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发明申请
US20070138338A1 Active cancellation and vibration isolation with feedback and feedfoward control for an aircraft engine mount 有权
主动取消和隔振，具有飞机发动机支架的反馈和进给控制

Active cancellation and vibration isolation with feedback and feedfoward control for an aircraft engine mount
摘要：
An engine mount structure is provided with active vibration mechanisms which are attached in the vicinity of the engine mount to prevent engine vibrations from propagating into the engine mounting structure, for example, the wing or fuselage structure of an aircraft. Additionally, sensors are provided on the engine and/or wing/fuselage structure to provide control signals to the active vibration mechanisms so that the active vibration mechanism react to the sensed data to minimize the vibration transmissibility from the engine into the wing/fuselage.
摘要（中）：

发动机安装结构设置有主动振动机构，其附接在发动机底座附近，以防止发动机振动传播到发动机安装结构中，例如飞行器的机翼或机身结构。 此外，传感器设置在发动机和/或机翼/机身结构上以向主动振动机构提供控制信号，使得主动振动机构对所感测的数据作出反应，以使从发动机到机翼/机身的振动传递率最小化。

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