Abstract: A power control system in which power from a power supply is buffered until a predetermined level of buffered power is available at which time the system activates a device to function powered by the buffered power. Thus, by buffering the available power, a higher power requirement load can be operated periodically e.g. data can be transmitted to/from a wireless transceiver periodically.

Abstract: A system includes three switches each having a single pole and dual throws. The respective single pole is on a supply side of the each respective switch. The dual throws are on a load side of each respective switch, and include a respective normally open (NO) throw and a respective normally closed (NC) throw. A first voltage detector is connected from the single pole of the first switch to the NC throw of the third switch. A second voltage detector is connected from the single pole of the second switch to the NC throw of the first switch. A third voltage detector is connected from the single pole of the third switch to a NC throw of the second switch.

Abstract: An aircraft galley insert is disclosed. In one or more embodiments, the aircraft galley insert includes a control unit including a control unit housing. The aircraft galley insert further includes one or more electronic components at least partially contained within the control unit housing, wherein at least one electronic component of the one or more electronic components is coupled to the control unit housing. The aircraft galley insert further includes one or more operating load components electrically coupled to the at least one electronic component via one or more electrical lines. In one or more embodiments, the control unit housing is configured to provide a grounding path for radiated emissions produced by the at least one electronic component by transferring radiated emissions back to the at least one electronic component.

Abstract: A circuit comprises an optical coupling including an illuminator optically coupled to an optical sensor to output a voltage from the optical sensor based on intensity of illumination from the illuminator. The circuit includes a voltage input node with a resistance connected in series between the voltage input and a Zener diode. A method includes powering an illuminator with current from a first voltage input node. The method includes sensing illumination level in illumination from the illuminator with a sensor and outputting output proportionate to illumination sensed by the sensor indicative of voltage detected at the voltage input node. The method can include limiting current between the voltage input node and the illuminator.

Abstract: A system includes three switches each having a single pole and dual throws. The respective single pole is on a supply side of the each respective switch. The dual throws are on a load side of each respective switch, and include a respective normally open (NO) throw and a respective normally closed (NC) throw. A first voltage detector is connected from the single pole of the first switch to the NC throw of the third switch. A second voltage detector is connected from the single pole of the second switch to the NC throw of the first switch. A third voltage detector is connected from the single pole of the third switch to a NC throw of the second switch.

Abstract: A system includes three switches each having a single pole and dual throws. The respective single pole is on a supply side of the each respective switch. The dual throws are on a load side of each respective switch, and include a respective normally open (NO) throw and a respective normally closed (NC) throw. A first voltage detector is connected from the single pole of the first switch to the NC throw of the third switch. A second voltage detector is connected from the single pole of the second switch to the NC throw of the first switch. A third voltage detector is connected from the single pole of the third switch to a NC throw of the second switch.

Abstract: A circuit comprises an optical coupling including an illuminator optically coupled to an optical sensor to output a voltage from the optical sensor based on intensity of illumination from the illuminator. The circuit includes a voltage input node with a resistance connected in series between the voltage input and a Zener diode. A method includes powering an illuminator with current from a first voltage input node. The method includes sensing illumination level in illumination from the illuminator with a sensor and outputting output proportionate to illumination sensed by the sensor indicative of voltage detected at the voltage input node. The method can include limiting current between the voltage input node and the illuminator.

Abstract: A system includes three switches each having a single pole and dual throws. The respective single pole is on a supply side of the each respective switch. The dual throws are on a load side of each respective switch, and include a respective normally open (NO) throw and a respective normally closed (NC) throw. A first voltage detector is connected from the single pole of the first switch to the NC throw of the third switch. A second voltage detector is connected from the single pole of the second switch to the NC throw of the first switch. A third voltage detector is connected from the single pole of the third switch to a NC throw of the second switch.

Abstract: An aircraft galley insert is disclosed. In one or more embodiments, the aircraft galley insert includes a control unit including a control unit housing. The aircraft galley insert further includes one or more electronic components at least partially contained within the control unit housing, wherein at least one electronic component of the one or more electronic components is coupled to the control unit housing. The aircraft galley insert further includes one or more operating load components electrically coupled to the at least one electronic component via one or more electrical lines. In one or more embodiments, the control unit housing is configured to provide a grounding path for radiated emissions produced by the at least one electronic component by transferring radiated emissions back to the at least one electronic component.

Abstract: A system for current measurement and ground fault detection is disclosed. In embodiments, the system includes a plurality of Hall Effect sensors configured to detect phase currents associated with at least one portion of a multi-phase system. The system further includes a plurality of phase current measurement circuits and a ground fault detection circuit connected to the Hall Effect sensors. The phase current measurement circuits are configured to measure the phase currents detected by the Hall Effect sensors, and the ground fault detection circuit is configured to measure a summation of the phase currents detected by the Hall Effect sensors.

Abstract: A system for current measurement and ground fault detection is disclosed. In embodiments, the system includes a plurality of phase current measurement coils configured to detect phase currents associated with at least one portion of a multi-phase system. The system further includes a plurality of phase current measurement circuits and a ground fault detection circuit connected to the phase current measurement coils. The phase current measurement circuits are configured to measure the phase currents detected by the phase current measurement coils, and the ground fault detection circuit is configured to measure a summation of the phase currents detected by the phase current measurement coils.

Abstract: A system for current measurement and ground fault detection is disclosed. In embodiments, the system includes a plurality of Hall Effect sensors configured to detect phase currents associated with at least one portion of a multi-phase system. The system further includes a plurality of phase current measurement circuits and a ground fault detection circuit connected to the Hall Effect sensors. The phase current measurement circuits are configured to measure the phase currents detected by the Hall Effect sensors, and the ground fault detection circuit is configured to measure a summation of the phase currents detected by the Hall Effect sensors.

Abstract: A system for current measurement and ground fault detection is disclosed. In embodiments, the system includes a plurality of phase current measurement coils configured to detect phase currents associated with at least one portion of a multi-phase system. The system further includes a plurality of phase current measurement circuits and a ground fault detection circuit connected to the phase current measurement coils. The phase current measurement circuits are configured to measure the phase currents detected by the phase current measurement coils, and the ground fault detection circuit is configured to measure a summation of the phase currents detected by the phase current measurement coils.