Patent ID: 8922978
Filing Date: 2014-12-30
Classification: H02B

Abstract:
1. A housing for housing electrical equipment in an aircraft, the housing comprising: one or more pairs of panels, each pair of panels provided as a respective parallel pair of panels that together define an enclosed space for housing electrical equipment in the aircraft, each panel of one pair of parallel panels having a receptive lip; and at least one electrical busbar having a receptive recess at each of end thereof and the at least one electrical busbar formed using a first conductor, a second conductor and a third conductor provided in stacked arrangement for providing electric power to the electrical equipment; wherein each receptive recess of the at least one electrical busbar is connected between the receptive lip of each panel of the one parallel pair of parallel panels to provide structural support for the housing; and wherein the enclosed space enclosed by the housing has a height dimension of from 50 cm to 150 cm, a width dimension of from 40 cm to 150 cm and a depth dimension of from 10 cm to 50 cm.