Abstract: A readily-removable protective modular enclosure (50) houses a plurality of utility conduits (42) which bridge a zoned annular volume (40) disposed between a turbine engine's core (20) and fan case (30) zones, the bridging utility conduits (42) completing a three-zoned wiring harness originating on the engine's fan case (30) and terminating at a plurality of engine core terminals (24). The enclosure (50) also houses a branching interface (70) through which a utility flow, originating at either the fan case (30) or engine core (20), is directed to a dedicated outgoing utility conduit (32, 22) which services a specific zone (100).

Abstract: For a long dual mixer nacelle housing a fan-jet engine powering aircraft, a pair of concentric sleeves sandwiching the cascades to effectuate thrust reversal are synchronously deployed axially to communicate the fan discharge air in the duct with ambient through the cascades. A rack and gear connection between sleeves permits the independent linear motion of each of the sleeves so that the actuation of one automatically actuates the other without the necessity of attaching both to each other.