Co-generator utilizing micro gas turbine engine
AssigneeJet Heat, Inc.
InventorsRichard W. Gordon, Richard Chute
Life of this patent
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AssigneeJet Heat, Inc.
InventorsRichard W. Gordon, Richard Chute
Estimating the term…
The present invention provides a turbo heater which utilizes a gas turbine engine and a heat exchanger assembly. The gas turbine engine is adapted to efficiently operate over a prolonged period of time and at varying power outputs without adverse or detrimental effects to the components thereof. For example, the gas turbine engine includes bearing assemblies and a fuel delivery systems which are uniquely designed for the demands of repeated cycling (i.e. starting and stopping), as well as operation at various power outputs without damage to the gas turbine engine. In addition, the use of exhaust gas from the gas turbine engine eliminates direct impingement of combustion on the heat exchanger element, thereby significantly increasing the durability and life span of the turbo heater.
A co-generator comprising:
A co-generator comprising:
Dependencies are inferred from the claim text.