MATEC Web Conf.
Volume 99, 20172016 Workshop on Contemporary Materials and Technologies in the Aviation Industry (CMTAI2016)
|Number of page(s)||5|
|Section||Aviation industry and engineering|
|Published online||08 February 2017|
Problems of Formation of Diagnostic Features in the Diagnosis of Aircraft Engines
Bauman Moscow State Technical University, 105005 Moscow, Russia
* Corresponding author: firstname.lastname@example.org
The article is devoted to the evaluation of current technical condition of aircraft engines. Deals with the choice of the detection method of diagnostic features required for degradation assessment, emergency protection and detection of incipient defects on the example of cyclic machines and mechanisms. For the formation of diagnostic features in the diagnosis of aircraft engines use different physical effects (vibration, shock, heat radiation, electrodynamic and thermal processes, wear debris in oil, etc.). Classification of defects and requirements for the development of diagnostics systems is formed based on them. The article describes the requirements for diagnostic signs. The article provides a promising phase method that allows obtaining stable diagnostic characters in exploitation. The result of applying the method is shown. Diagnostic signs are formed. In mathematical modeling it was used the traditional theory of the description of rotary mechanisms. The data obtained are compared with experimental data.
© The Authors, published by EDP Sciences, 2017
This is an Open Access article distributed under the terms of the Creative Commons Attribution License 4.0, which permits unrestricted use, distribution, and reproduction in any medium, provided the original work is properly cited.
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