发明名称 BRAIDED BLADES AND VANES HAVING DOVETAIL ROOTS
摘要 PROBLEM TO BE SOLVED: To provide a gas turbine engine composite article having a composite article airfoil extending outwardly from an article root to an article airfoil tip.SOLUTION: A core including a core airfoil attached to a core root including a core dovetail is present in the article airfoil. A continuous outer three-dimensional braided layer 14 including composite material tows are braided on the core, and the braided layer covers the entire core airfoil and the core root. The core may be an inflatable mandrel or a composite core made of a composite material. The core may include stiffeners such as an I beam or hollow rectangular cross-section box beams. A method for making such an article includes braiding a continuous outer three-dimensional braided layer including braided composite material tows braided on the core, where the braiding step includes covering the entire core airfoil and the core root with the continuous outer three-dimensional braided layer.SELECTED DRAWING: Figure 1
申请公布号 JP2016075272(A) 申请公布日期 2016.05.12
申请号 JP20150184571 申请日期 2015.09.18
申请人 GENERAL ELECTRIC CO <GE> 发明人 KRAY NICHOLAS JOSEPH;FANG XIAOMEI;CHRISTOPHER MADSEN;PRENTICE IAN FRANCIS;SULTAN SHAIR;SHIM DONG-JIN;WARD DOUGLAS DUANE
分类号 F01D5/28;D04C1/06;F01D9/02;F01D25/00;F02C7/00 主分类号 F01D5/28
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