Abstract: Systems and methods according to one or more embodiments are provided for capturing images of an area of interest proximate to an aircraft, and securely transmitting the images as data files over an encrypted communication network associated with the aircraft. In one example, a system includes an image capture device configured to be secured to an aircraft to capture a plurality of images of a field of view of an area of interest proximate to the aircraft. The system also includes a processor configured to receive the plurality of captured images and convert the captured images to a plurality of data files. The system further includes a memory configured to store the data files, and a communication interface configured to connect to an encrypted communication network associated with the aircraft, wherein the communication interface is configured to securely transmit the data files over the encrypted communication network.

Abstract: A linear optimized isolation transformer may include a magnetic core having a primary side and a secondary side; a primary side winding on the primary side; a primary side terminal electrically coupled to the primary side winding; a secondary side winding on a the secondary side; a secondary side terminal electrically coupled to the secondary side winding; an isolation dielectric placed between the primary side winding and the secondary side winding and having a shape that fills all of the space between the primary side and the secondary side that is not occupied by the core, the isolation dielectric including a permanent high-Q material selected to maintain a high value isolation independent of pressure differences resulting from operation at different altitudes; and wherein the primary side terminal and the secondary side terminal are positioned on opposing ends of a long axis of the magnetic core.

Abstract: A power system for an aircraft is disclosed. The power system comprises a power panel, at least one power rail coupled to the power panel, wherein the power rail is integrated with a mounting rail for the passenger service unit, and at least one universal serial bus (USB) port coupled to the power panel and mounted in the passenger service unit.

Abstract: A vehicle that includes an onboard connector including a conductive portion and an optical communication portion. The vehicle further includes an optical interface coupled in communication with the onboard connector and onboard systems of the vehicle. The optical interface is configured to at least one of receive or transmit optical signals via the optical communication portion. When a ground-system connector is connected to the onboard connector, data included in the optical signals is communicated between the ground system connector and the onboard systems of the vehicle.

Abstract: Systems, methods, and apparatus for testing a passenger service unit (PSU) of a cabin of a vehicle are disclosed. In one or more embodiments, the disclosed method involves installing a test interface panel (TIP) in the cabin of the vehicle such that the TIP is connected to a power source and is able to communicate with the PSU. The method further involves connecting a user interface to the TIP. Also, the method involves sending at least one command, from the user interface, to the PSU via the TIP. Further, the method involves sending, at least one response, from the PSU.

Abstract: Methods and systems for communicating data between a vehicle and a ground system are described. The system includes an integrated power and communications connector that couples to the vehicle so that power is supplied to at least selected systems on-board the vehicle. In addition, data is communicated between the vehicle on-board systems and the ground system via the integrated connector.

Abstract: An aircraft systems interface unit includes a multiplexer and a broadband over power line (BPL) modem. The multiplexer includes a plurality of inputs and an output for outputting data received through the plurality of inputs. Each input is configured for connection to at least one aircraft data bus. The BPL modem is coupled to the output of the multiplexer and configured to transmit data received from the multiplexer over a power line.

Abstract: Systems, methods, and apparatus for testing a passenger service unit (PSU) of a cabin of a vehicle are disclosed. In one or more embodiments, the disclosed method involves installing a test interface panel (TIP) in the cabin of the vehicle such that the TIP is connected to a power source and is able to communicate with the PSU. The method further involves connecting a user interface to the TIP. Also, the method involves sending at least one command, from the user interface, to the PSU via the TIP. Further, the method involves sending, at least one response, from the PSU.

Abstract: A cabin service system may include a control module unit, a pair of power rails, the power rails being configured to provide mechanical attachment and electrical power to the control module unit, and a plurality of cabin services, wherein the control module is communicatively coupled to the plurality of cabin services to provide control of the plurality of cabin services. The control module unit may include a plurality of communication ports, and a plurality of relays coupled to at least one communication port of the plurality of communication ports, wherein each communication port of the plurality of communication ports corresponds to at least one cabin service of the plurality of cabin services, and wherein each relay of the plurality of relays provides discrete control of an associated cabin service of the plurality of cabin services.

Abstract: Methods and systems for communicating data between a vehicle and a ground system are described. The system includes an integrated power and communications connector that couples to the vehicle so that power is supplied to at least selected systems on-board the vehicle. In addition, data is communicated between the vehicle on-board systems and the ground system via the integrated connector.

Abstract: Methods and systems for communicating data between a vehicle and a ground-based unit are provided. The method includes communicatively coupling the vehicle to the ground-based unit, initiating a Broadband over Power Line (BPL) link between the vehicle and the ground-based unit when power is supplied to the vehicle, and updating data stored in the vehicle with data received from the ground-based unit.

Abstract: An aircraft systems interface unit includes a multiplexer and a broadband over power line (BPL) modem. The multiplexer includes a plurality of inputs and an output for outputting data received through the plurality of inputs. Each input is configured for connection to at least one aircraft data bus. The BPL modem is coupled to the output of the multiplexer and configured to transmit data received from the multiplexer over a power line.

Abstract: Methods and systems for communicating data between an aircraft and a ground-based unit are provided. The method includes integrating a Broadband over Power Line (BPL) module and inductive coupler into the ground-based unit, communicatively coupling the aircraft to the ground-based unit, initiating a Broadband over Power Line (BPL) link between the aircraft and the ground-based unit when power is supplied to the aircraft, and updating data stored in the aircraft with data received from the ground-based unit.

Abstract: A linear optimized isolation transformer may include a magnetic core having a primary side and a secondary side; a primary side winding on the primary side; a primary side terminal electrically coupled to the primary side winding; a secondary side winding on a the secondary side; a secondary side terminal electrically coupled to the secondary side winding; an isolation dielectric placed between the primary side winding and the secondary side winding and having a shape that fills all of the space between the primary side and the secondary side that is not occupied by the core, the isolation dielectric including a permanent high-Q material selected to maintain a high value isolation independent of pressure differences resulting from operation at different altitudes; and wherein the primary side terminal and the secondary side terminal are positioned on opposing ends of a long axis of the magnetic core.

Abstract: Methods, systems, and a Broadband over Power Line (BPL) module cover assembly for enabling communication between an aircraft and a ground-based network are provided. The BPL module cover assembly includes a connection interface configured to be coupled to and receive power from a stringer connector and a BPL network interface coupled to and configured to receive power from said connection interface. The BPL module cover assembly also includes a fuse interface including a plurality of fuses coupled between the connection interface and the BPL network interface. The fuse interface is configured to prevent power provided by the connection interface from damaging the BPL network interface in the event of an electrical fault.

Abstract: Presented is a system and method for providing electrical isolation in vehicle power systems. The method comprises placing linear optimized isolation transformers in structures of a vehicle at positions that minimize the propagation of energy spikes into internal electronic systems, for example in the wing root of an aircraft where electrical cables from a generator associated with an engine enter the fuselage. The system includes a linear optimized isolation transformer with a core that has primary side winding isolated from a secondary side winding by an isolation dielectric. The isolation dielectric maintains a high value isolation independent of pressure differences due to operation at different altitudes.

Abstract: Methods and systems for communicating data between a vehicle and a ground-based unit are provided. The method includes communicatively coupling the vehicle to the ground-based unit, initiating a Broadband over Power Line (BPL) link between the vehicle and the ground-based unit when power is supplied to the vehicle, and updating data stored in the vehicle with data received from the ground-based unit.

Abstract: A system and method for transmitting wireless energy between two or more components housed within a faraday-like cage structure. In one preferred form a cooling plenum of an equipment rack supporting a plurality of independent components is used for transmitting wireless signals between the components. In another form a wireless backplane is formed in an equipment rack that houses a plurality of LRUs. In another example a card file housing a plurality of components forms a faraday-like cage for enabling transmission of wireless signals, either electromagnetic wave or optical signals, between various circuit boards held within the card file. The various preferred embodiments eliminate the need for expensive, bulky and heavy electrical or optical cabling to be used to intercouple the components supported within the support structure for communication.

Abstract: A wireless camera surveillance system for an aircraft is disclosed. The overhead video system comprises a wireless camera surveillance unit; and at least one mounting rail detachably coupled to the wireless camera surveillance unit. The mounting rail provides structural support and electrical power to the wireless camera surveillance unit. A system in one embodiment may use mounting rails that double as power rails supplying power to the wireless camera surveillance unit. Control is accomplished over a wireless link. The power rail control may be accomplished remotely via a standard or solid state relay. Normal rail power for the rail mounted wireless surveillance camera system may come from the utility bus.

Abstract: A power system for an aircraft is disclosed. The power system comprises a power module unit and at least one mounting rail detachably coupled to the power module unit. The mounting rail provides structural support and electrical power to the power module unit. A power system in one embodiment may use mounting rails that double as power rails supplying power to the power module unit. Control is accomplished over a wireless link. The power rail control may be accomplished remotely via a standard or solid state relay. Normal rail power for the rail mounted power module unit may come from the utility bus.