发明名称 STIFF-IN-PLANE GIMBALED TILTROTOR HUB
摘要 <p>A rotor-hub for a rotary-wing aircraft is disclosed. The rotor-hub comprises a yoke comprising a plurality of yoke arms and a plurality of yoke straps, wherein the yoke arms are joined together by the yoke straps, and wherein a plurality of inner walls of the yoke define a central void space. A pitch horn is movably connected to the yoke and a portion of the pitch horn is located within the central void space. A connecting shell is fixedly attached to the yoke.</p>
申请公布号 EP1971521(B1) 申请公布日期 2012.11.07
申请号 EP20060849210 申请日期 2006.01.13
申请人 BELL HELICOPTER TEXTRON INC. 发明人 STAMPS, FRANK, B.;RAUBER, RICHARD, E.;CAMPBELL, THOMAS, C.;BRASWELL, JAMES, L., JR.;POPELKA, DAVID, A.;STANNEY, KEITH;SOUTHERLAND, MICHAEL, J.;TISDALE, PATRICK, R.;WASIKOWSKI, MARK
分类号 B64C27/48 主分类号 B64C27/48
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