A method, system and device for controlling a front compartment lid of a vehicle includes a way of opening or closing of the lid of a front compartment of a vehicle via door handle of the vehicle. The system includes a control unit of the vehicle, a front compartment with a lid with electrically controlled locking and/or opening mechanism and at least one vehicle door handle, and a logical block configured to monitor a status of vehicle door handle by a sensor for position of door handle between open position and closed position; monitor the locking status of the locking and/or opening mechanism; and, in case of matching vehicle door handle sensor data with a preset threshold value, and depending on the current locking status of the front compartment lid, generate a control signal to the locking and/or opening mechanism of the front compartment lid.

A powered latch system for motor vehicles includes at least one powered latch that can be controlled based, at least in part, on vehicle operating conditions. The system may be configured to control unlatching of the vehicle doors utilizing data relating to the vehicle speed and/or the existence of a crash event. The powered latch system can be configured as required for various vehicles, and to accommodate specific operating requirements with respect to child locks in various geographic jurisdictions.

A powered latch system for motor vehicles includes at least one powered latch that can be controlled based, at least in part, on vehicle operating conditions. The system may be configured to control unlatching of the vehicle doors utilizing data relating to the vehicle speed and/or the existence of a crash event. The powered latch system can be configured as required for various vehicles, and to accommodate specific operating requirements with respect to child locks in various geographic jurisdictions.

Aircraft door (1) including a safety latch (7) having a first locking element (8) and a complementary second locking element (9) which is movable; a link (11) having at least one electroactive polymer portion (13) and adapted to take up: a lock position in which the electroactive polymer portion (13) is supplied with power and the movable second locking element (9) is engaged with the first locking element (8); and an unlock position in which the electroactive polymer portion (13) is not supplied with power and the movable second locking element (9) is kept away from the first locking element (8); a control unit (16) having a power supply (26) for the electroactive polymer portion (13).

Aircraft door (1) including a safety latch (7) having a first locking element (8) and a complementary second locking element (9) which is movable; a link (11) having at least one electroactive polymer portion (13) and adapted to take up: a lock position in which the electroactive polymer portion (13) is supplied with power and the movable second locking element (9) is engaged with the first locking element (8); and an unlock position in which the electroactive polymer portion (13) is not supplied with power and the movable second locking element (9) is kept away from the first locking element (8); a control unit (16) having a power supply (26) for the electroactive polymer portion (13).

A system for monitoring a pressure change within at least one compartment of an aircraft and operating a pyrotechnic device associated with a door latch, includes a securing mechanism arranged in an aircraft door that includes a pyrotechnic actuator and a latch bolt. The system includes the pyrotechnic actuator configured to move the latch bolt when the pyrotechnic actuator is actuated. The system also includes a pressure sensor configured to provide a pressure signal. The system also includes a controller configured to determine a pressure drop representing a decompression event. The system also includes an output driver configured to generate an output signal to actuate the pyrotechnic actuator when the controller determines the occurrence of a decompression event.

A system for monitoring a pressure change within at least one compartment of an aircraft and operating a pyrotechnic device associated with a door latch, includes a securing mechanism arranged in an aircraft door that includes a pyrotechnic actuator and a latch bolt. The system includes the pyrotechnic actuator configured to move the latch bolt when the pyrotechnic actuator is actuated. The system also includes a pressure sensor configured to provide a pressure signal. The system also includes a controller configured to determine a pressure drop representing a decompression event. The system also includes an output driver configured to generate an output signal to actuate the pyrotechnic actuator when the controller determines the occurrence of a decompression event.

A method for unlocking a hood of a vehicle in which a latch and a safety catch are arranged for engaging a striker and a locking member is arranged for engaging the safety catch. The method includes displacing the safety catch if a predetermined vehicle condition is fulfilled from a closed state wherein the safety catch is in locking engagement with the striker to an open state where the safety catch is disengaged from the striker for moving the hood locking mechanism from the intermediate locked mode to an open mode.

A method for unlocking a hood of a vehicle in which a latch and a safety catch are arranged for engaging a striker and a locking member is arranged for engaging the safety catch. The method includes displacing the safety catch if a predetermined vehicle condition is fulfilled from a closed state wherein the safety catch is in locking engagement with the striker to an open state where the safety catch is disengaged from the striker for moving the hood locking mechanism from the intermediate locked mode to an open mode.

A distributed safety lockout system for a vehicle, such as a recreational vehicle (RV), that includes a plurality of networked devices communicatively coupled via a communications network, and that is configured to implement a method for controlling an electromechanical operation of an electromechanical device based on a safety lockout condition determined through use of a consensus protocol in which a safety lockout status is agreed upon by the networked devices. The safety lockout status may be escalated by a safety lockout condition detection device that detects a safety lockout condition, such as movement of the RV. The safety lockout status may be de-escalated through a network contention mode of the consensus protocol in which each of the networked devices agree to de-escalate the safety lockout status.