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US Patent 10173780 Aircraft liquid heat exchanger anti-icing system
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Patent
Date Filed
January 26, 2016
Date of Patent
January 8, 2019
Patent Application Number
15006872
Patent Citations Received
US Patent 12116929 Bleed flow assembly for a gas turbine engine
0
US Patent 11427330 System and method for cooling a leading edge of a high speed vehicle
US Patent 12066254 Two-phase thermal protection of the hypersonic leading edge
0
US Patent 12085016 Nacelle inlet structures, engine assemblies and vehicles including the same, and related methods
0
US Patent 11577817 System and method for cooling a leading edge of a high speed vehicle
US Patent 11260953 System and method for cooling a leading edge of a high speed vehicle
US Patent 11260976 System for reducing thermal stresses in a leading edge of a high speed vehicle
US Patent 11267551 System and method for cooling a leading edge of a high speed vehicle
US Patent 11745847 System and method for cooling a leading edge of a high speed vehicle
US Patent 11352120 System and method for cooling a leading edge of a high speed vehicle
•••
Patent Jurisdiction
United States Patent and Trademark Office
Patent Number
10173780
Patent Primary Examiner
Richard R. Green
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