BS EN 4535-2:2016规定了自润滑铝合金法兰衬套的特性 用于航空航天应用的衬里提升载荷。衬套用于飞机结构和控制装置的固定或移动部件 机制。它们应在-55°C至121°C的温度范围内使用。交叉参考:EN 2101EN 2284EN 2311EN 2318EN 2424EN 4704ISO 2768-1AECMA TR 4475购买本文件时提供的所有当前修订版均包含在购买本文件中。

BS EN 4535-2:2016 specifies the characteristics of bushes flanged in aluminium alloy with selflubricating liner elevated load for aerospace applications.The bushes are intended for use in fixed or moving parts of the aircraft structure and control mechanisms.They shall be used in the temperature range -55 °C to 121 °C.Cross References:EN 2101EN 2284EN 2311EN 2318EN 2424EN 4704ISO 2768-1AECMA TR 4475All current amendments available at time of purchase are included with the purchase of this document.