BS EN 4035-2006 航空航天系列.减小内部径向间隙和带螺纹钛合金杆耐腐蚀钢可调自动对心双列球轴承的杆端.尺寸和载荷

标准号：BS EN 4035-2006
中文标准名称：航空航天系列.减小内部径向间隙和带螺纹钛合金杆耐腐蚀钢可调自动对心双列球轴承的杆端.尺寸和载荷
英文标准名称：Rod ends, adjustable with self-aligning double row ball bearing in corrosion resisting steel, reduced internal radial clearance and threaded shank in titanium alloy - Dimensions and loads
标准类型：V22
发布日期：2006/5/31 12:00:00
实施日期：2006/5/31 12:00:00
中国标准分类号：V22
国际标准分类号：49.035
引用标准：ISO 1132-1;ISO 3353-1;ISO 5855-2;ISO 8075;EN 2067
适用范围：This standard specifies the characteristics of adjustable rod ends with self-aligning double row ball bearing incorrosion resisting steel with reduced internal radial clearance and threaded shank in titanium alloy, designedto withstand only slow rotations and oscillations under load.They consist of:- a rod end comprising:- circumferential groove to identify location;- either seals or shields;- an optional longitudinal groove for locking purpose;- an inner ring with balls.These rod ends are intended for use with flight control rods or rods for aerospace structures.They are intended to be used in the temperature range: − 54 °C to 150 °C.However, being lubricated with the following greases:- very high pressure grease, ester type (code A), operational range − 73 °C to 121 °C or- very high pressure grease, synthetic hydrocarbons, general purpose (code B), operational range − 54 °Cto 177 °C (see EN 2067),their field of application when lubricated with code A grease is limited to 121 °C.