Aircraft enviromental control system with series bleed air turbines
An environmental control system of an aircraft includes a ram air circuit including a ram air shell having at least one heat exchanger positioned therein, at least one dehumidification system arranged in fluid communication with the ram air circuit, a compressing device arranged in fluid communication with the ram air circuit and the dehumidification system, and an expansion device separate from the compressing device and arranged in fluid communication with the ram air circuit and the at least one dehumidification system. The environmental control system receives a flow of a first medium and a flow of a second medium. The environmental control system is operable in a plurality of modes and in a first mode, a flow of the first medium is provided to the compressing device and the expansion device in series.
1. An environmental control system of an aircraft comprising:
a ram air circuit including a ram air shell having at least one heat exchanger positioned therein;
at least one dehumidification system arranged in fluid communication with the ram air circuit;
a compressing device arranged in fluid communication with the ram air circuit and the dehumidification system, the compressing device including a compressor and at least one turbine coupled via a first shaft, the at least one turbine including a first turbine and a second turbine; and
an expansion device separate from the compressing device and arranged in fluid communication with the ram air circuit and the at least one dehumidification system, the expansion device having another turbine mounted to a second shaft, the second shaft being offset from the first shaft, the environmental control system receiving a flow of a first medium and a flow of a second medium;
wherein the environmental control system is operable in a plurality of modes and in a first mode, a flow of the first medium is provided to the first turbine of the compressing device and the another turbine of the expansion device in series and a flow of the second medium is provided to the second turbine of the compressing device, and in a second mode, the flow of first medium bypasses the another turbine.
2. The environmental control system of claim 1 , wherein the environmental control system is operable in the first mode when the aircraft is on the ground.
3. The environmental control system of claim 1 , wherein in a second third mode, the flow of the first medium output from the expansion device is provided to a compressor of compressing device.
4. The environmental control system of claim 1 , wherein the environmental control system is operable in the third second mode when the aircraft is in flight.
5. The environmental control system of claim 1 , wherein in a fourth mode, the flow of the first medium bypasses the expansion device and is released into the ram air circuit.
6. The environmental control system of claim 5 , wherein when the environmental control system is in the fourth mode, only the second medium is provided to a volume of the aircraft.
7. The environmental control system of claim 1 , wherein the expansion device includes the another turbine and a fan operably coupled by the second shaft.
8. The environmental control system of claim 1 , wherein the expansion device is operable to draw ram air through the ram air circuit.
9. The environmental control system of claim 1 , wherein the compression device further includes:
a compressor configured to receive energy from the first medium being expanded across the turbine, the compressor being configured to compress the second medium, the at least one turbine is configured to provide energy to drive the compressor by expanding a first medium.
10. The environmental control system of claim 9 , wherein the first medium is bleed air.
11. The environmental control system of claim 10 , wherein the bleed air is drawn from at least one of an engine and an auxiliary power unit.
12. The environmental control system of claim 9 , wherein the second medium is fresh air.
13. The environmental control system of claim 10 , wherein the at least one turbine of the compression device further includes a power turbine configured to provide energy to the compressor by expanding a third medium.