This paper discusses infers and proves all the major technological problems about air-craft wearout life calculation which are used in single aircraft fatigue life monitoring .

对飞机 单机疲劳寿命监控使用的飞机 消耗寿命计算的各主要技术问题 做了 相应的论述、推导和证明；

The calculation method research of aircraft wearout life

飞机 消耗寿命计算方法研究

For positions and parts which are easily subjecting to corrosion and wear out in the desulfuration system anti corrosion and wear resistant materials or rubber lining method should be used as fully as possible so as to decrease the occurrence of corrosion and wearout problems .

对于脱硫系统中易腐蚀、磨损的部位及部件，应尽量采用防腐、耐磨的材料或采用衬胶的方法，以减少腐蚀和 磨损。

The anode holes injection model and the electron traps generation model is linked into a consistent model describing the oxide wearout as an electron correlated holes trap creation process .

把阳极空穴注入模型和电子陷阱产生模型统一起来，提出了 薄 栅氧化 层 的 击穿是与电子导致的空穴陷阱相关的。