飞机燃气涡轮发动机直流和交流发电机加速可靠性试验

A. Gishvarov, M. Davydov
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引用次数: 0

摘要

在本文中,我们考虑了一种选择加速试验的模式和持续时间的方法,以确保同时等效所有的主要元素和特性消耗发动机的使用寿命以及直流和交流发电机。发动机和发电机加速试验的模式和持续时间的确定是根据广义方法进行的,该方法尽可能确保发动机和发电机组件的所有"关键"元件同时进行加速和长时间损伤试验的等效性。根据所考虑的方法计算的制度和工业上商业使用的方法进行的发动机加速试验的比较表明,在整个发动机中,通过加速试验和长时间试验的等效水平估计的加速试验效率高出2倍,从而可以更准确地评估发电机和发动机的可靠性和使用寿命。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
Accelerated reliability tests of aircraft gas turbine engine with DC and AC generators
In this paper, we consider a methodology for choosing the modes and duration of accelerated tests that ensure equivalence at the same time for all the main elements and characteristics of the consumption of engine service life along with direct current and alternating current generators. The determination of the modes and duration of accelerated tests of the engine and generators is carried out according to the generalized method, which allows as much as possible to ensure the equivalence of accelerated and lengthy damage tests at the same time of all “critical” elements of engine and generator assemblies. Comparative accelerated engine tests carried out under the regimes calculated by the considered method and the method used commercially in the industry showed that in the engine as a whole, the accelerated test efficiency, which was estimated by the level of equivalence of accelerated and lengthy tests, is 2 times higher, which allows more accurate assessment reliability and service life of generators and engine by accelerated testing.
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