摘要
首先分析了加工时零件表面热量场和加工参数、余量场之间的关系；利用数字扫描及滤波的方法建立起复杂形面零件的数学模型；以此为基础，在加工过程中，对零件的几何质量和表面层质量进行了综合控制。研究表明，该方法是提高飞行器发动机中高负载复杂形状薄壁零件可靠性和寿命的有效新途径。
The paper analyses the relation of the heat field on the parts, surface processing parameter and allowance field, then constructs the mathematical model for parts complicated shape with digital scanning and filter. Based on this, the synthetical control of the geometric and the surface quality of parts is established in the processing course, This is the new effective method of improving the reliability and service life of the thin-wall parts of complicated shap under high-load in aircraft engine.
出处
《国防科技大学学报》
EI
CAS
CSCD
北大核心
1996年第3期59-62,共4页
Journal of National University of Defense Technology
