Abstract: A portable radar system that may leverage the processing power, input and/or display functionality in mobile computing devices. Some examples of mobile computing devices may include mobile phones, tablet computers, laptop computers and similar devices. The radar system of this disclosure may include a wired or wireless interface to communicate with the mobile computing device, or similar device that includes a display. The radar system may be configured with an open set of instructions for interacting with an application executing on the mobile computing device to accept control inputs as well as output signals that the application may interpret and display, such as target detection and tracking. The radar system may consume less power than other radar systems. The radar system of this disclosure may be used for a wide variety of applications by consumers, military, law enforcement and commercial use.

Abstract: An avionic system for a rotorcraft includes a data source and an enhanced ground proximity warning system. The data source has terrain data and obstacle data stored therein. The enhanced ground proximity warning system can be selectively switched, by a pilot, to operate in either a normal mode or a desensitized mode. The enhanced ground proximity warning system receives flight data, retrieves terrain data and obstacle data from the data source, evaluates the retrieved terrain data and the obstacle data to determine variations in elevations of terrain and obstacles in predetermined area that is a predetermined distance ahead of the current position and along the flight path, and based at least in part on the determined variations, selectively generate a prompt that suggests that the pilot switch the ground proximity warning system to the desensitized mode.

Abstract: A tunable optic includes a hexagonal-shaped housing, a polar liquid, a first electrode, a second electrode, a third electrode, a fourth electrode, a fifth electrode, a sixth electrode, and a grounding electrode. The hexagonal-shaped housing includes first, second, third, fourth, fifth, and sixth side walls and first and second light transmissive end walls, and the first, second, third, fourth, fifth and sixth side walls and the first and second light transmissive end walls define a hexagonal-shaped inner cavity. The polar liquid is disposed within the hexagonal-shaped inner cavity. The polar liquid has a surface, and the surface has a curvature and a two-dimensional tilt angle that is variable in response to voltages supplied to each of the first, second, third, fourth, fifth, and sixth electrodes, whereby lens characteristics and light deflection characteristics of the tunable optic are varied.

Abstract: Cloud-based systems and methods are provided for managing data uploaded from gateway devices at different sites. One method involves a platform service obtaining telemetry data from a gateway device, assigning a first subset of the telemetry data having first temporal characteristics to a first processing pipeline, and assigning a second subset of the telemetry data having second temporal characteristics to a second processing pipeline based at least in part on metadata associated with the telemetry data. The first processing pipeline is configurable to write the first subset of the telemetry data to a data storage element concurrent to the second processing pipeline writing the second subset of the telemetry data to the data storage element. The first and second subsets of the telemetry data are mutually exclusive, and the first temporal characteristics and the second temporal characteristics are different.

Abstract: A coating fabric and method of manufacturing the same are provided. A coated fabric includes a base coating layer. The base coating layer defines a smooth coating to resist liquid penetration to the fabric. The coated fabric also includes a middle foam coating layer that is deposited on at least a portion of the base coating layer. The middle foam layer defines a middle layer foam density and is configured to absorb at least a portion of liquid. The coated fabric further includes an outer foam coating layer that is deposited on at least a portion of the middle foam coating later. The outer foam layer defines an outer layer foam density and is configured with holes to allow liquid to penetrate to the middle foam layer. The middle layer foam density is less than the outer layer foam density. A corresponding method of manufacturing is also provided.

Abstract: A control system in a UVC-based aircraft sanitization system for controlling the UVC-based aircraft sanitization system to maintain a desired UVC (ultraviolet C) radiation level at a target surface in an aircraft under varying operating conditions is disclosed. The control system includes a controller configured to: receive measured radiation feedback from a radiation measurement device (e.g., dosimeter) on the target surface that identifies a radiation level that is applied at the target surface by the UVC-based aircraft sanitization system; and generate a UVC source control command for UVC sources in the UVC-based aircraft sanitization system. based on the received measured radiation feedback, to control the UVC sources to increase or decrease radiation level output (e.g., identify the amount of increase or decrease from the UVC sources) to generate sufficient radiation to achieve the desired radiation level at the target surface.

Abstract: Mobile apparatus and methods for ultraviolet (UV) light sanitization of an aircraft. The mobile apparatus generally comprises a mobile platform, such as a trolley, that has integrated therewith circuitry and devices that control and actuate ultra-violet C-spectrum (UV-C) light sources that are mechanically coupled to the trolley. The proposed mobile apparatus includes a controller that receives input from an operator and, optionally, from dosimeters mounted on the proposed system and/or within the aircraft. Based on the inputs received, the controller provides guidance to the operator in the form of alerts and messages, as well as automatically adjusting components of the mobile apparatus to adapt itself to a specific aircraft type.

Abstract: Methods, apparatuses and systems for providing offset calibration and fault monitoring are disclosed herein. An example controller component may comprise: a resistance-based bridge circuit; a signal conditioning circuit configured to condition an output of the resistance-based bridge circuit; a first diagnostic circuit coupled to the signal conditioning circuit configured to monitor an output of a first branch of the resistance-based bridge circuit; and a second diagnostic circuit coupled to the signal conditioning circuit configured to monitor an output of a second branch of the resistance-based bridge circuit.

Abstract: Systems and methods for detection of network issues and health reporting to ground-based stakeholders are described herein. In exemplary embodiments, a system includes multiple aircraft, wherein an aircraft in the multiple aircraft communicates through one or more communication links. The aircraft includes processors that compile network event information related to degraded communication link events. Further, the aircraft includes memory units that store a degraded link event report and a configuration database, wherein the degraded link event report stores the network event information related to the degraded communication link events as directed the configuration database.

Abstract: An inline transducer meter body can include a channel that can accept a separate core to enable formation of a port to accept a sensor assembly and a notch to help stabilize the sensor assembly in alignment with fluid flow. The inline transducer meter body can include a circular shelf adapted to receive a transducer assembly that interfaces in a complimentary manner with a circular ledge of a circular head section of the transducer assembly, a portal formed between the circular shelf and an inner surface of the housing adapted to interface in a complimentary manner with an alignment section of the transducer, and a notch formed in the inner surface of the flow tube opposite the portal to interface with a positioner formed on and extending from a transducer holder.

Abstract: Disclosed are refrigerants comprising at least about 97% by weight of a blend of three compounds, said blend consisting of: from about 38% by weight to about 48% by weight difluoromethane (HFC-32), from about 6% by weight to about 12% by weight pentafluoroethane (HFC-125), from about 33% by weight to about 41% by weight trifluoroiodomethane (CF3I) and from about 2% by weight to about 16% by weight 2,3,3,3-tetrafluoropropene (HFO-1234yf) wherein the percentages are based on the total weight of the three compounds in the blend, and methods and systems which use same.

Abstract: A method of manufacturing a part with a CMAS-resistant thermal barrier coating (TBC) includes providing a part body having a surface and providing a source of coating material. The coating material includes a thermal protection material and a CMAS-reactive material. The method also includes delivering the coating material from the source toward the surface of the part body to form the CMAS-resistant TBC on the surface. The CMAS-resistant TBC includes both the thermal protection material and the CMAS-reactive material. The CMAS-reactive material is included as a substantially uniform distribution within the thermal protection material.

Abstract: In one embodiment, a stator coil that includes a first turn with two or more strands is provided. The first turn includes first and second opposite sides, a coil termination at a first end of the first turn and an inversion region disposed at a second end, opposite the coil termination. The stator coil also includes at least one additional turn with two or more strands. The at least one additional turn includes first and second opposite sides, and an inversion region located adjacent to the inversion region of the first turn. The first and second sides of the first turn are inverted relative to the first and second sides of the at least one additional turn outside their respective inversion regions.

Abstract: Devices, systems, and methods for a lid of an aspirating smoke detector device are described herein. In some examples, one or more embodiments include an aspirating smoke detector device, comprising a plurality of light pipes, a cover including a plurality of apertures to interface with the plurality of light pipes, a housing including a housing inlet and a housing outlet, and a reversible lid connectable to the cover in a first lid orientation and a second lid orientation, where when the cover and the housing are in a first device orientation, the reversible lid is to connect to the cover in the first lid orientation and when the cover and the housing are in a second device orientation, the reversible lid is to connect to the cover in the second lid orientation.

Abstract: One implementation is a device for determining the position of a valve. The device uses a current profile including at least the magnitude of current, and an analysis module for using the current profile and the state of the valve to perform at least one action.

Abstract: Devices, methods, and systems for a self-testing fire sensing device are described herein. One device includes a fan, an optical scatter chamber configured to measure a quantity of particles therein, and a controller configured to compare the quantity to a baseline quantity and transmit a command to a fan responsive to the quantity being greater than the baseline quantity, wherein the fan is configured to activate for a particular period of time to remove particles from the optical scatter chamber responsive to receiving the command, wherein the optical scatter chamber is configured to measure the quantity of particles therein after the particular period of time, and wherein the controller is configured to compare the quantity of particles after the particular period of time to the baseline quantity and report a confirmed fire responsive to the quantity of particles after the particular period of time being greater than the baseline quantity.

Abstract: Methods and systems for speech recognition in an aircraft are disclosed. Methods and systems include executing an air traffic control transcription application using first acoustic and language models and executing a command and control speech recognition application using second acoustic and language models. Flight context data is processed to identify additional words not included in training of the second acoustic and language model but included in training of the first acoustic and language models. Acoustic and language model parameters are extracted corresponding to the additional words from the first acoustic and language models. The extracted acoustic and language model parameters are added to the second acoustic and language models. An aircraft control command is generated that encapsulates at least one of the additional words using the command and control speech recognition application.

Abstract: In some examples, a system includes a digital-to-analog converter (DAC) configured to operate at a clock rate; a mixer configured to up-convert an intermediate-frequency (IF) signal from the DAC to a radio-frequency (RF) signal based on a local oscillator (LO) signal; and an RF filter configured to generate a filtered signal by at least removing, from the RF signal, frequency components greater than a difference between a frequency of the LO signal and one-half of the clock rate and less than a sum of a frequency of the LO signal and one-half of the clock rate, wherein an output node of the RF filter is configured to be coupled to an antenna for transmission of the filtered signal.

Abstract: A rotor for a turbomachine and a method of manufacturing the same. The method includes providing a lug with a lug body and an interface material disposed on the lug body. The method also includes friction welding the lug to a hub member via the interface material to define a projected structure for an outer radial area of a disc assembly of the rotor. The projected structure is configured to support a first side of a rotor blade of the rotor in cooperation with a second projected structure of the disc assembly supporting a second side of the rotor blade. The lug body and the hub member are made from different materials.

Abstract: A flame analytics system that may incorporate a burner, one or more sensors at the burner, a historical database connected to the one or more sensors, a model training module connected to the historical database, and a runtime algorithm module connected to the one or more sensors and the model training module. The runtime algorithm may compare realtime data from the one or more sensors and historical data from the model training module in accordance with a machine learning algorithm. The system may further incorporate a fault detection module connected to the runtime algorithm module, a fault diagnostics module connected to the fault detection module, and an enunciator connected to the fault detection module. The one or more sensors may also include having video or acoustic sensitivity of combustion in the burner.