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Review of gliding arc plasma assisted ignition and combustion for gas turbine application

  • Ka Gong , Yibo Liu , Honghua Zhao and Zhikai Wang EMAIL logo
Published/Copyright: August 29, 2024
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International Journal of Turbo & Jet-Engines
From the journal International Journal of Turbo & Jet-Engines Volume 42 Issue 2

Abstract

The potential of gliding arc plasma-assisted ignition and combustion technology to enhance ignition and combustion performance is attracting increasing attention from the scientific community. A multitude of experimental studies have been conducted by scientists and engineers on its application in gas turbine combustors. This paper presents a review of the research conducted on gliding arc plasma-assisted ignition and combustion over the past five years. Gliding arc plasma exerts a multitude of effects on combustion processes. These effects can be broadly categorized as follows: (1) reduction in ignition delay time; (2) expansion of ignition and lean blowout boundaries; (3) enhancement of ultra-lean burning combustion and low-temperature flame stability; (4) improvement in combustion efficiency; (5) reduction in pollutant emissions; (6) augmentation of stability of unstable fuels such as ammonia. Finally, a prospection on the application of gliding arc plasma assisted ignition and combustion technology in gas turbine combustor is presented.

Keywords: gliding arc plasma; plasma-assisted ignition; plasma-assisted combustion; gas turbine; lean blowout
Corresponding author: Zhikai Wang, AECC Hunan Aviation Powerplant Research Institute, Zhuzhou 412002, China, E-mail:

  1. Research ethics: Not applicable.

  2. Author contributions: The authors have accepted responsibility for the entire content of this manuscript and approved its submission.

  3. Competing interests: The authors state no conflict of interest.

  4. Research funding: None declared.

  5. Data availability: Not applicable.

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Received: 2024-05-21
Accepted: 2024-06-26
Published Online: 2024-08-29
Published in Print: 2025-05-26

© 2024 Walter de Gruyter GmbH, Berlin/Boston

Articles in the same Issue

  1. Frontmatter
  2. Deep residual ensemble model for predicting remaining useful life of turbo fan engines
  3. Review of gliding arc plasma assisted ignition and combustion for gas turbine application
  4. Interaction effects between the rotor wake and hub leakage flow in a multi-stage cantilevered compressor
  5. Determination of the modern marine single shaft gas turbine rotor blades fatigue strength parameters
  6. Role of different cavity flame holders on the performance characteristics of supersonic combustor
  7. Thermal performance of teardrop pin fins and zig zag ribs in a wedge channel
  8. Investigation of varying tip clearance gap and operating conditions on the fulfilment of low-speed axial flow fan
  9. Upgraded one-dimensional code for the design of a micro gas turbine mixed flow compressor stage with various crossover diffuser configurations
  10. Performance evaluation of a scramjet engine utilizing varied cavity aft wall divergence with parallel injection in a reacting flow field
  11. Speed controller design for turboshaft engine using a high-fidelity AeroThermal model
  12. Multi-nozzle thrust matching control of STOVL engine
  13. Numerical analysis of brush seal hysteresis based on orthogonal test method
  14. Conjugated heat transfer characteristics of ribbed-swirl cooling in turbine blade under rotation condition
  15. Flow pattern formation due to the interdependency of multi-component interactions and their impact on the performance of turbine and exhaust duct of gas turbine
  16. Flight trajectory optimization study of a variable-cycle turbine-based combined cycle engine hypersonic vehicle based on airframe/engine integration
  17. Constant temperature line identification on prototype gas turbine combustor with multi-colour change coating
  18. Sensitivity analysis of aero-engine performance optimization control system and its hardware test verification
  19. Compensator based improved model predictive control for Aero-engine
  20. Ignition experimental study based on rotating gliding arc
https://doi.org/10.1515/tjj-2024-0045
Keywords for this article
gliding arc plasma; plasma-assisted ignition; plasma-assisted combustion; gas turbine; lean blowout

Articles in the same Issue

  1. Frontmatter
  2. Deep residual ensemble model for predicting remaining useful life of turbo fan engines
  3. Review of gliding arc plasma assisted ignition and combustion for gas turbine application
  4. Interaction effects between the rotor wake and hub leakage flow in a multi-stage cantilevered compressor
  5. Determination of the modern marine single shaft gas turbine rotor blades fatigue strength parameters
  6. Role of different cavity flame holders on the performance characteristics of supersonic combustor
  7. Thermal performance of teardrop pin fins and zig zag ribs in a wedge channel
  8. Investigation of varying tip clearance gap and operating conditions on the fulfilment of low-speed axial flow fan
  9. Upgraded one-dimensional code for the design of a micro gas turbine mixed flow compressor stage with various crossover diffuser configurations
  10. Performance evaluation of a scramjet engine utilizing varied cavity aft wall divergence with parallel injection in a reacting flow field
  11. Speed controller design for turboshaft engine using a high-fidelity AeroThermal model
  12. Multi-nozzle thrust matching control of STOVL engine
  13. Numerical analysis of brush seal hysteresis based on orthogonal test method
  14. Conjugated heat transfer characteristics of ribbed-swirl cooling in turbine blade under rotation condition
  15. Flow pattern formation due to the interdependency of multi-component interactions and their impact on the performance of turbine and exhaust duct of gas turbine
  16. Flight trajectory optimization study of a variable-cycle turbine-based combined cycle engine hypersonic vehicle based on airframe/engine integration
  17. Constant temperature line identification on prototype gas turbine combustor with multi-colour change coating
  18. Sensitivity analysis of aero-engine performance optimization control system and its hardware test verification
  19. Compensator based improved model predictive control for Aero-engine
  20. Ignition experimental study based on rotating gliding arc
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