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18982445. GAS TURBINE ENGINE WITH THIRD STREAM (General Electric Company)

From WikiPatents

GAS TURBINE ENGINE WITH THIRD STREAM

Organization Name

General Electric Company

Inventor(s)

William Joseph Bowden of Cleves OH US

Keith Edward James Blodgett of Milford OH US

Mustafa Dindar of West Chester OH US

David Cerra of Highlands Ranch CO US

James Hamilton Grooms of Hamilton OH US

Brandon Wayne Miller of Middletown OH US

Randy M. Vondrell of Newport KY US

David Marion Ostdiek of Liberty Township OH US

Craig Williams Higgins of Liberty Township OH US

Alexander Kimberely Simpson of Cincinnati OH US

GAS TURBINE ENGINE WITH THIRD STREAM

This abstract first appeared for US patent application 18982445 titled 'GAS TURBINE ENGINE WITH THIRD STREAM

Original Abstract Submitted

A gas turbine engine includes a turbomachine having a compressor section, a combustion section, and a turbine section arranged in serial flow order. The turbomachine defines an engine inlet to an inlet duct, a fan duct inlet to a fan duct, and a core inlet to a core duct. The primary fan is driven by the turbomachine, and a secondary fan is located downstream of the primary fan within the inlet duct. One or more actuation devices operably associated with the fan duct, the one or more actuation devices actuable to increase or decrease an exit area of the fan duct.

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