Wyniki wyszukiwania dla: COMPRESSOR BLADE

• The Unsteady Low-Frequency Forces Acting on the Rotor Blade in the First Stage on an Axial Compressor of SO-3 Jet Engine

  Publikacja

  • M. Soliński
  • R. Rządkowski
  • A. Pająk
  • R. Szczepanik

  - Rok 2012

• Dynamic analysis of the first stage compressor bladed disc of an aircraft engine

  Publikacja

  • R. Rządkowski
  • M. Drewczyński
  • M. Soliński
  • A. Maurin
  • A. Maciejewska
  • R. Szczepanik

  - Journal of Machine Construction and Maintenance - Rok 2011

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• Exhaust gas temperature measurements in diagnostic examination of naval gas turbine engines. Part II. Unsteady processes

  Publikacja

  • Z. Korczewski

  - Polish Maritime Research - Rok 2011

  The second part of the article presents the results of operating diagnostic tests of a two- and three-shaft engine with a separate power turbine during the start-up and acceleration of the rotor units. Attention was paid to key importance of the correctness of operation of the automatic engine load control system, the input for which, among other signals, is the rate of increase of the exhaust gas flow temperature. The article...

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• Suitableness of SLM Manufactured Turbine Blade for Aerodynamical Tests

  Publikacja

  • J. Telega
  • P. Kaczynski
  • M. Śmiałek-Telega
  • P. Pawłowski
  • R. Szwaba

  - Materials - Rok 2023

  settingsOrder Article Reprints Open AccessArticle Suitableness of SLM Manufactured Turbine Blade for Aerodynamical Tests by Janusz Telega 1,*ORCID,Piotr Kaczynski 1ORCID,Małgorzata A. Śmiałek 2ORCID,Piotr Pawlowski 3ORCID andRyszard Szwaba 1ORCID 1 Institute of Fluid Flow Machinery Polish Academy of Sciences (IMP PAN), Fiszera 14, 80-231 Gdansk, Poland 2 Faculty of Mechanical Engineering and Ship Technology, Institute of Naval...

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