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Optimization of a Welded Portion of the High Pressure Compressor Rotor

  • Aircraft and Rocket Engine Design and Development
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Abstract

An integrated method for optimization of a welded portion of a high pressure compressor rotor as a single object is developed. The minimum mass criterion is used in the optimization method; limitations are imposed in accordance with strength and stiffness requirements. An example is given of optimization of a typical welded portion of a high pressure compressor rotor resulting in mass reduction and increase of cyclic durability.

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References

  1. Birger, I.A., Shorr, B.F., and losilevich, G.B., Raschet na prochnost’ detalei mashin. Spravochnik (Strength Analysis of Machine Parts. Handbook), Moscow: Mashinostroenie, 1993.

    Google Scholar 

  2. Dem’yanushko, I.V. and Birger, I.A., Raschet na prochnost’ vrashchayushchikhsya diskov (Strength Analysis of Rotating Disks), Moscow: Mashinostroenie, 1978.

    Google Scholar 

  3. Bratchik, V.Ya., Numerical Design of GTE Disks by Dynamic Programming Method, Trudy TsIAM, 1982, no. 996, Problemy prochnosti i dinamiki v aviadvigatelestroenii (Problems of Strength and Dynamics in Aircraft Engine Design), issue 2, pp. 57–69.

    Google Scholar 

  4. Temis, Yu.M. and Yakushev, D.A., Optimal Design of Turbine Engine Structural Components, Tekhnika Vozdushnogo Flota, 2009, no. 1(694), pp. 54–64.

    Google Scholar 

  5. Wang, Z.J., Kang, L.H., Kretov, A.S., and Sheng, H., Strength Design Model for Thin-Walled Structures, Izv. Vuz. Av. Tekhnika, 2016, vol. 59, no. 1, pp. 116–122 [Russian Aeronautics (Engl. Transl.), vol. 59, no. 1, pp. 126–133].

    Google Scholar 

  6. Reklatis, G.V., Ravindran, A., and Ragsdell, K.M., Engineering Optimization, New York: John Wiley and Sons, 1983.

    Google Scholar 

  7. Birger, I.A., Fundamentals of the Computer-Aided Design, Izv. Vuz. Mashinostroenie, 1977, no. 8, pp. 32–35.

    Google Scholar 

  8. Egorov, I.N., Kretinin, G.V., Leshchenko, I.A., and Kuptzov, S.V., IOSO Optimization Toolkit—Novel Software to Create Better Design, URL: http://www.iosotech.com/text/2002_4329.pdf.

  9. Pakhomenkov, A.V., Azimov, R.A., and Bukatyi, S.A., Calculation of Low Cycle Fatigue Life for Gas-Turbine Engine Critical Parts, Izv. Vuz. Av. Tekhnika, 2017, vol. 60, no. 3, pp. 95–100 [Russian Aeronautics (Engl. Transl.), vol. 60, no. 3, pp. 421–427].

    Google Scholar 

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Authors and Affiliations

  1. P.I. Baranov Central Institute of Aviation Motors (CIAM), ul. Aviamotornaya 2, Moscow, 111116, Russia

    A. V. Sal’nikov

Authors
  1. A. V. Sal’nikov
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Correspondence to A. V. Sal’nikov.

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Russian Text © The Author(s), 2020, published in Izvestiya Vysshikh Uchebnykh Zavedenii, Aviatsionnaya Tekhnika, 2020, No. 1, pp. 109–116.

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Sal’nikov, A.V. Optimization of a Welded Portion of the High Pressure Compressor Rotor. Russ. Aeronaut. 63, 117–125 (2020). https://doi.org/10.3103/S1068799820010171

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  • DOI: https://doi.org/10.3103/S1068799820010171

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