Systems and methods for laminated buswork with flexible conductors for an electric aircraft

Abstract

A system for a laminated buswork with flexible conductors for an electric aircraft is presented. The system includes a plurality of electrical devices and an electrical bridging device electrically connected to each electrical device of the plurality of devices. The electrical bridging device includes a laminated busbar and a plurality of flexible contactors, wherein each flexible contactor is configured to attach the laminated busbar to each electrical device of the plurality of electrical devices, apply pressure to each electrical device as a function of at least a spring, and provide electrical connection to the electric aircraft as a function of the tension of the at least a spring.

Dependencies are inferred from the claim text.