Abstract: An actuator assembly includes an actuation member, a release member, and a source of pressurized gas, wherein during a normal mode of operation, the actuation member and the release member are engaged to move in unison, and wherein during an emergency mode of operation, pressurized gas automatically decouples the actuation member from the release member to move separately. In accordance with yet other aspects of the present disclosure, an electro-mechanical actuator includes an electro-mechanical drive system and an integrated backup system operated by a gas generator, wherein when the backup system is activated, the electro-mechanical drive system is decoupled, and the actuator moves to a predetermined position and mechanically locks in place.

Abstract: A freeze resistant manifold includes a plurality of conduits, junction, and expansion device. Each conduit of the plurality of conduits includes a respective first end in fluid communication with a respective second end. The junction is defined by each of the respective first ends of the plurality of conduits in direct fluid communication with a remainder of the first ends of the plurality of conduits. The expansion device includes a housing, plug, and linear actuator. The housing has a first housing end and a second housing end. The first housing end is in fluid communication with the junction. The plug is disposed between the first housing end and the second housing end. The plug has a substantially fluid-tight, sliding engagement with an inner wall of the housing. The linear actuator is to urge the plug towards the first housing end with a predetermined amount of force.

Abstract: A freeze resistant manifold includes a plurality of conduits, junction, and expansion device. Each conduit of the plurality of conduits includes a respective first end in fluid communication with a respective second end. The junction is defined by each of the respective first ends of the plurality of conduits in direct fluid communication with a remainder of the first ends of the plurality of conduits. The expansion device includes a housing, plug, and linear actuator. The housing has a first housing end and a second housing end. The first housing end is in fluid communication with the junction. The plug is disposed between the first housing end and the second housing end. The plug has a substantially fluid-tight, sliding engagement with an inner wall of the housing. The linear actuator is to urge the plug towards the first housing end with a predetermined amount of force.

Abstract: A surface-mounted fuselage skin appliqué panel having an aperture to a reference static air input port is rugged, replaceable, and independently calibratable. The static port skin appliqué generally conforms to the fuselage surface, and is held in place either with adhesive or with a mounting frame. The appliqué size enables airflow in the vicinity of the static port to be substantially uniform. Because the appliqué is not part of the fuselage structure, distorting stress loads are avoided. The appliqué material resists scratches and bumps that can distort flow. A static port skin appliqué and its mounting provisions can be made using a range of materials, and can receive finishes to meet user preferences.