DIN 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

Aerospace series - 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; German and English version EN 4035:2006


 

 

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标准号
DIN EN 4035-2006
发布日期
2006年09月
实施日期
废止日期
中国标准分类号
V22
国际标准分类号
49.035
发布单位
DE-DIN
引用标准
ISO 1132-1 ISO 3353-1 ISO 5855-2 ISO 8075 EN 2067
被代替标准
DIN EN 4035-1996
适用范围
This standard specifies the characteristics of adjustable rod ends with self-aligning double row ball bearing in corrosion resisting steel with reduced internal radial clearance and threaded shank in titanium alloy, designed to 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 ?to 150 ? However, being lubricated with the following greases: very high pressure grease, ester type (code A), operational range 73 ?to 121 ?or very high pressure grease, synthetic hydrocarbons, general purpose (code B), operational range 54 ?to 177 ?(see EN 2067), their field of application when lubricated with code A grease is limited to 121 ?




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