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

=GAS TURBINE ENGINE WITH THIRD STREAM=


==Organization Name==

[[:Category:General Electric Company|General Electric Company]]


[[Category:General Electric Company]]

==Inventor(s)==

[[:Category:William Joseph Bowden of Cleves OH US|William Joseph Bowden of Cleves OH US]][[Category:William Joseph Bowden of Cleves OH US]]

[[:Category:Keith Edward James Blodgett of Milford OH US|Keith Edward James Blodgett of Milford OH US]][[Category:Keith Edward James Blodgett of Milford OH US]]

[[:Category:Mustafa Dindar of West Chester OH US|Mustafa Dindar of West Chester OH US]][[Category:Mustafa Dindar of West Chester OH US]]

[[:Category:David Cerra of Highlands Ranch CO US|David Cerra of Highlands Ranch CO US]][[Category:David Cerra of Highlands Ranch CO US]]

[[:Category:James Hamilton Grooms of Hamilton OH US|James Hamilton Grooms of Hamilton OH US]][[Category:James Hamilton Grooms of Hamilton OH US]]

[[:Category:Brandon Wayne Miller of Middletown OH US|Brandon Wayne Miller of Middletown OH US]][[Category:Brandon Wayne Miller of Middletown OH US]]

[[:Category:Randy M. Vondrell of Newport KY US|Randy M. Vondrell of Newport KY US]][[Category:Randy M. Vondrell of Newport KY US]]

[[:Category:David Marion Ostdiek of Liberty Township OH US|David Marion Ostdiek of Liberty Township OH US]][[Category:David Marion Ostdiek of Liberty Township OH US]]

[[:Category:Craig Williams Higgins of Liberty Township OH US|Craig Williams Higgins of Liberty Township OH US]][[Category:Craig Williams Higgins of Liberty Township OH US]]

[[:Category:Alexander Kimberely Simpson of Cincinnati OH US|Alexander Kimberely Simpson of Cincinnati OH US]][[Category: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.



[[Category:F02K3/065]]
[[Category:F02C3/06]]
[[Category:CPC_F02K3/065]]