发明名称 Turbomachine Blade Assembly
摘要 Embodiments of the present disclosure include a system comprising a turbomachine blade assembly having a blade portion, a shank portion, and a mounting portion, wherein the blade portion, the shank portion, and the mounting portion comprise a first plurality of plies extending from a tip of the airfoil to a base of the dovetail.
申请公布号 US2014301850(A1) 申请公布日期 2014.10.09
申请号 US201313856303 申请日期 2013.04.03
申请人 GENERAL ELECTRIC COMPANY 发明人 Garcia Crespo Andres Jose
分类号 F01D11/00;F01D5/30;F01D5/28 主分类号 F01D11/00
代理机构 代理人
主权项 1. A system, comprising: a turbomachine blade assembly, comprising: a blade portion;a shank portion; anda mounting portion,wherein the blade portion, the shank portion, and the mounting portion comprise a first plurality of plies extending from a tip of the blade portion to a base of the mounting portion.
地址 Schenectady NY US