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1. 发明申请

WO2009055007A2 DISTRIBUTED ACTIVE VIBRATION CONTROL SYSTEMS AND ROTARY WING AIRCRAFT WITH SUPPRESSED VIBRATIONS 审中-公开
标题翻译：分布式主动振动控制系统和具有抑制振动的旋转式飞机
公开(公告)号：WO2009055007A2
公开(公告)日：2009-04-30
申请号：PCT/US2008012081
申请日：2008-10-24
申请人： LORD CORP , MARK R JOLLY , BADRE-ALAM ASKARI , ALTIERI RUSSELL , MEYERS ANDREW D
发明人： MARK R JOLLY , BADRE-ALAM ASKARI , ALTIERI RUSSELL , MEYERS ANDREW D
CPC分类号： B64C27/001 , B64C2027/004 , B64C2027/005 , F16F15/002 , F16F15/223
摘要： An aircraft with at least one rotating machine creating troublesome vibrations, the aircraft comprised of an aerostructure, the aircraft including: a power source, the power source outputting a plurality of electromagnetic force generator power outputs, the aerostructure including a plurality of distributed actiye vibration control system sites, at least a first distributed active vibration electromagnetic force generator, the first distributed active vibration electromagnetic force generator including a first distributed electronic control system and a first electromagnetically driven mass, the first distributed active vibration electromagnetic force generator fixed to the aerostructure at a first distributed active vibration control system site, at least a second distributed active vibration electromagnetic force generator, the second distributed active vibration electromagnetic force generator including a second distributed electronic control system and a second electromagnetically driven mass, the second distributed active vibration electromagnetic force generator fixed to the aerostructure at a second distributed active vibration control system site, a plurality of electrical power distribution lines, the electrical power distribution lines connecting the electromagnetic force generators with the power source with the electromagnetic force generator power outputs outputted to the electromagnetic force generators, a distributed force generator data communications network, the distributed force generator data communications system network linking together the at least first and second distributed electronic control systems wherein the distributed electronic control systems communicate force generator vibration control data through the distributed force generator data communications network independently of the electrical power distribution lines to minimize the troublesome vibrations.
摘要翻译：一种具有至少一个旋转机器的飞机产生麻烦的振动，该飞行器由航空结构组成，飞行器包括：电源，电源输出多个电磁力发生器功率输出，该航空结构包括多个分布式动力学振动控制系统站点，至少第一分布式主动振动电磁力发生器，所述第一分布式主动振动电磁力发生器包括第一分布式电子控制系统和第一电磁驱动质量块，所述第一分布式主动振动电磁力发生器固定在所述空气结构第一分布式主动振动控制系统现场，至少第二分布式主动振动电磁力发生器，所述第二分布式主动振动电磁力发生器包括第二分布式电子控制系统和第二电磁第二分布式主动振动电磁力发生器在第二分布式主动振动控制系统现场固定到航空结构，多个电力分配线，电力分配线将电磁力发生器与电源连接，电磁输出到电磁力发生器的力发电机功率输出，分布式力发生器数据通信网络，分布式力发生器数据通信系统网络将至少第一和第二分布式电子控制系统连接在一起，其中分布式电子控制系统将力发电机振动控制数据通过分布式力发生器数据通信网络独立于电力配电线路，以尽量减少麻烦的振动。

2. 发明申请

WO2009055007A3 DISTRIBUTED ACTIVE VIBRATION CONTROL SYSTEMS AND ROTARY WING AIRCRAFT WITH SUPPRESSED VIBRATIONS 审中-公开
标题翻译：分布式主动振动控制系统和具有抑制振动的旋转式飞机
公开(公告)号：WO2009055007A3
公开(公告)日：2009-07-30
申请号：PCT/US2008012081
申请日：2008-10-24
申请人： LORD CORP , MARK R JOLLY , BADRE-ALAM ASKARI , ALTIERI RUSSELL , MEYERS ANDREW D
发明人： MARK R JOLLY , BADRE-ALAM ASKARI , ALTIERI RUSSELL , MEYERS ANDREW D
IPC分类号： B64C27/00
CPC分类号： B64C27/001 , B64C2027/004 , B64C2027/005 , F16F15/002 , F16F15/223
摘要： An aircraft (20) with at least one rotating machine (22) including: a power source (26), outputting a plurality of electromagnetic force generator power outputs, an aerostructure (24) including a plurality of distributed actiye vibration control system sites, at least a first distributed active vibration electromagnetic force generator (30), including a first distributed electronic control system (32) and a first electromagnetically driven mass (34), the first force generator fixed to the aerostructure at a first site (28), at least a second distributed active vibration electromagnetic force generator including a second distributed electronic control system and a second electromagnetically driven mass, the second force generator fixed to the aerostructure at a second site, a plurality of electrical power distribution lines (40), connecting the electromagnetic force generators with the power source-with the power outputs outputted to the electromagnetic force generators, a distributed force generator data communications network (50) linking together the at least first. and second distributed electronic control systems wherein the control systems communicate force generator vibration control data through the distributed force generator data communications network independently of the electrical power distribution lines to minimize the troublesome vibrations.
摘要翻译：一种具有至少一个旋转机器（22）的飞机（20），包括：输出多个电磁力发生器功率输出的电源（26），包括多个分布式活动振动控制系统位置的航空结构（24），至少一个第一分布式主动振动电磁力发生器（30），其包括第一分布式电子控制系统（32）和第一电磁驱动质量块（34），所述第一力发生器在第一位置（28）处固定到所述航空结构，至少一个第二分布式主动振动电磁力发生器，其包括第二分布式电子控制系统和第二电磁驱动质量块，所述第二力发生器固定在第二场所的航空结构，多个配电线路（40）具有电源的力发生器 - 输出到电磁力发生器的功率输出，分布式f 所述发电机数据通信网络（50）至少连接在一起。以及第二分布式电子控制系统，其中控制系统通过分布式力发生器数据通信网络与电力分配线路独立地传递力发生器振动控制数据，以最小化麻烦的振动。

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