A scientometric analysis and critical review of gas turbine aero-engines control: From Whittle engine to more-electric propulsion
The gas turbine aero-engine control systems over the past eight decades have been thoroughly investigated. This review purposes are to present a comprehensive reference for aero-engine control design and development based on a systematic scientometric analysis and to categorize different methods, al...
| Main Authors: | , , , |
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| Format: | Article |
| Language: | English |
| Published: |
SAGE Publishing
2021-05-01
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| Series: | Measurement + Control |
| Online Access: | https://doi.org/10.1177/0020294020956675 |
| _version_ | 1818731990517547008 |
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| author | Seyed Jalal Mohammadi Seyed Alireza Miran Fashandi Soheil Jafari Theoklis Nikolaidis |
| author_facet | Seyed Jalal Mohammadi Seyed Alireza Miran Fashandi Soheil Jafari Theoklis Nikolaidis |
| author_sort | Seyed Jalal Mohammadi |
| collection | DOAJ |
| description | The gas turbine aero-engine control systems over the past eight decades have been thoroughly investigated. This review purposes are to present a comprehensive reference for aero-engine control design and development based on a systematic scientometric analysis and to categorize different methods, algorithms, and approaches taken into account to improve the performance and operability of aircraft engines from the first days to present to enable this challenging technology to be adopted by aero-engine manufacturers. Initially, the benefits of the control systems are restated in terms of improved engine efficiency, reduced carbon dioxide emissions, and improved fuel economy. This is followed by a historical coverage of the proposed concepts dating back to 1936. A comprehensive scientometric analysis is then presented to introduce the main milestones in aero-engines control. Possible control strategies and concepts are classified into four distinct phases, including Single input- single output control algorithms, MIN-MAX or Cascade control algorithms, advanced control algorithms, More-electric and electronic control algorithms and critically reviewed. The advantages and disadvantages of milestones are discussed to cover all practical aspects of the review to enable the researchers to identify the current challenges in aircraft engine control systems. |
| first_indexed | 2024-12-17T23:26:27Z |
| format | Article |
| id | doaj.art-a17a39b6996145bfbde16fa61174afbf |
| institution | Directory Open Access Journal |
| issn | 0020-2940 |
| language | English |
| last_indexed | 2024-12-17T23:26:27Z |
| publishDate | 2021-05-01 |
| publisher | SAGE Publishing |
| record_format | Article |
| series | Measurement + Control |
| spelling | doaj.art-a17a39b6996145bfbde16fa61174afbf2022-12-21T21:28:45ZengSAGE PublishingMeasurement + Control0020-29402021-05-015410.1177/0020294020956675A scientometric analysis and critical review of gas turbine aero-engines control: From Whittle engine to more-electric propulsionSeyed Jalal Mohammadi0Seyed Alireza Miran Fashandi1Soheil Jafari2Theoklis Nikolaidis3Iran University of Science and Technology, Tehran, IranIran University of Science and Technology, Tehran, IranCranfield University, Cranfield, UKCranfield University, Cranfield, UKThe gas turbine aero-engine control systems over the past eight decades have been thoroughly investigated. This review purposes are to present a comprehensive reference for aero-engine control design and development based on a systematic scientometric analysis and to categorize different methods, algorithms, and approaches taken into account to improve the performance and operability of aircraft engines from the first days to present to enable this challenging technology to be adopted by aero-engine manufacturers. Initially, the benefits of the control systems are restated in terms of improved engine efficiency, reduced carbon dioxide emissions, and improved fuel economy. This is followed by a historical coverage of the proposed concepts dating back to 1936. A comprehensive scientometric analysis is then presented to introduce the main milestones in aero-engines control. Possible control strategies and concepts are classified into four distinct phases, including Single input- single output control algorithms, MIN-MAX or Cascade control algorithms, advanced control algorithms, More-electric and electronic control algorithms and critically reviewed. The advantages and disadvantages of milestones are discussed to cover all practical aspects of the review to enable the researchers to identify the current challenges in aircraft engine control systems.https://doi.org/10.1177/0020294020956675 |
| spellingShingle | Seyed Jalal Mohammadi Seyed Alireza Miran Fashandi Soheil Jafari Theoklis Nikolaidis A scientometric analysis and critical review of gas turbine aero-engines control: From Whittle engine to more-electric propulsion Measurement + Control |
| title | A scientometric analysis and critical review of gas turbine aero-engines control: From Whittle engine to more-electric propulsion |
| title_full | A scientometric analysis and critical review of gas turbine aero-engines control: From Whittle engine to more-electric propulsion |
| title_fullStr | A scientometric analysis and critical review of gas turbine aero-engines control: From Whittle engine to more-electric propulsion |
| title_full_unstemmed | A scientometric analysis and critical review of gas turbine aero-engines control: From Whittle engine to more-electric propulsion |
| title_short | A scientometric analysis and critical review of gas turbine aero-engines control: From Whittle engine to more-electric propulsion |
| title_sort | scientometric analysis and critical review of gas turbine aero engines control from whittle engine to more electric propulsion |
| url | https://doi.org/10.1177/0020294020956675 |
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