高逼真度燃油重心控制仿真平台开发  

The Development of High Fidelity Aircraft Fuel Barycentre Simulation Platform

作　　者：杨朋涛[1] 戴晨峰[1] 

机构地区：[1]中航工业第一飞机设计研究院,陕西西安710089

出　　处：《航空科学技术》2015年第7期37-41,共5页Aeronautical Science & Technology

摘　　要：针对现有燃油重心控制仿真手段存在的不足,提出了基于Flowmaster、CATIA与VB交联仿真的燃油重心控制仿真技术方案,重点论述了该技术方案中涉及的燃油质量特性数据库建立和燃油系统交联仿真,在此基础上搭建了燃油重心控制仿真平台。以某型飞机为例,进行了燃油重心控制仿真分析,验证了平台的可行性和有效性。In view of the deficiency of existing calculation methods about fuel barycentre, presented a correlative simulation scheme based on the Flowmaster, CATIA and VB. It also described two key parts of the scheme, the creation of fuel mass characteristic database and fuel system correlative simulation. Based on this research, the software of aircraft fuel barycentre correlative simulation was developed. In order to validate the feasibility and efifciency of the platform, the fuel barycentre of an aircraft was simulated as example.

关 键 词：燃油重心 交联仿真 平台开发 

分 类 号：V228.1[航空宇航科学与技术—飞行器设计]