US Patent 10329925 Vibration-damped composite airfoils and manufacture methods
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Patent abstract
A turbine engine component (100) comprises a fiber structure (125, 126) forming at least a portion of an airfoil (102). A matrix (128) embeds the fiber structure. A carbon nanotube filler (130) is in the matrix.
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Patent Inventor Names
Christopher M. Quinn0
Sreenivasa R. Voleti0
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Patent Number
103299250
Date of Patent
June 25, 2019
0Patent Application Number
149030760
Date Filed
June 26, 2014
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US Patent 10329925 Vibration-damped composite airfoils and manufacture methods
Infobox
Is a
Patent applicant
Patent jurisdiction
Patent number
10329925
Date of patent
June 25, 2019
Patent application number
14903076
Date Filed
June 26, 2014
Patent primary examiner
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