Mixing ram and bleed air in a dual entry turbine system
A system is provided. The system includes a first medium at a first pressure, a second medium at a second pressure, and a medium conditioning sub-system. The medium conditioning sub-system includes a compressor, a first heat exchanger, a second heat exchanger, and a turbine. The turbine receives the first medium and the second medium.
1. A pack of an aircraft environmental control system of, comprising:
a first medium at a first pressure;
a second medium at a second pressure;
a pressurized volume;
a third medium sourced from the pressurized volume; and
a medium conditioning sub-system comprising:
a compressor,
a ram air circuit including a first heat exchanger and a second heat exchanger,
a turbine configured to receive the first medium and the second medium; and
a third heat exchanger arranged upstream from the first heat exchanger relative to a flow of the first medium output from the compressor, wherein heat is transferred from the first medium to the third medium within the third heat exchanger.
2. The environmental control system of claim 1 , wherein the first medium comprises fresh air, and
wherein the compressor compresses the first medium.
3. The environmental control system of claim 2 , wherein the first heat exchanger is downstream of the compressor.
4. The environmental control system of claim 3 , wherein the first heat exchanger is upstream of the turbine.
5. The environmental control system of claim 1 , wherein the second medium comprises pressured air from a pressurized volume.
6. The environmental control system of claim 5 , wherein the second heat exchanger is configured to receive the second medium.
7. The environmental control system of claim 6 , wherein the second heat exchanger is upstream of the turbine.
8. The environmental control system of claim 1 , wherein the turbine has a first nozzle and a second nozzle,
wherein the first nozzle is configured to accelerate the first medium for entry into an impeller of the turbine, and
wherein the second nozzle is configured to accelerate the second medium for entry into the impeller of the turbine.
9. The environmental control system of claim 8 , wherein the second nozzle comprises vanes variable in area.
10. The environmental control system of claim 9 , wherein the turbine is configured with a first path configured to receive the first medium from the first nozzle, and
wherein the turbine is configured with a second path configured to receive the second medium from the second nozzle.
11. The environmental control system of claim 10 , wherein the first medium and the second medium mix at an exit of the turbine.
12. The environmental control system of claim 1 , further comprising:
a second turbine downstream of the third heat exchanger configured to receive the third medium.
13. The environmental control system of claim 1 , wherein the compressor has a variable area diffuser.
14. The environmental control system of claim 1 , wherein the compressor comprises a mixed flow compressor.
15. The environmental control system of claim 1 , wherein the compressor rotor has high backsweep.
16. The environmental control system of claim 1 , wherein the compressor has a low solidity diffuser.