Patent classifications
E05B81/56
Actuator apparatus and related methods for use with vehicle locks
Actuator apparatus and related methods for use with vehicle locks are disclosed. A disclosed locking system for a vehicle includes a movable component of the vehicle and a lock operatively coupled to the movable component. The locking system also includes an actuator assembly. The actuator assembly includes a housing coupled to a vehicle body, an actuator supported by the housing, and a linkage mechanism connecting the actuator to the lock. The locking system also includes an input device supported by the housing. Activation of the input device causes the actuator to change a state of the lock.
Actuator apparatus and related methods for use with vehicle locks
Actuator apparatus and related methods for use with vehicle locks are disclosed. A disclosed locking system for a vehicle includes a movable component of the vehicle and a lock operatively coupled to the movable component. The locking system also includes an actuator assembly. The actuator assembly includes a housing coupled to a vehicle body, an actuator supported by the housing, and a linkage mechanism connecting the actuator to the lock. The locking system also includes an input device supported by the housing. Activation of the input device causes the actuator to change a state of the lock.
AIRCRAFT DOOR WITH A SAFETY LATCH COMPRISING AN ELECTROACTIVE POLYMER LINK
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 WITH A SAFETY LATCH COMPRISING AN ELECTROACTIVE POLYMER LINK
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).
SYSTEM AND METHOD FOR OPENING BOARDING DOOR
The present disclosure provides a method of opening a boarding door of a vehicle that provides use of a trunk room to a passenger reserving the trunk room. The method comprises keeping the boarding door closed until both a first condition and a second condition are satisfied and opening the boarding door or enabling the boarding door to be opened in response to both the first condition and the second condition being satisfied. Here, the first condition is that the passenger is in the vicinity of the boarding door. The second condition is that the trunk door is closed or that a reservation of the trunk room is cancelled.
SYSTEM AND METHOD FOR OPENING BOARDING DOOR
The present disclosure provides a method of opening a boarding door of a vehicle that provides use of a trunk room to a passenger reserving the trunk room. The method comprises keeping the boarding door closed until both a first condition and a second condition are satisfied and opening the boarding door or enabling the boarding door to be opened in response to both the first condition and the second condition being satisfied. Here, the first condition is that the passenger is in the vicinity of the boarding door. The second condition is that the trunk door is closed or that a reservation of the trunk room is cancelled.
ANTITHEFT SECURITY SYSTEM AND METHOD FOR A MOTOR VEHICLE
An antitheft security system for a motor vehicle includes a license plate locking mechanism and a control module. The license plate locking mechanism functions to secure a license plate to the motor vehicle. The control module includes a controller configured to interrupt power from a power source of the motor vehicle in response to disconnection of the license plate from the motor vehicle. A related antitheft method is also disclosed.
ANTITHEFT SECURITY SYSTEM AND METHOD FOR A MOTOR VEHICLE
An antitheft security system for a motor vehicle includes a license plate locking mechanism and a control module. The license plate locking mechanism functions to secure a license plate to the motor vehicle. The control module includes a controller configured to interrupt power from a power source of the motor vehicle in response to disconnection of the license plate from the motor vehicle. A related antitheft method is also disclosed.
Pyrotechnic latch actuator responsive to a decompression detection system and method
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.
Pyrotechnic latch actuator responsive to a decompression detection system and method
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.