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US Patent 10539025 Airfoil assembly with leading edge element

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US Patent 12123324 Engine airfoil metal edge
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US Patent 12091768 Method of depositing a metal layer on a component
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US Patent 12085019 Object direction mechanism for turbofan engine
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Patent abstract

An airfoil assembly including a composite body having a mounting edge and a trailing edge which is secured to a leading edge element defining a 3-D leading edge geometry with both chord and camber variation.

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Dong-Jin Shim0
Nicholas Joseph Kray0
Pranav Dhoj Shah0
Trevor Howard Wood0
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US Patent 11767607 Method of depositing a metal layer on a component
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US Patent 11346320 Wind turbine blade leading edge pairing
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US Patent 11047238 Leading edge profile of vanes
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US Patent 10934851 Leading edge shield
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 US Patent 10539025 Airfoil assembly with leading edge element

Infobox
Is a
Patent
Patent
Patent jurisdiction
United States Patent and Trademark Office
United States Patent and Trademark Office
Patent number
10539025
Date of patent
January 21, 2020
Patent application number
15040582
Date Filed
February 10, 2016
Patent primary examiner
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Justin D Seabe

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