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1. 发明授权

US08082707B1 Air-film vibration damping apparatus for windows 有权
标题翻译：用于窗户的气膜减震装置
公开(公告)号：US08082707B1
公开(公告)日：2011-12-27
申请号：US11580791
申请日：2006-10-13
申请人： Thomas M. Lewis , Michael L. Parin
发明人： Thomas M. Lewis , Michael L. Parin
IPC分类号： B64C1/14 , E06B3/66 , F16F7/00
CPC分类号： B64C1/1484 , B64C1/1492
摘要： An improved vibration damping apparatus is provided for use with window structures, including windows used in vehicles, aircraft, and spacecraft. The vibration damping system includes at least two separate layers of solid material that are typically substantially clear at visible wavelengths, in which the two layers are spaced-apart by a predetermined distance to form a space or gap therebetween. This gap will be of a size and shape to enhance vibration damping when it is filled with a gaseous compound, such as air. The air-film vibration damping system created by the above structure can be applied to an external pane of a window structure, or to the interior pane of a window structure, or perhaps to both an exterior pane and an interior pane of the same window structure, if desired.
摘要翻译：提供了一种改进的减震装置，用于窗构件，包括用于车辆，飞机和航天器中的窗户。振动阻尼系统包括至少两个单独的固体材料层，其通常在可见波长处基本上是清晰的，其中两层间隔开预定距离以在它们之间形成空间或间隙。当填充气体化合物（例如空气）时，该间隙将具有尺寸和形状以增强振动阻尼。通过上述结构产生的气膜振动阻尼系统可以应用于窗户结构的外部窗格，或者可应用于窗户结构的内部窗格，或可能应用于同一窗口结构的外部窗格和内部窗格如果需要的话。

2. 发明授权

US08439154B1 Air-film vibration damping apparatus for windows 有权
标题翻译：用于窗户的气膜减震装置
公开(公告)号：US08439154B1
公开(公告)日：2013-05-14
申请号：US13331999
申请日：2011-12-20
申请人： Thomas M. Lewis , Michael L. Parin
发明人： Thomas M. Lewis , Michael L. Parin
IPC分类号： F16F7/00 , B64C1/14
CPC分类号： B64C1/1484 , B64C1/1492
摘要： An improved vibration damping apparatus is provided for use with window structures, including windows used in vehicles, aircraft, and spacecraft. The vibration damping system includes at least two separate layers of solid material that are typically substantially clear at visible wavelengths, in which the two layers are spaced-apart by a predetermined distance to form a space or gap therebetween. This gap will be of a size and shape to enhance vibration damping when it is filled with a gaseous compound, such as air. The air-film vibration damping system created by the above structure can be applied to an external pane of a window structure, or to the interior pane of a window structure, or perhaps to both an exterior pane and an interior pane of the same window structure, if desired.
摘要翻译：提供了一种改进的减震装置，用于窗构件，包括用于车辆，飞机和航天器中的窗户。振动阻尼系统包括至少两个单独的固体材料层，其通常在可见波长处基本上是清晰的，其中两层间隔开预定距离以在它们之间形成空间或间隙。当填充气体化合物（例如空气）时，该间隙将具有尺寸和形状以增强振动阻尼。通过上述结构产生的气膜振动阻尼系统可以应用于窗户结构的外部窗格，或者可应用于窗户结构的内部窗格，或可能应用于同一窗口结构的外部窗格和内部窗格如果需要的话。

3. 发明授权

US07721844B1 Vibration damping apparatus for windows using viscoelastic damping materials 有权
标题翻译：使用粘弹阻尼材料的窗户振动阻尼装置
公开(公告)号：US07721844B1
公开(公告)日：2010-05-25
申请号：US11580790
申请日：2006-10-13
申请人： Thomas M. Lewis , Michael L. Parin
发明人： Thomas M. Lewis , Michael L. Parin
IPC分类号： F16F7/00
CPC分类号： F16F9/306 , F16F15/0232
摘要： An improved vibration damping system is provided for use with window structures. The window damping system employs both air-film damping technology and viscoelastic damping materials to increase mechanical and/or acoustic vibration damping in window structures.
摘要翻译：提供了一种改进的减振系统，用于窗户结构。窗户阻尼系统采用气膜阻尼技术和粘弹阻尼材料来增加窗户结构中的机械和/或声振动阻尼。

4. 发明申请

US20110079477A1 Tuned vibration absorber mountable to aircraft skin panel 审中-公开
标题翻译：调谐减震器可安装到飞机皮肤面板
公开(公告)号：US20110079477A1
公开(公告)日：2011-04-07
申请号：US12587109
申请日：2009-10-01
申请人： Indranil Dandaroy , Thomas M. Lewis , Heather J. Czechowski , Peggy S. Hardison , Michael L. Parin
发明人： Indranil Dandaroy , Thomas M. Lewis , Heather J. Czechowski , Peggy S. Hardison , Michael L. Parin
IPC分类号： F16F7/10
CPC分类号： F16F7/108 , B64C1/40 , B64C2027/005 , Y02T50/46
摘要： An apparatus and method for attenuating noise and vibration in a propeller aircraft comprises a tuned vibration absorber adapted to be mounted to the skin of a fuselage of a propeller aircraft. The tuned vibration absorber may be tuned to the second harmonic of a blade passage frequency of a propeller of the aircraft. The tuned vibration absorber may be connectable to a separately formed mount, which can be mounted to the fuselage skin independently of the tuned vibration absorber. The apparatus may include a cover to prevent interference between the tuned vibration absorber and other components in the aircraft. The apparatus may be used in combination with other attenuation systems to attenuate noise and vibration over a broad range of frequencies.
摘要翻译：用于衰减螺旋桨飞机中的噪声和振动的装置和方法包括适于安装到螺旋桨飞机的机身的皮肤上的调谐振动吸收器。调谐的振动吸收器可以调谐到飞行器的螺旋桨的叶片通过频率的二次谐波。调谐的振动吸收器可以连接到单独形成的支架，其可以独立于调谐的振动吸收器安装到机身皮肤上。该装置可以包括盖，以防止调谐的振动吸收器与飞行器中的其它部件之间的干涉。该装置可以与其它衰减系统组合使用以在宽范围的频率上衰减噪声和振动。

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