PHYSICAL MODEL OF A RADIAL TURBINE WITH UNSTEADY FLOW USED FOR OPTIMIZATION OF TURBINE MATCHING

Kód výsledku v IS VaVaI

<a href="https://www.isvavai.cz/riv?ss=detail&h=RIV%2F68407700%3A21220%2F17%3A00320358" target="_blank" >RIV/68407700:21220/17:00320358 - isvavai.cz</a>

Výsledek na webu

<a href="https://lccn.loc.gov/2017028105" target="_blank" >https://lccn.loc.gov/2017028105</a>

DOI - Digital Object Identifier

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Jazyk výsledku

angličtina

Název v původním jazyce

PHYSICAL MODEL OF A RADIAL TURBINE WITH UNSTEADY FLOW USED FOR OPTIMIZATION OF TURBINE MATCHING

Popis výsledku v původním jazyce

Advantages of physical models of different complexity compared to map-based model employed in engine thermodynamics simulation codes. No need for dimensionless coefficients, only power and mass flow rate are relevant. Principles of physical modelling of radial turbines based on a central streamline model for single- and twin-scroll layout with controlable blades - variable geometry turbines - or vaneless nozzle ring. Basic conservation equations, description of turbine geometry, aerodynamic and friction losses and use of commercial solvers for finding numerical results. Central streamline model using quasi-steady approach or fully one-dimensional unsteady description of in-turbine processes including flow in a scroll, a nozzle ring, vaneless nozzle ring, mixing zone upstream an impeller, an impeller itself and outlet diffuser. Sonic limits. Definitions of averaged angles of flow and loss coefficients (partial isentropic efficiencies), Reynolds number influence. Predictive ability of physical model by using experimentally or in CFD found loss coefficients. Basic issues of turbine map measurements in single- or twin-scroll arrangement using a compressor for turbine loading. Model-based experiments, measurement evaluation and model calibration using optimization methods. Specific features of turbine operation with pulse exhaust manifold at an engine and measurement of unsteady operation under pressure/temperature pulses at fluctuating turbine shaft speed. Application of the model: Methods for turbine – engine – compressor matching using the physical model. Extrapolation of experience from similar systems before detailed CFD simulation or experiments are done. Transferring turbine features found during mapping back to the design stage at a turbocharger manufacturer.

Název v anglickém jazyce

PHYSICAL MODEL OF A RADIAL TURBINE WITH UNSTEADY FLOW USED FOR OPTIMIZATION OF TURBINE MATCHING

Popis výsledku anglicky

Advantages of physical models of different complexity compared to map-based model employed in engine thermodynamics simulation codes. No need for dimensionless coefficients, only power and mass flow rate are relevant. Principles of physical modelling of radial turbines based on a central streamline model for single- and twin-scroll layout with controlable blades - variable geometry turbines - or vaneless nozzle ring. Basic conservation equations, description of turbine geometry, aerodynamic and friction losses and use of commercial solvers for finding numerical results. Central streamline model using quasi-steady approach or fully one-dimensional unsteady description of in-turbine processes including flow in a scroll, a nozzle ring, vaneless nozzle ring, mixing zone upstream an impeller, an impeller itself and outlet diffuser. Sonic limits. Definitions of averaged angles of flow and loss coefficients (partial isentropic efficiencies), Reynolds number influence. Predictive ability of physical model by using experimentally or in CFD found loss coefficients. Basic issues of turbine map measurements in single- or twin-scroll arrangement using a compressor for turbine loading. Model-based experiments, measurement evaluation and model calibration using optimization methods. Specific features of turbine operation with pulse exhaust manifold at an engine and measurement of unsteady operation under pressure/temperature pulses at fluctuating turbine shaft speed. Application of the model: Methods for turbine – engine – compressor matching using the physical model. Extrapolation of experience from similar systems before detailed CFD simulation or experiments are done. Transferring turbine features found during mapping back to the design stage at a turbocharger manufacturer.

Druh

C - Kapitola v odborné knize

CEP obor

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OECD FORD obor

20303 - Thermodynamics

Projekt

Výsledek vznikl pri realizaci vícero projektů. Více informací v záložce Projekty.

Návaznosti

P - Projekt vyzkumu a vyvoje financovany z verejnych zdroju (s odkazem do CEP)

Rok uplatnění

2017

Kód důvěrnosti údajů

S - Úplné a pravdivé údaje o projektu nepodléhají ochraně podle zvláštních právních předpisů

Název knihy nebo sborníku

Turbochargers and turbocharging: Advancements, applications and research

ISBN

978-1-5361-2239-8

Počet stran výsledku

84

Strana od-do

271-354

Počet stran knihy

538

Název nakladatele

Nova Science Publisher, Inc.

Místo vydání

Hauppauge NY

Kód UT WoS kapitoly

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