ELECTRICAL DISTRIBUTION BOX COMPRISING AN INPUT POWER BUSBAR

An electrical distribution box for an aircraft includes first housings configured to receive power modules, second housings configured to receive electronic control modules, and an interface configured for connection of the power and control modules and external electrical members. The interface inc...

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Bibliographische Detailangaben
1. Verfasser:	Deshayes Olivier
Format:	Patent
Sprache:	eng
Schlagworte:	AIRCRAFT ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT AVIATION CASINGS OR CONSTRUCTIONAL DETAILS OF ELECTRIC APPARATUS CONVERSION OR DISTRIBUTION OF ELECTRIC POWER COSMONAUTICS ELECTRIC TECHNIQUES NOT OTHERWISE PROVIDED FOR ELECTRICITY EQUIPMENT FOR FITTING IN OR TO AIRCRAFT FLYING SUITS GENERATION INSTALLATION OF ELECTRIC CABLES OR LINES, OR OF COMBINEDOPTICAL AND ELECTRIC CABLES OR LINES MANUFACTURE OF ASSEMBLAGES OF ELECTRICAL COMPONENTS PARACHUTES PERFORMING OPERATIONS PRINTED CIRCUITS TRANSPORTING
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Beschreibung
Zusammenfassung:	An electrical distribution box for an aircraft includes first housings configured to receive power modules, second housings configured to receive electronic control modules, and an interface configured for connection of the power and control modules and external electrical members. The interface includes at least one input power busbar extending into at least one of the first housings for connection to at least one of the power modules. The at least one input power busbar is adapted to be connected to a cable of a wiring harness for connection of the at least one power module to the wiring harness.