航空精密制造技术
航空精密製造技術
항공정밀제조기술
AVIATION PRECISION MANUFACTURING TECHNOLOGY
2013年
6期
37-40
,共4页
曾婧雯%任军学%尹佳%郑小伟
曾婧雯%任軍學%尹佳%鄭小偉
증청문%임군학%윤가%정소위
TC18钛合金%切削力%刀具几何参数优化
TC18鈦閤金%切削力%刀具幾何參數優化
TC18태합금%절삭력%도구궤하삼수우화
TC18 titanium alloy%cutting force%tool geometry optimization
用正交实验法研究了硬质合金立铣刀铣削TC18钛合金过程中不同刀具结构参数对切削力的影响规律,并以最小切削力为优化目标,对刀具结构参数进行了优选。结果表明:当刀具参数选择前角为10°,容屑槽角为40°,螺旋角为45°,端齿前角为8°,不等分角为5°时,可获得较低的切削力,此时X向切削力为25.17N,Y向切削力为9.95N,为进一步优化TC18钛合金的铣削参数提供了依据。
用正交實驗法研究瞭硬質閤金立鐉刀鐉削TC18鈦閤金過程中不同刀具結構參數對切削力的影響規律,併以最小切削力為優化目標,對刀具結構參數進行瞭優選。結果錶明:噹刀具參數選擇前角為10°,容屑槽角為40°,螺鏇角為45°,耑齒前角為8°,不等分角為5°時,可穫得較低的切削力,此時X嚮切削力為25.17N,Y嚮切削力為9.95N,為進一步優化TC18鈦閤金的鐉削參數提供瞭依據。
용정교실험법연구료경질합금립선도선삭TC18태합금과정중불동도구결구삼수대절삭력적영향규률,병이최소절삭력위우화목표,대도구결구삼수진행료우선。결과표명:당도구삼수선택전각위10°,용설조각위40°,라선각위45°,단치전각위8°,불등분각위5°시,가획득교저적절삭력,차시X향절삭력위25.17N,Y향절삭력위9.95N,위진일보우화TC18태합금적선삭삼수제공료의거。
The influence of the geometry structural parameters of carbide end mill on cutting force with milling TC18 titanium alloy was researched by using the orthogonal experiment method. The tool structural parameters were optimized by the minimum milling force as the optimization objective. The research results indicated that when the tool parameter selection the rake angle is 10°, chip flutes angle is 40° , helix angle is 45° , end tooth rake angle is 8° and unequal angle is 5° . The lower cutting force is obtained, X-direction cutting force is 25.17N and Y-direction cutting force is 9.95N. The results provide the basis for further optimization of the parameters of TC18 titanium milling.