MULTI-DISCIPLINARY FLIGHT CONTROL DEVELOPMENT AND ITS INTEGRATION INTO MULTI-ATTRIBUTE COMPUTER AIDED ENGINEERING ANALYSIS PROCESS

摘要：

As flight control actuation systems become more complex，a multidisciplinary approach is needed to understand the interactions between diverse systems including electrical，mechanical，hydraulic，and control systems. In addition，the development of flight control actuation(FCA)systems is being transformed by its integration into computer aided engineering process. This presentation explores the interactions between diverse systems including electrical，mechanical，hydraulic，control systems in a FCA system and its integration into different CAE attribute analysis like flexible multi-body analysis，stress analysis，and fatigue damage prediction.

关键词： Flight Control Actuator Leading Edge Slat High Lift Devices Electrical hydraulics virtual prototype

作者: Chris Paulson Juan Betts Christophe Leguay

作者单位: LMS International2651 Crosspark RoadCoralville, IA 52241(UNITED STATES) LMS InternationalResearchpark Z1Interleuvenlaan 683001 Leuven, Belgium IMAGINE Toulouse BUROLINES I 2 bis rue Marcel DORET 31700 Blagnac, France

会议类型: 国内会议

会议名称: 2008年LMS中国用户大会

会议地点: 西安

会议语种:英文

页码: 1-5

在线出版日期: 2008-10-20（万方平台首次上网日期，不代表论文的发表时间）