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  • Aerodynamic investigations were performed on planar blade cascades representing two alternative root sections of rotor blades 54%22 in length with straight fir-tree root. Each of the variants was designed for different number of blades in the rotor. This paper presents the results of measurements showing the dependency of the kinetic energy loss coefficient and the exit flow angle on the exit isoentropic Mach number and the angle of incidence. Images of the flow fields are also presented. The experimental data is analyzed to assess and document the difference between the two root section designs. Results show that requirement of straight fir tree root leading to high design incidence angles significantly limit operation range. Also in case of root sections with high exit Mach numbers a limit load conditions are an issue. In order to utilize available pressure drop blade cascade throat/pitch ratios should be kept as high as possible which favorites variant with lower number of blades and higher outlet metal angle (relative to axial direction).
  • Aerodynamic investigations were performed on planar blade cascades representing two alternative root sections of rotor blades 54%22 in length with straight fir-tree root. Each of the variants was designed for different number of blades in the rotor. This paper presents the results of measurements showing the dependency of the kinetic energy loss coefficient and the exit flow angle on the exit isoentropic Mach number and the angle of incidence. Images of the flow fields are also presented. The experimental data is analyzed to assess and document the difference between the two root section designs. Results show that requirement of straight fir tree root leading to high design incidence angles significantly limit operation range. Also in case of root sections with high exit Mach numbers a limit load conditions are an issue. In order to utilize available pressure drop blade cascade throat/pitch ratios should be kept as high as possible which favorites variant with lower number of blades and higher outlet metal angle (relative to axial direction). (en)
Title
  • Aerodynamic Data for Two Variants of Root Turbine Blade Sections for A 54%22 Turbine Rotor Blade
  • Aerodynamic Data for Two Variants of Root Turbine Blade Sections for A 54%22 Turbine Rotor Blade (en)
skos:prefLabel
  • Aerodynamic Data for Two Variants of Root Turbine Blade Sections for A 54%22 Turbine Rotor Blade
  • Aerodynamic Data for Two Variants of Root Turbine Blade Sections for A 54%22 Turbine Rotor Blade (en)
skos:notation
  • RIV/61388998:_____/14:00429082!RIV15-GA0-61388998
http://linked.open...avai/riv/aktivita
http://linked.open...avai/riv/aktivity
  • I, P(GAP101/10/1329), P(TA03020277)
http://linked.open...vai/riv/dodaniDat
http://linked.open...aciTvurceVysledku
http://linked.open.../riv/druhVysledku
http://linked.open...iv/duvernostUdaju
http://linked.open...titaPredkladatele
http://linked.open...dnocenehoVysledku
  • 1778
http://linked.open...ai/riv/idVysledku
  • RIV/61388998:_____/14:00429082
http://linked.open...riv/jazykVysledku
http://linked.open.../riv/klicovaSlova
  • steam turbine; rotor; blade cascade; root section (en)
http://linked.open.../riv/klicoveSlovo
http://linked.open...ontrolniKodProRIV
  • [62F16C39089D]
http://linked.open...v/mistoKonaniAkce
  • Düsseldorf
http://linked.open...i/riv/mistoVydani
  • Düsseldorf
http://linked.open...i/riv/nazevZdroje
  • Proceedings of the ASME Turbo Expo 2014
http://linked.open...in/vavai/riv/obor
http://linked.open...ichTvurcuVysledku
http://linked.open...cetTvurcuVysledku
http://linked.open...vavai/riv/projekt
http://linked.open...UplatneniVysledku
http://linked.open...iv/tvurceVysledku
  • Šimurda, David
  • Luxa, Martin
  • Synáč, J.
  • Šafařík, P.
  • Rudas, B.
http://linked.open...vavai/riv/typAkce
http://linked.open.../riv/zahajeniAkce
number of pages
http://bibframe.org/vocab/doi
  • 10.1115/GT2014-25323
http://purl.org/ne...btex#hasPublisher
  • ASME
https://schema.org/isbn
  • 978-0-7918-4562-2
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