咨询与建议

看过本文的还看了

相关文献

该作者的其他文献

文献详情 >Active control system for a ro... 收藏

Active control system for a rotor blade trailing-edge flap

作     者:Duvernier, Marc Reithler, Livier Guerrero, Jean Yves Rossi, Rinaldo 

作者机构:AEROSPATIALE MATRA CCR Suresnes France 

出 版 物:《Proceedings of SPIE - The International Society for Optical Engineering》 

年 卷 期:2000年第3985卷

页      面:52-61页

核心收录:

主  题:Actuators 

摘      要:Reducing the external noise is now a major issue for helicopter manufacturers. The idea beyond this goal is to reduce or even avoid the blade vortex interaction (BVI). EUROCOPTER is currently investigating several strategies to reach this goal. One such strategy is to control the local incidence of the blade by a direct lift flap. AEROSPATIALE MATRA Corporate Research Center and AEROSPATIALE MATRA MISSILES provide the actuator system for the direct lift flap.

读者评论 与其他读者分享你的观点

用户名:未登录
我的评分