Abstract: Disclosed is a pressure regulator, comprising: a first cylindrical chamber; a second cylindrical chamber located concentrically within the first cylindrical chamber and in thermal communication with the first cylindrical chamber; and further comprising at least one of: an internal valve, wherein the internal valve is connected at a first end to the first cylindrical chamber and at a second end to the second cylindrical chamber, wherein the internal valve allows the flow of gas from the second cylindrical chamber to the first cylindrical chamber; and an external gas chamber and an external valve, wherein the external gas chamber is located outside the first cylindrical chamber, wherein the external valve is connected at a first end to the first cylindrical chamber and at a second end to the external gas chamber, wherein the external valve allows the flow of gas from the external gas chamber to the first cylindrical chamber.

Abstract: A friction disk may comprise a first wear surface formed from a carbon fiber-carbon matrix composite material. A wear plug may be located in an opening defined by the carbon fiber-carbon matrix composite material. The wear plug may extend axially from the wear surface. The wear plug may comprise a rod or a particulate.

Abstract: An actuator assembly may comprise a control unit and a shape memory coil spring in electrical communication with the control unit. The shape memory coil spring may increase from a first length to a second length in response to receiving a current from the control unit. The shape memory coil spring may be configured to translate a spacer and/or a slider shaft in response to increasing in length. The shape memory coil spring may be configured to transition a pawl in a latch assembly from a retracted state to an erected state, and vice versa.

Abstract: A manufacturing process may comprise: stacking a plurality of friction discs together, each friction disc comprising a lug defining a surface; and depositing a composition to bond to the surface of a first friction disc in the plurality of friction discs to form a wear pad defining a wear surface.

Abstract: An ice protection system for an aircraft component includes a plurality of heaters. The aircraft component has at least two section and a junction area. At least one of the heaters is an H-shape carbon allotrope heater designed to apply heat to the junction area and prevent ice accumulation in the junction area.

Abstract: A heat shield assembly for a wheel is disclosed. The heat shield assembly includes a heat shield having a pair of heat shield ends. A bifurcated seam mounting bracket includes a first bracket section that is fixed relative one of the heat shield ends, along with a second bracket section that is fixed relative to the other of the heat shield ends. The second bracket section may be directly mounted to the heat shield. A seam clasp section may be directly mounted to both the heat shield and the first bracket section such that the first bracket section is indirectly mounted to the heat shield.

Abstract: The present disclosure provides a water activated transmitter assembly configured to provide a signal to a wireless light assembly when the water activated transmitter assembly is exposed to water. A water emergency device system is also disclosed, which comprises the water activated transmitter assembly and the wireless light assembly coupled to a water flotation device. A method of manufacture of the water activated transmitter assembly is also disclosed.

Abstract: Methods, systems, and apparatuses for component manufacturing are provided. A component may be manufactured via an extrusion of loose substrate material into a unitary tubing. Features may be added to the tubing via friction stir additive manufacturing to manufacture a component. In this manner, a component may be manufactured from titanium alloys while processing challenges such as iron segregation or material loss through machining are ameliorated. Such a component may replace steel or other high strength components and further exhibits corrosion resistance.

Abstract: An inflatable girt for an evacuation slide may comprise a sleeve section, an upper section coupled to the sleeve section, and a lower section coupled to at least one of the sleeve second and the upper section. The sleeve section defines a plurality of first inflatable chambers. The upper section defines a plurality of second inflatable chambers. The lower defines a plurality of third inflatable chambers.

Abstract: A brake roller assembly may comprise: a shaft; a first roller bearing coupled to the shaft and disposed at a first axial end of the shaft a second roller bearing coupled to the shaft and disposed at a second axial end of the shaft; a roller cylinder disposed radially outward of the first roller bearing and the second roller bearing; and a braking arrangement, including a plurality of electrodes, and a plurality of rotor disks coupled to the roller cylinder, each rotor disk in the plurality of rotor disks disposed between an anode in the plurality of electrodes and a cathode in the plurality of electrodes.

Abstract: A above floor wiring system is disclosed herein. The above floor wiring system includes a tray including a sidewall, a wire bundle secured to the sidewall, and a junction card coupled to the sidewall and electrically coupled to the wire bundle.

Abstract: Disclosed herein is a system including a primary brake control unit, a secondary brake control unit, a first remote data power concentrator configured to receive a first command from the primary brake control unit and a second command from the secondary brake control unit, and an electric brake actuator configured to receive the first command or the second command from the first remote data power concentrator in response to a first signal.

Abstract: A convertible cargo handling system is provided. The convertible cargo handling system includes a roller tray mounting system and a first roller tray. The roller tray mounting system includes a sealing plate and a first floor fitting coupled to the sealing plate, where the first floor fitting is configured such that a top edge of the first floor fitting is flush with a surface of a floor. The first roller tray includes a first set of walls and a first roller tray fitting, where the first set of walls are configured to nest along sides of the first floor fitting below the surface of the floor and where the first roller tray fitting is configured to rest on the top edge of the first floor fitting.

Abstract: A single event upset (SEU) mitigation system is disclosed herein. The SEU system includes a trigger circuit configured to receive an input signal, a hold circuit operatively coupled to the trigger circuit and configured to receive a first signal from the trigger circuit, a reset circuit operatively coupled to the hold circuit and configured to output a reset signal in response to receiving one or more hold signals from the hold circuit, and a controller operatively coupled to the reset circuit, the controller configured to reset in response to the reset signal.

Abstract: A helically shaped dynamic seal ring is provided. The helically shaped dynamic seal ring includes a spirally wound body and a snubbing orifice area formed in the spirally wound body. The spirally wound body is configured to expand in response to contacting a snubbed stroke range of an actuator piston. The spirally wound body is configured to contract in response to distancing from the snubbed stroke range of the actuator piston.

Abstract: An inflation control system for an inflatable device may comprise: a compressed fluid source; a solenoid valve connected to the compressed fluid source and configured to control a flow of gas to the inflatable device; and a control circuit comprising a power source, a pressure switch, and an electrical switch, the control circuit configured to energize, via the power source, the solenoid valve in response to both the pressure switch and the electrical switch being in a closed state, the pressure switch configured to open and de-energize the solenoid valve in response to being exposed to a pressure at or exceeding a pressure threshold.

Abstract: An evacuation slide light system may comprise a sensor, a controller configured to receive a signal from the sensor, and a projector light operably coupled to the controller. The sensor may be configured to measure at least one of a pressure of the evacuation slide or a stretch of a material of the evacuation slide. The controller may determine the pressure of the evacuation slide based on the signal from the sensor. The controller may be configured to command the projector light to emit a first image if the pressure of the evacuation slide is less than a threshold pressure and to emit a second image if the pressure of the evacuation slide is greater than or equal to the threshold pressure.

Abstract: A sanitization apparatus includes an excimer lamp and a power converter. The power converter comprises a wide band gap device and a planar inductor. The wide band gap device is selectively switchable between a first mode wherein the inductor is electrically charged and a second mode wherein the inductor is electrically discharged. The wide band gap may be repeatedly switched between the first and second modes to generate a nano second pulse output voltage waveform.

Abstract: A method of taxiing an aircraft may comprise: determining, via a brake controller, whether the aircraft is taxiing with a first thrust provided from a first side of the aircraft, a second thrust from a second side of the aircraft, or both the first thrust and the second thrust; and modifying, via the brake controller, a first brake pressure supplied to a first brake disposed on the first side of the aircraft as a function of pedal deflection in response to the taxiing with the first thrust only.

Abstract: Ice may form along the leading edge of an aircraft wing. A pneumatic deicing system may be configured to crack and dislodge ice along the leading edge of the wing. The pneumatic deicing system may comprise a deicing boot assembly having a deicing boot attached to the leading edge, and a gas generator fluidly coupled to the deicing boot assembly. The gas generator may comprise a propellant and may decompose the propellant, liberating a compressed gas. The compressed gas may be directed to the deicing boot assembly, inflating the deicing boot, which may crack and dislodge the ice.