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QPQ salt bath composite processing on microstrueture and property of certain type aviation piston engine ring

机译:QPQ盐浴复合加工对某种型航空活塞圈的微结构和性能

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QPQ treatment was carried out on the circulation of a certain type of aero-piston engine. Nitrification treatment of 570 °C and 180 min was performed first, oxidation treatment of 400 °C and 20 min was performed, and secondary oxidation of 370 °C and 20 min was performed after polishing. The surface characteristics of the high cycle treated by QPQ were studied by optical microscope, micro hardness tester and friction and wear tester. The results show that the surface of the rising ring after QPQ treatment forms an oxidation film, a Nitriding layer and a diffusion layer from the outside to the inside. The maximum hardness of the ring surface treated by QPQ is 592 HV, which is nearly twice as high as before untreated, and its wear resistance is nearly five times higher than before untreated.
机译:QPQ处理是在某种类型的航空活塞发动机的循环上进行的。首先进行硝化处理570℃和180分钟,进行400℃和20分钟的氧化处理,抛光后进行370℃和20分钟的二次氧化。通过光学显微镜,微型硬度测试仪和摩擦和磨损测试仪研究了QPQ处理的高循环的表面特征。结果表明,QPQ处理后上升环的表面形成氧化膜,氮化层和从外部的扩散层。通过QPQ处理的环表面的最大硬度为592HV,其几乎是未处理前的两倍,其耐磨性比未处理前的耐磨性几乎高出五倍。

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