Abstract: Systems and methods for automatic uplink of weather information are provided. In one embodiment, a ground-based system for automatically communicating crowdsourced weather information comprises: at least one transceiver configured to communicate with vehicles via one or more communication links; a weather data processing system coupled to the at least one transceiver, the weather data processing system comprising at least one processor coupled to a memory, the at least one processor configured to: receive weather information from the vehicles; aggregate the weather information received from the vehicles and store aggregated weather information in the memory; automatically transmit aggregated weather information to a first vehicle of the vehicles via the one or more communication links in response to the weather data processing system receiving a radar error report from the first vehicle.

Abstract: Methods and systems are provided for operating a vehicle that supports an automated action, such as an aircraft supporting autopilot, autothrottle, and various other autonomous operations and operating modes. One exemplary method of operating a vehicle involves obtaining one or more user inputs pertaining to an automated action to be performed by an onboard system, obtaining current vehicle status information, determining an operational objective for the automated action based at least in part on the current status information and the one or more user inputs, and providing guidance information pertaining to the automated action in a manner that is influenced by the operational objective and the current status information. For example, the guidance information may include indication of a remedial action to resolve a discrepancy between the operational objective and a projected aircraft behavior in the context of the operational objective or the current vehicle status.

Abstract: An integrity monitoring method for navigation systems with heterogeneous measurements is provided. Measurements from a plurality of different type navigation aiding sources are categorized by an information domain, an aiding class and an aiding section. The information domain is a category of at least one of estimated states and measurements that represent a same physical category. The aiding class is a category that uses a same physical method to acquire measurements. The aiding section is a category of measurements from the same aiding source. The measurements are organized into a plurality of measurement clusters based at least in part on measurement fault modes to be detected, measurement fault modes to be excluded, available computer resources and required performance. An integrity monitoring algorithm is applied to the measurement clusters to determine an integrity solution for all defined integrity monitoring classes.

Abstract: Multistage gas turbine engine (GTE) compressors having optimized stall enhancement feature (SEF) configurations are provided, as are methods for the production thereof. The multistage GTE compressor includes a series of axial compressor stages each containing a rotor mounted to a shaft of a gas turbine engine. In one embodiment, the method includes the steps or processes of selecting a plurality of engine speeds distributed across an operational speed range of the gas turbine engine, identifying one or more stall limiting rotors at each of the selected engine speeds, establishing an SEF configuration in which SEFs are integrated into the multistage GTE compressor at selected locations corresponding to the stall limiting rotors, and producing the multistage GTE compressor in accordance with the optimized SEF configuration.

Abstract: Quantum resolution imaging methods and devices are disclosed herein. The quantum resolution imaging device comprises an optical component provided to receive incoming radiation, a mode separating structure for separating the received incoming radiation into multiple modes, and an imaging array having multiple array elements for measuring an energy level of each mode to construct an image of the received incoming radiation as it comes in contact with a surface of one of the array elements.

Abstract: An example device for performing a write operation using a spintronic Hall effect includes a Spin Hall Effect (SHE) structure, a Magnetic Tunnel Junction (MTJ) element, and processing circuitry. The MTJ element includes a free structure, a pinned structure, and a tunnel barrier arranged between the free structure and the pinned structure. The free structure comprises a plurality of free layers. The free structure is arranged with the SHE structure such that current in the SHE structure induces spin transfer into the free structure. The processing circuitry is configured to receive an instruction to set the MTJ element to a target state of a plurality of states and in response to receiving the instruction, generate electrical current through the spin Hall effect structure to modify a resistance of the MTJ element to correspond to the target state.

Abstract: Additively-manufactured flow restrictors are provided, as are methods for producing additively-manufactured flow restrictors. In various embodiments, the additively-manufactured flow restrictor includes a flowbody through which a flow path extends, a restricted orifice located in the flowbody and providing a predetermined resistance to fluid flowing along the flow path in a first flow direction, and a first internal perforated screen positioned in the flow path upstream of the restricted orifice taken in the first flow direction. The flowbody and the first internal perforated screen integrally formed as a single additively-manufactured piece utilizing, for example, Direct Metal Laser Sintering (DMLS) or another additive manufacturing process. In certain embodiments, the first internal perforated screen may include an endwall and a peripheral sidewall, which is integrally formed with the endwall and spaced from an inner circumferential surface of the flowbody by an annular clearance.

Abstract: A demand response management system which may be implemented with demand response logic. The system may be used by utilities, independent system operators, intermediaries and others to manage operations of demand response programs relative to customers, clients, participants, and users of outputs from the utilities, independent system operators, and the like. Demand response logic of the demand response management system may provide demand signal propagation and generation from demand response events.

Abstract: An inertial inlet particle separator system for a vehicle engine is provided. A separator assembly and collector assembly are coupled to the scavenge flow path and configured to receive the scavenge air. The collector inlet has a throat defining a cumulative throat area at each position along the throat length from the first throat end to the second throat end. The collector body defines a cross-sectional area associated with each position along the throat length between the first throat end and the second throat end. The collector outlet is coupled to the collector body such that scavenge air flows into the collector inlet, through the collector body, and out through the collector outlet. At a first position between the first throat end and the second throat end, the respective cross-sectional area of the collector body is greater than or equal to the respective cumulative throat area.

Abstract: A method of forming a high strength copper alloy. The method comprises heating a copper material including from about 2 wt. % to about 20 wt. % manganese by weight of the copper material to a temperature above 400° C., allowing the copper material to cool to a temperature from about 325° C. to about 350° C. to form a cooled copper material, and extruding the cooled copper material with equal channel angular extrusion to form a cooled copper manganese alloy.

Abstract: Systems and methods for selecting a runway record for a target runway are provided. The system includes: a first database having a first runway record with a first runway threshold; a second database having a second runway record with a second runway threshold; a transceiver for receiving an ILS signal; and a computer system. The computer system is configured to determine when the ILS signal is substantially zero. When the ILS signal is substantially zero, the computer system is configured to receive, from one or more databases, a plurality of runway records including corresponding runway thresholds; and select a most accurate runway record from the plurality of runway records based, at least in part, on which of the corresponding runway thresholds deviates least from the aiming point. In various embodiments, the most accurate runway record is then utilized for rendering images in a cockpit display system.

Abstract: Devices, methods, and systems for detecting faults on a spur wired alarm circuit are described herein. One system includes a bipolar capacitor coupled to a last device on a spur wired alarm circuit, a voltage supply coupled to the spur wired alarm circuit, and a controller configured to operate the voltage supply such that a current flows through the spur wired alarm circuit, operate the voltage supply such that the current stops flowing through the spur wired alarm circuit for a particular amount of time, determine a voltage across the bipolar capacitor while the current has stopped flowing through the spur wired alarm circuit, and determine whether a fault has occurred on the spur wired alarm circuit based on the determined voltage.

Abstract: Method and system for automatically generating data points in a data management system. A control strategy and variables used in the control strategy can be configured, wherein the control strategy governs a data management system associated with a controller. The control strategy and the variables can be downloaded to the controller after configuring the control strategy and variables. The control strategy is then run on the controller and published to the data management system before, during, or after downloading of the control strategy. All available variables in the controller are then automatically listed so as to generate data points that can be downloaded and updated through a communication channel between the data management system and the controller.

Abstract: A method comprises: determining if a personal computing system in a vehicle is authentic using a radio system in the vehicle, where the radio system is configured (a) to communicate with at least one ground system and (b) to be coupled to a vehicle system; if the personal computing system is authenticated, creating a link between the personal computing system and the radio system; and at least one of: restricting data routing to and from at least one of: (a) vehicle system type(s), and (b) application program(s) of at least one of the vehicle system and the personal computing system; restricting data type(s) transmitted between the personal computing system and the vehicle system; and routing data between the personal computing system, and at least one of (a) at least one ground system not through a communications management system and (b) the vehicle system.

Abstract: A differential signature detection system is provided. The system comprises: a target sensor, wherein the target sensor is configured to measure acoustical signals within a first narrow band around a target frequency; an offset sensor, wherein the offset sensor is configured to measure acoustical signals within a second narrow band around an offset frequency; and a controller coupled to the target sensor and the offset sensor, wherein the controller is configured to: compare a signal output of the target sensor with an output of the signal output of the offset sensor to calculate a differential measurement that comprises a difference in signal peak intensity; compare the differential measurement to a reference signal, wherein the reference signal comprises a threshold indicative of a presence of a characteristic signature peak associated with a target object; and produce an output based on the comparison between the differential measurement and the reference signal.

Abstract: Methods, devices, and systems for building system commissioning using mixed reality are described herein. One system includes a computing device comprising computer readable instructions stored thereon that are executable by a processor to retrieve configuration data for a physical controller from a remote distributed database in response to receiving a query, display the configuration data for the physical controller in a mixed reality display on a mixed reality device, and install the configuration data on the physical controller.

Abstract: An example device for performing a write operation, the device including a Magnetic Tunnel Junction (MTJ) element and processing circuitry. The MTJ element including a free structure, a pinned structure, and a tunnel barrier arranged between the free structure and the pinned structure. The processing circuitry is configured to receive an instruction to set the MTJ element to a low-resistance state and provide a write voltage to the MTJ element such that the tunnel barrier breaks down to generate a low-resistance channel between the free structure and the pinned structure.

Abstract: An automatic diversion management system on-board an aircraft is provided. The diversion management system is configured to automatically detect a need for the aircraft to divert from a primary airport to a diversion airport; automatically initiate diversion planning to a suitable diversion airport responsive to detecting conditions that can cause a need for diversion; automatically create a diversion flight plan; automatically send a clearance request to air traffic control (ATC) for a first type of conditions causing a need for diversion and send a clearance request to ATC, responsive to flight crew action, for a second type of conditions causing a need for diversion; and automatically activate the diversion flight plan after receipt of ATC clearance for the first type of conditions causing a need for diversion and activate the diversion flight plan, responsive to flight crew action, for the second type of conditions causing a need for diversion.

Abstract: A system comprises a GNSS unit onboard an aircraft, with the GNSS unit operative to generate horizontal and vertical deviation signals. An onboard converter unit is in communication with the GNSS unit, and an onboard radio navigation computer is in communication with the converter unit. The converter unit performs a method for converting the deviation signals to equivalent VHF instrument landing system signals.

Abstract: Provided are enhanced flight guidance systems and methods for an aircraft. The method includes recognizing when the aircraft is in manual operation and an active flight path is different than the planned flight path. An interrupt is received and categorized as one of (i) obstacle, (ii) equipment/fuel, or (iii) pilot health monitor. A managed mode begins, including identifying a rejoining leg of the planned flight path at which to rejoin and a location on the rejoining leg at which to rejoin. A recapture path strategy is selected from (i) lateral, (ii) vertical, and (iii) mixed lateral and vertical. A recapture path to the location on the rejoining leg is computed. The computed recapture path includes speed targets and configuration requirements at dedicated points along the recapture path. Aircraft state data along the recapture path is predicted and guidance controls for the aircraft along the recapture path are generated.