HARVESTING ENERGY FROM COMPOSITE AIRCRAFT ENGINE COMPONENTS

The present disclosure is directed to an engine component for a gas turbine engine, the engine component including a substrate that includes a composite fiber and defines a surface. An energy harvesting fiber is positioned within the substrate. La présente invention concerne un élément de moteur des...

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Bibliographic Details
Main Authors KRAY, Nicholas, Joseph, SELLINGER, Aaron, Todd
Format Patent
LanguageEnglish
French
Published 01.02.2018
Subjects
BLASTING
ELECTRICITY
HEATING
LIGHTING
MACHINES OR ENGINES FOR LIQUIDS
MECHANICAL ENGINEERING
MECHANICAL-POWER PRODUCING DEVICES OR MECHANISMS, NOTOTHERWISE PROVIDED FOR OR USING ENERGY SOURCES NOT OTHERWISEPROVIDED FOR
OR A REACTIVE PROPULSIVE THRUST, NOT OTHERWISE PROVIDED FOR
PRODUCING MECHANICAL POWER
SPRING, WEIGHT, INERTIA OR LIKE MOTORS
WEAPONS
WIND, SPRING WEIGHT AND MISCELLANEOUS MOTORS
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Summary:The present disclosure is directed to an engine component for a gas turbine engine, the engine component including a substrate that includes a composite fiber and defines a surface. An energy harvesting fiber is positioned within the substrate. La présente invention concerne un élément de moteur destiné à un moteur de turbine à gaz, le composant de moteur comprenant un substrat qui comprend une fibre composite et délimite une surface. Une fibre de récupération d'énergie est positionnée à l'intérieur du substrat.
Bibliography:Application Number: WO2017US38754