Abstract: Stator clips may be disposed in the recesses of aircraft brake stator disks to increase the lug strength of the stator disk. The clips may interface with the splines of a torque plate and may comprise ridges that reduce contact between the torque plate barrel and the clip, while maintaining the overall integrity of the clip structure. Furthermore, reduced contact may enable a reduction in drag, improving brake performance.

Abstract: A method for braking an aircraft is disclosed herein. The method includes receiving, by a brake controller, a first signal from a position sensor of a first pedal, receiving, by the brake controller, a second signal from a pedal sensor of the first pedal, determining, by the brake controller, that the pedal is being pressed based on the first and second signals, and sending, by the brake controller, an instruction to apply a brake pressure in response to the determination that the pedal is being pressed.

Abstract: A method is provided for refurbishing a C/C disk of a first thickness and coated with a first ceramic solution for a second life. The method includes machining the C/C disk of the first thickness to remove a coating of the first ceramic solution from the wear surfaces of the C/C disk of the first thickness. Removing the coating of the first ceramic solution further removes a portion of the C/C disk thereby forming a C/C disk of a second thickness. The second thickness is less than the first thickness. The method further includes coating the wear surfaces of the C/C disk of the second thickness with a second ceramic solution, thereby forming a C/C disk of the second thickness coated with the second ceramic solution. Additionally, the method includes drying the C/C disk of the second thickness coated with the second ceramic solution.

Abstract: An in-floor adapter for a cargo deck of a cargo handling system may comprise: a plate extending from a proximal end to a distal end; a pocket disposed in the plate, the pocket having a sidewall and a bottom wall; a fitting disposed in the pocket, the fitting configured to mount a leg of a seat; and a slot disposed through the plate, the slot configured to guide an attachment mechanism during installation of the in-floor adapter in the cargo deck.

Abstract: A brake control system includes a servo valve and a brake control unit in electronic communication with the servo valve. The servo valve is configured to receive a hydraulic fluid and provide the hydraulic fluid to apply braking force to a wheel via a hydraulic line. The brake control unit is configured to calibrate the servo valve and determine whether a calibration of the servo valve was successful. In response to the calibration of the servo valve being successful, the brake control unit can operate the servo valve in an open-loop system. In response to the calibration of the servo valve being unsuccessful, the brake control unit can operate the servo valve in a closed-loop system.

Abstract: A method is disclosed here. The method includes receiving an input from an aircraft, determining a towing status of the aircraft based on the input, and sending a message to a transmitter to transmit the towing status of the aircraft. Also disclosed herein is a system including an aircraft including a nose landing gear, a first controller, and a transmitter, wherein the first controller is configured to determine a towing status of the aircraft based on a number of sensor signals received from the aircraft, and the transmitter is configured to transmit the towing status and a tow truck configured to tow the aircraft, the tow truck including a second controller and a receiver, wherein the receiver is configured to receive the towing status from the transmitter, and the second controller is configured to provide an indication of the towing status of the aircraft.

Abstract: In accordance with at least one aspect of this disclosure, a composite structure can be formed of or including a plurality of composite strips. The plurality of composite strips include one or more filler strips which can have at least one filler edge having a filler edge geometry between a first surface and second surface, the second surface being opposite the first surface. The filler edge geometry can be configured to prevent formation of one or more gaps between one or more adjacent composite strips.

Abstract: A method for forming a bi-layer coating on a substrate is disclosed herein. The method includes placing the substrate in a chemical vapor deposition (CVD) furnace, the substrate including a surface, applying a reactant vapor to the surface of the substrate to form a first coating, applying methyl trichlorosilane (MTS) to the substrate after applying the reactant vapor to the substrate, and heating the CVD furnace, including the substrate, to a first temperature to form a second coating.

Abstract: An extending cargo restraint assembly for a cargo handling system mobile is provided. The extending cargo restraint assembly includes a base assembly, The base assembly includes a primary plunger and a secondary plunger. Responsive to be activated, the primary plunger is configured to extend in a first direction into an opening within a modular container thereby restraining the modular container in a second direction, the second direction being perpendicular to the first direction. Responsive to being activated, the secondary plunger is configured to extend in the second direction within the opening of the modular container thereby further restraining the modular container in the second direction.

Abstract: A method is provided for forming a carbon/carbon (C/C) disk with boron nitride (BN) doping. Borazine is generated using a set of borazine precursors. Starting carbon fibers are coated or impregnated with the borazine in an inert atmosphere. The starting carbon fibers are needled into layered fabric and the layered fabric is needled into boards from which a preform is cut, the needling and cutting performed in the inert atmosphere. The borazine in the preform is stabilized to convert the borazine to polyborazylene. The polyborazylene in the preform is cured. The polyborazylene in the preform is then crystalized to form BN particulates. The preform with the BN particulates is carbonized and then densified with pyrolytic carbon.

Abstract: A controller for a cargo handling system. The controller includes a touch screen display, a processor, and a memory operatively coupled to the processor. The memory includes instructions stored thereon that, when executed by the processor, cause the processor to: present multiple cargo operating modes to an operator via the touch screen display; responsive to receiving a selection of a cargo operating mode from the multiple cargo operating modes, present a set of operations associated with the cargo operating mode to the operator; and, responsive to receiving a selection of at least one operation from the set of operations associated with the cargo operating mode, sending at least one command to the cargo handling system.

Abstract: A system is provided for carbon dioxide (CO2) emission recovery. The system includes a methanization reactor. The methanization reactor is configured to receive CO2 separated from one or more off gases of a brake manufacturing process, convert the CO2 and supplied hydrogen (H2) via methanization to produce methane (CH4); and supply the produced CH4 to at least one of a carbon/carbon (C/C) preform production process or another system for heat generation.

Abstract: A cargo restraint system may comprise an inner shaft and a first outer tube coaxially configured to rotate about an axis and a first restraint located about the first outer tube and configured to rotate about the axis. A second outer tube coupled to the inner shaft configured to rotate about the axis and a second restraint located about the second outer tube and configured to rotate about the axis. The first restraint and the second restraint may include a head configured to rotate about the axis and a plunger configured to translate between an engaged state and a disengaged state.

Abstract: A bushing for use in an aircraft includes a hollow cylindrical shaft having a first end and a second end opposite the first end, a radially outwardly extending flange disposed at the first end of the hollow cylindrical shaft, an entry way disposed along the radially outwardly extending flange, and a lubrication passageway fluidly coupled to the entry way. The lubrication passageway extends between the first end and the second end.

Abstract: A testing device includes a first member to be positioned on one surface of a part to be tested. A second member to be positioned on an opposed surface of the part to be tested. One of the first and second members have an ultrasonic transmitter and the other has an ultrasonic receiver. At least one of the first and second members have at least one magnetic element and the other of the first and second member have at least one magnetic or at least one ferromagnetic metallic element such that when one of the first and second members moves along the surface of the tested part the other of the first and second members will move along an opposed surface with the one of the members.

Abstract: A rack assembly for a rack and pinion gear system may comprise: a rack housing; and a rack disposed within the rack housing, the rack and the rack housing at least partially defining a first hydraulic chamber disposed between a first side of the rack and the rack housing, a second hydraulic chamber disposed between a second side of the rack and the rack housing, a third hydraulic chamber disposed within the rack proximal the first hydraulic chamber, and a fourth hydraulic chamber disposed within the rack proximal the second hydraulic chamber.

Abstract: A drive shaft for transferring torque including a tubular insert extending along an axis and defining a first layer of the drive shaft including at least one straight portion and at least one undulation, wherein the tubular insert includes a first material having a first deformation temperature, and a polymeric tubular covering defining a second layer of the drive shaft surrounding the tubular insert including a second material having a deformation temperature lower than the deformation temperature of the first material, wherein the covering includes at least one straight portion adjacent to the straight portion of the tubular insert and at least one undulation adjacent to the at least one undulation of the tubular insert.

Abstract: A method for forming an oxidation protection system on a composite structure are provided. The method includes applying a composite slurry to the composite structure, wherein the composite slurry comprises boron carbide, silicon carbide, borosilicate glass, an oxygen reactant compound including a silica forming component, and a carrier fluid and heating the composite structure to a temperature sufficient to form a boron-silicon-glass-oxygen reactant layer on the composite structure.

Abstract: A method of manufacturing a metal component with an anti-microbial molecular layer may comprise: disposing the metal component in a piranha solution; washing the metal component; and grafting a surface of the metal component with a Si-Quat or hybrid Si-Quat molecular layer.

Abstract: A method is provided for decreasing a wear rate of a brake stack or a heat sink wear rate and increasing a brake life of the brake stack or the heat sink. The method includes coating a wear surface of a brake disk with at least one of an engineered ceramic material or ceramic solution, thereby forming a coated brake disk and installing the coated brake disk in a multi-disk brake system.