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Контроль и диагностика технического состояния газотурбинных двигателей

51852

Новиков А.С.

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The main causes and mechanisms of damage to structural elements of gas turbine engines during operation are considered, the tasks and principles for constructing a system for technical diagnostics of aircraft gas turbine engines and power plants are formulated, as well as the relationship between the development of this system and the improvement of the design, manufacture and operation of engines. The physical and mathematical methods of technical diagnostics are presented, it is shown that the cornerstone principle of constructing an effective diagnostic system is an individual assessment of the technical condition of a gas turbine engine during operation. Practical recommendations are given for the construction of automated and human-assisted systems for diagnosing gas turbine aircraft engines and power plants at the stages of design, production and operation. For specialists in the field of diagnostics, design, manufacture, development and operation of aircraft engines and power plants, students, graduate students of higher educational institutions.

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ISBN 978-5-02-035300-8
Publisher Наука. Москва. 2007
Bookbinding твердый переплет, 469 стр.

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