US Patent 10125724 Start system for gas turbine engines
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Patent abstract
A gas turbine engine includes a flow control mechanism operable to direct at least a portion of a fan airflow from a secondary flow path into a core flow path.
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Patent Number
101257240
Date of Patent
November 13, 2018
0Patent Application Number
133522960
Date Filed
January 17, 2012
0Patent Citations Received
Patent Primary Examiner
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Patent Number
101257240
Date of Patent
November 13, 2018
0Patent Application Number
133522960
Date Filed
January 17, 2012
0Patent Citations Received
Patent Primary Examiner
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US Patent 10125724 Start system for gas turbine engines
Infobox
Is a
Patent jurisdiction
Patent number
10125724
Date of patent
November 13, 2018
Patent application number
13352296
Date Filed
January 17, 2012
Patent primary examiner
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