Abstract: An apparatus for machining a web made of electrode material includes a track extending continuously between a web path and an offload path, and supports operatively coupled to the track and moveable continuously along the web path and the offload path. The track is operable to control a conveying speed of each support along the web path. Each support includes a work surface that engages with the web at a first end of the web path to convey the web in the down-web direction at the conveying speed along the web path between the first end and a second end of the web path. The web is disengaged from the work surface at the second end of the web path. The apparatus also includes a machining device operable to act on the web as the web is conveyed in the down-web direction at the conveying speed along the web path.

Abstract: A system and method for detecting ground resonance and providing a warning regarding the same includes supplying, from an inertial navigation system (INS), inertial data indicative of an inertial profile of a rotorcraft, and supplying, from a sensor system, sensor data that indicates when the rotorcraft is at least partially on a landing surface. The sensor data is processed, in a processing system, to determine when the rotorcraft is at least partially on the landing surface, and when the rotorcraft is determined to be at least partially on the landing surface, the inertial data is processed, in the processing system to determine when the inertial profile of the rotorcraft indicates ground resonance may occur. Upon determining that ground resonance may occur, one or more alert signals are generated in the processing system.

Abstract: A system and method for detecting ground resonance and providing a warning regarding the same includes supplying, from an inertial navigation system (INS), inertial data indicative of an inertial profile of a rotorcraft, and supplying, from a sensor system, sensor data that indicates when the rotorcraft is at least partially on a landing surface. The sensor data is processed, in a processing system, to determine when the rotorcraft is at least partially on the landing surface, and when the rotorcraft is determined to be at least partially on the landing surface, the inertial data is processed, in the processing system to determine when the inertial profile of the rotorcraft indicates ground resonance may occur. Upon determining that ground resonance may occur, one or more alert signals are generated in the processing system.

Abstract: An adaptive aircraft electrical power distribution system includes an aircraft power source, a power connector, an aircraft power distribution bus, and a bidirectional power controller. The aircraft power source is operable to generate and supply electrical power. The power connector is mounted on a fuselage of the aircraft. The aircraft power distribution bus is operable to distribute electrical power to an aircraft electrical load. The bidirectional power controller is mounted in the aircraft and is electrically coupled to the aircraft power source, the aircraft power connector, and the aircraft power distribution bus. The bidirectional power controller is configured to: sense when the aircraft power source is generating and supplying electrical power, sense when electrical power is being supplied to the power connector from an external power source, and selectively couple at least one of the aircraft power source or the power connector to the aircraft power distribution system.

Abstract: An adaptive aircraft electrical power distribution system includes an aircraft power source, a power connector, an aircraft power distribution bus, and a bidirectional power controller. The aircraft power source is operable to generate and supply electrical power. The power connector is mounted on a fuselage of the aircraft. The aircraft power distribution bus is operable to distribute electrical power to an aircraft electrical load. The bidirectional power controller is mounted in the aircraft and is electrically coupled to the aircraft power source, the aircraft power connector, and the aircraft power distribution bus. The bidirectional power controller is configured to: sense when the aircraft power source is generating and supplying electrical power, sense when electrical power is being supplied to the power connector from an external power source, and selectively couple at least one of the aircraft power source or the power connector to the aircraft power distribution system.

Abstract: A system comprises a GNSS unit onboard an aircraft, with the GNSS unit operative to generate horizontal and vertical deviation signals. An onboard converter unit is in communication with the GNSS unit, and an onboard radio navigation computer is in communication with the converter unit. The converter unit performs a method for converting the deviation signals to equivalent VHF instrument landing system signals.

Abstract: Systems and methods of providing information via a computer network are provided. A request for content to display with a resource can be received via a computer network at a data processing system. The request can include user information and resource information. The data processing system can retrieve a timestamp of a last request for content from a user associated with the user information. The data processing system can determine if a difference between current time and the timestamp reaches a threshold, and can retrieve a plurality of content items based at least in part on whether the threshold is reached and at least one attribute of the content items. The data processing system can select at least one content item and provide it for display with the resource. The data processing system can store the current time as the timestamp of the last request for content from the user.