航空发动机涡轮工作叶片表面积碳去除工艺研究  

Study on Carbon Removal Process of Aeroengine Turbine Blade Surface Area

作　　者：曲洪业 王伟平 QU Hongye;WANG Weiping(AECC Shenyang Liming Aero Engine Co.,Ltd.,Shenyang,Liaoning,110043,China)

机构地区：[1]中国航发沈阳黎明航空发动机有限责任公司,辽宁沈阳110043

出　　处：《智能城市应用》2021年第6期80-81,共2页Smart City Application

摘　　要：文章首先分别就机械物理去除法、水剂溶液清洗法、综合分析三个方面分析航空发动机涡轮工作叶片表面积碳去除方法的可行性,进而运用磨粒流抛光和振动光饰工艺试验验证,旨在合理选择表面积碳去除工艺方法,切实提高叶片使用寿命,提高航空发动机应用质量,降低安全隐患。Firstly,this paper analyzes the feasibility of carbon removal method on the surface area of aeroengine turbine blade from three aspects:mechanical and physical removal method,aqueous solution cleaning method and comprehensive analysis,and then uses abrasive flow polishing and vibration polishing process test to verify,in order to reasonably select the carbon removal process method on the surface area and effectively improve the service life of the blade,and improve the application quality of aeroengine and reduce potential safety hazards.

关 键 词：航空发动机 涡轮工作叶片 机械物理去除法 

分 类 号：V263[航空宇航科学与技术—航空宇航制造工程]