Safety power disconnection for remote power distribution in power distribution systems is disclosed. The power distribution system includes one or more power distribution circuits each configured to remotely distribute power from a power source over current carrying power conductors to remote units to provide power for remote unit operations. A remote unit is configured to decouple power from the power conductors thereby disconnecting the load of the remote unit from the power distribution system. A current measurement circuit in the power distribution system measures current flowing on the power conductors and provides a current measurement to the controller circuit. The controller circuit is configured to disconnect the power source from the power conductors for safety reasons in response to detecting a current from the power source in excess of a threshold current level indicating a load.

A battery management system (BMS) recognition system, comprising: a master BMS including a master light emitter, the master BMS being configured to flicker the master light emitter to transmit an operation mode shifting signal to a slave BMS when it is intended to shift an operation mode of the slave BMS; and a slave BMS including a slave light receiver configured to correspond to the master light emitter, the slave BMS being configured to: recognize the flickering of the master light emitter through the slave light receiver; and shift the operation mode thereof in response to the operation mode shifting signal.

A device may include a power supply module (PSM). The PSM may receive information regarding one or more programmable restrictions associated with a power supply. The PSM may receive a measurement of voltage associated with the power supply. The PSM may determine a current associated with the power supply based on the one or more programmable restrictions, the measurement of voltage, and a first amount of power associated with the power supply. The PSM may cause a load associated with the power supply to be adjusted based on determining the current without removing power for a connection between the power supply and a power source associated with the power supply. The PSM may cause the power supply to provide a second amount of power based on causing the load associated with the power supply to be adjusted.

A wireless control device includes a power source, one or more sensors, one or more switches, a wireless transceiver circuit, an antenna connected to the wireless transceiver circuit, and a processor communicably coupled to the power source, the one or more sensors, the one or more switches, and the wireless transceiver circuit. The processor receives a data from the one or more sensors or the one or more switches, determines a pre-defined action associated with the data that identifies one or more external devices and one or more tasks, and transmits one or more control signals via the wireless transceiver circuit and the antenna that instruct the identified external device(s) to perform the identified task(s).

Disclosed is a reactance-injecting module used to balance the currents among the phases of polyphase electric power transmission lines or to manage power flow among alternate paths, where the reactance-injecting module has high-speed, dedicated communication links to enable the immediate removal of injected reactance from all phases of a phase balancing cluster when a fault is detected on any one of the multiple phases. The reactance-injecting module may communicate information on a detected fault to the other reactance-injecting modules of the phase balancing cluster within 10 microseconds after the fault is detected to allow the phase balancing cluster to eliminate injected reactance from all phases within 1 millisecond after the fault is detected. This provides extremely fast neutralization of injected reactance to minimize interference with fault localization analyses.

A wireless control device includes a power source, one or more sensors, one or more switches, a wireless transceiver circuit, an antenna connected to the wireless transceiver circuit, and a processor communicably coupled to the power source, the one or more sensors, the one or more switches, and the wireless transceiver circuit. The processor receives a data from the one or more sensors or the one or more switches, determines a pre-defined action associated with the data that identifies one or more external devices and one or more tasks, and transmits one or more control signals via the wireless transceiver circuit and the antenna that instruct the identified external device(s) to perform the identified task(s).

An aircraft seat having a voltage supply connection assigned only to the aircraft seat and/or at least one data connection assigned only to the aircraft seat, a voltage supply unit assigned to the aircraft seat and having a voltage input for connection to an on-board voltage network of an aircraft and at least one voltage output, each connected to another of the voltage supply connections. A switching arrangement is assigned only to the aircraft seat and connected between the voltage output and the voltage supply connection and/or between the data connection and a data network. A control unit is assigned only to the aircraft seat and connected to the switching arrangement. An infrared reading device is connected to the control unit and assigned only to the aircraft seat to wirelessly receive infrared signals from an external infrared transmitting device. The infrared reading device can receive infrared signals from a predetermined group of predetermined infrared signals, and the control unit can activate the voltage supply connections and/or at least one of the data connections by the switching arrangement, only in response to reception of a predetermined infrared signal.

Provided are an accurate load shedding system, and a communication method and an access apparatus thereof. The access apparatus includes: two E1 interfaces, eight optical fiber interfaces, a CPU and an FPGA. The two E1 interfaces are respectively connected to a control apparatus A and a control apparatus B of a control substation. The eight optical fiber interfaces are respectively connected to eight control terminals. The FPGA includes eight optical fiber transceivers respectively connected to the eight optical fiber interfaces through serial interfaces, and two E1 transceivers respectively connected to the two E1 interfaces through serial interfaces. Each optical fiber transceiver includes a reset submodule. Each E1 transceiver also includes a reset submodule. The CPU is connected to the FPGA through a parallel bus.

The induction memory cell includes an electronic circuit that can control internally the on or off state of a magnetic field within a magnetic induction circuit. The induction memory cell can control external devices. When the induction memory cell is used in an array it can be programmed to retain binary information such as on as a binary digit of one or off as a binary digit of zero. The induction memory cell on or off state can be controlled via a one second burst of laser light, aim at one photo resistor for controlling the magnetic field on state in the primary coil or another photo resistor controlling the magnetic field off state in the primary coil. The induction memory cell requires a 1.5 volt, 5 amp power source in order to maintain an on or off switching effect in the primary coil.

A power control arrangement for an aircraft galley including a power control unit and an interface unit. A power input of the power control unit includes a main switch and connects to a power feed. Each of a power outlets of the power control unit includes an outlet switch and connects to a galley insert. A main switch interface on the interface unit is provided for switching of the main switch. Each outlet switch interface of the interface unit is associated with one of the outlet switches for switching the outlet switch. The interface unit is arranged remote from the power control unit and the switch interfaces are connected to the corresponding switch via an electrical, radio or optical connection for controlling switching of the switches. Further, an aircraft galley and an aircraft are disclosed.