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dc.contributor.authorMillsaps, Knox T.
dc.date.accessioned2012-07-11T15:55:09Z
dc.date.available2012-07-11T15:55:09Z
dc.date.issued2010-02-16
dc.identifier.other7661271
dc.identifier.urihttp://hdl.handle.net/10945/7254
dc.descriptionPatenten_US
dc.description.abstractAn integrated electric gas turbine comprises a compressor that includes a plurality of airfoils. An electric motor is arranged to drive the compressor, and a combustor is arranged to receive compressed air from the compressor and further arranged to receive a fuel input. A turbine is arranged to receive the combustion gases from the combustor. A generator is integrated with the turbine and arranged to provide a power output. A controller is connected between the generator and the electric motor and arranged to direct a portion of the power output from the generator to the electric motor.en_US
dc.publisherThe United States of America as represented by the Secretary of the Navy, Washington, DC (US)en_US
dc.rightsThis publication is a work of the U.S. Government as defined in Title 17, United States Code, Section 101. Copyright protection is not available for this work in the United States.en_US
dc.titleIntegrated Electric Gas Turbineen_US
dc.typePatenten_US
dc.contributor.corporateMonterey, California, Naval Postgraduate School
dc.contributor.corporateMonterey, California : Naval Postgraduate School


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