Plural engine power producing system
AssigneeAvco Corporation
InventorsClifford Banthin, Jochen Deman
Life of this patent
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AssigneeAvco Corporation
InventorsClifford Banthin, Jochen Deman
Estimating the term…
Two gas turbine engines are interconnected through a pneumatic, mechanical, hydraulic, or power link. This power link runs from the gas producer shaft of one engine to the gas producer shaft of the other engine either delivering or absorbing power directly to or from each other. The gas producer section of a gas turbine engine comprises a compressor directly coupled to a turbine which drives the compressor and a combustor positioned between the compressor and the turbine. The unit delivers hot gases to another turbine on a separate independent shaft which is the output power shaft for the engine. Through the use of clutches, swash plates or valves, selectable operating modes are achieved. Such a two engine system has been found to exhibit superior performance over a single engine system which includes maximum power boost and better full consumption at low powers.
A system for producing power utilizing gas turbine engines comprising:
A method of operating a power producing system utilizing a primary gas turbine engine including a gas generator having an operatively associated primary drive shaft and a secondary gas turbine engine including a compressor, a combustor, a turbine, and a secondary drive shaft drivingly interconnecting the turbine and compressor comprising the step of:
A method of operating a power plant system including a primary gas turbine engine and a secondary gas turbine engine so as to achieve optimum power augmentation and also minimal fuel consumption at low power levels comprising the steps of:
A method of operating a power plant system including a primary gas turbine engine and a secondary gas turbine engine comprising the steps of:
A method of operating a power plant system including a primary gas turbine engine and a secondary gas turbine engine including a compressor and a turbine rotatably mounted on a secondary drive shaft and having a substantially lower power rating than the primary engine so as to achieve optimum power augmentation and also minimal fuel consumption at low power levels comprising the steps of:
Dependencies are inferred from the claim text.