Definition of optimum parameters of workpieces and superplastic forming and isothermal stamping operations for the manufacturing of thin-walled details of gas-turbine engines



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Abstract

The technique of mathematical simulation of isothermal stamping and superplastic molding for determination of optimum parameters of work pieces and manufacturing operations is presented. Application of the technique for thinwalled case and hollow vane manufacturing are shown.

About the authors

J. M Temis

Central Institute of Aviation Motors; Bauman Moscow State Technical University

Email: tejoum@ciam.ru
Dr. Sc, Prof.

A. P Khudyakov

Central Institute of Aviation Motors

A. V Cherednichenko

Bauman Moscow State Technical University

PhD

References

  1. Serra D. Superplastic forming applications on aero engines. A review of ITP manufacturing processes. 6th EUROSPF Conference, Carcassonne, France, 3-5 September, 2008.
  2. Чумаченко Е.Н., Смирнов О.М., Цепин М.А. Сверхпластичность: материалы, теория, тех- нологии. Изд. 2-е, М.: Книжный дом «ЛИБРОКОМ», 2009. - 320 с.
  3. Васин Р.А., Еникеев Ф.У. Введение в механику сверхпластичности: В 2 ч. Ч. II. - Уфа: Гилем, 1999. - 626 с.

Copyright (c) 2015 Temis J.M., Khudyakov A.P., Cherednichenko A.V.

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This work is licensed under a Creative Commons Attribution-NonCommercial-NoDerivatives 4.0 International License.

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