Transport element clamp system

Transport element clamp system

TRANSPORT ELEMENT CLAMP SYSTEM A transport element clamp system (206) comprising a lower portion (222), an upper portion (224), and a channel system (226). The lower portion (222) has a first number of cutouts (228) and the upper portion (224) has a second number of cutouts (230). The lower portion...

Ausführliche Beschreibung

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Bibliographische Detailangaben
Hauptverfasser: CARPENTER, Mark L, GILBERTSON, Michael Leslie, MICHEL, Jon P
Format: Patent
Sprache:eng
Schlagworte:
AEROPLANES
AIRCRAFT
AVIATION
COSMONAUTICS
HELICOPTERS
PERFORMING OPERATIONS
TRANSPORTING
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Beschreibung
Zusammenfassung:TRANSPORT ELEMENT CLAMP SYSTEM A transport element clamp system (206) comprising a lower portion (222), an upper portion (224), and a channel system (226). The lower portion (222) has a first number of cutouts (228) and the upper portion (224) has a second number of cutouts (230). The lower portion (222) is configured to bridge a gap (220) between two support structures (202) in an aircraft (201). The upper portion (224) is configured to interlock with the lower portion (222). The channel system (226) is formed by the first number of cutouts (228) and the second number of cutouts (230). The channel system (226) is configured to receive a number of transport elements (208) when the upper portion (224) and the lower portion (222) are coupled to each other. The transport element clamp system (206) electrically isolates the number of transport elements (204) from the two support structures (202). clco v o