Search Results

Search Results

• Identification system for the technical condition of gas turbine engines of aircraft

  Arif Pashayev, Djakhangir Askerov, Ramiz Sadiqov, Parviz Abdullayev

  Abstract 1031 | PDF Downloads 637 | DOI https://doi.org/10.3846/1648-7788.2008.12.101-112

  Page 101-112
  

  2008-12-31

• Heat and erosion-resistant nanostructured coatings for gas turbine engines

  Aleksandrs Urbahs, Konstantins Savkovs, Margarita Urbaha, Kristine Carjova

  Abstract 1080 | PDF Downloads 718 | DOI https://doi.org/10.3846/16487788.2013.861225

  Page 137-144
  

  2013-12-24

• Raising gas-dynamic stability margin of axial and centrifugal compressor stages by means of vaned diffuser boundary layer control

  Ivan Lastivka

  Abstract 1017 | PDF Downloads 802 | DOI https://doi.org/10.3846/16487788.2011.624262

  Page 76-81
  

  2011-10-04

• Wireless-based information model of the common operation of the elements of the aviation gas turbine engine

  Serhii Tovkach

  Abstract 1133 | PDF Downloads 664 | DOI https://doi.org/10.3846/aviation.2024.22143

  Page 141–147
  

  2024-09-20

• Analysis of repaired gas turbine and compressor blades

  Alexander Tishkunov, Sergejs Gluhihs, Aleksandrs Korjakins, Andris Popovs

  Abstract 1096 | PDF Downloads 896 | DOI https://doi.org/10.3846/1648-7788.2008.12.46-50

  Page 46-50
  

  2008-06-30

• A case study of vibration fault diagnosis applied at Rolls-Royce T-56 turboprop engine

  Christos Skliros

  Abstract 3422 | PDF Downloads 2405 | DOI https://doi.org/10.3846/aviation.2019.11900

  Page 78-82
  

  2019-12-31