Hybrid third air condition pack
An airplane is provided. The airplane includes a pack. The pack includes a shaft, a compressor, a turbine coupled to the compressor via the shaft; and a heat exchanger. The compressor receives and compresses a first medium in accordance with power provided by the turbine via the shaft. The turbine receives and expands a second medium to provide the power to the compressor via the shaft. The heat exchanger is configured to cool the first medium.
1. A pack, comprising:
a shaft;
a compressor;
a turbine coupled to the compressor via the shaft; and
at least one heat exchanger,
wherein the compressor receives and compresses a first medium in accordance with power provided by the turbine via the shaft,
wherein the turbine receives and expands a second medium to provide the power to the compressor via the shaft,
wherein the at least one heat exchanger is configured to cool the first medium,
wherein the at least one heat exchanger comprises a first heat exchanger downstream of the turbine on a flow path of the second medium and a second heat exchanger upstream of the turbine on the flow path of the second medium,
wherein the second heat exchanger upstream of the turbine utilizes a third medium to heat the second medium.
2. The pack of claim 1 , wherein the first heat exchanger is configured to cool the first medium by utilizing the second medium.
3. The pack of claim 1 , wherein the second heat exchanger upstream of the turbine utilizes the second medium to cool the third medium.
4. The pack of claim 1 , wherein the first medium is fresh air and the second medium is cabin discharge air.
5. The pack of claim 1 , wherein the second medium flows to a ram circuit or overboard after exiting the pack.
6. The pack of claim 1 , wherein an environmental control system of an aircraft comprises the pack.
7. The pack of claim 6 , wherein the environmental control system further comprises at least one air conditioning pack.
8. An environmental control system, comprising:
a first air conditioning pack;
a second air conditioning pack;
a mixing circuit; and
a supplemental pack comprising a shaft, a compressor, a turbine coupled to the compressor via the shaft, and at least one heat exchanger,
wherein the compressor receives and compresses a first medium in accordance with power provided by the turbine via the shaft,
wherein the turbine receives and expands a second medium to provide the power to the compressor via the shaft,
wherein the at least one heat exchanger is configured to cool the first medium,
wherein the at least one heat exchanger comprises a first heat exchanger downstream of the turbine on a flow path of the second medium and a second heat exchanger upstream of the turbine on the flow path of the second medium,
wherein the second heat exchanger upstream of the turbine utilizes a third medium to heat the second medium.
9. The environmental control system of claim 8 , wherein the first heat exchanger is configured to cool the first medium by utilizing the second medium.