摘要:
A method for interconnecting electronic equipment within an aircraft (200, 300) is described. The method includes installing a multi-dimensional backplane (320, 400) within the aircraft (200, 300), the backplane (320, 400) including a plurality of connectors (380, 410) mounted thereon, contacts associated with the connectors (380, 410) interconnected by electrical conductors formed within the backplane (320, 400), attaching shipside wiring (340, 342, 344, 346) to a first portion of the connectors (380, 410) on the backplane (320, 400), and attaching electrical connectors of the electronic equipment to corresponding connectors (380, 410) on the backplane.
摘要:
An interconnect for transferring signals herein includes one or more signal contacts to transfer the power or data to or from an integrated truss system. An interconnect may be configured to transfer power or data between layers of the integrated truss system or within the same layer of the integrated truss system. An interconnect may be configured with one or more compression mechanisms that secure the interconnect in the integrated truss system.
摘要:
An interconnect for transferring signals herein includes one or more signal contacts to transfer the power or data to or from an integrated truss system. An interconnect may be configured to transfer power or data between layers of the integrated truss system or within the same layer of the integrated truss system. An interconnect may be configured with one or more compression mechanisms that secure the interconnect in the integrated truss system.
摘要:
An interconnect for transferring signals herein includes one or more signal contacts to transfer the power or data to or from an integrated truss system. An interconnect may be configured to transfer power or data between layers of the integrated truss system or within the same layer of the integrated truss system. An interconnect may be configured with one or more compression mechanisms that secure the interconnect in the integrated truss system.
摘要:
A method for interconnecting electronic equipment within an aircraft (200, 300) is described. The method includes installing a multi-dimensional backplane (320, 400) within the aircraft (200, 300), the backplane (320, 400) including a plurality of connectors (380, 410) mounted thereon, contacts associated with the connectors (380, 410) interconnected by electrical conductors formed within the backplane (320, 400), attaching shipside wiring (340, 342, 344, 346) to a first portion of the connectors (380, 410) on the backplane (320, 400), and attaching electrical connectors of the electronic equipment to corresponding connectors (380, 410) on the backplane.