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Detailed Simulations of a Three-Stage Supercritical Carbon Dioxide Axial Compressor with a Focus on the Shrouded Stator Cavities Flow

Journal Article · · Processes
DOI:https://doi.org/10.3390/pr11051358· OSTI ID:2418728
 [1];  [2]
  1. Univ. of Cincinnati, OH (United States); University of Cincinnati, OH (United States)
  2. Univ. of Cincinnati, OH (United States)
This paper describes the findings of detailed simulations performed to investigate the impact of seal teeth cavity leakage flow on the aerodynamic and thermal performance of a three-stage supercritical CO2 axial compressor. The study compares a shrouded stator configuration (with cavities) to a cantilevered stator configuration (without cavities) to highlight their differences. High-fidelity computational fluid dynamics simulations were performed using non-linear harmonic (NLH) and mixing plane assumptions, considering various possible rotor/stator interface configurations for mixing plane calculations. The key performance parameters for each case were compared, and the best-performing configuration selected for further analysis. The individual stage performance parameters are also examined and compared between the cantilevered and shrouded configurations. It was observed that in the shrouded case, the leakage flow enters the cavity downstream of the stator trailing edge and gets entrained into the primary flow upstream of the stator, leading to boundary layer changes at the hub and degradation of stator and downstream rotor performance. Vortical flow structures were also observed in the stator wells, which tended to change the flow angles around the region, thereby affecting mixing and velocity distribution, resulting in a slight deterioration of compressor performance. Additionally, the study examines windage heating due to shear work from rotating walls, including the seal teeth surface. The amount of shear work done on the leakage flow and the corresponding rise in fluid temperature were quantified, tabulated, and further compared with a simple analytical model, showing good agreement between them and, hence, validating the numerical approach used.
Research Organization:
Echogen Power Systems (Delaware), Inc., Akron, OH (United States)
Sponsoring Organization:
USDOE Office of Energy Efficiency and Renewable Energy (EERE), Renewable Power Office. Solar Energy Technologies Office
Grant/Contract Number:
EE0008997
OSTI ID:
2418728
Journal Information:
Processes, Journal Name: Processes Journal Issue: 5 Vol. 11; ISSN 2227-9717
Publisher:
MDPICopyright Statement
Country of Publication:
United States
Language:
English

References (18)

Heat transfer in cylindrical shrouded cavities journal June 1977
Aerodynamic and heat transfer performances of a highly loaded transonic turbine rotor with upstream generic rim seal cavity journal December 2021
The NIST REFPROP Database for Highly Accurate Properties of Industrially Important Fluids journal June 2022
The Influence of Shrouded Stator Cavity Flows on Multistage Compressor Performance journal July 1999
On the Conservation of Rothalpy in Turbomachines journal July 1993
Effect of the Stator Hub Configuration and Stage Design Parameters on Aerodynamic Loss in Axial Compressors journal September 2015
Details of Shrouded Stator Hub Cavity Flow in a Multistage Axial Compressor Part 2: Leakage Flow Characteristics in Stator Wells journal November 2021
A Wall Function for Calculating the Skin Friction With Surface Roughness conference January 2004
A Turbomachinery Design Tool for Teaching Design Concepts for Axial-Flow Fans, Compressors, and Turbines conference January 2006
Numerical Investigation on the Flow Characteristics of a Supercritical CO2 Centrifugal Compressor
  • Zhao, Hang; Deng, Qinghua; Zheng, Kuankuan
  • Volume 3B: Oil and Gas Applications; Organic Rankine Cycle Power Systems; Supercritical CO2 Power Cycles; Wind Energy https://doi.org/10.1115/GT2014-26646
conference June 2014
Modeling Capability for Cavity Flows in an Axial Compressor conference June 2017
Open Source Axial Compressor Mean-Line Design Tool for Supercritical Carbon Dioxide conference June 2021
Detailed Design and Optimization of the First Stage of an Axial Supercritical CO2 Compressor
  • Ha, Matthew; Holder, Justin; Ghimire, Saugat
  • Volume 10C: Turbomachinery — Design Methods and CFD Modeling for Turbomachinery; Ducts, Noise, and Component Interactions https://doi.org/10.1115/GT2022-82590
conference June 2022
Research on Flow Characteristics of Supercritical CO2 Axial Compressor Blades by CFD Analysis conference January 2009
Compressor Design for the Supercritical CO2 Brayton Cycle conference August 2004
Aerothermal Investigation of Seal Teeth Cavity Leakage Flow in Supercritical CO2 Compressor conference January 2023
Investigation of Seal Cavity Leakage Flow Effect on Multistage Axial Compressor Aerodynamic Performance with a Circumferentially Averaged Method journal April 2021
Preliminary Design and Model Assessment of a Supercritical CO2 Compressor journal April 2018

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