進階搜尋


   電子論文尚未授權公開,紙本請查館藏目錄
(※如查詢不到或館藏狀況顯示「閉架不公開」,表示該本論文不在書庫,無法取用。)
系統識別號 U0026-1608201612471600
論文名稱(中文) 渦輪螺旋槳引擎飛行性能與控制邏輯模擬研究
論文名稱(英文) Flight Performance and Control Logic Simulation of a Turboprop Engine
校院名稱 成功大學
系所名稱(中) 航空太空工程學系
系所名稱(英) Department of Aeronautics & Astronautics
學年度 104
學期 2
出版年 105
研究生(中文) 陳昱廷
研究生(英文) Yu-Ting Chen
學號 p46031165
學位類別 碩士
語文別 英文
論文頁數 58頁
口試委員 指導教授-賴維祥
口試委員-王振源
口試委員-洪嘉宏
口試委員-陳震宇
中文關鍵字 渦輪螺旋槳引擎  飛行性能  控制邏輯 
英文關鍵字 Turboprop  Flight Performance  Control Logic 
學科別分類
中文摘要 在渦輪螺旋槳引擎的應用上,擁有較高的推進效率以降低油耗的優點,因此,在短程飛行過程當中,不需要太大的推力,並且擁有其一定的速度與方便性,隨著無人飛機的發展越加興盛渦輪螺旋槳為一具有發展潛能的引擎。
在飛機飛行時,隨著高度變化,會影響環境的空氣密度與溫度,因而影響引擎的操作條件,此篇文獻在於探討其各層面的變化對飛機引擎的影響,除了引擎本身的壓縮器會因流量變化而導致湧振(Surge)或失速(Stall),葉輪的材料耐熱限度外,亦對飛行性能的表現作搭配,以期完成一引擎控制邏輯,能將之使用於我國未來航太工業之發展。
引擎之控制邏輯須使引擎在提供足夠的能量時,並確保引擎的各操作條件不會使超越極限值,以免發生引擎失效或損毀的情況,此文獻以探討各層面的影響為基礎,自行發展了一最小油量控制邏輯。
英文摘要 In the applications of a turboprop, it has a good propulsion efficiency to reduce the fuel cost. Therefore, it is a proper choice for a short-range flight that doesn’t need large thrust to fly at a fast speed. With the growing interest in unmanned aerial vehicles (UAVs), the turboprop is also a potential engine in this field.
During a flight, the ambient condition of the air density and temperature vary with changes in altitude and further affect both flight and engine performance. This study focused on any aspect that alternating the engine performance, in addition to compressor surge or stall due to the alternating flow rate, or the temperature limit of the turbine blade, a combination of the flight performance has been investigated.
The control logic of the engine is required to provide sufficient power and prevent the operating point from exceeding any structural limit to keep the engine operating safely. This study based on numerous aspects of the effect of the engine and developed a minimum of fuel supply control logic.
論文目次 中文摘要 I
Abstract II
誌謝 V
Table of Contents VI
List of Figures VIII
Nomenclature X
Chapter I Background and Literature Review 1
1.1 Introduction 1
1.2 Literature review 5
1.2.1 Control system design 5
1.2.2 The overall control logic 9
1.2.3 Control System Analysis 11
1.3 Motivation 16
Chapter II Engine Performance Considerations 17
2.1 Atmosphere 17
2.2 Brayton Cycle 20
2.3 Compressor and turbine efficiencies 22
2.3.1 Stagnation properties 22
2.3.2 Efficiencies calculation 23
2.3.3 Compressor map 24
2.4 Turboprop and Propeller performance 25
2.4.1 Turboprop Performance 25
2.4.2 Propeller Performance 26
2.5 Fight mechanics 28
Chapter III Engine Simulation 30
3.1 TPE-331-10 Turboprop Engine 30
3.2 GasTurb11 32
3.3 Simulation Processes and Result 33
3.3.1 Simulation Processes 33
3.3.2 Validity of Result 36
Chapter IV Control Logic Derivation and Verification 41
4.1 Control logic derivation 41
4.1.1 TPE331 fuel control system 41
4.1.2 Control logic derivation 44
4.1.2.1 Underspeed governor 44
4.1.2.2 Overspeed governor 45
4.2 Verification 48
4.2.1 Labview 48
4.1.2 Verification result 48
Chapter V Conclusions 52
Chapter VI Future Work 55
References 57


參考文獻 [1] Beno, V. and Adamcik Jr., F., “Unmanned Combat air Vehicle: MQ-9 Reaper,” International Conference of Scientific paper. AFASES, Brasov, 2014.
[2] Saravanamuttoo, H. I. H., “Modern Turboprop Engines,” Progress in Aerospace Science, Vol.24, pp.225-248, 1987.
[3] Mattingly, J.D., Elements of Propulsion, Gas Turbines and Rockets, AIAA, Reston, VA, 2006.
[4] Grag, S., “Aircraft Turbine Engine Control Research at NASA Glenn Research Center,” NASA/TM-2013-217821, 2013.
[5] Jaw, L. C. and Mattingly, J. D., Aircraft Engine Controls Design, System Analysis, and Health Monitoring, AIAA Education Series, American Institute of Aeronautics and Astronautics Inc., 2009.
[6] Mattingly, J. D., Heiser, W. H. and Pratt, D. T., Aircraft Engine Design, 2nd Edition, AIAA Education Series, American Institute of Aeronautics and Astronautics Inc., 2002.
[7] Saravanamuttoo, H. I. H., Rogers, G. F. C. and Cohen, H., Gas Turbine Theory 5th Edition, Pearson Education Limited, 2001
[8] Jaw, L. C., and Garg, S., Propulsion Control Technology Development in the United States-A Historical Perspective, NASA/TM - 2005-213978, 2005.
[9] Bernie, M. and Roy, L., Gas Turbine Propulsion System, John Wiley & Sons, Ltd, 2009.
[10] Sawyer, J.W., Gas Turbine Engineering Handbook, Gas Turbine Publications, Inc., 1966.
[11] Saravanamuttoo, H. I. H., Sjolander, S. A., Gauthier, J. E. D., Straznicky, P. V., Maclsaac, B. D., Gas Turbine Performance and Design - Short Course, Carleton University, 2003.
[12] Ogata, K., Modern Control Engineering 4th edition, Prentice Hall, 2002
[13] Spang, H. A., III, and Brown, H., “Control of Jet Engines,” Control Engineering Practice, Vol. 7, No. 9, pp.1043-1059, Sept. 1999.
[14] Chipperfield, A. J., Bica, B., and Fleming, P. J., “Fuzzy Scheduling Control of a Gas Turbine Aero-Engine: A Multiobjective Approach,” IEEE Transaction on Industrial Electronics, Vol. 49, No. 3, Jun. 2002.
[15] Bazazzadeh, M., Badihi, H., and Shahriari, A., “Gas Turbine Engine Control Design Using Fuzzy Logic and Neural Networks,” International Journal of Aerospace Engineering, Vol. 2011, 2011.
[16] U.S. Standard Atmosphere, U.S. Government Printing Office, Washington, D.C., Oct, 1976.
[17] https://en.wikipedia.org/wiki/Compressor_map
[18] Richard, S. S., Fundamentals of flight, Englewood Cliffs, N.J., Prentice Hall, 1989.
[19] Bronz, M., Moschetta, J. M., and Hattenberger, G., “Multi-Point Optimisation of a Propulsion Set as Applied to a Multi-Tasking MAV,” International Micro Aerial Vehicle Conference and Competition, Braunschweig, Germany, Jul 2012.
[20] Honeywell company, TPE331-10 Turboprop Engine-Advanced Engine Performance and Power Generation Capability, N61-0346-000-002, Mar, 2014.
[21] Honeywell company, TPE331 Pilot Tips, PA02-3203, May, 2004.
[22] Kurzke, J., Advanced User-friendly Gas Turbine Performance Calculations on a Personal Computer, 95-GT-147, International Gas Turbine and Aeroengine Congress and Exposition, Houston, Texas, USA, June 5-8, 1995.
[23] Thomas, W. W, and Michael, J. K., Aircraft Powerplants 8th edition, McGraw-Hill Education, 2014.
論文全文使用權限
  • 同意授權校內瀏覽/列印電子全文服務,於2021-08-18起公開。
  • 同意授權校外瀏覽/列印電子全文服務,於2021-08-18起公開。


  • 如您有疑問,請聯絡圖書館
    聯絡電話:(06)2757575#65773
    聯絡E-mail:etds@email.ncku.edu.tw