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现行 EN 2790:1991
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Aerospace series - Rod ends, adjustable, self-aligning plain bearing with self-lubricating liner and threaded shank with engagement: 1,5 x thread diameter - Dimensions and loads 航空航天系列 - 杆端 可调节自调心滑动轴承 带有自润滑衬套和螺纹杆 配合:1.5 x螺纹直径 - 尺寸和载荷
发布日期: 1991-04-24
实施日期: 1991-04-24
本标准规定了可调节杆端的特性,包括: - 具有自润滑衬套EN 2501的自调心球轴承; - 具有螺纹杆的杆端主体,包括: - 周向槽,用于识别接合; - 用于锁定目的的可选纵向凹槽。这些杆端用于飞机结构的飞行控制杆。它们旨在在-55°C至150°C的温度范围内使用
This standard specifies the characteristics of adjustable rod ends consisting o of: - a self-aligning ball bearing with self-lubricating liner EN 2501; - a rod end body with threaded shank comprising: - a circumferential groove to identify engagement; - an optional longitudinal groove for locking purposes. These rod ends are intended for use with flight control rods for aircraft structures. They are intended to be used within the temperature range: -55°C to + 150°C
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