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US Patent 10113559 Gas turbine engine impact liner

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US Patent 12104536 Nacelle liner comprising unit cell resonator networks
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Patent abstract

A gas turbine engine impact liner is disclosed. The impact liner may include a base sheet, a plurality of stanchions extending from the base sheet, and a plurality of supports, each being operatively associated with one of the plurality of stanchions.

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US Patent 11804206 Acoustic panel for noise attenuation
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US Patent 11781485 Unit cell resonator networks for gas turbine combustor tone damping
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US Patent 11512608 Passive transpirational flow acoustically lined guide vane
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Infobox
Is a
Patent
Patent
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Patent Jurisdiction
United States Patent and Trademark Office
United States Patent and Trademark Office
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Patent Number
101135590
Date of Patent
October 30, 2018
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Patent Application Number
148504380
Date Filed
September 10, 2015
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Patent Citations Received
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US Patent 11339720 Acoustic liner with non-uniform volumetric distribution
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US Patent 11408349 Active flow control transpirational flow acoustically lined guide vane
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Patent Primary Examiner
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Craig Kim
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Edits on 23 Sep, 2022
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US Patent 11408349 Active flow control transpirational flow acoustically lined guide vane
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US Patent 11339720 Acoustic liner with non-uniform volumetric distribution
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 US Patent 10113559 Gas turbine engine impact liner

Infobox
Is a
Patent
Patent
Patent jurisdiction
United States Patent and Trademark Office
United States Patent and Trademark Office
Patent number
10113559
Date of patent
October 30, 2018
Patent application number
14850438
Date Filed
September 10, 2015
Patent primary examiner
‌
Craig Kim

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