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US Patent 10113444 Heated inlet guide vane

OverviewStructured DataIssuesContributorsActivity
Is a
Patent
Patent
0
Date Filed
May 11, 2015
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Date of Patent
October 30, 2018
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Patent Application Number
14708819
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Patent Citations Received
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US Patent 12116929 Bleed flow assembly for a gas turbine engine
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US Patent 11655768 High fan up speed engine
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US Patent 11767790 Object direction mechanism for turbofan engine
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US Patent 11788465 Bleed flow assembly for a gas turbine engine
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US Patent 11365647 Closed loop fan inlet vane anti icing system
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US Patent 12085019 Object direction mechanism for turbofan engine
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US Patent 11480063 Gas turbine engine with inlet pre-swirl features
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US Patent 10598191 Vane for turbomachinery, such as an aircraft turbojet or turbofan engine or an aircraft turboprop engine
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US Patent 11535386 System and method for operating a multi-engine rotorcraft for ice accretion shedding
Patent Inventor Names
Zhen Wu
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Brian C. Lund
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Jianming Huang
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Patent Jurisdiction
United States Patent and Trademark Office
United States Patent and Trademark Office
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Patent Number
10113444
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Patent Primary Examiner
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Igor Kershteyn
0

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