Evaluation of effect of size of wear particles (accumulated on filter element) on the intensity of their x-ray fluorescence when diagnosing the oil system of aviation GTE
UDC 621.452.3:53.082.56 BBK 39.55:22.345/.346
The article gives the assessment of the aviation engine technical status based on intensity of the flush x-ray fluorescence from its filter element. The evaluation rests on dependence of x-ray fluorescence analytical signal on the size of metal particles in the flush. The number of the large particles characterizes the level of wear of the engine.
Key words: x-ray fluorescence; aviation engine technical status; flush from filter element; impact of the size of particles on intensity; wear processes.
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