Estimation method of change of parameters of gas-turbine engine on-stream
DOI:
https://doi.org/10.15587/1729-4061.2010.2695Keywords:
GTE tests, measured parameters, parametrical estimation, degradation of characteristics during life cycleAbstract
This article deals with a serial gas turbine engines parameters changing estimation method that gives possibility to choose the optimum number of measured parameters. Parametrical process of experimental data collected by tests and controlled operation with ageing processes consideration during GTE life cycle.References
- Ахмедзянов A. M., Диагностика состояния ВРД по термогазодинамическим параметрам [Текст] / A. M. Ахмедзянов, А. П. Тунаков - М.: Машиностроение, 1993. -206с.
- Тунаков А. П. Методы оптимизации при доводке и проектировании ГТД [Текст] / А. П. Тунаков. - М.: Машиностроение, 1989.-184 с.
- Александров В. Г. Контроль технической исправности самолетов и вертолетов [Текст] / В. Г. Александров. - М.: Транспорт, 1976.-360с.
- Ямпольский В. И., Контроль и диагностирование гражданской авиационной техники [Текст] / В. И. Ямпольский, Н. И. Белоконь, Б. И. Пилипосян. - М.: Транспорт, 1990.-182с.
- Сиротин Н. Н., Техническая диагностика авиационных газотурбинных двигателей [Текст] / Н. Н. Сиротин, Ю. М. Коровкин. - М.: Машиностроение, 1979.-272с.
- Ахмедзянов А. М., Диагностика состояния ВРД по термогазодинамическим параметрам [Текст] / А. М. Ахмедзянов, Н. Г. Дубравский, А. П. Тунаков. - М.: Машиностроение, 1983.-206с.
- Симбирский Д. Ф., Программный комплекс для эксплуатационного мониторинга выработки ресурса основных деталей авиационного двигателя Д-18Т [Текст] / Д. Ф. Симбирский, А. В. Олейник, В. А. Филяев и др. //Авіаційно-космічна техніка і технологія. - Х.: НАКУ “ХАІ”.-2004.-вип. 7/15.-с.145-150.
- Панин В. В. Моделирование условий совместной работы элементов ТРДД при оценке запасов устойчивости на переходных режимах в эксплуатации [Текст] / В. В. Панин // Проблеми експлуатації та надійності авіаційної техніки. – К.: КМУЦА, – 1997. – С. 97–99. (139п).
- Панин В. В. Газодинамическая устойчивость компрессоров авиационных ГТД [Текст] / В. В. Панин. - К.: КМУГА, 1998. - 152с. (60м).
Downloads
Published
How to Cite
Issue
Section
License
Copyright (c) 2014 А.П. Вознюк
This work is licensed under a Creative Commons Attribution 4.0 International License.
The consolidation and conditions for the transfer of copyright (identification of authorship) is carried out in the License Agreement. In particular, the authors reserve the right to the authorship of their manuscript and transfer the first publication of this work to the journal under the terms of the Creative Commons CC BY license. At the same time, they have the right to conclude on their own additional agreements concerning the non-exclusive distribution of the work in the form in which it was published by this journal, but provided that the link to the first publication of the article in this journal is preserved.
A license agreement is a document in which the author warrants that he/she owns all copyright for the work (manuscript, article, etc.).
The authors, signing the License Agreement with TECHNOLOGY CENTER PC, have all rights to the further use of their work, provided that they link to our edition in which the work was published.
According to the terms of the License Agreement, the Publisher TECHNOLOGY CENTER PC does not take away your copyrights and receives permission from the authors to use and dissemination of the publication through the world's scientific resources (own electronic resources, scientometric databases, repositories, libraries, etc.).
In the absence of a signed License Agreement or in the absence of this agreement of identifiers allowing to identify the identity of the author, the editors have no right to work with the manuscript.
It is important to remember that there is another type of agreement between authors and publishers – when copyright is transferred from the authors to the publisher. In this case, the authors lose ownership of their work and may not use it in any way.