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. 本公开涉及用于燃气涡轮发动机的发动机部件,该发动机部件包括基体,该基体包括复合纤维并限定了表面。能量收集纤维定...

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Bibliographische Detailangaben
Hauptverfasser: KRAY NICHOLAS JOSEPH, SELLINGER AARON TODD
Format: Patent
Sprache:chi ; eng
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Zusammenfassung: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. 本公开涉及用于燃气涡轮发动机的发动机部件,该发动机部件包括基体,该基体包括复合纤维并限定了表面。能量收集纤维定位在基体内。