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

DIN EN 4035-2006 发布历史

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 ?

DIN EN 4035-2006由德国标准化学会 DE-DIN 发布于 2006-09。

DIN EN 4035-2006 在中国标准分类中归属于: V22 机械配件、构件，在国际标准分类中归属于: 49.035 航空航天制造用零部件。

DIN EN 4035-2006 发布之时，引用了标准

• ISO 1132-1 滚动轴承 公差 第1部分:术语和定义 三种语言版
• ISO 3353-1 航空航天. 引导和收尾螺纹. 第1部分: 滚压外螺纹*， 2020-11-30 更新
• ISO 5855-2 航空航天 MJ螺纹 第2部分:螺栓和螺母螺纹的极限尺寸
• ISO 8075 航空航天 可淬硬的不锈钢零件表面处理
• EN 2067 航空航天系列.用于杆端的自测球状轴承.技术规范

* 在 DIN EN 4035-2006 发布之后有更新，请注意新发布标准的变化。

DIN EN 4035-2006的历代版本如下：

• 2006年09月 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
• 2021年07月 DIN EN 4035-2021

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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

无

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 ?