The influence of design and performance parameters of an angular ball bearing on the stiffness of gas turbine engine rotor supports

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Abstract

The paper deals with the influence of a radial bearing clearance, frequency rotation, as well as radial and axial forces on the displacement and stiffness of a ball bearing. The influence of the bearing stiffness on that of the support is assessed.

About the authors

V. B. Balyakin

Samara State Aerospace University

Author for correspondence.
Email: 029-029@mail.ru

Ddoctor of Technical Science, Professor

Head of the Department of Elements of Mechanical Design

Russian Federation

E. P. Zhilnikov

Samara State Aerospace University

Email: okm@ssau.ru

Candidate of Technical Science

Professor of the Department of Elements of Mechanical Design

Russian Federation

I. S. Barmanov

Samara State Aerospace University

Email: isbarmanov@mail.ru

Candidate of Technical Science

Associate Professor of the Department of Elements of Mechanical Design

Russian Federation

References

  1. Балякин, В.Б. Обобщённая методика расчёта и проектирования упруго-демпферных опор роторов авиационных газотурбинных двигателей [Текст] / В.Б. Балякин, И.С. Барманов // Изв. Самар. науч. центра РАН – Самара, 2012. – Т. 14, № 4 – C. 282-287.
  2. Белоусов, А.И. Теория и проектирование гидродинамических демпферов опор роторов [Текст] / А.И. Белоусов, В.Б. Балякин, Д.К. Новиков; под ред. А.И. Белоусова – Самара: Изд-во Самарского научного центра РАН, 2002. – 335 с.
  3. Теория и проектирование опор роторов авиационных ГТД [Текст] / В.Б. Балякин, Е.П. Жильников, В.Н. Самсонов [и др.] – Самара: Изд-во СГАУ, 2007. – 254 с.

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