Published February 15, 2016 | Version v1
Journal article

An investigation on unsteadiness of a mixed-flow turbine under pulsating conditions

  • 1. School of Mechanical Engineering, Shanghai Jiao Tong University, Shanghai 200240 (China)
  • 2. Mechanical Engineering Department, Imperial College London, London SW7 2AZ (United Kingdom)
  • 3. Automotive Engineering Department, Tsinghua University, Beijing 100084 (China)

Description

Highlights: • Analytical model proves gradient of total pressure as the root of the unsteadiness. • Product of Strouhal number and magnitude is proportional to turbine unsteadiness. • Asymptotic curves exist in hysteresis loops for influence of frequency or magnitude. - Abstract: The turbocharger is the key enabler for energy conservation in Internal Combustion Engine (ICE). A turbine of a turbocharger is fed by highly pulsating flow due to the reciprocating engine, resulting in different behavior from that at steady conditions. This paper investigates the behavior of a mix-flow turbine under pulsating conditions via an analytical model and an in-house developed 1-D unsteady code ONDAS. Firstly, an analytical model of the 'unsteadiness' based on the mass flow imbalance is built and the mechanism of the unsteady behavior is discussed in details. Next, a 1-D unsteady model of the turbine under pulsating conditions is established and validated by experimental results. Finally, influence of the frequency, the magnitude and their product on unsteady behavior of the turbine is investigated by the reduced order model for further exploration of the analytical model. The investigation clearly demonstrates the impact of pulsating flow on the unsteady performance and unveils the mechanism of the 'unsteadiness' of turbine under pulsating conditions.

Availability note (English)

Available from http://dx.doi.org/10.1016/j.enconman.2015.12.007

Additional details

Identifiers

DOI
10.1016/j.enconman.2015.12.007;
PII
S0196-8904(15)01095-X;

Publishing Information

Journal Title
Energy Conversion and Management
Journal Volume
110
Journal Page Range
p. 51-58
ISSN
0196-8904
CODEN
ECMADL

INIS

Country of Publication
United Kingdom
Country of Input or Organization
International Atomic Energy Agency (IAEA)
INIS RN
48003050
Subject category
S42: ENGINEERING;
Descriptors DEI
COMBUSTION; DIAGRAMS; ENERGY CONSERVATION; FLUID FLOW; FREQUENCY DEPENDENCE; HYSTERESIS; INTERNAL COMBUSTION ENGINES; TURBINES; TURBOCHARGERS
Descriptors DEC
CHEMICAL REACTIONS; COMPRESSORS; ENGINES; EQUIPMENT; HEAT ENGINES; INFORMATION; MACHINERY; OXIDATION; SUPERCHARGERS; THERMOCHEMICAL PROCESSES; TURBOMACHINERY

Optional Information

Copyright
Copyright (c) 2015 Elsevier Science B.V., Amsterdam, The Netherlands, All rights reserved.