Patent ID: 9156553
Filing Date: 2015-10-13
Classification: B64D,H05K

Abstract:
1. Aircraft mission equipment comprising: a base comprising a plurality of pressure chambers, each pressure chamber having first and second ports; an air manifold having a first port and a plurality of second ports; a plurality of flow restrictors in fluid communication with said first ports of respective pressure chambers of said plurality of pressure chambers; a plurality of air hoses, each air hose connecting a respective second port of said air manifold to a respective flow restrictor; a rack for supporting components, said rack being mounted to said base; and a plurality of air casters attached to said base, each air caster having a port that is in fluid communication and aligned with said second port of a respective one of said plurality of pressure chambers, wherein said plurality of flow restrictors, said plurality of pressure chambers and said plurality of air casters are arranged so that compressed air supplied by said air manifold and said plurality of air hoses will flow first through said plurality of flow restrictors, then into said plurality of pressure chambers and then into said air casters.