SCHWENKSTEIFE KARDANISCHE KIPPROTORNABE

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 pitc...

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Bibliographische Detailangaben
Hauptverfasser: STAMPS, FRANK B, BRASWELL, JAMES L. JR, POPELKA, DAVID A, CAMPBELL, THOMAS C, RAUBER, RICHARD E, TISDALE, PATRICK R, STANNEY, KEITH, SOUTHERLAND, MICHAEL J, WASIKOWSKI, MARK
Format: Patent
Sprache:ger
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Zusammenfassung: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.