A transport refrigeration system includes a trailer having an axle; a transport refrigeration unit mounted to the trailer, transport refrigeration unit configured to cool a cargo compartment of the trailer; an axle driven generator connected to the axle, the axle driven generator configured to provide power to the transport refrigeration unit; a controller in communication with the axle driven generator, the controller configured to disengage the axle driven generator from the axle in response to the presence of one or more disengagement conditions.

A transport refrigeration system includes a trailer having an axle; a transport refrigeration unit mounted to the trailer, transport refrigeration unit configured to cool a cargo compartment of the trailer; an axle driven generator connected to the axle, the axle driven generator configured to provide power to the transport refrigeration unit; a controller in communication with the axle driven generator, the controller configured to disengage the axle driven generator from the axle in response to the presence of one or more disengagement conditions.

A load adaptive linear electrical generator system is provided for generating DC electrical power. The electrical generation system includes one or more power generation modules which will be selectively turned on or off and additively contribute power depending on the DC power demand. Each power generating module includes a pair of linear electrical generators connected to respective ones of a pair of internal combustion piston based power assemblies. The piston in the internal combustion assembly is connected to a magnet in the linear electrical generator. The piston/magnet assembly oscillates in a simple harmonic motion at a frequency dependent on a power load of the electrical generator. A stroke limiter constrains the piston/magnet assembly motion to preset limits.

A load adaptive linear electrical generator system is provided for generating DC electrical power. The electrical generation system includes one or more power generation modules which will be selectively turned on or off and additively contribute power depending on the DC power demand. Each power generating module includes a pair of linear electrical generators connected to respective ones of a pair of internal combustion piston based power assemblies. The piston in the internal combustion assembly is connected to a magnet in the linear electrical generator. The piston/magnet assembly oscillates in a simple harmonic motion at a frequency dependent on a power load of the electrical generator. A stroke limiter constrains the piston/magnet assembly motion to preset limits.

The wind power generation device includes a blade, a power distribution unit, a first generator, a second generator, a clutch unit, and a control unit. The control unit controls connection and disconnection of the clutch unit such that the clutch unit is disconnected when the wind speed input to the blade is smaller than a predetermined first wind speed value and the clutch unit is connected when the wind speed input to the blade is larger than a predetermined second wind speed value.

The wind power generation device includes a blade, a power distribution unit, a first generator, a second generator, a clutch unit, and a control unit. The control unit controls connection and disconnection of the clutch unit such that the clutch unit is disconnected when the wind speed input to the blade is smaller than a predetermined first wind speed value and the clutch unit is connected when the wind speed input to the blade is larger than a predetermined second wind speed value.

A power generation controller of an aircraft includes a low-temperature start-up control section and a power generation control section. When it is determined that an oil temperature of a hydraulic actuator configured to change an operation position of a speed change element of a hydraulic transmission satisfies a predetermined low-temperature condition when starting up an aircraft engine, the low-temperature start-up control section sets a power generator to a power non-generating state and controls the hydraulic actuator such that the speed change element is positioned at an acceleration side of a median in a speed change range. When it is determined that the oil temperature satisfies a predetermined low-temperature start-up completion condition, the power generation control section sets the power generator to a power generating state and controls the hydraulic actuator in accordance with a rotational frequency of the aircraft engine.

A power generation controller of an aircraft includes a low-temperature start-up control section and a power generation control section. When it is determined that an oil temperature of a hydraulic actuator configured to change an operation position of a speed change element of a hydraulic transmission satisfies a predetermined low-temperature condition when starting up an aircraft engine, the low-temperature start-up control section sets a power generator to a power non-generating state and controls the hydraulic actuator such that the speed change element is positioned at an acceleration side of a median in a speed change range. When it is determined that the oil temperature satisfies a predetermined low-temperature start-up completion condition, the power generation control section sets the power generator to a power generating state and controls the hydraulic actuator in accordance with a rotational frequency of the aircraft engine.

A method of operating an electric or hybrid system comprising a synchronous reluctance electric motor coupled to an electric or hybrid powertrain is described herein. The method comprises determining (i) a torque demand required of the electric motor and (ii) a speed of rotation of the rotor of the electric motor, and storing kinetic energy in a rotor of the electric motor from the powertrain in response to at least one of (i) the determined torque demand falling below a selected torque demand threshold and (ii) the speed of the rotor being below a selected rotor speed threshold. The method further comprises operating the electric motor by powering the electric motor with electricity to deliver energy to the powertrain in response to at least one of: (i) the determined torque demand rising above a selected torque demand threshold and (ii) the speed of the rotor falling below a selected rotor speed threshold.

A system and method are provided for controlling a wind. Accordingly, a current condition of a generator of the wind turbine is determined, and an approach of the current condition to a current-dependent limit is detected. The speed of the generator is affected so as to alter a rotor/stator balance of the generator such that the current-dependent limit is not exceeded and the wind turbine can operate at a rated power.