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1·Tighten the engine mount-to-bracket bolts.

拧紧引擎架至支架的螺栓。

2·Open the caps for the engine mount brackets.

打开发动机吊点支架的盖子。

3·Make sure the caps for the engine mount brackets are open.

确证发动机吊点支架的盖子是打开的。

4·An active engine mount with electrostrictive actuator was studied.

一种采用电致伸缩作动器的主动悬置。

5·Do not remove the cap or the hinge bolt for the engine mount bracket.

不要拆下盖子或发动机吊点支架上的铰链螺栓。

6·First up are revisions to the engine mount brackets that optimize chassis flex and improve handling.

首先登场的是安装在发动机支架，优化调整底盘弯曲和改善处理。

7·The sound pressure response character excitated by force of engine mount and spring system is analyzed.

分析了车内声场在发动机悬置和悬架激励力下的响应特性。

8·Therefore, correct calculation of the load on engine mount is full of great significance in aircraft design and flight safety.

因此，如何准确计算发动机固定装置的载荷，对飞机的设计乃至其飞行安全都有着重要意义。

9·For a practical rubber engine mount, empirical formulae are established which vary with material hardness and compression level.

结合某型发动机悬置，计算得到了不同硬度胶料产品在不同变形量情况下形状系数的经验公式。

10·A mechanics model for engine mount system is established with MATLAB based on dynamic stiffness of engine mounts in idle condition.

建立了基于悬置元件怠速工况下动刚度的发动机悬置系统MATLAB力学模型。