发明名称 ROOT PADS FOR COMPOSITE BLADES
摘要 A composite filament reinforced rotor blade having a splayed root construction is provided with a pad on each side of the blade in the area of transition between the airfoil portion and root portion of the blade. The pad is designed to be wedged between the blade and its corresponding disc slot during rotor operation and to transmit blade centrifugal forces from the blade to the disc in such a manner so as to produce a compressive force on the surface of the blade in the transition area for preventing delamination of the filaments within the blade. In one embodiment of this invention, the pads on either side of the blade are connected by a flexible band closely fitting along the underside of the root portion to prevent metallic wedge-shaped inserts, which are sometimes used in the root, from being expelled therefrom.
申请公布号 CA959034(A) 申请公布日期 1974.12.10
申请号 CA19720149317 申请日期 1972.08.09
申请人 UNITED AIRCRAFT CORPORATION 发明人 WALSH, THOMAS C.;STREET, DAVID
分类号 F01D5/28 主分类号 F01D5/28
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