Abstract: A method for identifying ghost aircraft and a system for displaying information in an aircraft including a flight display onboard the aircraft and configured to display a visual expression of at least some air traffic information and an interrogation module configured to determine information about an other aircraft based on the identification address to define interrogated data, determine real-time information about the other aircraft, compare the real-time information and the interrogated data and update the flight display based on the comparison.

Abstract: A contactor apparatus and method for operating the contactor apparatus can include a contactor assembly with a contactor coil operably coupled to a contactor switch. One or more sensors can be provided in the contactor assembly adapted to measure one or more aspects of the contactor assembly. Based upon the measured aspects, a controller can initiate operation of the contactor switch to effectively toggle the contactor switch at a zero-crossing point along an alternating current waveform.

Abstract: An electromagnetic device and method for cooling the electromagnetic device comprising a permeable magnetic core having a plurality of legs, a former located adjacent the permeable magnetic core wherein the former is thermally conductive, and at least one winding configured to conduct an electrical current there through wound on the former, the at least one winding including a coil having a plurality of turns.

Abstract: A system and method relates to analysing data indicative of system performance for a vehicular transport system. More particularly, the present invention relates to integrating aircraft management, monitoring, and maintenance systems, such as Health & Usage Monitoring/Management Systems (HUMS), On-board Maintenance Systems (OMS), Cockpit Voice & Flight Data Recorders (CVFDR), and/or Quick Access Recorder (QAR) previously distributed over multiple systems, into a single circuit card assembly (CCA). The single circuit card may consist of the electronics needed for data acquisition, processing, storage and transmission to support all of the above systems and similar. The present system and method is further related to running the software to perform aircraft management, monitoring, and maintenance functions on the single common CCA.

Abstract: A method and system of designing control logic for an avionics system, the method and system including receiving a function requirement defining a desired control logic for the desired control system, designing, by a user in a user interface (UI) of a toolset, the desired control logic comprising an arrangement of predefined library blocks to enable the functional requirement in the desired control system, and generating, by the toolset, a data file representative of the desired control logic to enable the functional requirement during run-time operation in the avionics system.

Abstract: A power distribution panel with a backplane, an insulating panel covering the backplane, and at least one electronic component mounted to the insulating panel. A set of feet can be mounted to the insulating panel and configured to absorb stress applied to the insulating panel where the set of feet are located in the same plane as the backplane.

Abstract: A method and apparatus for recording flight information of aircraft, such as position, mass, or type, in order to record the position of a wake turbulence of the aircraft. Weather information can be recorded as affecting the wake turbulence. Such information can be provided into a model or algorithm to determine a path of a wake turbulence. An aircraft on a flight path to encounter the wake turbulence can determine a vortex magnitude of the wake turbulence and determine if an advisory alert needs to be provided if the vortex magnitude satisfies a predetermined threshold.

Abstract: A power distribution assembly comprising a chassis having at least one wall, a deformable material layer positioned on the at least one wall of the chassis and configured to deform in response to a triggering even. The power distribution assembly further comprising a conductive sense layer positioned on the deformable material layer opposite the at least one wall of the chassis.

Abstract: A method and circuit for detecting a fault in a power transformer having an conductive shield layer sandwiched between electrical insulating layers separating the conductive shield layer from a first conductor and a second conductor, the second conductor opposite the conductive shield layer from the first conductor, and including, sensing a voltage energizing the shield layer, comparing the sensed voltage to a threshold voltage value corresponding to a fault, and upon satisfaction of the comparison, providing a fault indication when the comparison indicates the presence of a fault.

Abstract: A method of restoring navigational performance for a navigational system, the method comprising receiving by a first navigational system and a second navigational system a collection of data points to establish a real-time navigational route for the aircraft, comparing navigational performance values and/or drift ranges and establishing a new navigational route based on the collection of data points.

Abstract: A system and method preserves raw vibration data for a physical event involving a transport vehicle such as a helicopter, plane, boat, car, or truck. The event may involve unexpected mechanical stresses on the vehicle. The system and method preserves raw vibration data for parts of the transport vehicle, such as from multiple points along the drive train. The preserved raw vibration data includes data from time prior to the physical event. In an embodiment, the system and method continuously detects vibration data, and stores the most recent vibration data in a circular memory buffer. The buffer is continually updated with the most current vibration data. When an event is automatically detected or manually triggered, the most recently saved vibration data is transferred from the buffer to permanent storage, along with vibration data obtained subsequent to the event. This allows for a more thorough post-event analysis.

Abstract: Techniques for employing a smart sensor device (102) that has a primary sensing function for sensing a state of a physical component and can concurrently enable one or more backup functions for sensing one or more states of one or more other physicals components in response to one or more other smart sensor devices (102 and/or 116) not being able to perform their primary function of sensing and/or reporting on the one or more states of the one or more other physical components.

Abstract: A tool verification system and a method of verifying an unqualified component includes receiving communications between a tool and an unverified component, comparing the communications with a previously-qualified set of communications, and determining whether the unqualified component can be qualified based on the comparison.

Abstract: There is provided a method and system for monitoring an asset. For example, there is provided a method that includes executing, by a system configured to monitor the asset, a series of operations that can include fetching, from a database communicatively coupled to the system, a data structure including information relative to one or more sources containing event data relative to the asset. The method may include generating, from the data structure, a first table including a list of sources. The method may include generating, from the data structure, a second table including a list of unique consolidated events. The method may include generating, based on a set of predetermined rules, a mapping table configured to relate the first table and the second table. The method may include associating, based on the mapping table, an event in the second table to the one or more sources in the first table.

Abstract: A method for detecting the spoofing of a signal from a satellite in orbit. A receiver can be located on an aircraft to receive an apparent satellite signal. The method can include determining at least two characteristic signatures of the signal including a power level, and indicating the apparent satellite signal is a spoofed satellite signal.

Abstract: A method and apparatus for arranging fuses in a printed circuit board includes a power input configured to connect to a power source, at least one electrical component connected to the power input, a first output connected to the at least one electrical component and configured to connect to a load, and a fuse disposed between the at least one electrical component and the first output, and having a first trip rating.

Abstract: A method and apparatus for no-break power transfer in a power distribution system, including providing, from a first power source, a first power supply to a power bus, disabling the first power supply from the power bus, and providing, from a second power source, a second power supply to the power bus, the second power supply having the second set of electrical characteristics.

Abstract: A system and method preserves raw vibration data for a physical event involving a transport vehicle such as a helicopter, plane, boat, car, or truck. The event may involve unexpected mechanical stresses on the vehicle. The system and method preserves raw vibration data for parts of the transport vehicle, such as from multiple points along the drive train. The preserved raw vibration data includes data from time prior to the physical event. In an embodiment, the system and method continuously detects vibration data, and stores the most recent vibration data in a circular memory buffer. The buffer is continually updated with the most current vibration data. When an event is automatically detected or manually triggered, the most recently saved vibration data is transferred from the buffer to permanent storage, along with vibration data obtained subsequent to the event. This allows for a more thorough post-event analysis.

Abstract: A method and apparatus for detecting an electrical fault in a printed circuit board includes a first conductive layer interconnecting a set of electrical components, a second conductive layer connected to an electrical ground, a set of fuses arranged about the printed circuit board, and a fault detection circuit electrically connected to the printed circuit board.

Abstract: An aerial vehicle is provided. The aerial vehicle can include a plurality of sensors mounted thereon, an avionics system configured to operate at least a portion of the aerial vehicle, and a machine vision controller in operative communication with the avionics system and the plurality of sensors. The machine vision controller is configured to perform a method. The method includes obtaining sensor data from at least one sensor of the plurality of sensors, determining performance data from the avionic system or an additional sensor of the plurality of sensors, processing the sensor data based on the performance data to compensate for movement of the unmanned aerial vehicle, identifying at least one geographic indicator based on processing the sensor data, and determining a geographic location of the aerial vehicle based on the at least one geographic indicator.