Abstract: A liquid measurement system for determining a quantity of a liquid within a tank includes a pressurized air supply, a valve connected to the pressurized air supply with the valve able to introduce a known mass of air into the tank, a pressure sensor able to measure the change in air pressure within the tank, and a processor operatively connected to the valve and the pressure sensor. The processor is able to determine the volume of the liquid within the tank from the known mass of air introduced into the tank and the change in air pressure within the tank.

Abstract: A system and method includes a structural body, a plurality of structural health monitoring (SHM) sensors, and first and second computer systems. The structural body includes a plurality of structures. The SHM sensors are configured to sense structural health data for a plurality of zones of the structures. The first computer system is configured to collect the structural health data from the SHM sensors. The second computer system includes a display and is configured to receive the structural health data from the first computer system and groups the zones into a plurality of structural regions, and groups the plurality of structural regions into at least one structural area. The display is configured to provide a visual representation of a structural region health of a first one of the plurality of structural regions based on the structural data for respective ones of the zones within the first one of the plurality of structural regions.

Abstract: A brake monitoring and adjustment control system includes an electromechanical brake actuator controller (EBAC) and at least one sensor operatively connected to the EBAC. The sensor is configured to sense a characteristic of a brake and provide a feedback signal to the EBAC. The system includes a switch for turning power to the sensor on and off to reduce the duration with voltage applied to the sensor. Reducing the duration in which voltage is applied to the sensor reduces power consumption and assists with mitigating electro-migration growth.

Abstract: A method can include generating reference image data representing a field of view of an interior of a fuel tank, and generating active image data representing the field of view of the interior of the fuel tank when the fuel tank contains fuel. The method can further include producing, by a processing device, a fuel measurement value representing an amount of fuel contained in the fuel tank based on the reference image data and the active image data, and outputting, by the processing device, an indication of the fuel measurement value.

Abstract: Apparatus and associated methods relate to generating a trigger signal in response to detection of a triggering acoustic event sensed by one of a distributed network of optical acoustic sensors mechanically coupled to an aircraft structure. Each of the optical acoustic sensors is configured to generate an optical response signal indicative of an acoustic condition detected by the optical acoustic sensor. A controller receives the optical response signals and generates, if a triggering one of the optical response signals is indicative of a triggering acoustic event, a trigger signal. The controller also determines a location of the specific one of the distributed network of optical acoustic sensors that generated the triggering one of the optical response signals. In some embodiments, the trigger signal is sent to a Health & Usage Monitoring System configured to perform a health scan, in response to receiving the trigger signal, of the aircraft structure.

Abstract: A system and method includes an arbitrating data bus and a plurality of sensing nodes connected to communicate on the arbitrating data bus. The plurality of sensing nodes are configured to digitize and monitor a first amount of data during a listening mode of an event monitoring mode and detect an event based upon the first amount of data. The plurality of sensing nodes are further configured to output an event message to the arbitrating data bus upon detection of the event. The plurality of sensing nodes are further configured to digitize and retain a second amount of data following detection of the event message on the arbitrating data bus.

Abstract: An inductive sensor includes a core body, a coil wound on the core body, a cavity having a fixed volume within the core body, and an epoxy mixture filling a controlled portion of the fixed volume. The controlled portion of the fixed volume filled with the epoxy mixture controls an inductance of the sensor.

Abstract: A method for estimating rotational speed of a system includes receiving vibrational data from a sensor, estimating a speed from the vibrational data to create estimated speed data, and filtering the estimated speed data through an adaptively weighted filter to minimize incorrect speed estimation.

Abstract: A multi-level network system of an aircraft includes at least one equipment area network and a wide area network. The equipment area network includes equipment of the aircraft, at least one wireless device, and at least one equipment area network coordinator. The at least one wireless device is configured to transmit and receive data using a first wireless link. The at least one equipment area network coordinator is configured to transmit to and receive data from the at least one wireless device using the first wireless link and to transmit data to and receive data from the wide area network using a second wireless link, the first wireless link using lower power than the second wireless link. The wide area network includes a wide area network coordinator that is configured to transmit and receive data from the at least one equipment area network coordinator using the second wireless link.

Abstract: Redundant wireless sensor networks include a plurality of wireless sensors and a wireless data concentrator. The plurality of wireless sensors sense a parameter and transmit sensor signals representative of the parameter sensed. The wireless data concentrator receives the sensor signals and adjusts the transmission schedules of at least one of the plurality of wireless sensors based on a change in operating status of one or more of the plurality of wireless sensors.

Abstract: A method can include illuminating an interior of a fuel tank with one or more light pulses, and receiving reflected returns of the one or more light pulses at a light sensor array. The method can further include producing, by a processing device, three-dimensional image data of the interior of the fuel tank based on the received reflected returns, producing, by the processing device, a fuel measurement value representing an amount of fuel contained in the fuel tank based on the three-dimensional image data, and outputting, by the processing device, an indication of the fuel measurement value.

Abstract: A method for determining an operational condition of a vibratory system, comprising receiving vibration signals from one or more sensors associated with the vibratory system preprocessing the vibration signals to remove known noise to create a preprocessed signal, processing the preprocessed signal in both a time domain and a frequency domain to create time domain data and frequency domain data, respectively, and fusing the time domain data and the frequency domain data to determine the existence of abnormal operations.

Abstract: A method for monitoring for a surge condition includes detecting a surge condition through vibration signals measured at at least one location in a turbomachine. Detecting a surge condition includes determining a ratio-metric indicator RBR by comparing a blade frequency band ?B to a reference frequency band ?R. Detecting a surge condition includes calculating a surge score SS with the following equation: SS = R BR - R ? R ? wherein R? is a sample mean of a set of ratio-metric indicators and R? is a sample standard deviation of a set of ratio-metric indicators. Detecting a surge condition includes determining whether a surge condition exists based on the surge score.

Abstract: A control system for a flight vehicle includes first and second pivot pins each having a hollow cylindrical shape with an opening therein, first and second deployable wings configured to pivot about the first and second pivot pins between a stowed position and a deployed position with the first and second deployable wings each having first and second wing tip shafts extending between the first and second pivot pins and first and second ailerons at a tip of the deployable wings, first and second lever pins within the opening in the pivot pins with the first and second lever pins each having a first end that extends out from a top of the pivot pin and a second end connected to the wing tip shaft and with the first and second lever pins configured to rotate the wing tip shafts to control the ailerons.

Abstract: Apparatus and associated methods relate to selectively bypassing a daisy-chained network device based on a timing of a series of reset signals. The daisy-chained network device is bypassed if an elapsed time from a last of the reset signals of the series is longer than a predetermined time period. While no interval between adjacent reset signals of the series exceeds the predetermined time period, the daisy-chained network device is not bypassed. In some embodiments, the daisy-chained network device generates the series of reset signals. If the daisy-chained network device fails to generate a next reset signal within the predetermined time period as measured from a previous reset signal, the daisy-chained network device is bypassed. If the daisy-chained network device loses power, it will be bypassed as the reset signals will not be generated, but if the daisy-chained network device regains power, it can be reinserted into the network daisy-chain.

Abstract: Apparatus and associated methods relate to determining the wavelength of a narrow-band light beam. Two portions of the narrow-band light beam are projected onto two dissimilar photodetectors, respectively. The two dissimilar photodetectors have dissimilar spectral responses over a domain of wavelengths that includes the wavelength of the narrow-band light beam. Each of the two dissimilar photodetectors generates an output signal indicative of a photocurrent induced by the projection of the portion of the narrow-band light beam thereon. A ratio of the differences between the photocurrents to the sum of the photocurrents of the two dissimilar photodetectors is determined. The determined ratio is a monotonic function of wavelength over the domain wavelengths including the wavelength of the narrow-band light beam. The determined ratio is thereby indicative of the wavelength of the narrow-band light beam.

Abstract: Apparatus and associated methods relate to continuously providing power to a load throughout an interruption of a power source. While the power source is providing power, a converter is exciting a primary winding of a transformer. A load winding of the transformer delivers power to a load connected thereto, and a holdup winding provides power to a holdup circuit, which stores energy for use when the power source is interrupted. A turns ratio of the holdup winding to the primary winding is greater than one so that the energy stored by the holdup circuit is at a voltage that is greater than or equal to the voltage used for exciting the primary windings. If the voltage used for exciting the primary windings falls below a predetermined threshold, a one-shot controls the transfer of energy stored in the holdup circuit to a storage capacitor supplying current to the primary windings.

Abstract: A smart sensor system can include one or more configurable input and output channels, each configurable channel including one or more switches configured to activate the input and/or output and/or to select a type of input and/or output signal, at least one analog-to-digital converter and at least one digital-to-analog converter operatively connected to the one or more switches for the one or more configurable channels, and at least one controller configured to control the configurable channels.

Abstract: A sensor system and method includes first and second sensing elements, digital sensors, a host computer and a digital bus. The first sensing element is configured to collect first sensor data and the second sensing element is configured to collect second sensor data. The digital sensor includes a controller that is configured to receive the first and second sensor data and process the first sensor data together with the second sensor data to generate processed data. The host computer is configured to receive the processed data from the digital sensor over the digital bus.

Abstract: A first air data value is generated based on a first set of parameters. A second set of parameters that does not include any of the first set of parameters is processed through an artificial intelligence network to generate a second air data value. The second set of parameters is processed through a plurality of diagnostic artificial intelligence networks to generate a plurality of diagnostic air data values. Each of the plurality of diagnostic artificial intelligence networks excludes a different one of the second set of parameters. One of the second set of parameters is identified, based on the first air data value and the plurality of diagnostic air data values, as a fault source parameter that is associated with a fault condition.