A review of active control approaches in stabilizing combustion systems in aerospace industry. (February 2018)
- Record Type:
- Journal Article
- Title:
- A review of active control approaches in stabilizing combustion systems in aerospace industry. (February 2018)
- Main Title:
- A review of active control approaches in stabilizing combustion systems in aerospace industry
- Authors:
- Zhao, Dan
Lu, Zhengli
Zhao, He
Li, X.Y.
Wang, Bing
Liu, Peijin - Abstract:
- Abstract: Self-sustained combustion instabilities are one of the most plaguing challenges and problems in lean-conditioned propulsion and land-based engine systems, such as rocket motors, gas turbines, industrial furnace and boilers, and turbo-jet thrust augmenters. Either passive or active control in open- or closed-loop configurations can be implemented to mitigate such instabilities. One of the classical disadvantages of passive control is that it is only implementable to a designed combustor over a limited frequency range and can not respond to the changes in operating conditions. Compared with passive control approaches, active control, especially in closed-loop configuration is more adaptive and has inherent capacity to be implemented in practice. The key components in closed-loop active control are 1) sensor, 2) controller (optimization algorithm) and 3) dynamic actuator. The present work is to outline the current status, technical challenges and development progress of the active control approaches (in open- or closed-loop configurations). A brief description of feedback control, adaptive control, model-based control and sliding mode control are provided first by introducing a simplified Rijke-type combustion system. The modelled combustion system provides an invaluable platform to evaluate the performance of these feedback controllers and a transient growth controller. The performance of these controllers are compared and discussed. An outline of theoretical,Abstract: Self-sustained combustion instabilities are one of the most plaguing challenges and problems in lean-conditioned propulsion and land-based engine systems, such as rocket motors, gas turbines, industrial furnace and boilers, and turbo-jet thrust augmenters. Either passive or active control in open- or closed-loop configurations can be implemented to mitigate such instabilities. One of the classical disadvantages of passive control is that it is only implementable to a designed combustor over a limited frequency range and can not respond to the changes in operating conditions. Compared with passive control approaches, active control, especially in closed-loop configuration is more adaptive and has inherent capacity to be implemented in practice. The key components in closed-loop active control are 1) sensor, 2) controller (optimization algorithm) and 3) dynamic actuator. The present work is to outline the current status, technical challenges and development progress of the active control approaches (in open- or closed-loop configurations). A brief description of feedback control, adaptive control, model-based control and sliding mode control are provided first by introducing a simplified Rijke-type combustion system. The modelled combustion system provides an invaluable platform to evaluate the performance of these feedback controllers and a transient growth controller. The performance of these controllers are compared and discussed. An outline of theoretical, numerical and experimental investigations are then provided to overview the research and development progress made during the last 4 decades. Finally, potential, challenges and issues involved with the design, application and implementation of active combustion control strategies on a practical engine system are highlighted. … (more)
- Is Part Of:
- Progress in aerospace sciences. Volume 97(2018:Feb.)
- Journal:
- Progress in aerospace sciences
- Issue:
- Volume 97(2018:Feb.)
- Issue Display:
- Volume 97 (2018)
- Year:
- 2018
- Volume:
- 97
- Issue Sort Value:
- 2018-0097-0000-0000
- Page Start:
- 35
- Page End:
- 60
- Publication Date:
- 2018-02
- Subjects:
- Active control -- Engine system -- Propulsion -- Aeroacoustics -- Combustion instability -- Feedback control -- Thermoacoustics
Aeronautics -- Periodicals
Astronautics -- Periodicals
Aéronautique -- Périodiques
Astronautique -- Périodiques
629.1 - Journal URLs:
- http://www.sciencedirect.com/science/journal/03760421 ↗
http://www.elsevier.com/journals ↗ - DOI:
- 10.1016/j.paerosci.2018.01.002 ↗
- Languages:
- English
- ISSNs:
- 0376-0421
- Deposit Type:
- Legaldeposit
- View Content:
- Available online (eLD content is only available in our Reading Rooms) ↗
- Physical Locations:
- British Library DSC - 6865.902000
British Library DSC - BLDSS-3PM
British Library HMNTS - ELD Digital store - Ingest File:
- 5863.xml