English translation for "航空发动机叶片"

blade of aviation engine

Related Translations:

定型叶片:  profile blade

标记叶片:  index blade

叶片螺距:  blade pitch

三维叶片:  three dimensional blade

支撑叶片:  support blade

叶片工作面:  front side of vaneleading face of vaneleading side of bladeleading-out side of blade

螺旋叶片:  auger flighthelical bladehelicallobe

旋流叶片:  intervaneswirl vaneswirler vane

叶片深度:  depth of blade

尖头叶片:  sharp-nosed blade

Example Sentences:

	1.	The blade inner channel cooling is very important in the design of turbine blade , with the ever - increasing inlet temperature , the new heat transfer enhancement structures of higher performance are demanded . because of the complexity of the flow and heat transfer of the blade inner channel cooling , the numerical modulation is superior to the experiment . this thesis studied the blade inner channel cooling with the method of numerical modulation 叶片内部通道冷却在航空发动机叶片的设计中占有重要的位置，航空发动机进口温度的增高对其提出了更高的要求。由于叶片内部通道冷却的流动与传热的复杂性，数值模拟较实验的研究方法有其优越性，本文利用数值模拟的方法对叶片内部通道冷却进行了研究。
	2.	Directionally solidified refractory metal matrix eutectic in - suit composites possess excellent mechanical and physical properties such as low density , high enduring temperatures , good room - temperature fracture - toughness and high elevated - temperature strength , therefore are expected to be used as a new type of ultra - high temperature structural materials 定向凝固难熔金属基共晶自生复合材料由于具有密度低、承温能力高、室温断裂韧性好、高温强度高和高温持久寿命长等性能优势，有望成为新一代航空发动机叶片用超高温结构材料。
	3.	At first , the model about information requirement in manufacturability evaluation is set up . based on the feature technology and object - oriented mechanism , the manufacture - oriented part model with three levels ( namely part , feature and geometry ) and the resource model is build ; secondly , the evaluation guidelines on the basis of evaluation strategy of fining with levels is constituted ; thirdly , an evaluation method according the evaluation guidelines is put forward , which is the rule - based and fuzzy evaluation - based method associated with resources . fourthly , a manufacturing - oriented evaluation system for machining blade part is built 以特征技术为基础，面向对象的编程机制为手段，建立了面向制造的三层次(即零件层、特征层、几何层)零件模型，同时进行了面向制造的资源建模；第二，采用分层逐步细化的评价策略，建立可制造性评价指标；第三，以评价指标为基础，采用基于约束规则和模糊综合评判的加工可行性评价方法；第四，以ug为开发平台， vc6 . 0为编程工具，航空发动机叶片为应用对象，初步构建了面向制造的叶片类零件的可制造性评价系统。

Similar Words：

"航空发动机工业" English translation, "航空发动机燃料" English translation, "航空发动机润滑剂" English translation, "航空发动机维修" English translation, "航空发动机压气发动机" English translation, "航空发动机噪音研究设备" English translation, "航空发动机装配工" English translation, "航空发烟发光标志弹" English translation, "航空发展史" English translation, "航空发展中心" English translation