| 1. | The development and trends of multiple - processing textured yarn
多重加工变形丝的开发及其发展趋势 |
| 2. | Study on the machining deformation of milling because of part structure type
零件结构形式对铣削加工变形的影响研究 |
| 3. | Framework part machining deformation research based on residual stress in blank
基于毛坯残余应力框类零件铣削加工变形研究 |
| 4. | Promoting molding technique : reducing a molding deformation for workpiece to achieve precision size
2 .提升加工技术：减少工件加工变形达到精密尺寸。 |
| 5. | The data obtained lay a basis for prediction of the machining distortion caused by the residual stresses
测试数据为定量预测初始残余应力引起的加工变形奠定了基础。 |
| 6. | The machining distortion is one of the neck problems during the manufacture of the aero integrated - structure parts
因此,开展航空整体结构件加工变形研究具有重大的现实意义。 |
| 7. | The machining distortion becomes one of the neck problems in the rapid development and the effecient productin of our national defense weapons
该类零件的加工变形已成为制约国防武器装备快速研制和高效生产的最突出问题之一。 |
| 8. | The agreement of simulation and experimental results proves the validity of the model for predicting distortion law of aerospace monolithic components due to milling process
该模型对三种加工顺序的模拟结果与试验结果一致，可用于预测整体结构件的加工变形。 |
| 9. | Some machining cases are simulated by using of the fem model . the machining distortion caused by residual stress are analyzed and summarized using the simulation results
对实例进行了仿真计算,分析了残余应力引起的加工变形规律,为三维铣削变形分析奠定了基础。 |
| 10. | It is very difficult to predict the cnc machining distortion of monolithic multi - frame components in aero - industry by either theoretical analysis or experimental research , because of their complicated structure
航空多框整体结构件,由于其结构的复杂性,对于其数控加工变形预测的理论分析与试验研究均具有很高的难度。 |
