发明名称 Low drag rotor system
摘要 A rotor assembly includes a rotor hub rotatable about a central axis including a plurality of rotor hub arms and blade yokes, each blade yoke including yoke arms located at opposing lateral sides of a corresponding one of the rotor hub arms to which the rotor hub arm is operably connected. The rotor assembly further includes blade retention bearings, each blade retention bearing being a single-element bearing disposed at a corresponding one of the rotor hub arms and which is supportive of a corresponding one of the blade yokes. Rotor blades are secured to corresponding ones of the blade yokes.
申请公布号 US9415866(B2) 申请公布日期 2016.08.16
申请号 US201313856062 申请日期 2013.04.03
申请人 SIKORSKY AIRCRAFT CORPORATION 发明人 D'Anna Frank P.
分类号 B64C27/35;B64C7/00;B64C27/04;B64C27/48 主分类号 B64C27/35
代理机构 Cantor Colburn LLP 代理人 Cantor Colburn LLP
主权项 1. A rotor assembly comprising: a rotor hub rotatable about a central axis including a plurality of rotor hub arms integrally formed with and extending radially outwardly from the rotor hub, the plurality of rotor hub arms including: a plurality of rotor hub upper arms; anda plurality of rotor hub lower arms, the rotor hub lower arms offset from the rotor hub upper arms along the central axis and defining an arm opening therebetween; blade yokes, each blade yoke comprising: yoke arms located at opposing lateral sides of a corresponding one of the rotor hub arms to which the rotor hub arm is operably connected, each of the yoke arms includes a cantilevered end; anda bearing outer race secured to the cantilevered end of corresponding one of the yoke arms through a mechanical fastener and extending through the arm opening, the blade yoke in a noncontact arrangement with the rotor hub, wherein the mechanical fastener extends along an axis substantially parallel to the central axis; blade retention bearings, each blade retention bearing being a single-element bearing disposed at a corresponding one of the rotor hub arms and which is supportive of a corresponding one of the blade yokes and including: a bearing inner race extending between and secured to one of the rotor hub upper arms and the corresponding rotor hub lower arm radially outboard of the bearing outer race; anda bearing element disposed between the bearing outer race and the bearing inner race; rotor blades, each rotor blade being secured to a corresponding one of the blade yokes; wherein an entirety of each blade retention bearing is located radially inboard of an outer diameter of their respective rotor hub arms.
地址 Stratford CT US
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