Abstract: A method of chemically stripping a surface is described. The method comprises applying a sealant to at least a portion of a surface of an object, the surface comprising a coating and one or more ingression points, the sealant filling the one or more ingression points to form a sealed surface. The method further comprises applying a stripping agent to the sealed surface to remove at least a portion of the coating to form a stripped surface.

Abstract: A method is provided for classifying a maintenance record for a machine. The method includes receiving the maintenance record including maintenance event information expressed as a collection of terms of interest, and normalizing the terms of interest to their non-abbreviated, dictionary form. The method includes accessing a database of authoritative engineering information from electronic documents, expressed textually and indexed by class of a plurality of classes. The method includes weighted scoring the authoritative engineering information that uses one or more of the terms of interest represented in the weighted scoring by uniqueness scores. Matching authoritative engineering information is determined for the maintenance event information based on the weighted scoring, and the maintenance record is labeled with the class to which the matching authoritative engineering information is indexed.

Abstract: An aerial vehicle control surface actuation system comprises a rotary actuator having opposing output shaft ends that are coupled to first and second torque tubes via actuator universal joints. The first and second torque tubes extend angularly from the rotary actuator. The system further comprises first and second pivot joints that are coupled to a hinged end of a control surface. The first and second pivot joints are coupled to the first and second torque tubes, respectively, via control surface universal joints. In this configuration, rotation of the first and second torque tubes causes rotation of the control surface relative to a hinge axis.

Abstract: A method includes storing technical models in a network-accessible model repository. Each technical model is labeled with descriptive metadata and comprises one or more model views labeled with functional metadata. A request is received from a stakeholder device, the request specifying descriptive attributes and functional attributes applied to an associated stakeholder. Technical model(s) are retrieved based on the descriptive metadata labelling the retrieved technical models being determined to satisfy the descriptive attributes included in the request. For each retrieved technical model, one or more model views are compiled based on the functional metadata labelling the compiled model view being determined to satisfy the functional attributes included in the request.

Abstract: A wing lock and deployment apparatus for an air launched vehicle includes a ball screw and driver acted on by a single actuation event. The disclosed wing lock and deployment apparatus is capable of unlocking deployable wings of an air launched vehicle, deploying deployable wings of the air launched vehicle from a stored position, and locking deployable wings of the air launched vehicle in a deployed position in sequential order with the one single actuation event.

Abstract: A system and method for evaluating a bond is provided. The system uses an underwater spark discharge to generate a compression wave in a first vessel containing a liquid. The system further includes a second vessel in which a vacuum is pulled to hold the first vessel against a bonded structure being inspected. The compression wave is directed to propagate from the liquid into the bonded structure to apply a known force to the bond being inspected.

Abstract: Lateral sleep systems for aircraft are disclosed. A divider is located between a first seat and a second seat of the aircraft. The divider includes a first panel oriented toward the first seat and a second panel oriented toward the second seat. The first panel defines a first support ledge. The second panel defines a second support ledge. A first lateral sleep apparatus positioned on a first side of the divider adjacent the first seat includes a first headrest and a first cradle. The first cradle supports the first headrest and includes a first panel mounting interface coupling the first headrest to the first support ledge. A second lateral sleep apparatus positioned on a second side of the divider adjacent the second seat includes a second headrest and a second cradle. The second cradle supports the second headrest and includes a second panel mounting interface coupling the second headrest to the second support ledge.

Abstract: An analytical inspection system for determining concentration of mobile hydrogen of and/or on surfaces of a metallic object can include: a vacuum furnace; a hydrogen sensing device; and/or a flow path from the furnace to the sensing device. The sensing device can be configured to detect and/or measure the mobile hydrogen at levels less than or equal to 1 part per million (ppm). An analytical inspection method for determining concentration of mobile hydrogen of and/or on surfaces of a metallic object can include: placing the object into a vacuum furnace; drawing a vacuum in the furnace; and/or simultaneously heating the metallic object in the furnace and measuring a quantity of the mobile hydrogen released from the object using a hydrogen sensing device. The sensing device can be configured to detect and/or measure the mobile hydrogen at levels less than or equal to 1 ppm.

Abstract: There is provided a scalable area gripper that includes a structural frame and variable vacuum zones coupled to the structural frame. Each variable vacuum zone includes (i) vacuum ports, (ii) one or more movable barrier elements, and (iii) an actuator assembly to move each of the one or more movable barrier elements across one or more of the vacuum port(s), to cause the one or more vacuum port(s) to go between a closed state and an open state. One or more of the variable vacuum zone(s) is configured to be adjusted to each provide an adjusted vacuum zone that corresponds to a corresponding identified section of a material having a start portion and an end portion. Each adjusted vacuum zone is configured to be positioned adjacent to its corresponding identified section of the material, and is configured to be activated to pick up the material during a material handling process.

Abstract: An interface system for flight deck communications includes a chatbot configured to perform a conversation with a pilot. The conversation includes speech communications, visual communications using a display, or both. The interface system also includes a dynamic conversational graph generator. The dynamic conversational graph generator is configured to perform a set of functions including determining a flight operational procedure from the conversation with the pilot. The set of functions also include providing information associated with the flight operational procedure to the chatbot for communicating to the pilot. The set of functions also include responding to any requests received from the pilot by the chatbot during the conversation with the pilot.

Abstract: An avionics unit assembly for an aircraft can include an avionics unit (e.g., an underwater locator device, “ULD”), and a battery to power the avionics unit. The avionics unit assembly can further include a housing that encases the avionics unit and the battery. The housing includes a vent port for exhausting an emission from the housing during a failure of the avionics unit. The avionics unit assembly can further include one or more of a suppressor that filters the emission, a shield element that is resistant to chemical and/or thermal effects of the emission, and a bracket for mounting the avionics unit to a surface. A method integrating the avionics unit assembly onto a forward aircraft bulkhead at a mount location under an aircraft radome and for manufacturing the avionics unit, and an aircraft including the avionics unit are also described.

Abstract: Systems and methods are provided for indexing a layup mandrel. One embodiment is a method for indexing a layup mandrel for a composite part. The method includes identifying a surface of a layup mandrel that travels in a process direction during fabrication of a composite part, placing a lamination head in contact with the surface, traversing the surface of the layup mandrel with the lamination head, acquiring a stream of 3D coordinates of the lamination head as the lamination head traverses the surface, characterizing the layup mandrel based on the stream of 3D coordinates, altering a Numerical Control (NC) program that directs layup of fiber reinforced material at the layup mandrel, based on a difference between the alignment of the layup mandrel and a nominal alignment of the layup mandrel.

Abstract: A flight data aggregation system for a plurality of aircraft includes one or more portable electronic devices in electronic communication with one or more central computers. The one or more portable electronic devices each monitor flight data from a corresponding aircraft. The one or more portable electronic devices analyze the flight data in real-time to determine an insight event indicating an incident of significance is presently occurring upon the corresponding aircraft. Each central computer includes one or more processors and a memory coupled to the one or more processors. The central computers are caused to receive the flight data collected during the insight event from an individual portable electronic device. The central computers determine overall flight data patterns based on the flight data collected during the insight event received from the individual portable electronic device and historical data stored in the one or more databases.

Abstract: Devices and methods of a pod that deploys from an aircraft or vehicle and descends to safely land. The pod is configured to be attached to an aircraft or vehicle. The pod includes walls that extend around and form a contained interior space that houses one or more travelers or cargo containers. During flight of the aircraft or vehicle, the pod deploys from the aircraft or vehicle while at an elevation above ground. A landing location is determined for the pod. While the pod is descending, the pod is steered towards and lands at the landing location.

Abstract: Systems and methods for manufacturing a composite member. The system and methods are configured to move different types of composite plies from different supply stations. The composite plies are moved along a conveyance member and then with a transfer station to a forming tool. One or more forming members form the composite plies onto the forming tool.

Abstract: An assembly integrates an aft wing spar root fitting to an aircraft fuselage when joining the aircraft wing to the aircraft body. The assembly provides structural strength to the connection between the aircraft wing and the aircraft body, provides corrosion prevention and provides improved inspection capabilities and repair capabilities to the aircraft wing and aircraft body connection.

Abstract: A buck voltage regulator device comprises a coupled inductor, a high-side switch electrically connected between an electrical energy source and a primary winding of the coupled inductor, a first low-side switch electrically connected between the primary winding and a ground node, a second low-side switch electrically connected between an auxiliary winding of the coupled inductor and the ground node, a first output node electrically connected to the primary winding, a second output node electrically connected to the auxiliary winding, a first output storage capacitor electrically connected to the primary winding between the first output node and the ground node, and a second output storage capacitor electrically connected to the auxiliary winding and between the second output node and the ground node.

Abstract: A method of positioning a composite charge onto a forming tool using a composite charge positioning assembly. The composite charge is placed onto a first surface of a first charge support arm of the composite charge positioning assembly and a second surface of a second charge support arm of the composite charge positioning assembly. The composite charge is placed in contact with a portion of a forming surface of the forming tool.

Abstract: A method of controlling operation of a linear actuator, including maintaining the linear actuator in equilibrium when supporting a first load, determining application of a second load on the linear actuator, and selectively actuating the linear actuator in response to application of the second load on the linear actuator.

Abstract: A cargo restraint system includes a cargo conveyor system, which has a plurality of rollers and a cargo restraint. The cargo restraint includes an inner pawl rotatably attached to the cargo conveyor system and an outer pawl rotatably attached to the cargo conveyor system. A lever is rotatably attached to the cargo loading system. A mechanical linkage connects the lever to the outer pawl and to the inner pawl, the outer pawl and the inner pawl being controlled by movement of the lever through the mechanical linkage.