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Comparison and Sensibility Analysis of Warning Parameters for Rotating Stall Detection in an Axial Compressor

Article dans une revue avec comité de lecture
Auteur
MARGALIDA, Gabriel
ROUSSETTE, Olivier
ccDAZIN, Antoine
531216 Laboratoire de Mécanique des Fluides de Lille - Kampé de Fériet [LMFL]
ccJOSEPH, Pierric

URI
http://hdl.handle.net/10985/19179
DOI
10.3390/ijtpp5030016
Date
2020
Journal
International Journal of Turbomachinery, Propulsion and Power

Résumé

The present paper aims at evaluating the surveillance parameters used for early stall warning in axial compressors, and is based on unsteady pressure measurements at the casing of a single stage axial compressor. Two parameters—Correlation and Root Mean Square (RMS)—are first compared and their relative performances discussed. The influence of sensor locations (in both radial and axial directions) is then considered, and the role of the compressor’s geometrical irregularities in the behavior of the indicators is clearly highlighted. The influence of the throttling process is also carefully analyzed. This aspect of the experiment’s process appears to have a non-negligible impact on the stall warning parameters, despite being poorly documented in the literature. This last part of this research work allow us to get a different vision of the alert parameters compared to what is classically done in the literature, as the level of irregularity that is reflected by the magnitude of the parameters appears to be an image of a given flow rate value, and not a clear indicator of the stall inception.

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Documents liés

Visualiser des documents liés par titre, auteur, créateur et sujet.

  • Stall Margin Improvement in an Axial Compressor by Continuous and Pulsed Tip Injection 
    Article dans une revue avec comité de lecture
    MOUBOGHA MOUBOGHA, Joseph; MARGALIDA, Gabriel; ROUSSETTE, Olivier; ccDAZIN, Antoine; ccJOSEPH, Pierric (MDPI AG, 2022-03)
    Stall and surge are strong limitations in the operating range of compressors and thus one of the major limits of jet engine performance. A promising way to push the stability limit of compression machines is to inject a ...
  • Detailed Pressure Measurements During the Transition to Rotating Stall in an Axial Compressor: Influence of the Throttling Process 
    Communication avec acte
    MARGALIDA, Gabriel; ROUSSETTE, Olivier; ccDAZIN, Antoine; ccJOSEPH, Pierric (ASME, 2018)
    This paper presents experimental unsteady pressure measurements gathered on a single stage axial compressor during pre-stall and transition to stall operations. The aim of this study is to analyze the transition from a ...
  • Pulsed air injection system characterization for stall margin improvement in an axial compressor 
    Communication avec acte
    MARGALIDA, Gabriel; ROUSSETTE, Olivier; DELVA, Jérôme; ccDAZIN, Antoine; ccJOSEPH, Pierric (EUCASS association, 2022-06-27)
    This paper presents the design and the characterization of a pulsed air injection system on a single stage axial compressor. The goal of this system is to delay the rotating stall onset and to extend the compressor operating ...
  • Active flow control in an axial compressor for stability improvement : On the effect of flow control on stall inception 
    Article dans une revue avec comité de lecture
    MARGALIDA, Gabriel; ROUSSETTE, Olivier; ccDAZIN, Antoine; ccJOSEPH, Pierric (Springer Verlag (Germany), 2021)
    In this paper, the effect of an active flow control system on the onset mechanism of rotating stall in an axial compressor is experimentally investigated. A particular emphasis is thus given on the flow patterns present ...
  • Experimental Flow Investigation Inside an Axial Compressor with Active Flow Control 
    Communication avec acte
    MOUBOGHA MOUBOGHA, Joseph; ROUSSETTE, Olivier; ccDAZIN, Antoine; ccJOSEPH, Pierric (ASME, 2022-06)
    This paper describes the experimental study of the flow behavior in a rotor blade channel of an axial compressor equipped with an Active Flow Control (AFC) system using Particle Image Velocimetry. The AFC system consists ...

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