Little allowance forging process of a new TMC -2 composite blade is studied.
研究了新型TMC - 2复合材料的叶片小余量锻造工艺。
The design of structure and dynamics of a rotor blade is based on its section characteristic of composite blade.
复合材料桨叶剖面特性是旋翼桨叶设计的最基本原始参数，也是桨叶结构设计、动力学设计和结构分析的基础。
The composite blade as recited in claim 19 wherein the bundled core of filaments is twisted along its longitudinal axis.
综合叶片作为背诵，在索赔19，其中捆绑核心长丝是扭曲沿其长轴。
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