Mixing bleed and ram air using an air cycle machine with two turbines
An air cycle machine for an environmental control system for an aircraft is provided. The air cycle machine includes a compressor configured to compress a first medium, a turbine configured to receive second medium, a mixing point downstream of the compressor and downstream of the turbine; and a shaft mechanically coupling the compressor and the turbine.
1. An air cycle machine for an environmental control system for an aircraft, the air cycle machine comprising:
a compressor configured to compress a first medium;
a turbine configured to receive second medium;
a shaft mechanically coupling the compressor and the turbine;
a second turbine mounted on the shaft, the second turbine being arranged downstream from and in fluid communication with an outlet of the compressor, wherein in the second turbine is configured to selectively receive at least one of the first medium and a third medium;
a mixing point downstream of the compressor and the second turbine, and downstream of the turbine, wherein the first and second medium remain fluidly separate from each other until mixed at the mixing point; and
a fan driven by a motor.
2. The air cycle machine of claim 1 , further comprising the fan on a second shaft.
3. The air cycle machine of claim 2 , wherein the fan is located at a first end of the second shaft.
4. The air cycle machine of claim 3 , wherein the third medium is cabin discharge air.
5. The air cycle machine of claim 1 , wherein the first medium comprises fresh air, and wherein the second medium comprises bleed air.
6. An air conditioning system for an aircraft comprising:
a compressor configured to compress a first medium;
a turbine configured to receive a second medium;
a shaft mechanically coupling the compressor and the turbine;
a second turbine mounted on the shaft the second, turbine being arranged downstream from and in fluid communication with an outlet of the compressor, wherein the second turbine is configured to selectively receive at least one of the first medium and a third medium;
a mixing point downstream of the compressor and the second turbine, and downstream of the turbine, wherein the first and second medium remain fluidly separate from each other until mixed at the mixing point; and
a fan mounted to the shaft and driven by at least one of the turbine and the second turbine.
7. The air conditioning system of claim 6 , wherein the fan is located at a first end of the shaft.
8. The air conditioning system of claim 6 , wherein the third medium is cabin discharge air.
9. The air conditioning system of claim 6 , wherein the first medium comprises fresh air, and wherein the second medium comprises bleed air.