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method of manufacturing turbine blades u0441u043eu043fu0440u044fu0433u0430u0435u043cu044bu0445 in peru

机译:秘鲁制造涡轮叶片 u0441 u043e u043f u0440 u044f u0433 u0430 u0435 u043c u044b u0445的方法

摘要

method of manufacturing turbine blades u0441u043eu043fu0440u044fu0433u0430u0435u043cu044bu0445 in peru, including u0437u0430u043bu0438u0432u043au0443 metal u043eu0431u043eu043bu043eu0447u043au043eu0432u0443u044e form which is divided in the middle of the ceramic insert, p u043eu0441u043bu0435u0434u0443u044eu0449u0443u044e stretch mold blade from u043bu0438u0442u043du0438u043au043eu0432u043eu0439 system u043eu0431u043eu043bu043eu0447u043au043eu0432u043eu0439 form, training u0441u043eu043fu0440u044fu0433u0430u0435u043cu044bu0445 blade surfaces. under pike pike halves. u043fu0430u0442u043au0438 between themselves and the final processing of the scapula, and the fact thatin order to improve the quality of blades and reduce the labour intensity of the pre build model with a blade with two opposite ends the model, after receiving a mold to produce mechanical processing the last under the technological base, then cut the tides on the longitudinal axis of grea u0432u043au0438 and receive halves casting bladethe training u0441u043eu043fu0440u044fu0433u0430u0435u043cu044bu0445 surfaces under pike are u044du043bu0435u043au0442u0440u043eu044du0440u043eu0437u0438u043eu043du043du044bu043c method, then carry out the processing of the profile of a blade and techno the logical base of cut.
机译:在秘鲁制造涡轮叶片 u0441 u043e u043f u0440 u044f u0433 u0430 u0435 u043c u044b u0445的方法,包括 u0437 u0430 u043b u0438 u0432 u0432 u043a u0443金属 u043e u0431 u043e u043b u043e u0447 u043a u043e u0432 u0443 u044e形式位于陶瓷插入物的中间,p u043e u0441 u043b u0435 u0434 u0443 u044e u0449 u0443 从 u043b u0438 u0442 u043d u0438 u043a u043e u0432 u043e u043e u0439系统 u043e u0431 u043e u043e u043b u043e u0447 u043a u043a u043e u0432 u043e u0439形式的u044e拉伸模具刀片,培训 u0441 u043e u043f u0440 u044f u0433 u0430 u0435 u043c u044b u0445刀片表面。在派克派克一半的情况下。和肩the骨的最终加工之间,以及为了提高刀片的质量并减少带有两个相对两端的刀片的预制模型的劳动强度这一事实在技​​术基础下接受模具进行机械加工的最后零件后,在沟槽的纵轴上切下潮汐 u0432 u043a u0438并接受两半铸造叶片的训练 u0441 u043e u043f u0440 u044f u0433 u0430 u0435 u043c u044b u0445派克曲面是 u044d u043b u043b u0435 u043a u0442 u0440 u043e u044d u04d u0440 u043e u0437 u0438 u043e u043e u043e u043d u043d u044b u043c方法然后对刀片的轮廓进行处理,然后对切割的逻辑基础进行技术处理。

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