Transport element clamp system

TRANSPORT ELEMENT CLAMP SYSTEM A transport element clamp system comprising a lower portion, an upper portion, and a channel system. The lower portion has a first number of cutouts) and the upper portion has a second number of cutouts. The lower portion is configured to bridge a gap between two suppo...

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Bibliographische Detailangaben
Hauptverfasser:	CARPENTER MARK L, GILBERTSON MICHAEL LESLIE, MICHEL JON P
Format:	Patent
Sprache:	chi ; eng
Schlagworte:	AIRCRAFT ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT AVIATION BLASTING COSMONAUTICS ENGINEERING ELEMENTS AND UNITS EQUIPMENT FOR FITTING IN OR TO AIRCRAFT FLYING SUITS GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVEFUNCTIONING OF MACHINES OR INSTALLATIONS HEATING JOINTS OR FITTINGS FOR PIPES LIGHTING MEANS FOR THERMAL INSULATION IN GENERAL MECHANICAL ENGINEERING PARACHUTES PERFORMING OPERATIONS PIPES SUPPORTS FOR PIPES, CABLES OR PROTECTIVE TUBING THERMAL INSULATION IN GENERAL TRANSPORTING WEAPONS
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Beschreibung
Zusammenfassung:	TRANSPORT ELEMENT CLAMP SYSTEM A transport element clamp system comprising a lower portion, an upper portion, and a channel system. The lower portion has a first number of cutouts) and the upper portion has a second number of cutouts. The lower portion is configured to bridge a gap between two support structures in an aircraft. The upper portion is configured to interlock with the lower portion. The channel system is formed by the first number of cutouts and the second number of cutouts. The channel system is configured to receive a number of transport elements when the upper portion and the lower portion are coupled to each other. The transport element clamp systemelectrically isolates the number of transport elementsfrom the two support structures. 公开了种输送元件夹紧系统包括下部、上部和通道系统。下部具有第数量的切口，并且上部具有第二数量的切口。下部构造为使飞机中的两个支撑结构之间的间隙桥接。上部构造为与下部互锁。通道系统由第数量的切口和第二数量的切口形成。通道系统构造为当使上部和下部彼此耦接时接收多个输送元件。输送元件夹紧系统使多个输送元件与这两个支撑结构电绝缘。