航天制造技术
航天製造技術
항천제조기술
HANGTIAN ZHIXAO JI SHU
2013年
4期
18-21
,共4页
陈金存%王庆%刘大亮%吕祥照%樊莉%刘国华
陳金存%王慶%劉大亮%呂祥照%樊莉%劉國華
진금존%왕경%류대량%려상조%번리%류국화
涡轮转子%分度角%闭环反馈%坐标测量机
渦輪轉子%分度角%閉環反饋%坐標測量機
와륜전자%분도각%폐배반궤%좌표측량궤
turbine rotor%centripetal angle%closed loop feedback%coordinator measuring machine
提出一种基于数控转台和坐标测量机的测量方法,以涡轮转子为研究对象,实现其叶片分度误差的自动数字化测量。通过建立分度角模型,进行干涉分析,并提出一种闭环反馈测量算法,从而避免测针与叶片之间发生干涉。试验结果表明,该方法的扩展不确定度为18.14″,测量周期为1.5h/件。
提齣一種基于數控轉檯和坐標測量機的測量方法,以渦輪轉子為研究對象,實現其葉片分度誤差的自動數字化測量。通過建立分度角模型,進行榦涉分析,併提齣一種閉環反饋測量算法,從而避免測針與葉片之間髮生榦涉。試驗結果錶明,該方法的擴展不確定度為18.14″,測量週期為1.5h/件。
제출일충기우수공전태화좌표측량궤적측량방법,이와륜전자위연구대상,실현기협편분도오차적자동수자화측량。통과건립분도각모형,진행간섭분석,병제출일충폐배반궤측량산법,종이피면측침여협편지간발생간섭。시험결과표명,해방법적확전불학정도위18.14″,측량주기위1.5h/건。
Based on the numerical control running-platform and coordinator measuring machine, an automatic digital method is developed to measure the centripetal angle error of turbine rotor. The mode of centripetal angle is set up, the analysis of intervene problem is put forward, and an algorithm called closed loop feedback is designed to avoid the intervene between the probe and vane. The experimental results show that the expand uncertainty is 18.14″, and the measuring cycle is 1.5 hour per piece.