Patent classifications
G01R31/66
Probe for characteristic inspection of a connector
A probe for characteristic inspection of a connector includes a plunger, a coaxial cable, a flange, and a housing having an end portion on one side including an increased diameter portion. A recessed portion which receives the increased diameter portion is in an upper surface of the flange. The increased diameter portion has side walls in contact with or facing respective inner side surfaces of the flange partly, with the inner side surfaces forming the recessed portion, and a bottom wall in contact with an upper recessed surface of the flange that forms the recessed portion. The increased diameter portion has connection surfaces connecting the bottom and side walls and inclined inward from one of the side walls toward the bottom wall. Alternatively, the inner side surfaces each have a first surface inclined downward, and a vertical surface extending downward from the first surface to the upper recessed surface.
CONNECTOR WITH OVERVOLTAGE PROTECTION AND METHODS OF USE FOR CHARGING AN ELECTRIC AIRCRAFT
A connector with overvoltage protection, and methods of use, for charging an electric aircraft. The connector includes a housing, at least a current conductor, a protection circuit, at least a sensor and a controller. The housing is configured to mate with an electric aircraft port of the electric aircraft. The at least a current conductor is configured to conduct a current. The protection circuit is configured to control transmission of electrical power through the connector. The at least a sensor is configured to detect an output voltage of the connector. The controller is communicatively connected to the at least a sensor. The controller is configured to determine an overvoltage output as a function of the output voltage, and activate the protection circuit based on detection of the overvoltage output.
CONNECTOR WITH OVERVOLTAGE PROTECTION AND METHODS OF USE FOR CHARGING AN ELECTRIC AIRCRAFT
A connector with overvoltage protection, and methods of use, for charging an electric aircraft. The connector includes a housing, at least a current conductor, a protection circuit, at least a sensor and a controller. The housing is configured to mate with an electric aircraft port of the electric aircraft. The at least a current conductor is configured to conduct a current. The protection circuit is configured to control transmission of electrical power through the connector. The at least a sensor is configured to detect an output voltage of the connector. The controller is communicatively connected to the at least a sensor. The controller is configured to determine an overvoltage output as a function of the output voltage, and activate the protection circuit based on detection of the overvoltage output.
Ground-loss detection circuit
A ground-loss detection circuit for an integrated circuit, (IC) device including a first dynamic threshold metal oxide semiconductor (DTMOS) device operably coupled between a first ground plane of the IC device and at least one further ground plane of the IC device, at least one of the first and at least one further ground planes comprising an external ground connection of the IC device, at least one further DTMOS device operably coupled between the first and at least one further ground planes of the IC device in an opposing manner to the first DTMOS device, and at least one ground-loss detection component operably coupled to at least one of the first and at least one further DTMOS devices and arranged to detect a ground-loss for at least one of the first and at least one further ground planes based at least partly on a drain current of the at least one of the first and at least one further DTMOS device(s).
ELECTRICAL CONNECTOR AND TEST METHOD FOR ELECTRICAL CONNECTOR
Example implementations involve an electrical connector and a test method of the electrical connector, wherein the electrical conduction condition between a ground member and a ground terminal can be easily confirmed while reliably contacting the ground member and ground terminal. Electrical connector involves a plurality of terminals including two types of terminals, namely, signal terminals and ground terminals; a retaining body, made of an insulating material, that arranges and retains the plurality of terminals in a condition where the signal terminals and ground terminals are intermingled; and a ground member retained by the retaining body on the inward side of the retaining body, in a condition contacting at least two ground terminals; wherein the ground member has a detecting part exposed from the retaining body in order to detect an electrical conduction condition between the ground terminals and the ground member.
Electrical device installation improvement
An energy saving device that is adapted to be connected to a power outlet and further connected to at least one electrical device, said electrical devices drawing power through the energy saving device, the energy saving device including testing means adapted to perform at least one installation verification test and communication means adapted to communicate a validation signal to a monitoring entity when a result of the installation verification test indicates that a correct installation has occurred.
Connector with overvoltage protection and methods of use for charging an electric aircraft
A connector with overvoltage protection, and methods of use, for charging an electric aircraft. The connector includes a housing, at least a current conductor, a protection circuit, at least a sensor and a controller. The housing is configured to mate with an electric aircraft port of the electric aircraft. The at least a current conductor is configured to conduct a current. The protection circuit is configured to control transmission of electrical power through the connector. The at least a sensor is configured to detect an output voltage of the connector. The controller is communicatively connected to the at least a sensor. The controller is configured to determine an overvoltage output as a function of the output voltage, and activate the protection circuit based on detection of the overvoltage output.
Connector with overvoltage protection and methods of use for charging an electric aircraft
A connector with overvoltage protection, and methods of use, for charging an electric aircraft. The connector includes a housing, at least a current conductor, a protection circuit, at least a sensor and a controller. The housing is configured to mate with an electric aircraft port of the electric aircraft. The at least a current conductor is configured to conduct a current. The protection circuit is configured to control transmission of electrical power through the connector. The at least a sensor is configured to detect an output voltage of the connector. The controller is communicatively connected to the at least a sensor. The controller is configured to determine an overvoltage output as a function of the output voltage, and activate the protection circuit based on detection of the overvoltage output.
Accessory presence detection
Disclosed is an electronic circuit with a first terminal for connecting an accessory thereto, and with a functionality for detecting the presence of an accessory connected to the first terminal.
Electrical branch circuit deterioration test system
A system and method for detecting deteriorated junctions within an electrical circuit includes a voltage channel circuit, a load circuit, and a microcontroller. The voltage channel circuit is connectable to the electrical circuit and includes a multiplier circuit, a peak detector circuit, and a filter circuit. The multiplier circuit is configured to square a line voltage of the electrical circuit. The peak detector circuit is configured to detect peak voltages of the line voltage based on an output of the multiplier circuit. A DC output voltage is provided from the filter circuit based on the output of the multiplier circuit. The load circuit is connectable to the electrical circuit and includes a plurality of resistors and a plurality of switches controlled by the microcontroller to enable current flow through the plurality of resistors to control the line voltage. The microcontroller is configured to detect deteriorated junctions based upon comparison of an output of the peak detector circuit and the DC output voltage.