Disclosed herein is a fenestration assembly. The assembly includes a movable sash assembly, a first lock counterpart connected to the movable sash assembly, a fixed sash assembly, a second lock counterpart connected to the fixed sash assembly, and a sill configuration. While the fixed sash assembly is mounted to the sill configuration, and while the movable sash assembly is mounted to the sill configuration at a first height, the movable sash assembly is lockable to the fixed sash assembly. While the fixed sash assembly is mounted to the sill configuration, and while the movable sash assembly is mounted to the sill configuration at a second height, the movable sash assembly is lockable to the fixed sash assembly. While there is an absence of locking between the movable and fixed sash assemblies, the movable sash assembly is movable relative to the sill configuration.

The present lift lock includes a slide having feet and a slot between the feet, where such slide further includes an interior generally full length wall for acting as a stop, and where such slide further includes gripping ribs that increase in width from the front end of the slide to the rear end of the slide.

The present lift lock includes a slide having feet and a slot between the feet, where such slide further includes an interior generally full length wall for acting as a stop, and where such slide further includes gripping ribs that increase in width from the front end of the slide to the rear end of the slide.

An intelligent lock, overlock, and lock system can be electrically controlled to open and close one or more locks. The lock, lock system, and method may function on a frequency selected to avoid cross talk, which permits numerous locks to function simultaneously on the same central system with little interruption or delay. A lock may be used as an overlock for an existing lock or be a primary lock and may include a pivoting engagement structure that engages a locking mechanism to provide added strength.

The invention relates to a lock (5) for a hinged closure, comprising a housing (8) adapted to be mounted on a frame (3) of the closure, and seating internally thereof a bolt device (4) reciprocable relative to the housing between respective open and closed positions of the closure and having a throw of substantially 70 mm to bridge in use a gap between the frame and a facing keeper, characterised by a Eurocylinder lock means (5) adapted to engage and retain the bolt (4) in the locked, or closed, position of the closure. There is also disclosed means to protect the said lock (5) against vandalism, the means comprising in disclosed embodiments a cover plate (305,305a), an inclined escutcheon (6), or smooth fillet weld(s) securing the escutcheon (6) to the housing (8).

The invention relates to a lock (5) for a hinged closure, comprising a housing (8) adapted to be mounted on a frame (3) of the closure, and seating internally thereof a bolt device (4) reciprocable relative to the housing between respective open and closed positions of the closure and having a throw of substantially 70 mm to bridge in use a gap between the frame and a facing keeper, characterised by a Eurocylinder lock means (5) adapted to engage and retain the bolt (4) in the locked, or closed, position of the closure. There is also disclosed means to protect the said lock (5) against vandalism, the means comprising in disclosed embodiments a cover plate (305,305a), an inclined escutcheon (6), or smooth fillet weld(s) securing the escutcheon (6) to the housing (8).

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 lock with a sole plate and a slider, guided in translation relative to one another by a guide between two positions, an extended position and a retracted position. The slider includes a bearing surface which extends in a sliding plane defined by the guide and an indentation relative to the bearing surface forming a translation stop in one of the two positions. The sole plate cooperates with a retractable pin of a lock carried by the slider, to lock it in the extended position and in the retracted position. The slider comprises, opposite the indentation relative to the retractable pin of the locking means, a translation stop in the extended position.

The invention relates to a bolt lock device for securely locking doors of fixed-walled storage or transport containers, in particular large-capacity storage or transport containers made of metal, such as in particular freight containers or commercial vehicle trailers, and the container having a bolt lock device of this kind.