1) cone hole
锥孔
1.
Technological design for processing the large-scale rudder blade's cone holes;
大型舵叶锥孔加工工艺设计
2.
In this paper, the drive principle and the structure design of a combined machine tool for processing the cone hole, the fixing mouth and the underside face of large type oil tanker rudder blade are introduced.
介绍了一种用于加工巨型油轮舵叶的锥孔、安装止口及端面的组合工装传动原理及结构设计。
3.
According to the conventional technological requirements,the tool structure in cone hole and the angle of cutting tool parameters are designed.
本文主要介绍了机械加工中常见细长型锥孔的车削工艺,根据常规的工艺要求设计锥孔内车刀的结构、刀具角度参数,同时结合刀具的角度参数和结构特点对车削过程进行切削性能分析,并对影响锥孔车削质量的切削控制方案进行重点阐述。
2) taper hole
锥孔
1.
the analysis of taper hole lapping damage proves friction from normal pressure of center bottom and hole ,changed torque is less than the torque from radial bearing preload ,it proves the error touch of taped 1:7 working condition is the mostly reason of lapping damage .
通过对一系列的锥孔研伤情况分析论证,排除了顶尖下部与孔之间形成的正压力所产生的摩擦力,在转换成扭矩后小于径向轴承预紧力产生的扭矩的影响因素。
3) drilling hole on conical surface
锥面钻孔
4) taper bore
圆锥孔
1.
Repair machining methods for the high precision taper bore with small machining allowance have been described.
介绍大齿轮高精度圆锥孔小余量进行修复的加工方法。
5) Taper pinhole
锥形销孔
6) deep tine taper hole
深小锥孔
1.
Theory research on the maximum reduction of deep tine taper hole formed by open-die cold extrusion;
深小锥孔挤压成形极限变形程度理论判据建立
2.
Theoretical and experimental research on the forming limit of deep tine taper hole formed by open-die cold extrusion;
深小锥孔开式冷挤压成形极限的理论及实验研究
3.
In the paper, maximum reduction when deep tine taper hole is formed by open-die extrusion is defined.
给出了深小锥孔件开式冷挤压成形时极限变形程度的定义,建立了变形区非稳态连续速度场;利用上限原理得到了极限变形程度的理论判据。
补充资料：第二孔(继发孔)型缺损
第二孔(继发孔)型缺损
ostium secondary defect
是心房间隔在形成上发生障碍，一般缺损较大，多在卵圆孔附近称第二孔(继发孔)型缺损。
说明：补充资料仅用于学习参考，请勿用于其它任何用途。
参考词条