium, wherein the compressor has a rotor backsweep between 0° and 90° with a shroud bleed and a low solidity diffuser, and
a turbine downstream of the compressor;
at least one heat exchanger, and
an electric motor configured to operate the compressor;
wherein the system is configured to be powered by mechanical power from the medium and by electrical power from the electric motor, and
wherein the motor input power of the electric motor is less than 0.5 kilowatts per pound per minute of medium compressed.