发明名称 Propeller blade with internal stiffener
摘要 A propeller blade (100) includes a foam core (104) having a slot formed through it from a camber side (125) to a face side (127). An internal stiffener (105) is disposed through the slot and includes flanges (107) in contact with both the camber and face sides (125, 127). A structural layer (106) surrounds at least a portion of the foam core (104) and is in contact with the flanges (107) on both the camber and face sides (125, 127).
申请公布号 EP2653380(A2) 申请公布日期 2013.10.23
申请号 EP20130163997 申请日期 2013.04.16
申请人 HAMILTON SUNDSTRAND CORPORATION 发明人 NAGLE, DAVID P.;CARVALHO, PAUL A.
分类号 B64C11/26 主分类号 B64C11/26
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