Abstract: A method includes determining that at least one diesel emissions fluid (DEF) doser of an exhaust aftertreatment system is likely frozen based on at least one of an ambient air temperature or a DEF source temperature; operating an engine in a cylinder cutout mode in response to the determination that the at least one DEF doser is likely frozen; and, discontinuing the cylinder cutout mode in response to determining that the at least one DEF doser is in a predefined condition.

Abstract: A method includes determining that at least one diesel emissions fluid (DEF) doser of an exhaust aftertreatment system is likely frozen based on at least one of an ambient air temperature or a DEF source temperature; operating an engine in a cylinder cutout mode in response to the determination that the at least one DEF doser is likely frozen; and, discontinuing the cylinder cutout mode in response to determining that the at least one DEF doser is in a predefined condition.

Abstract: A system includes an exhaust aftertreatment system in exhaust gas receiving communication with an engine including a plurality of cylinders where the engine is structured to operate according to low load conditions and where a controller is structured to determine that at least one diesel emissions fluid (DEF) doser is frozen based on at least one of an ambient air temperature and a DEF source temperature. The controller is structured to operate the engine according to a skip-fire mode in response to a DEF flag indicating that the at least one DEF doser is frozen. The skip-fire mode comprises firing a portion of the plurality of cylinders that is less than a total amount of cylinders of the plurality of cylinders. The controller is structured to discontinue the skip-fire mode in response to determining that the at least one DEF doser is likely thawed.

Abstract: A system includes an exhaust aftertreatment system in exhaust gas receiving communication with an engine including a plurality of cylinders where the engine is structured to operate according to low load conditions and where a controller is structured to determine that at least one diesel emissions fluid (DEF) doser is frozen based on at least one of an ambient air temperature and a DEF source temperature. The controller is structured to operate the engine according to a skip-fire mode in response to a DEF flag indicating that the at least one DEF doser is frozen. The skip-fire mode comprises firing a portion of the plurality of cylinders that is less than a total amount of cylinders of the plurality of cylinders. The controller is structured to discontinue the skip-fire mode in response to determining that the at least one DEF doser is likely thawed.

Abstract: A personal propulsion device adapted to achieve flight by discharging a fluid, including a passenger assembly adapted to support an individual person; at least one fluid discharge nozzle coupled to the passenger assembly, where the nozzle is movable with respect to the passenger assembly to define a range of motion, and where the nozzle is biased towards at least one position in the range of motion.

Abstract: A personal propulsion device adapted to achieve flight by discharging a fluid, including a passenger assembly adapted to support an individual person; at least one fluid discharge nozzle coupled to the passenger assembly, where the nozzle is movable with respect to the passenger assembly to define a range of motion, and where the nozzle is biased towards at least one position in the range of motion.

Abstract: A personal propulsion device adapted to achieve flight by discharging a fluid, including a passenger assembly adapted to support an individual person; at least one fluid discharge nozzle coupled to the passenger assembly, where the nozzle is movable with respect to the passenger assembly to define a range of motion, and where the nozzle is biased towards at least one position in the range of motion.

Abstract: A personal propulsion device adapted to achieve flight by discharging a fluid, including a passenger assembly adapted to support an individual person; at least one fluid discharge nozzle coupled to the passenger assembly, where the nozzle is movable with respect to the passenger assembly to define a range of motion, and where the nozzle is biased towards at least one position in the range of motion.

Abstract: A personal propulsion device adapted to achieve flight by discharging a fluid, including a passenger assembly adapted to support an individual person; at least one fluid discharge nozzle coupled to the passenger assembly, where the nozzle is movable with respect to the passenger assembly to define a range of motion, and where the nozzle is biased towards at least one position in the range of motion.