鱼雷涡轮动力系统仿真研究
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摘要
现代海战对鱼雷的各战术指标提出了更高更新的要求，而研究更高效的鱼雷动力系统更是鱼雷发展的迫切要求。由于仿真技术具有安全性和经济性的两大特点，因而在各个领域内逐步兴起。采用仿真技术来研究鱼雷动力系统，为鱼雷动力系统的设计和发展提供了一种新的思路。
本文对鱼雷涡轮机结构类型、鱼雷涡轮机的三速制工况进行了计算研究，对涡轮发动机的工作过程进行了分析。以工程热力学为基础，建立了涡轮机内部参数和热力计算的数学模型，并对鱼雷涡轮机的各个部分进行了热力计算和结构设计计算。分析了各个参数之间的相互影响。对鱼雷处于非设计工况时的参数进行了分析。
建立了开式鱼雷涡轮动力系统的稳态过程、开环状念下的恒深变速过程、恒速变深过程的动态数学模型，采用经典的四阶龙格—库塔算法对其进行了仿真计算，得到了比较满意的结果。并采用面向对象语言Delphi6.0编制了具有友好用户界面的仿真程序，用MATLAB6.0对仿真过程进行了分析。相信得到的仿真曲线和仿真程序在鱼雷涡轮动力装置的设计过程中发挥良好的作用，并在未来鱼雷总体设计、仿真中同样具有重要的参考价值。
More and more higher performance of thermodynamic propulsion system of torpedo is required to adapt to the modern sea tight. So the research of efficient thermodynamic propulsion system becomes urgent in the research and development of torpedo. Because of its security and economical use. digital simulation technology is widely being used in all kind of engineering fields. The use of digital simulation technology in thermodynamic torpedo provides a new way to the design and development of thermodynamic propulsion system.
In the paper, the structure type of torpedo turbine engine and the three-speed system states of work gas were researched. The work process of torpedo turbine engine was analyzed. Based on the theory of engineering thermodynamics, inner parameter and thermodynamic calculation mathematic model of turbine engine were established. The thermodynamic calculation and the structure design of torpedo turbine engine were completed at the same time. In addition, the interaction of all parameters was analyzed. The non-design condition parameters of torpedo turbine engine were also analyzed.
It was established that the dynamic mathematic models of typical work state: steady states, process of changing speed of the open-loop propulsion system in the same depth, process of changing depth in the same speed. Four steps Runge-Kutta was adopted in the simulation of the process mentioned above, satisfying results gained. After simulator program with friendly interface programmed using object oriented language, Delphi 6.0, the simulator process was analyzed with MATLAB 6.0. Simulator curves and programs will work well in the design of torpedo turbine propulsion system and have important reference value in the design and simulation of whole torpedo.
本文对鱼雷涡轮机结构类型、鱼雷涡轮机的三速制工况进行了计算研究，对涡轮发动机的工作过程进行了分析。以工程热力学为基础，建立了涡轮机内部参数和热力计算的数学模型，并对鱼雷涡轮机的各个部分进行了热力计算和结构设计计算。分析了各个参数之间的相互影响。对鱼雷处于非设计工况时的参数进行了分析。
建立了开式鱼雷涡轮动力系统的稳态过程、开环状念下的恒深变速过程、恒速变深过程的动态数学模型，采用经典的四阶龙格—库塔算法对其进行了仿真计算，得到了比较满意的结果。并采用面向对象语言Delphi6.0编制了具有友好用户界面的仿真程序，用MATLAB6.0对仿真过程进行了分析。相信得到的仿真曲线和仿真程序在鱼雷涡轮动力装置的设计过程中发挥良好的作用，并在未来鱼雷总体设计、仿真中同样具有重要的参考价值。
More and more higher performance of thermodynamic propulsion system of torpedo is required to adapt to the modern sea tight. So the research of efficient thermodynamic propulsion system becomes urgent in the research and development of torpedo. Because of its security and economical use. digital simulation technology is widely being used in all kind of engineering fields. The use of digital simulation technology in thermodynamic torpedo provides a new way to the design and development of thermodynamic propulsion system.
In the paper, the structure type of torpedo turbine engine and the three-speed system states of work gas were researched. The work process of torpedo turbine engine was analyzed. Based on the theory of engineering thermodynamics, inner parameter and thermodynamic calculation mathematic model of turbine engine were established. The thermodynamic calculation and the structure design of torpedo turbine engine were completed at the same time. In addition, the interaction of all parameters was analyzed. The non-design condition parameters of torpedo turbine engine were also analyzed.
It was established that the dynamic mathematic models of typical work state: steady states, process of changing speed of the open-loop propulsion system in the same depth, process of changing depth in the same speed. Four steps Runge-Kutta was adopted in the simulation of the process mentioned above, satisfying results gained. After simulator program with friendly interface programmed using object oriented language, Delphi 6.0, the simulator process was analyzed with MATLAB 6.0. Simulator curves and programs will work well in the design of torpedo turbine propulsion system and have important reference value in the design and simulation of whole torpedo.
引文
1、赵寅生 鱼雷涡轮机原理 西北工业大学出版社 2002
2、赵连峰 鱼雷活塞发动机原理 西北工业大学出版社 1991
3、刘讯谦 鱼雷推进剂及供应系统 西北工业大学出版社 1991
4、马世杰 鱼雷热动力装置设计原理 兵器工业出版社 1992
5、李启炎 PASCAL程序设计语言 同济大学出版社 1999
6、张可村 数值计算的算法与分析 科学出版社 2003
7、鲁宗相 Delphi5入门与提高 清华大学出版社 2000
8、宋明玉 开式循环鱼雷热动力系统数字仿真及H_∞控制研究 西北工业大学硕士学位论文 1997
9、翁史烈 船舶动力装置仿真技术 上海交通大学出版社 1991
10、张宇文 鱼雷弹道与弹道设计 西北工业大学出版社 1999
11、李继坤 工程热力学 国防工业出版社 1989
12、宋志明 复速级鱼雷涡轮机工作过程仿真研究 西北工业大学硕士学位论文 2001
13、康凤举 现代仿真技术与应用 国防工业出版社 2001
14、汪成为 面向对象分析设计及应用 国防工业出版社 1992
15、张进军 高速鱼雷涡轮机研究 西北工业大学硕士学位论文2000
16、李留成 鱼雷热动力系统启动过程数字仿真 西北工业大学硕士学位论文 1994
17、朱明善 汽轮机原理 水利电力出版社 1992
18、朱方元 航空轴流叶片机气动设计 西北工业大学讲义 1984
19、潘锦珊 气体动力学基础 国防工业出版社 1989
20、石秀华 水中兵器概论(鱼雷部分) 西北工业大学出版社 1995
21、易忠亮 鱼雷面向对象建模与仿真应用构架研究 西北工业大学博士学位论文 1997
22、徐德民 鱼雷自动控制系统 西北工业大学出版社 1991
23、施阳 MATLAB语言精要及动态仿真工具SIMULINK 西北工业大学出版社 1998
24、薛定宇 控制系统计算机辅助设计—MATLAB语言及应用 清华大学出版社 1996
25、何长富 国内外鱼雷热动力系统发展动态及途径 水中兵器 1997(4)
26、周昌成 燃气涡轮发动机气动热力学理论及其应用 发电设备 1996
27、屠秋野 化学平衡对燃气涡轮发动机循环性能影响 航空动力学报1998
28、Long Xiaoqing Chemical Reaction Mechanism of Hot Corrosion in High Temperature Parts of Gas Turbine Engine JOURNAL OF CIVIL AVIATION UNIVERSITY OF CHINA 1994
29、Lenonard Greiner Underwater Missile propulsion Compass Publications 1967
30、LouisJF Axial Flow Contra—Rotating Gas Turbine Conference and Exhibit Houston 18～21 1985
31、Ennio Macchi, Giovanni Lozza Comparison of Partial vs Full Admission for Small Tutbines at low specific speed Gas Turbine Conferences and Exhibit Houston 18～21 985
32、Shinners S M Modern Control System Theory and Application Addison-Wesley 1978
33、Smith J M Mathematical Modeling and Digital Simulation for Engineers and Scientists J Wiley and Sons 1977
34、Korn G A Digital Continuous-System Simulation Prentice-Hall 1978
35、Shannon R E System Simulation the Art and Science Prentice-Hall INC 1975
36、Zeigder B P Object-Oriented Simulation with Hierachical, Modular Models Academic Press 1990
37、Coad P, Yourdon E Object-Oriented Analysis Yourdon Press 1989
38、 J K Watterson and S Raghunathan Numerical Analysis of Wells Turbine Aerodynamics Department of Aeronautical Engineering. The queen's University of Belfast. Belfast United Kingdom. AIAA. 98-0363
39、 Lambert J D Computational Methods in Ordinary Differential Equations John Wiley & Sons 1973
40、 Fred Maryanski Digital Computer Simulation Hayden Book Company Inc.N.J. 1990
41、 V.A.Lashko. A.V.Passar Computer-added design of the flow part geometry of the centripetal turbine of combined internal combustion engine. Russia. Khabarovsk State University of Technology 2000
42、 SONG Ying-dong Turbine engine composite route flight loading spectrum derivation JOURNAL OF PROPULSION TECHNOLOGY 2000
43、 Fein, H Application of holographic interferometry for dynamic vibration analysis of a jet engine turbine compressor rotor Proc. SPIE-Int. Soc. Opt. Eng. (USA) 5005 307-15 2003
44、 Chaker, M., Meher-Homji, C.B., Mee, T., Ⅲ, et al Inlet fogging of gas turbine engines detailed climatic analysis of gas turbine evaporation cooling potential in the USA Trans. ASME, J. Eng. Gas Turbines Power (USA) 125 (1): 300-9 Jan. 2003
45、 Lukachko, S.P., Kirk, D.R., Waitz, I.A Gas turbine engine durability impacts of high fuel-air ratio combustors-part Ⅰ: potential for secondary combustion of partially reacted fuel Trans. ASME, J. Eng. Gas Turbines Power (USA) 125 (3): 742-50 July 2003
46、 Bu Guang-zhi, Zhang Yu-wen The overall design method for torpedo weapon based on the operational effectiveness Syst. Eng. Electron. (China) 24 (9): 44-129 Sept. 2002
47、 Chai Lin, Fang Qun The simulation of a torpedo's guidance trajectory based
on MATLAB/Simulink J. Syst. Simul. (China) 15 (2): 231-4 Feb. 2003
48、 Uluyol, O., Kyusung Kim, Menon, S., et al Synergistic use of soft computing technologies for fault detection in gas turbine engines SMCia/03. Proceedings of the 2003 IEEE International Workshop on Soft Computing in Industrial Applications (Cat. No.03EX688) 115-20 2003
49、 Xiaoping Qian, Dutta, D Design of heterogeneous turbine blade Comput. Aided Des. (UK) 35 (3): 319-29 March 2003
50、 Motta, R, Bregani, F., De Michelis, C New materials for more efficient generation of electricity Energ. Elettr. (Italy) 79 (4): 33-45 July-Aug. 2002
51、 Peacock, RE, Yost, JO Addressing the measurement problem in the gas turbine AEROSP CONF PROC: 3061-3068 2003
2、赵连峰 鱼雷活塞发动机原理 西北工业大学出版社 1991
3、刘讯谦 鱼雷推进剂及供应系统 西北工业大学出版社 1991
4、马世杰 鱼雷热动力装置设计原理 兵器工业出版社 1992
5、李启炎 PASCAL程序设计语言 同济大学出版社 1999
6、张可村 数值计算的算法与分析 科学出版社 2003
7、鲁宗相 Delphi5入门与提高 清华大学出版社 2000
8、宋明玉 开式循环鱼雷热动力系统数字仿真及H_∞控制研究 西北工业大学硕士学位论文 1997
9、翁史烈 船舶动力装置仿真技术 上海交通大学出版社 1991
10、张宇文 鱼雷弹道与弹道设计 西北工业大学出版社 1999
11、李继坤 工程热力学 国防工业出版社 1989
12、宋志明 复速级鱼雷涡轮机工作过程仿真研究 西北工业大学硕士学位论文 2001
13、康凤举 现代仿真技术与应用 国防工业出版社 2001
14、汪成为 面向对象分析设计及应用 国防工业出版社 1992
15、张进军 高速鱼雷涡轮机研究 西北工业大学硕士学位论文2000
16、李留成 鱼雷热动力系统启动过程数字仿真 西北工业大学硕士学位论文 1994
17、朱明善 汽轮机原理 水利电力出版社 1992
18、朱方元 航空轴流叶片机气动设计 西北工业大学讲义 1984
19、潘锦珊 气体动力学基础 国防工业出版社 1989
20、石秀华 水中兵器概论(鱼雷部分) 西北工业大学出版社 1995
21、易忠亮 鱼雷面向对象建模与仿真应用构架研究 西北工业大学博士学位论文 1997
22、徐德民 鱼雷自动控制系统 西北工业大学出版社 1991
23、施阳 MATLAB语言精要及动态仿真工具SIMULINK 西北工业大学出版社 1998
24、薛定宇 控制系统计算机辅助设计—MATLAB语言及应用 清华大学出版社 1996
25、何长富 国内外鱼雷热动力系统发展动态及途径 水中兵器 1997(4)
26、周昌成 燃气涡轮发动机气动热力学理论及其应用 发电设备 1996
27、屠秋野 化学平衡对燃气涡轮发动机循环性能影响 航空动力学报1998
28、Long Xiaoqing Chemical Reaction Mechanism of Hot Corrosion in High Temperature Parts of Gas Turbine Engine JOURNAL OF CIVIL AVIATION UNIVERSITY OF CHINA 1994
29、Lenonard Greiner Underwater Missile propulsion Compass Publications 1967
30、LouisJF Axial Flow Contra—Rotating Gas Turbine Conference and Exhibit Houston 18～21 1985
31、Ennio Macchi, Giovanni Lozza Comparison of Partial vs Full Admission for Small Tutbines at low specific speed Gas Turbine Conferences and Exhibit Houston 18～21 985
32、Shinners S M Modern Control System Theory and Application Addison-Wesley 1978
33、Smith J M Mathematical Modeling and Digital Simulation for Engineers and Scientists J Wiley and Sons 1977
34、Korn G A Digital Continuous-System Simulation Prentice-Hall 1978
35、Shannon R E System Simulation the Art and Science Prentice-Hall INC 1975
36、Zeigder B P Object-Oriented Simulation with Hierachical, Modular Models Academic Press 1990
37、Coad P, Yourdon E Object-Oriented Analysis Yourdon Press 1989
38、 J K Watterson and S Raghunathan Numerical Analysis of Wells Turbine Aerodynamics Department of Aeronautical Engineering. The queen's University of Belfast. Belfast United Kingdom. AIAA. 98-0363
39、 Lambert J D Computational Methods in Ordinary Differential Equations John Wiley & Sons 1973
40、 Fred Maryanski Digital Computer Simulation Hayden Book Company Inc.N.J. 1990
41、 V.A.Lashko. A.V.Passar Computer-added design of the flow part geometry of the centripetal turbine of combined internal combustion engine. Russia. Khabarovsk State University of Technology 2000
42、 SONG Ying-dong Turbine engine composite route flight loading spectrum derivation JOURNAL OF PROPULSION TECHNOLOGY 2000
43、 Fein, H Application of holographic interferometry for dynamic vibration analysis of a jet engine turbine compressor rotor Proc. SPIE-Int. Soc. Opt. Eng. (USA) 5005 307-15 2003
44、 Chaker, M., Meher-Homji, C.B., Mee, T., Ⅲ, et al Inlet fogging of gas turbine engines detailed climatic analysis of gas turbine evaporation cooling potential in the USA Trans. ASME, J. Eng. Gas Turbines Power (USA) 125 (1): 300-9 Jan. 2003
45、 Lukachko, S.P., Kirk, D.R., Waitz, I.A Gas turbine engine durability impacts of high fuel-air ratio combustors-part Ⅰ: potential for secondary combustion of partially reacted fuel Trans. ASME, J. Eng. Gas Turbines Power (USA) 125 (3): 742-50 July 2003
46、 Bu Guang-zhi, Zhang Yu-wen The overall design method for torpedo weapon based on the operational effectiveness Syst. Eng. Electron. (China) 24 (9): 44-129 Sept. 2002
47、 Chai Lin, Fang Qun The simulation of a torpedo's guidance trajectory based
on MATLAB/Simulink J. Syst. Simul. (China) 15 (2): 231-4 Feb. 2003
48、 Uluyol, O., Kyusung Kim, Menon, S., et al Synergistic use of soft computing technologies for fault detection in gas turbine engines SMCia/03. Proceedings of the 2003 IEEE International Workshop on Soft Computing in Industrial Applications (Cat. No.03EX688) 115-20 2003
49、 Xiaoping Qian, Dutta, D Design of heterogeneous turbine blade Comput. Aided Des. (UK) 35 (3): 319-29 March 2003
50、 Motta, R, Bregani, F., De Michelis, C New materials for more efficient generation of electricity Energ. Elettr. (Italy) 79 (4): 33-45 July-Aug. 2002
51、 Peacock, RE, Yost, JO Addressing the measurement problem in the gas turbine AEROSP CONF PROC: 3061-3068 2003