发明名称 ROTORCRAFT TAIL ROTOR BLADE ASSEMBLY AND METHOD OF FORMING THE SAME
摘要 A rotor blade assembly includes a rotor blade (504) comprising an inboard end (506) and an outboard end (508). A composite yoke fitting (502) made from a composite material is attached to the rotor blade (504). The composite yoke fitting (502) includes an outboard portion (510) inserted into the inboard end (506) of the rotor blade (504), an inboard portion (512), and a flexure region (514) about which the rotor blade (504) is configured to flex. The inboard portion (512) and the flexure region (514) are outside the rotor blade (504).
申请公布号 EP3072814(A1) 申请公布日期 2016.09.28
申请号 EP20150188195 申请日期 2015.10.02
申请人 BELL HELICOPTER TEXTRON INC. 发明人 HALDEMAN, ANDREW;STAMPS, FRANK BRADLEY;SUTTON, DREW
分类号 B64C27/48;B64C27/473 主分类号 B64C27/48
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