1) subframe
发动机架，下支架
2) engine bracket lower plate
发动机支架下板
1.
By analyzing the forming process to engine bracket lower plate, and introduced the design of bending die,some measures to control spring back were extracted, the spring back problem of engine bracket lower plate was solved.
通过对发动机支架下板成形工艺的分析及其弯曲模结构的介绍,总结了几种控制回弹的措施,解决了发动机支架下板回弹难以解决的问题。
3) Engine Bracket
发动机支架
1.
Design and Improvement of Die Casting Die for PQ35 Engine Bracket;
PQ35发动机支架压铸模具的设计和改进
2.
The three-dimensional model of the bracket is built by UG,and modal analysis is conducted on the 4G1 engine bracket through the software of ANSYS Workbench so as to identify the modal parameters of the bracket,the natural frequency and vibration features.
运用UG对支架进行三维建模,通过ANSYSWorkbench软件对4G1发动机支架结构进行模态分析,从而求解出支架结构的模态参数,并得到支架的固有频率和振型特征,可为进一步研究整车振动、疲劳奠定基础,也为支架结构的优化设计提供参考依据。
3.
The application of topology optimization in Engine bracket design is aimed to improve the structure performance and get a lighter structure.
在发动机支架设计中运用拓扑优化方法,改善发动机支架结构,保证支架强度和模态的同时降低重量,为CAD设计工程师指明设计方向。
4) engine support
发动机支架
1.
Light-weight design on engine support based on structural topology optimization method;
基于结构拓扑优化方法的发动机支架轻量化设计
2.
In order to further improve the structural design and realize the CAE standardization of the engine support,we adopt finite element software ANSYS to calculate and emulate the stress distribution,and draw out the stress and strain distribution maps in the paper.
为进一步改进发动机支架的结构设计,实现发动机支架的CAE标准化生产,本文采用大型有限元分析软件ANSYS对发动机支架的应力分布进行了计算和仿真分析,得出了该构件的应力和应变分布图,从而为发动机支架的强度分析研究提供了比较实用的有限元分析方法。
5) bonnet strut
发动机舱盖支架
6) engine rear support
发动机后支架
补充资料：航空发动机推重比(见航空发动机推力)
航空发动机推重比(见航空发动机推力)
thrust to weight ratio of aeroengine
hQngkong角dong)1 tuizhongbi航空发动机推重比〔thros*:。wdgh:ra-tio of aeroengine)见航空发动机推力。
说明：补充资料仅用于学习参考，请勿用于其它任何用途。
参考词条