Abstract: Apparatuses, systems, and methods comprising acoustically absorptive air ducts comprising an internally positioned structure component as an endoskeleton and an air impervious inner layer, and an acoustically absorptive foam outer layer, environmental control systems comprising such air ducts, and vehicles incorporating such environmental control systems are disclosed with methods for manufacture and installations are disclosed.

Abstract: An environmental control system for use in an aircraft includes at least one component positioned along a length of the aircraft and a decompression panel assembly comprising an array of apertures. The array of apertures is based on a location of the decompression panel assembly along the length of the aircraft relative to the at least one component.

Abstract: A system includes an outflow vent that has a cap releasably mounted to a panel within an internal cabin of a vehicle. The cap is elongated from a first end of the cap to a second end of the cap opposite the first end. The cap has a base wall that is overlaid on the panel and defines at least one slot therethrough. The cap receives an airflow generated by an airflow generator, and the at least one slot emits the airflow from the cap to form an air curtain within the internal cabin.

Abstract: An environmental control system for use in an aircraft includes at least one component positioned along a length of the aircraft and a decompression panel assembly comprising an array of apertures. The array of apertures is based on a location of the decompression panel assembly along the length of the aircraft relative to the at least one component.

Abstract: An aircraft including a fuselage having a side wall at least partially defining a passenger cabin and a crown section of the aircraft. The passenger cabin includes an overhead zone, a passenger zone, and a floor zone. An air supply duct is positioned within the crown section, and the air supply duct is configured to pressurize the crown section with air. At least one return air outlet is defined in the floor zone. An interior structure is coupled to the side wall and extends between the passenger cabin and the crown section. The interior structure includes a plurality of nozzles oriented to discharge the pressurized air from the crown section along an airflow path that extends downward through the overhead zone, downward through the passenger zone, and then towards the at least one return air outlet.

Abstract: An additive manufacturing system is disclosed and includes a first heating element configured to receive a first supply of thermoplastic material and a second heating element configured to receive a second supply of plastic material. A foaming agent is incorporated into the second supply of plastic material and is configured to expand at an activation temperature. The additive manufacturing system also includes a control module in electronic communication with both the first heating element and the second heating element. The control module executes instructions to instruct the first heating element to heat the first supply of thermoplastic material to a first extrusion temperature and instruct the second heating element to heat the second supply of plastic material to a second extrusion temperature. The second extrusion temperature is equal to or greater than the activation temperature of the foaming agent.

Abstract: A composite duct with reinforcement comprises an inner ply, an outer ply, and a plurality of cellular core rings. The inner ply forms a channel with a circular cross-section. The plurality of cellular core rings is positioned at set intervals along a length of the composite duct and between the inner ply and the outer ply.

Abstract: An aerospace vessel including a fuselage, a means for causing the fuselage to fly coupled to the fuselage, and an environmental control system within the fuselage. The environmental control system includes a duct made of closed cell thermoplastic foam, such as polyvinylidene fluoride foam.

Abstract: A composite duct with reinforcement comprises an inner ply, an outer ply, and a plurality of cellular core rings. The inner ply forms a channel with a circular cross-section. The plurality of cellular core rings is positioned at set intervals along a length of the composite duct and between the inner ply and the outer ply.

Abstract: Duct segments that define a channel for conveying a fluid, where the duct wall includes a sheath of reinforcing fabric incorporating multiple reinforcing fibers, and a thermoplastic fused with the sheath of reinforcing fabric. The duct segments may be prepared by wrapping a mandrel configured to define the inner mold line of a desired duct segment with a thermoplastic film, enveloping the wrapped mandrel with a reinforcing sheath incorporating reinforcing fibers; wrapping the enveloped mandrel with another thermoplastic film to form a multilayer duct segment precursor; enclosing the mandrel and multilayer duct segment precursor within an outer mold defining the outer mold line for the desired duct segment; heating the duct segment precursor at a temperature and for a time sufficient to fuse the layers of the multilayer duct segment precursor; and then cooling the resulting duct segment.

Abstract: An aerospace vessel including a fuselage, a means for causing the fuselage to fly coupled to the fuselage, and an environmental control system within the fuselage. The environmental control system includes a duct made of closed cell thermoplastic foam, such as polyvinylidene fluoride foam.

Abstract: An aerospace vessel including a fuselage, a means for causing the fuselage to fly coupled to the fuselage, and an environmental control system within the fuselage. The environmental control system includes a duct made of closed cell thermoplastic foam, such as polyvinylidene fluoride foam.

Abstract: A method of forming a closed cell thermoplastic foam duct and a method of forming a duct and attaching it to an aircraft environmental control system. The environmental control system includes a duct made of closed cell thermoplastic foam, such as polyvinylidene fluoride foam.

Abstract: An aerospace vessel including a fuselage, a means for causing the fuselage to fly coupled to the fuselage, and an environmental control system within the fuselage. The environmental control system includes a duct made of closed cell thermoplastic foam, such as polyvinylidene fluoride foam.

Abstract: Apparatus and methods described herein provide for the management of noise associated with a duct. A sound-dampening apparatus is provided consisting of a duct through which a fluid flows, such as an air duct. A flexuous cord is helically wound around the inner or outer surface of the duct at a pitch corresponding to a selected acoustical frequency range associated with the fluid flow through the duct.

Abstract: Apparatus and methods described herein provide for the management of noise associated with a duct. A sound-dampening apparatus is provided consisting of a duct through which a fluid flows, such as an air duct. A flexuous cord is helically wound around the inner or outer surface of the duct at a pitch corresponding to a selected acoustical frequency range associated with the fluid flow through the duct.

Abstract: An aerospace vessel including a fuselage, a means for causing the fuselage to fly coupled to the fuselage, and an environmental control system within the fuselage. The environmental control system includes a duct made of closed cell thermoplastic foam, such as polyvinylidene fluoride foam.