Closed-loop cooling system for a hydrogen/oxygen based combustor
AssigneeLockheed Martin Corporation
InventorsJeffrey S. Goldmeer, William H. Girodet
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AssigneeLockheed Martin Corporation
InventorsJeffrey S. Goldmeer, William H. Girodet
Estimating the term…
A closed-loop cooling system is provided for a hydrogen/oxygen based combustor. A combustion reaction between hydrogen and oxygen in the combustor produces steam. The steam is used to generate work from a turbine shaft, which is used to drive a propulsion system for the underwater vessel. After the steam passes through the turbine, the steam is cooled back to liquid water by a condenser that uses a seawater cooling loop to cool the steam into cold water. The cold water is then injected into the combustor, and pumped into passages along the walls of the combustor, thus absorbing the heat. The cold water absorbs this heat until it becomes hot water or steam, which is then injected into the combustor with the hydrogen and oxygen to act as a diluent, thus reducing the reaction temperature of the hydrogen/oxygen combustion reaction. The reaction produces more steam, and the cycle repeats.
An apparatus for cooling a hydrogen/oxygen based combustor for an underwater vessel, said apparatus comprising:
An apparatus for cooling a hydrogen/oxygen based combustor for an underwater vessel, said apparatus comprising:
A closed-loop cooling method for cooling a hydrogen/oxygen based combustor for an underwater vessel, the method comprising:
A closed-loop cooling method for cooling a hydrogen/oxygen based combustor for an underwater vessel, the method comprising:
An apparatus for cooling a hydrogen/oxygen based combustor for an underwater vessel, said apparatus comprising:
A closed-loop cooling method for cooling a hydrogen/oxygen based combustor for an underwater vessel, the method comprising:
Dependencies are inferred from the claim text.