摘要
从工业和船用燃气轮机控制系统特点出发,研究了航空改型机组控制系统的设计特点,分析了改型机组利用航空原型机控制技术的可能性及必须采取的技术改进措施。通过几个实例,分别对由涡喷、涡桨和涡扇等不同类型航空发动机改型的燃气轮机控制系统的设计要求、特点和方法作了较详细的讨论,对于控制系统设计中的一些主要问题作了归纳,指出了技术发展的趋势。
On the basis of the control characteristics, operation mode and service requirements of industrial and marine gas turbines, the author studied the design features of an aeroderived engine control system and analysed the possibility of adopting a prototype aeroengine control technology for an aeroderivative gas turbine with all concomitant technical improvement measures being also specified. By citing some examples of design and development efforts on several types of gas turbines a detailed discussion has been made of the design specifications, features and design methods used for the control system of a gas turbine derived respectively from turbojet, turboprop and turbofan engines. The author recapitulated some main problems involved in the design of the control system with technical development trends being pinpointed.
出处
《热能动力工程》
CAS
CSCD
北大核心
1992年第4期200-204,共5页
Journal of Engineering for Thermal Energy and Power
关键词
改装
燃气轮机
控制
aeroderived engine, gas turbine, control
