Abstract: A system and a method are provided for safely and efficiently transferring cargo and freight packed in ULD containers directly between an airport freight terminal and freight aircraft. An enclosed freightway is designed to provide a direct connection between the freight terminal and aircraft cargo doors. The enclosed freightway is structured and sized to move ULD containers automatically or manually between freight aircraft and freight terminals. Different freightway configurations enable direct connection between the freight terminal and freight aircraft main cargo door when freight aircraft are driven by electric taxi drive systems or aircraft engines and parked in nose-in orientations and when freight aircraft are driven by electric taxi drive systems and parked in parallel orientations at the freight terminal. An alternative embodiment provides direct connections between freight aircraft cargo doors and interior loading docks for aircraft driven with electric taxi drive systems.

Abstract: A monitoring system and method are provided for real time monitoring of flaps, landing gears, or tail skids to determine safe taxi, takeoff, and flight readiness. Monitoring units, including scanning LiDAR devices combined with cameras or sensors, mounted in aircraft exterior locations produce a stream of meshed data that is securely transmitted to a processing system to generate a real time visual display of the flaps, landing gears, or tail skid for communication to aircraft pilots to ensure safe aircraft taxi, takeoff, and flight readiness. Actual flap position alignment with optimal flap setting, proper retraction and extension positions of landing gears, and tail skid condition is ensured. Safety of aircraft taxi, takeoff and flight and airport operations are improved when the present system and method are used to prevent incidents related to misaligned flaps and improperly positioned landing gears or tail skids.

Abstract: Systems and methods for operating a hybrid vehicle are presented. In one example, electric current may be supplied to or withheld from a positive temperature coefficient (PTC) heater and an electrically heated catalyst. In particular, electric current may be delivered to the PTC heater and withheld from the electrically heated catalyst, or vice-versa, in response to a catalyst temperature and battery state of charge.

Abstract: A system and a method are provided for safely and efficiently transferring cargo and freight packed in ULD containers directly between an airport freight terminal and freight aircraft. An enclosed freightway is designed to provide a direct connection between the freight terminal and aircraft cargo doors. The enclosed freightway is structured and sized to move ULD containers automatically or manually between freight aircraft and freight terminals. Different freightway configurations enable direct connection between the freight terminal and freight aircraft main cargo door when freight aircraft are driven by electric taxi drive systems or aircraft engines and parked in nose-in orientations and when freight aircraft are driven by electric taxi drive systems and parked in parallel orientations at the freight terminal. An alternative embodiment provides direct connections between freight aircraft cargo doors and interior loading docks for aircraft driven with electric taxi drive systems.

Abstract: A monitoring system and method are provided for real time monitoring of flaps, landing gears, or tail skids to determine safe taxi, takeoff, and flight readiness. Monitoring units, including scanning LiDAR devices combined with cameras or sensors, mounted in aircraft exterior locations produce a stream of meshed data that is securely transmitted to a processing system to generate a real time visual display of the flaps, landing gears, or tail skid for communication to aircraft pilots to ensure safe aircraft taxi, takeoff, and flight readiness. Actual flap position alignment with optimal flap setting, proper retraction and extension positions of landing gears, and tail skid condition is ensured. Safety of aircraft taxi, takeoff and flight and airport operations are improved when the present system and method are used to prevent incidents related to misaligned flaps and improperly positioned landing gears or tail skids.

Abstract: Systems and methods provide voltage stability for a low voltage bus coupling a DC/DC converter with a low voltage load comprising one or more vehicle accessories. The DC/DC converter can be coupled to a high voltage battery, the low voltage load, and a starter circuit configured for starting an engine. Prior to engaging a starter motor to start the engine, the DC/DC converter can be isolated from the starter circuit so as to be shielded from any large current demand during an engine start event. While starting the engine, the starter motor can draw current from a secondary battery, while the DC/DC converter provides a sufficient and stable voltage to the vehicle low voltage accessories. After completion of the engine start event, the DC/DC converter can be recoupled to the starter circuit, allowing the high voltage battery to charge the secondary battery.

Abstract: Systems and methods provide voltage stability for a low voltage bus coupling a DC/DC converter with a low voltage load comprising one or more vehicle accessories. The DC/DC converter can be coupled to a high voltage battery, the low voltage load, and a starter circuit configured for starting an engine. Prior to engaging a starter motor to start the engine, the DC/DC converter can be isolated from the starter circuit so as to be shielded from any large current demand during an engine start event. While starting the engine, the starter motor can draw current from a secondary battery, while the DC/DC converter provides a sufficient and stable voltage to the vehicle low voltage accessories. After completion of the engine start event, the DC/DC converter can be recoupled to the starter circuit, allowing the high voltage battery to charge the secondary battery.