Research on Application of TRIP Steel in Chassis Structure

1、

Application of Corrosion Resistant Epoxy Impregnating Varnish in Motorcar Chassis

高耐蚀性环氧浸漆在汽车底盘件上的应用

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2、

At present, the company's leading product for Tatra ( TATRA) T815, T815-II type, Type III's long march chassis Series Mercedes-Benz parts and accessories, such as heavy vehicles.

目前，公司的主导产品为太脱拉（TATRA）T815、T815-II型、长征III型车的底盘件和奔驰系列等重型汽车配件。

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3、

A mathematical model is set up for life consumption of the high temperture parts in aero-engine.

在航空发动机热端件寿命消耗模型中考虑了离心负荷、热负荷及蠕变的影响。

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4、

Protective Coating of Modified Silicon Sol on the surface of Magnesium Alloy in Aircraft Engine

发动机镁合金件改性硅溶胶防护涂层的研究

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5、

Application of the Feature Modeling in the Parametric Design of the Typical Structures of Aeroengine

特征建模技术在航空发动机典型结构件参数化设计中的应用

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6、

Push wiring harness into the bonnet reinforcement.

将线束推入发动机舱盖加强件。

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7、

The Optimal Design of the Moving Bar Lengths in Swing Piston Engine

摆动活塞发动机运动杆件长度的优化设计

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8、

A computational model for life consumption and life monitoring of Aeroengine

某航空发动机热端件寿命消耗计算模型及寿命监视

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9、

Three-dimensional elastoplastic finite element analysis of the back-joint subassembly of SRM

固体火箭发动机接头组合件三维弹塑性有限元分析

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10、

Based on object oriented BP network, a software prototype of scheme selection of aeroengine rotor coupling is developed in Visual C++ 6.0 development environment. An example is adopted to validate the rationality of this method.

基于面向对象的BP网络模型，在Visual c++6.0的开发环境中实现了航空发动机转子连接件方案选择的软件原型，并用实例进行了验证。

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11、

Finally, the paper by analysis the step bar and engine cylinder head specimen variable energy scan imaging detection data to verify the feasibility and effectiveness of the variable energy X-ray detection method.

最后，论文通过对阶梯试块和发动机缸盖试件的变能量扫描成像检测试验数据的分析，验证了变能量扫描X射线检测方法的可行性和有效性。

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12、

Firstly, the monitoring status quo of the lube oil consumption rate which reflects the wear state of the rotating parts of the aero-engine is analyzed, a method of forewarning the superscale of the lube oil consumption rate by forecasting the consumption rate is presented.

首先分析反映航空发动机转动件磨损状况的滑油消耗率监控现状及其不足，提出通过对滑油消耗率预测以预警滑油消耗率超标的方法。

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13、

A method which is applied to measure the surface temperature of the aeroengine rotor parts by using the thermoscope-piece to accomplish static state temperature measurement for a certain aeroengine compress rotor blade is introduced.

介绍了一种应用于航空发动机旋转件表面的温度测量方法，即使用测温片完成某航空发动机压气机转子叶片的稳态温度测试。

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14、

All the parts for one engine are completely assembled with work pieces supplied in one traveling cycle of the trays.

托盘运行一周完成发动机内部件的全部装配和上下料工作。

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15、

Additional Mass Method to Determine the Moment of Inertia of Total Moving Components in a Engine integral one-piece mainshaft

用附加质量法确定发动机运动件的总转动惯量（多缸转子发动机用的）整体式偏心轴

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16、

The Finite Element Analysis of the Hot Intensity of the Heat Insulation Part in the Low Heat Rejection Engine

低散热发动机隔热件热强度有限元分析

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17、

The Development of CAD/ CAE/ CAM for Drawn Components' Moulds of High-speed Engine

高速发动机拉延件模具CAD/CAE/CAM开发

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18、

Directions of Repairing and Maintaining Engine Sealing

发动机密封件的维修保养

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19、

Features, Causes and Preventive Measures for Common Mode Failures of Rotational Components in Aeroengines

航空发动机转动件共模失效的特征、原因与对策

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20、

Main Causes of Thermal Stress and Solving Methods for Heated Components of Engines

热应力产生的根源及针对发动机受热件的解决方法

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