Abstract: Stage outputs of a respective cascade half stage of the high voltage cascade are connected to stage inputs of the respective next cascade half stage of the high voltage cascade. Diode circuits are arranged on first additional circuit boards, which are connected electrically and mechanically to a main board of the high voltage cascade. The first additional circuit boards are oriented orthogonally to the main board and follow on sequentially from one another corresponding to the electrical sequence of the cascade half stages. Capacitor circuits of the cascade half stages are arranged to the side next to the first additional circuit boards on the main board, are arranged corresponding to the electrical sequence of the cascade half stages, and alternate on sides of the first additional circuit boards.

Abstract: One or more example embodiments relates to an X-ray generator comprising a high-voltage transformer, the high-voltage transformer including a core; a primary winding module including the primary windings enclosing a core in a primary section in a shape of a coil; and a secondary winding module including secondary windings and a plastic section made from a plastic, the secondary windings enclosing the core in a secondary section in the shape of the coil, the plastic section at least one of enclosing or comprising the secondary windings, the plastic forming an electrical insulator, wherein the primary section and the secondary section have a common overlap area, and the high-voltage transformer is configured to at least one of generate a voltage of at least 70 kV with respect to ground or act as a unipolar high-voltage transformer to output a voltage of at least 70 kV.

Abstract: A method for operating a display unit such as an avionics display interface is provided. The method comprises displaying a plurality of logical categories of options available, with each of the logical categories including a plurality of items of information, selecting a first item of information in a first logical category when a first input key is pressed, and selecting a next item of information in the first logical category when the first input key is pressed again. The method further includes selecting a first item of information in a second logical category when a second input key is pressed, and selecting a next item of information in the second logical category when the second input key is pressed again.

Abstract: An avionics messaging system comprises a memory configured to store a plurality of pre-defined avionics message elements; a display unit configured to display data; a user input device configured to receive input from a user; and a processing unit configured to output a user-customizable list of pre-defined avionics message elements to the display unit, the user-customizable list comprising at least a subset of the plurality of pre-defined avionics message elements; wherein the processing unit is further configured to update the user-customizable list based on input received from the user input device; wherein the processing unit is further configured to provide a message composition screen to the display unit based on user input received from the user input device; and wherein the message composition screen corresponds to a pre-defined avionics message element selected from the user-customizable list of pre-defined avionics message elements.

Abstract: Systems and methods for detecting a loss of communications between an aircraft and a ground station are provided. In one embodiment, a system for detecting a loss of communication for an aircraft comprises: a communication detection software module resident as an application on an aircraft communication management unit (CMU); a CMU message router in communication with the communication detection software module; at least one radio coupled to the communication management unit; a statistical model of communications traffic density for an RF zone associated with a ground station; wherein the communication detection software module performs a statistical analysis of a current communications traffic density of radio communications observed by the at least one radio to determine when the aircraft has a lost a communications link with the ground station.

Abstract: Systems and methods for detecting a loss of communications between an aircraft and a ground station are provided. In one embodiment, a system for detecting a loss of communication for an aircraft comprises: a communication detection software module resident as an application on an aircraft communication management unit (CMU); a CMU message router in communication with the communication detection software module; at least one radio coupled to the communication management unit; a statistical model of communications traffic density for an RF zone associated with a ground station; wherein the communication detection software module performs a statistical analysis of a current communications traffic density of radio communications observed by the at least one radio to determine when the aircraft has a lost a communications link with the ground station.

Abstract: Systems and methods for providing an active prompt for a timed response are provided. In one embodiment, a system comprises a human machine interface that presents controller pilot data link communication (CPDLC) information to a user, and a CPDLC computer configured to process received CPDLC messages. In certain embodiments, the CPDLC computer comprises a memory device that stores received CPDLC messages, and a processing unit that starts a timer when a CPDLC message is received, wherein the timer counts a response period for responding to the CPDLC message. Further the processing unit instructs the human machine interface to display a time remaining in the response period when the timer reaches a message expiration warning period.

Abstract: Systems and methods for providing an active prompt for a timed response are provided. In one embodiment, a system comprises a human machine interface that presents controller pilot data link communication (CPDLC) information to a user, and a CPDLC computer configured to process received CPDLC messages. In certain embodiments, the CPDLC computer comprises a memory device that stores received CPDLC messages, and a processing unit that starts a timer when a CPDLC message is received, wherein the timer counts a response period for responding to the CPDLC message. Further the processing unit instructs the human machine interface to display a time remaining in the response period when the timer reaches a message expiration warning period.

Abstract: A computing-platform emulator for use on a vehicle is provided. The computing-platform emulator includes a display, a processor communicatively coupled to the display, a data-entry interface communicatively coupled to the processor, and at least one electronic interface to interface a host system in the vehicle to the processor. The host system implements at least one application and at least one protocol for use on the computing-platform emulator. The display, the data-entry interface, and the at least one electronic interface function as a multifunction control display unit.

Abstract: Systems and methods for detecting a loss of communications between an aircraft and a ground station are provided. In one embodiment, a system for detecting a loss of communication for an aircraft comprises: a communication detection software module resident as an application on an aircraft communication management unit (CMU); a CMU message router in communication with the communication detection software module; at least one radio coupled to the communication management unit; a statistical model of communications traffic density for an RF zone associated with a ground station; wherein the communication detection software module performs a statistical analysis of a current communications traffic density of radio communications observed by the at least one radio to determine when the aircraft has a lost a communications link with the ground station.

Abstract: An avionics messaging system comprises a memory configured to store a plurality of pre-defined avionics message elements; a display unit configured to display data; a user input device configured to receive input from a user; and a processing unit configured to output a user-customizable list of pre-defined avionics message elements to the display unit, the user-customizable list comprising at least a subset of the plurality of pre-defined avionics message elements; wherein the processing unit is further configured to update the user-customizable list based on input received from the user input device; wherein the processing unit is further configured to provide a message composition screen to the display unit based on user input received from the user input device; and wherein the message composition screen corresponds to a pre-defined avionics message element selected from the user-customizable list of pre-defined avionics message elements.

Abstract: A method for operating a display unit such as an avionics display interface is provided. The method comprises displaying a plurality of logical categories of options available, with each of the logical categories including a plurality of items of information, selecting a first item of information in a first logical category when a first input key is pressed, and selecting a next item of information in the first logical category when the first input key is pressed again. The method further includes selecting a first item of information in a second logical category when a second input key is pressed, and selecting a next item of information in the second logical category when the second input key is pressed again.