Utilizing phase change material, heat pipes, and fuel cells for aircraft applications
A heat transfer system includes a fuel cell module that produces heat and water, and a thermal energy storage module that stores the heat produced by the fuel cell module. The thermal energy storage module includes a phase-change material. A conduit couples the fuel cell module to the thermal energy storage module. The conduit is oriented to channel the water produced by the fuel cell module through the thermal energy storage module.
1. A method of operating a heat transfer system for use in an aircraft galley, said method comprising:
coupling a plurality of heat pipes to a load in the aircraft galley, and to a fuel cell module configured to produce heat, wherein the load is a device or a machine;
transferring the heat to a thermal energy storage module from the fuel cell module, the thermal energy storage module including a phase-change material capable of storing the heat, wherein the heat is stored in the thermal energy storage module;
coupling the thermal energy storage module to the plurality of heat pipes to facilitate transferring the heat towards the load.
2. A method in accordance with claim 1 further comprising providing electricity to a plurality of heating elements oriented to transfer heat towards the phase-change material.
3. A method in accordance with claim 1 , wherein coupling the thermal energy storage module further comprises removably coupling the thermal energy storage module to at least one of the load and the plurality of heat pipes.
4. An aircraft comprising:
a galley comprising at least one load positioned therein;
a fuel cell module configured to produce heat and water; and
a heat transfer system comprising:
a first plurality of heat pipes coupled to said at least one load; and
a thermal energy storage module coupled to said first plurality of heat pipes to facilitate transferring the heat produced by said fuel cell module towards said at least one load, said thermal energy storage module comprising a phase-change material capable of storing the heat.
5. The aircraft in accordance with claim 4 , wherein said heat transfer system further comprises a second plurality of heat pipes are coupled between said fuel cell module and said thermal energy storage module such that heat produced by said fuel cell module is stored within the phase-change material.
6. The aircraft in accordance with claim 5 further comprising a water storage tank, wherein said thermal energy storage module is coupled to said water storage tank such that the heat stored within the phase-change material is transferred towards water stored in said water storage tank.
7. The aircraft in accordance with claim 4 , wherein said heat transfer system further comprises a conduit that couples said fuel cell module to said thermal energy storage module, said conduit configured to channel the water produced by said fuel cell module through said thermal energy storage module, thereby forming a stream of heated water, said conduit further extending from said thermal energy storage module for channeling the stream of heated water towards said at least one load.
8. The aircraft in accordance with claim 7 , wherein said at least one load configured to receive the stream of heated water comprises at least one of a sink or a coffee machine.
9. The aircraft in accordance with claim 4 , wherein said first plurality of heat pipes are coupled to said at least one load such that the heat produced by said fuel cell module is transferred towards said at least one load.
10. The aircraft in accordance with claim 4 further comprising an insulating layer substantially circumscribing said thermal energy storage module.