Abstract: Systems and methods to fuse aviation-related data systems for comprehensive aircraft system health monitoring are provided. One example method includes obtaining, by one or more computing devices, fault data indicative of a plurality of fault indications provided by a first plurality of components of an aircraft. The method includes obtaining, by the one or more computing devices, condition indicators describing the respective operational conditions of a second plurality of components of the aircraft. The method includes fusing, by the one or more computing devices, the fault data with the condition indicators to form a comprehensive data set. The method includes identifying, by the one or more computing devices, one or more causes of the plurality of fault conditions based at least in part on the comprehensive data set. One example system includes a data fuser, a cause identifier, and an alert generator.

Abstract: A compound of formula (I), or a pharmaceutically acceptable salt thereof.

Abstract: A wireless sensor system of a gas turbine engine of an aircraft can include a plurality of wireless sensors distributed within an engine core of the gas turbine engine and an energy harvesting system including one or more energy harvesting devices configured to convert mechanical or thermal energy within the gas turbine engine into electric power and provide the electric power to the wireless sensors. The wireless sensor system can also include a data concentrator coupled to the gas turbine engine. The data concentrator can be configured to receive a plurality of wireless sensor data from the wireless sensors and transmit the wireless sensor data to a communication adapter of the gas turbine engine.

Abstract: A system includes first, second and third input data sets. The first input data set includes demographic information characterizing a patient. The second and third input data sets characterize a healthcare treatment history of the patient. A neural network includes first, second and third neural subnetworks. The first neural subnetwork is configured to process the first input data set to produce a first output data set. The second neural subnetwork is configured to process the second input data set to produce a second output data set. The third neural subnetwork is configured to process the third input data set to produce a third output data set. An autoencoder layer has an input layer comprising the first, second and third output data sets and is configured to process the first, second and third output data sets to produce a secondary output data set.

Abstract: A gas turbine engine of an aircraft includes an engine control configured to monitor and control operation of the gas turbine engine in real-time and a communication adapter that includes a housing and a plurality of antennas in the housing. The communication adapter is configured to establish communication with the engine control and wireless communication with an offboard system external to the aircraft through at least one of the antennas of the communication adapter. The housing includes a metal chassis with a non-conductive substrate between the metal chassis and the antennas. The antennas are partitioned into two or more portions. A communication interface of the communication adapter is configured to establish wireless communication through the antennas using two or more different wireless communication protocols.

Abstract: Amplifier having input power protection. In some embodiments, an amplifier circuit can include an input node and an output node, and an amplifier implemented between the input node and the output node. The amplifier circuit can further include a bias circuit configured to provide a bias signal to the amplifier. The amplifier circuit can further include a protection circuit configured to generate a detected voltage representative of a peak of a radio-frequency signal present at the input node. The protection circuit can be further configured to enable a protection mode when the detected voltage is greater than a first threshold value and to disable the protection mode when the detected voltage is less than a second threshold value that is less than the first threshold value.

Abstract: The invention concerns a plurality of peptides or polypeptides, in, or for use in, an adhesive; ideally said peptides or ploypeptides include at least one, including any combination, of the following sequences: an adhesive sequence, a cross-linking sequence, an elastic conferring sequence, and a de-bonding or cleavable sequence.

Abstract: A filling, coating or spread for use in food applications comprising a structured fat system, wherein the structured fat system comprises from 10 w/w % to 90 w/w % of a lipid and from 10 w/w % to 90 w/w % of an edible porous particle, wherein the lipid is present as a continuous phase in said structured fat system. The use of a structured fat system for reducing the trans- and saturated fat content of a filling, coating or spread, wherein the structured fat system comprises from 10 w/w % to 90 w/w % of a lipid and from 10 w/w % to 90 w/w % of an edible porous particle, wherein the lipid is present as a continuous phase in said structured fat system.

Abstract: A communication adapter of a gas turbine engine of an aircraft includes a communication interface configured to wirelessly communicate with an offboard system and to communicate with an engine control of the gas turbine engine. The communication adapter also includes a memory system and processing circuitry configured to receive one or more configuration items from the offboard system, apply a cryptographic algorithm using one or more parameters received and cryptographic information to decrypt the one or more configuration items, wherein the cryptographic information includes a combination of received cryptographic information and previously stored cryptographic information, and transfer the one or more configuration items to the engine control after applying the cryptographic algorithm.

Abstract: A communication adapter of a gas turbine engine of an aircraft includes an internal sensor system including a plurality of sensors within the communication adapter, a memory system, and processing circuitry. The processing circuitry is configured to receive a plurality of time series data at the communication adapter from an engine control of the gas turbine engine, record a plurality of internal sensor data of the internal sensor system, correlate the time series data with the internal sensor data based on an alignment in time to form an enhanced data set, and transmit the enhanced data set from the communication adapter to an offboard system.

Abstract: A broadband power splitter can include an input port, a first output port and a second output port. The power splitter can further include a first signal path implemented between the input port and the first output port, and a second signal path implemented between the input port and the second output port. Each of the first and second signal paths can include a variable capacitance configured to provide a plurality of capacitance values that result in different frequency responses of the respective signal path.

Abstract: There is provided a method comprising: determining an occupancy status of a first region of a vehicle; determining, based at least in part on the occupancy status, a first climate control setting for the first region; controlling a climate control system of the vehicle to adjust a climate of the first region according to the first climate control setting; determining that a second region of the vehicle is unoccupied, wherein the second region is fluidly connected to the first region; determining a second climate control setting, wherein the second climate control setting is based at least in part on the occupancy status of the first region and characteristic data associated with a predicted potential change in occupancy status for the second region; and controlling the climate control system to adjust a climate of the second region according to the second climate control setting.

Abstract: A communication adapter of a gas turbine engine of an aircraft includes a communication interface configured to wirelessly communicate with an offboard system and to communicate with an engine control of the gas turbine engine. The communication adapter also includes a memory system and processing circuitry configured to receive one or more configuration items from the offboard system, confirm an authentication between the communication adapter and the engine control, apply a cryptographic algorithm using one or more parameters received and cryptographic information to decrypt the one or more configuration items, wherein the cryptographic information includes a combination of received cryptographic information and previously stored cryptographic information, and transfer the one or more configuration items to the engine control based on the authentication.

Abstract: A method of operating a communication adapter of a gas turbine engine of an aircraft includes receiving a plurality of time series data at the communication adapter from an engine control of the gas turbine engine. The method also includes recording a plurality of internal sensor data of an internal sensor system of the communication adapter. The method further includes correlating the time series data with the internal sensor data based on an alignment in time to form an enhanced data set and transmitting the enhanced data set from the communication adapter to an offboard system.

Abstract: There is disclosed a nanopore support structure comprising a wall layer comprising walls defining a plurality of wells, and overhangs extending from the walls across each of the wells, the overhang defining an aperture configured to support a membrane suitable for insertion of a nanopore. There is further disclosed a nanopore sensing device comprising a nanopore support structure, and methods of manufacturing the nanopore support structure and the nanopore sensing device.

Abstract: A system includes a memory system configured to store a plurality of instructions to provide aircraft communication visualization and a processing system. The processing system configured to execute the instructions to result in retrieving a plurality of status data associated with aircraft communication at a target location from a database, determining a plurality of geographic location information for a plurality of aircraft parking locations at the target location, accessing a plurality of imagery data associated with a view at the target location, and generating an aircraft communication visualization map for the target location. The aircraft communication visualization map includes aircraft communication information overlaid upon an image based on the imagery data and the aircraft parking locations at the target location.

Abstract: A communication adapter of a gas turbine engine of an aircraft includes a communication interface configured to wirelessly communicate with an offboard system and to communicate with an engine control of the gas turbine engine, a memory system, and processing circuitry. The processing circuitry is configured to receive an engine control dynamic data recording request from the offboard system, confirm an authentication between the communication adapter and the engine control, transfer the engine control dynamic data recording request received at the communication adapter from the offboard system to the engine control based on the authentication, and transmit an update completion confirmation of the engine control from the communication adapter to the offboard system based on a confirmation message from the engine control.

Abstract: A filling, coating or spread for use in food applications comprising a structured fat system, wherein the structured fat system comprises from 10 w/w % to 90 w/w % of a lipid and from 10 w/vv % to 90 w/w % of an edible porous particle, wherein the lipid is present as a continuous phase in said structured fat system. The use of a structured fat system for reducing the trans- and saturated fat content of a filling, coating or spread, wherein the structured fat system comprises from 10 w/w % to 90 w/w % of a lipid and from 10 w/w % to 90 w/w % of an edible porous particle, wherein the lipid is present as a continuous phase in said structured fat system.

Abstract: The invention relates to emulsions for use in food products. In particular, the invention relates to stable water-in-oil emulsions for reduced fat food products such as confectionery, spreads, and bakery goods.

Abstract: A gas turbine engine of an aircraft includes an engine control configured to monitor and control operation of the gas turbine engine in real-time and a communication adapter that includes a housing and a plurality of antennas in the housing. The communication adapter is configured to establish communication with the engine control and wireless communication with an offboard system external to the aircraft through at least one of the antennas of the communication adapter. The housing includes a metal chassis with a non-conductive substrate between the metal chassis and the antennas. The antennas are partitioned into two or more portions. A communication interface of the communication adapter is configured to establish wireless communication through the antennas using two or more different wireless communication protocols.