高精度Ti6Al4V制孔工艺的实验说明,工艺在深度方向上孔径有待确定

IF 2 Q3 ENGINEERING, MANUFACTURING
H. Yagishita
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引用次数: 0

摘要

Ti6Al4V是一种难以切割的金属,广泛应用于飞机结构、燃气轮机部件和医疗设备中,因此为了紧固零件,Ti6Al4V的打孔操作是必不可少的。传统麻花钻高速钻孔加工Ti6Al4V时,由于其导热系数小,导致切削温度升高,很难在孔深上获得高精度的孔径、圆度和进出口边缘质量。此外,众所周知,Ti6Al4V在相变温度达到883 °C(1621°F)左右时,从α相(密集的六方晶格)转变为β相(体心立方晶格)。由于常规钻削和轨道钻削对孔内表面的冷却效果有较大差异,为明确Ti6Al4V深度方向的高精度制孔工艺,采用φ15 mm常规钻削和φ11 mm 6刃立铣刀轨道钻削提供冷却剂,进行了φ15 mm × 258 mm深度的大量制孔试验。为了阐明待确定深度方向孔径的变化过程,将常规钻削和轨道钻削的切削速度设置为接近相等,并在23 m/min ~ 85 m/min范围内变化12个值。绘制了孔深方向上6个位置同时测量的孔径和圆度与孔深的关系,并对两种钻孔方法在孔深方向上的孔径进行了比较和深入考虑。由此可以确定,虽然常规钻孔在孔深方向上从上到下钻孔直径变小,但轨道钻孔在孔深方向上钻孔直径变大,因为在一次钻孔过程中,Ti6Al4V相变温度下,除孔出口区域外,邻近钻孔内壁区域的温度是保持不变的。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
Highly accurate hole making technology of Ti6Al4V experimental elucidation of process for hole diameter in the depth direction to be determined
Ti6Al4V, which is one of difficult-to-cut metals, is widely used in an aircraft structure, parts of a gas turbine and medical equipment so that a hole making operation of Ti6Al4V is indispensable to fasten the parts. When a highspeed drilling by a conventional twist drill is applied to hole making of Ti6Al4V, it is very difficult to obtain highly accurate hole diameter in the depth of hole, also roundness and inlet–outlet edge quality due to a rise of cutting temperature caused by its small heat conductivity. Moreover, it is well-known that Ti6Al4V causes transiently phase transformation from α phase (close-packed hexagonal lattice) to β phase (body-centered cubic lattice) as soon as it reaches the phase transformation temperature of about 883 °C (1621 °F). Since cooling effect by coolant upon inner surface of hole being drilled would be considerably different between conventional drilling and orbital drilling, to make clear highly accurate hole making technology in the depth direction of Ti6Al4V a lot of hole making tests of φ15 mm × 258 mm depth were executed supplying coolant by conventional drilling of φ15 mm twist drill and by orbital drilling of φ11 mm endmill having 6 blades. In order to elucidate the process for hole diameter in the depth direction to be determined, both cutting speeds of conventional drilling and orbital drilling were set to nearly equal and they were varied at 12 values in the range from 23 m/min to 85 m/min. Hole diameter and roundness measured simultaneously at six positions in the depth direction of hole were drawn in relation to depth of hole and hole diameter in the depth direction was compared and considered deeply between the two drilling methods. Consequently, it is ascertained that although the hole diameter drilled by conventional drilling becomes smaller from top to bottom in the depth direction of hole, the hole diameter drilled by orbital drilling becomes slightly larger in the depth direction of hole since the temperature at the area neighboring inner wall of hole being drilled would be maintained under phase transformation temperature of Ti6Al4V over a drilling operation except the exit area of hole.
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来源期刊
Manufacturing Letters
Manufacturing Letters Engineering-Industrial and Manufacturing Engineering
CiteScore
4.20
自引率
5.10%
发文量
192
审稿时长
60 days
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