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直升机涡轴发动机燃油调节系统建模与仿真
引用本文:丁琳,王道波,李猛,张元.直升机涡轴发动机燃油调节系统建模与仿真[J].航空兵器,2011(4):30-34.
作者姓名:丁琳  王道波  李猛  张元
作者单位:南京航空航天大学,南京,210016
摘    要:依据直升机涡轴发动机控制原理,分析了直升机动力系统的控制回路,在已有对直升机动力系统研究的基础上,给出某型涡轴发动机及直升机旋翼的数学模型,并对某型直升机涡轴发动机燃油调节器进行具体的机理分析,建立了该调节器的数学模型。在以上数学模型的基础上,对该型直升机涡轴发动机燃油调节系统进行了全数字仿真研究,揭示了该型燃油调节器...

关 键 词:涡轴发动机  机械液压  燃油调节器  控制规律  全数字仿真

Modeling and Simulation of Fuel Conditioning System for Turbo-Shaft Engine of Helicopter
DING Lin,WANG Dao-bo,LI Meng,ZHANG Yuan.Modeling and Simulation of Fuel Conditioning System for Turbo-Shaft Engine of Helicopter[J].Aero Weaponry,2011(4):30-34.
Authors:DING Lin  WANG Dao-bo  LI Meng  ZHANG Yuan
Affiliation:DING Lin,WANG Dao-bo,LI Meng,ZHANG Yuan(Nanjing University of Aeronautics & Astronautics,Nanjing 210016,China)
Abstract:According to the controlling principle of the helicopter turbo-shaft engine,this paper analyzes the controlling loop of the helicopter dynamical system.Based on the study of the helicopter dynamical system,it builds the mathematical models of a certain turbo-shaft engine and the helicopter rotor wing,and analyzes the fuel controller.Based on the mathematical models,this paper makes the full digital simulations for the turbo-shaft engine fuel control system associated with hydraulic-mechanism controller,then...
Keywords:turbo-shaft engine  mechanism hydraulic  fuel controller  control law  full digital simulation  
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