发明名称 FAN BLADE WITH SEGMENTED FAN BLADE COVER
摘要 A lightweight fan blade for use in turbofan gas turbine engines is disclosed. The fan blade includes a metallic body having a pressure side and a suction side. The suction side of the body includes one or more cavities. A cover is then attached to the suction side of the body to cover or enclose the one or more cavities. The cover includes one or more transverse weakened areas, such as a transverse slit so that the cover separates into one or more smaller segments in the event of a foreign object damage (FOD) or fan blade out (FBO) event occurs. The smaller segments of the cover are less likely to do damage to downstream components such as the low and high-pressure compressors. A single smaller segment of the cover may allow for continued operation of the engine because the imbalance created by the event may be tolerated by the engine.
申请公布号 US2017023009(A1) 申请公布日期 2017.01.26
申请号 US201415039276 申请日期 2014.09.29
申请人 UNITED TECHNOLOGIES CORPORATION 发明人 Roche Charles H.
分类号 F04D29/38;F04D29/02;F04D29/32 主分类号 F04D29/38
代理机构 代理人
主权项 1. A fan blade comprising: a body including a pressure side and a suction side; the suction side including at least one cavity; a cover that overlays the cavity and that is adhered to the body; and the cover including at least one transverse slit that divides the cover into a plurality of segments.
地址 Farmington CT US