发明名称 Composite rotor having recessed radial splines for high torque applications
摘要 A composite rotor is provided having a main body portion and a plurality of circumferentially spaced blades extending radially from the body portion. The rotor also includes a plurality of recessed radial splines in the body portion thereof. The splines are adapted for engaging a coupler, such as a gearwheel, and transmitting torque thereto. The amount of shear area provided by the recessed splines for transmitting torque from the rotor to the coupler is significantly increased over conventional designs because the shear area includes not only area in the inter-laminar plane, but also in the cross-laminar plane.
申请公布号 US6595751(B1) 申请公布日期 2003.07.22
申请号 US20000590548 申请日期 2000.06.08
申请人 THE BOEING COMPANY 发明人 STRAUB ANDREAS;PETERVARY MIKLOS;HOOD WILLIAM
分类号 F01D5/02;F01D5/06;F01D5/28;F01D5/34;(IPC1-7):F04D29/00 主分类号 F01D5/02
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