Ram air turbine powered cabin air compressor
A pressurization system for a vehicle includes an inlet for receiving a medium and a cabin air compressing device arranged in fluid communication with the inlet. The cabin air compressing device includes a shaft, a compressor connected to the shaft, a motor operably connected to the shaft and configured to drive the compressor, and a turbine connected to the shaft and also configured to drive the compressor upon receipt of the medium. A heat exchanger has a first inlet fluidly connected to the compressor outlet and a second inlet fluidly connected to the turbine outlet. The compressor inlet and the turbine inlet are fluidly connected to and are arranged in parallel relative to the inlet.
1. A pressurization system for a vehicle comprising:
an inlet for receiving a medium;
a cabin air compressing device arranged in fluid communication with the inlet, the cabin air compressing device comprising:
a shaft;
a compressor connected to the shaft, the compressor having a compressor inlet and a compressor outlet, the compressor inlet being fluidly connected to the inlet by a first conduit;
an electric motor operably connected to the shaft and configured to drive the compressor; and
a turbine connected to the shaft and also configured to drive the compressor upon receipt of the medium, the turbine having a turbine inlet and a turbine outlet, the turbine inlet being fluidly connected to the first conduit downstream from the inlet and upstream from the compressor inlet via a second conduit; and
a heat exchanger having a first inlet fluidly connected to the compressor outlet and having a second inlet fluidly connected to the turbine outlet, the first inlet of the heat exchanger being directly connected to the compressor outlet;
a bypass conduit having an inlet end fluidly connected to the second conduit at a location upstream from the turbine and an outlet end fluidly connected to the second inlet of the heat exchanger, wherein only one or more of a flow of medium output from the turbine and a flow of medium from the bypass conduit is provided to the second inlet of the heat exchanger;
wherein the compressor inlet, the turbine inlet, and the bypass conduit are fluidly connected to and are arranged in parallel relative to the inlet.
2. The pressurization system of claim 1 , wherein the medium is ram air.
3. The pressurization system of claim 1 , wherein an expanded medium is provided at the turbine outlet and a compressed medium is provided at the compressor outlet, and within the heat exchanger, heat is configured to transfer from the compressed medium to the expanded medium.
4. The pressurization system of claim 3 , wherein the compressed medium at an outlet of the heat exchanger is provided to at least one component configured to further condition the compressed medium.
5. The pressurization system of claim 4 , wherein the at least one component configured to further condition the compressed medium further comprises a load heat exchanger.
6. The pressurization system of claim 3 , wherein the expanded medium provided at an outlet of the heat exchanger is exhausted overboard.
7. The pressurization system of claim 6 , wherein the expanded medium at the outlet of the heat exchanger is provided to another cooling heat exchanger.
8. The pressurization system of claim 1 , further comprising:
a valve associated with the bypass conduit.
9. The pressurization system of claim 1 , wherein the vehicle is an aircraft.
10. A method of conditioning a load of a vehicle comprising:
compressing a first portion of a medium provided from an inlet within a compressor to create a compressed medium that is output at a compressor outlet;
expanding a second portion of the medium provided from the inlet within a turbine to create an expanded medium, wherein compressing the first portion of the medium and expanding the second portion of the medium occur simultaneously;
providing the compressed medium from the compressor outlet directly to a cooling heat exchanger;
cooling the compressed medium within the cooling heat exchanger connected to the compressor outlet via a cooling medium;
operating a valve arranged within a bypass conduit such that at least some of the second portion of the medium provided from the inlet bypasses the turbine, wherein the cooling medium provided to the cooling heat exchanger is only one or more of the expanded medium and the at least some of the second portion of the medium that bypasses the turbine.
11. The method of claim 10 , wherein the expanded medium output from the turbine is provided to the cooling heat exchanger as the cooling medium.
12. The method of claim 10 , wherein in a first mode, the compressor is driven in response to expanding the second portion of the medium within the turbine, and in a second mode, the compressor is driven by an electric motor and in response to expanding the second portion of the medium within the turbine.
13. The method of claim 10 , further comprising exhausting the cooling medium from the cooling heat exchanger overboard.
14. The method of claim 10 , further comprising providing the cooling medium from the cooling heat exchanger to another cooling heat exchanger.
15. The method of claim 10 , further comprising delivering the compressed medium provided at an outlet of the cooling heat exchanger to at least one component configured to further condition the compressed medium.
16. The method of claim 10 , further comprising further cooling the expanded medium within a load heat exchanger via another cooling medium.
17. The method of claim 10 , wherein the medium is ram air.