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    • 2. 发明申请
    • COMPOSITE BLADE ROOT STUCTURE
    • 复合叶片根结构
    • WO2009111568A1
    • 2009-09-11
    • PCT/US2009/036040
    • 2009-03-04
    • KAREM AIRCRAFT, INC.GUPTA, NeilKAREM, Abe
    • GUPTA, NeilKAREM, Abe
    • F03B3/12
    • B64C11/20B64C27/473B64C2027/4736Y02T50/66
    • A spar of a rotor blade having moderate depth transitions to a relatively much deeper shank over a relatively short distance. This rapid transition enables a low-weight blade root that is structurally efficient, offers a high moment capability, and enables high Mach number axial flow. A transition could advantageously reduce section depth by at least 15%, 20%, 30%, or even 40% over at most 5%, 6%, 10%, or 12% of a total length of the rotor blade. Such a transition could advantageously be accomplished using a cuff, which has interfaces with each of the spar and the shank. The rotor blade shank has a generally circular cross-section which allows for a rotary attachment to a hub, where the attachment may advantageously comprise a mechanical or elastomeric bearing. Preferred embodiments have a spar with a generally rectangular cross-section.
    • 转子叶片的翼梁在相对较短的距离上具有适度的深度转变到相对较深的柄部。 这种快速过渡使得能够在结构上有效的低重量叶片根部提供高力矩能力,并实现高马赫数轴向流动。 在转子叶片的总长度的最多5%,6%,10%或12%的情况下,转变可以有利地减少截面深度至少15%,20%,30%,甚至40%。 这样的转变可以有利地使用具有与每个翼梁和柄部的接合的袖带来实现。 转子叶片柄具有大致圆形的横截面,其允许旋转连接到轮毂,其中附接可以有利地包括机械或弹性轴承。 优选实施例具有大致矩形横截面的翼梁。