对耐高温复合涂层系统进行了研究。
This paper studies the multilayer coatings system resistant to high temperature.
这也就是说总的涂层系统的厚度在任何一点都不能低于该规定值。
This means the total layer system thickness must not fall below the specified value at any point.
如果使用背离默认值的涂层系统，则必须事先得到GEWE的批准。
If a coating system is to be used deviating the default, it must be approved by GEWE before.
部件组装及运输至GEWE或建筑现场的工作仅能在涂层系统完全硬化后才能进行。
Assembly and transport of components to GEWE or the construction site may only take place after the coating system has hardened.
复合热障涂层系统包括蜂窝金属结构具有高的热膨胀磷酸盐保税基陶瓷空心球填补。
A composite thermal barrier coating system includes a honeycomb metallic structure filled with high thermal expansion ceramic hollow spheres in a phosphate bonded matrix.
复合热障涂层系统的制造，可在目前的热障涂层厚度超过系统，从而提高热保护传授。
The composite thermal barrier coating system may be manufactured to thicknesses in excess of current thermal barrier coating systems, thereby imparting greater thermal protection.
系统介绍：在下表中对每种涂层系统的底漆、基层、加强层、骨料及面层分别作相应的介绍。
System Description: Include in table below each primer, base coat, reinforcing, aggregate, and top coats as appropriate for each coating system.
说明：混凝土配重涂层系统由水泥、水、骨料(按照具体的密度要求使用重骨料或轻骨料)和加固材料组成。
Desciption: Weight coating system composed of cement, water, aggregates, heavy or light depending on the required density and reinforcement.
测试结果表明，热障涂层系统的显微硬度存在压痕尺寸效应，即表观显微硬度随施压载荷的增加而显著降低。
Through centrifugal model tests, the influence of plate size on the results of plate loading tests was studied.
将确定的优化配套涂料与国外同类涂料进行了性能对比，结果表明，由该磷化底漆组成的飞机蒙皮涂层系统的综合性能达到国际同类产品的技术水平。
The results show that the comprehensive properties of the aircraft skin coating containing this kind of primer reach the levels of similar foreign products in technology.
将确定的优化配套涂料与国外同类涂料进行了性能对比，结果表明，由该磷化底漆组成的飞机蒙皮涂层系统的综合性能达到国际同类产品的技术水平。
The results show that the comprehensive properties of the aircraft skin coating containing this kind of primer reach the levels of similar foreign products in technology.
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