Seat track assemblies for vibration isolation of floor mounted components

Aircraft, vibration isolation assemblies, and methods of assembling vibration isolation assemblies are provided. An aircraft includes a vibration isolation assembly. The vibration isolation assembly includes a mounting track, a plate, a clamp block, a vibration isolator, and a support fitting. The m...

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Bibliographische Detailangaben
Hauptverfasser: KRISTOPHER P. LYNCH, JEFFREY JONAS, BENJAMIN FRANK WILSON, MICHAEL LUCAS
Format: Patent
Sprache:chi ; eng
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Beschreibung
Zusammenfassung:Aircraft, vibration isolation assemblies, and methods of assembling vibration isolation assemblies are provided. An aircraft includes a vibration isolation assembly. The vibration isolation assembly includes a mounting track, a plate, a clamp block, a vibration isolator, and a support fitting. The mounting track defines a cavity and includes flanges that define an opening to the cavity. The plateis configured to be positioned on the flanges outside of the cavity. The clamp block is configured to be fastened to the plate under the flanges of the mounting track within the cavity. The vibrationisolator is configured to be laterally constrained by the clamp block within the cavity. The support fitting is configured to be secured to the vibration isolator outside of the cavity. 提供种飞机、隔振组件以及组装隔振组件的方法。飞机包括隔振组件。该隔振组件包括安装导轨、板、夹持块、振动隔离器和支撑配件。该安装导轨限定空腔并且包括凸缘,该凸缘限定通向该空腔的开口。该板构造成在该空腔的外部定位在该凸缘上。该夹持块构造成在该空腔内在该安装导轨的凸缘下方紧固到该板。该振动隔离器构造成在该空腔内被该夹持块横向约束。该支撑配件构造成在该空腔的外部固定到该振动隔离器。