US Patent 10113561 Secondary flow baffle for turbomachinery
Patent 10113561 was granted and assigned to Pratt & Whitney on October, 2018 by the United States Patent and Trademark Office.
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Patent abstract
A stage of a fan for a gas turbine engine may include a rotor blade and a stator vane disposed aft of the rotor blade. A baffle may be coupled to the stator vane. The baffle may define a secondary airflow path from aft of the stator vane to forward of the rotor blade. The baffle may further define the secondary airflow path from aft of the stator vane to forward of the stator vane.
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Patent Inventor Names
Jordan T. Wall0
Victor G. Filipenco0
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Is a
Current Assignee
Patent Jurisdiction
Patent Number
101135610
Date of Patent
October 30, 2018
0Patent Application Number
151535780
Date Filed
May 12, 2016
0Patent Citations Received
Patent Primary Examiner
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Patent Citations Received
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Patent Citations Received
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US Patent 10113561 Secondary flow baffle for turbomachinery
Infobox
Is a
Current assignee
Patent jurisdiction
Patent number
10113561
Date of patent
October 30, 2018
Patent application number
15153578
Date Filed
May 12, 2016
Patent primary examiner
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