Abstract: A hand drying system and method for a lavatory includes a blower housing that includes a blower that is configured to generate airflow within an air chamber. An exhaust vent is configured to be secured to the lavatory. The exhaust vent defines an air outlet. A conduit includes a first end in fluid communication with the air chamber and a second end in fluid communication with the air outlet. The conduit distally locates the blower housing from the lavatory.

Abstract: Apparatuses and methods are described for use of an ultraviolet (UV) light source, such as in a cleaning device, in which ozone creation due to reaction of the UV light with oxygen in the air is reduced. An example method includes dispersing, by a gas outlet, oxygen-depleted gas over a UV light source, and directing UV light from the UV light source to pass through the oxygen-depleted gas onto an area. An example apparatus includes a UV light source to direct UV light onto an area, and a gas outlet to disperse oxygen-depleted gas over the UV light source, such that the UV light passes through the oxygen-depleted gas onto the area.

Abstract: An ultraviolet (UV) light sanitizing system and method are configured to sanitize at least one surface within an enclosed space. The UV light sanitizing system includes a UV light assembly that is selectively moveable between a stowed position and a deployed position. The UV light assembly is stowed within a stowage chamber connected to the enclosed space in the stowed position. The UV light assembly deploys out of the stowage chamber and into the enclosed space in the deployed position.

Abstract: Systems and methods for aerially delivering cargo into a body of water while avoiding parachute entrapment and entanglement are described. The system includes a parachute having a canopy and suspension lines. The system further includes a weight coupled to a first end of the suspension lines and a ring that is configured to float in the body of water. The weight is coupled to the cargo, and the ring is disposed between the weight and the canopy with the suspension lines passing through the center of the ring.

Abstract: A system includes a dry floor assembly that is configured to be located within an interior space. The dry floor assembly includes a vacuum layer. A vacuum system is coupled to the vacuum layer. The vacuum system is configured to remove liquid from the dry floor assembly via the vacuum layer.

Abstract: A thermal radiation-generating decoy mounted adjacent an aircraft engine structure, such as an engine nacelle, includes a heat source inside of an aerodynamic enclosure with a mounting interface to attach the enclosure to the engine structure. The decoy can further be located at the lower extreme of and adjacent the forward-most portion of the engine nacelle in order to attract an infrared-seeking threat to the vicinity of the fan containment portion of the engine nacelle. The decoy can be designed to have a thermal signature that mimics a scaled overall aircraft thermal signature. In addition, the decoy can include a fuse shield adjacent the enclosure to detonate a threat in the case that the threat approach trajectory is imprecise and the threat bypasses the enclosure within an aspect of the fuse shield as viewed from the approach direction of the threat.