Model operation of thermo elastic deformation at the electrochemical working compressor blades with using method of final elements in the software environment “ANSYS”

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Abstract

The article is devoted to the actual problem of the up-to-date aviation propulsion engineering – the model operation of thermo elastic deformation at the electrochemical working compressor blades. In the article the results of the development work of creation methodology of model operation of thermal load and value calculation of blade deformation by method of final elements in the software environment “Ansys” are presented. Areas of using this method are discussed.

About the authors

1 1

Samara State Aerospace University

Author for correspondence.
Email: sadohina@ssau.ru
Russian Federation

1 1

Samara State Aerospace University

Email: sadohina@ssau.ru
Russian Federation

1 1

Samara State Aerospace University

Email: sadohina@ssau.ru
Russian Federation

1 1

Samara State Aerospace University

Email: sadohina@ssau.ru
Russian Federation

References

  1. Смирнов Г.В., Совершенствование окончательной электрохимической размерной обработки лопаток ГТД с учетом технологической наследственности.- Диссертация на соискание учёной степени докт. техн. наук." Самара, 2004, 453 с.
  2. Чигарев А.В., Кравчук А.С., Смалюк А.Ф. ANSYS для инженеров. Справочное пособие, Изд.: Машиностроение, 2004, 512 с.
  3. Басов К.А. ANSYS в примерах и задачах, Изд.: Компьютер-Пресс, 2002, 224 с.
  4. Каплун А.Б., Морозов Е.М., Олферьева М.А. ANSYS в руках инженера. Практическое руководство. Изд.: Едиториал УРСС, 2003, 272 с.

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