H02J4/00

Multi-port split-phase power system

A multi-port split-phase power system that includes a control panel including a plurality of breakers, a multi-port converter including an AC port coupled to a second breaker, a DC port coupled to a DC energy source device, and galvanically isolated converters coupled to the AC port and DC port, where the AC port includes a first line, a second line, and a neutral and structured to supply, from the AC energy source device during islanded mode, at least one of 240V to the load device via the first line and the second line or 120V to the load device via the first line and the neutral, and an energy management system including a software for controlling the plurality of breakers, the energy management system structured to perform islanding, reconnection to the utility, and interlocking of the plurality of breakers during the islanding.

Energy service system of multi-machine production line and design method of shared drive system

Disclosed are an energy service system of a multi-machine production line and a control method thereof, the method includes reorganizing respective machines in the production line into three types of controllable entities: a drive system, an energy supply bus and an execution device, equipping them with a control center, and selecting a sub-drive system that is idle and is capable of completing the work stage with high energy efficiency to supply energy service for the corresponding execution device through the energy supply bus. Further disclosed is a design method of a multi-machine shared drive system of a production line, which increases the number of basic flow units of each drive unit to a maximum value one by one, and coordinates action time to form a variety of scheduling schemes, and selects a configuration scheme whose total time and total energy consumption are less as the shared drive system.

Energy service system of multi-machine production line and design method of shared drive system

Disclosed are an energy service system of a multi-machine production line and a control method thereof, the method includes reorganizing respective machines in the production line into three types of controllable entities: a drive system, an energy supply bus and an execution device, equipping them with a control center, and selecting a sub-drive system that is idle and is capable of completing the work stage with high energy efficiency to supply energy service for the corresponding execution device through the energy supply bus. Further disclosed is a design method of a multi-machine shared drive system of a production line, which increases the number of basic flow units of each drive unit to a maximum value one by one, and coordinates action time to form a variety of scheduling schemes, and selects a configuration scheme whose total time and total energy consumption are less as the shared drive system.

A POWER-DISTRIBUTION SYSTEM FOR AN AIRCRAFT ON THE GROUND

A power distribution system is provided for an aircraft on the ground, comprising a first electrical load, operably coupled to the aircraft on the ground and configured to receive at least a first portion of a predetermined maximum input power provided by a power supply; at least one second electrical load, electrically coupleable to the aircraft on the ground and configured to receive at least a second portion of said predetermined maximum input power provided by said power supply, and a controller, adapted to monitor at least one parameter of the power consumed by any one of said first electrical load and said at least one second electrical load, and control the power consumption of at least said first electrical load so that the total power consumption of said first electrical load and said at least one second electrical load does not exceed said predetermined maximum input power; wherein said predetermined maximum input power is provided via a single power line between said power supply and an input port of said first electrical load.

A POWER-DISTRIBUTION SYSTEM FOR AN AIRCRAFT ON THE GROUND

A power distribution system is provided for an aircraft on the ground, comprising a first electrical load, operably coupled to the aircraft on the ground and configured to receive at least a first portion of a predetermined maximum input power provided by a power supply; at least one second electrical load, electrically coupleable to the aircraft on the ground and configured to receive at least a second portion of said predetermined maximum input power provided by said power supply, and a controller, adapted to monitor at least one parameter of the power consumed by any one of said first electrical load and said at least one second electrical load, and control the power consumption of at least said first electrical load so that the total power consumption of said first electrical load and said at least one second electrical load does not exceed said predetermined maximum input power; wherein said predetermined maximum input power is provided via a single power line between said power supply and an input port of said first electrical load.

Redundant actuation power and control

A redundant power supply system for aircraft seats, includes: a first power supply module having a first AC to DC power converter configured to supply power to a first auxiliary board, the first auxiliary board being configured to supply power to a plurality of aircraft seats via a plurality of communication bus channels; a second power supply module having a second AC to DC power converter configured to supply power to a second auxiliary board, the second auxiliary board being configured to supply power to the plurality of aircraft seats via the plurality of communication bus channels; and a power supply link configured to connect the first auxiliary board and the second auxiliary board enabling the first AC to DC power converter to power the second auxiliary board via the power supply link.

Redundant actuation power and control

A redundant power supply system for aircraft seats, includes: a first power supply module having a first AC to DC power converter configured to supply power to a first auxiliary board, the first auxiliary board being configured to supply power to a plurality of aircraft seats via a plurality of communication bus channels; a second power supply module having a second AC to DC power converter configured to supply power to a second auxiliary board, the second auxiliary board being configured to supply power to the plurality of aircraft seats via the plurality of communication bus channels; and a power supply link configured to connect the first auxiliary board and the second auxiliary board enabling the first AC to DC power converter to power the second auxiliary board via the power supply link.

HYBRID ENERGY SYSTEMS

A hybrid energy system is configured to carry a power load for a generator configured to output a first AC signal. The hybrid energy system includes a battery bank, a DC/DC converter, an AC/DC converter, and a DC/AC converter. The battery bank includes a plurality of batteries and outputs a first DC signal. The DC/DC converter, operating in a first mode, receives and converts the first DC signal into a second DC signal, which is output to a DC bus. The AC/DC converter receives and converts the first AC signal into a third DC signal. The second DC signal and the third DC signal are tied together on the DC bus. The DC/AC converter receives and converts the second DC signal from the DC bus into a plurality of second AC signals, which are output to an AC outlet interface.

HYBRID ENERGY SYSTEMS

A hybrid energy system is configured to carry a power load for a generator configured to output a first AC signal. The hybrid energy system includes a battery bank, a DC/DC converter, an AC/DC converter, and a DC/AC converter. The battery bank includes a plurality of batteries and outputs a first DC signal. The DC/DC converter, operating in a first mode, receives and converts the first DC signal into a second DC signal, which is output to a DC bus. The AC/DC converter receives and converts the first AC signal into a third DC signal. The second DC signal and the third DC signal are tied together on the DC bus. The DC/AC converter receives and converts the second DC signal from the DC bus into a plurality of second AC signals, which are output to an AC outlet interface.

Persistent Dc circuit breaker
11831167 · 2023-11-28 · ·

A persistent DC circuit breaker provides a persistent single or dual DC voltage for a power distribution circuit coupled to a power panel. A control mechanism ensures a constant and consistent DC power output from the persistent DC circuit breaker. The persistent DC circuit breaker can replace an AC circuit breaker to convert an AC power panel into a co-existing AC and DC power panel or an entire DC power panel.