Latch assemblies and systems are disclosed. One latch includes a latch and a receiver. The latch has a housing and a pin extending from the housing. The pin is mounted for longitudinal movement along a pin axis. The latch further includes a motor coupled to move the pin longitudinally. The receiver defines an aperture extending along a receiver axis and positioned to receive the pin of the latch. The receiver has a retainer biased toward the receiver axis. The latch assembly has an open position in which the pin is extended distally along the pin axis and received in the aperture, and a latched position in which the pin is retracted proximally along the pin axis while the retainer is engaged with the pin. One latch system includes a plurality of latch assemblies configured to move to the latched position after all latch assemblies are in the open position.

A bar lock assembly including a lock rod having first and second lock rod portions and defines a rotational axis. A second lock rod portion section telescopically extends from the first lock rod portion when the bar lock assembly is in a first condition. The second lock rod portion is substantially retracted within the first lock rod portion when the bar lock assembly is in a second condition. An elongated handle having opposed ends extends from the first lock rod portion. One handle end is pivotally connected to the first lock rod about a fixed axis. Linkage between the handle and the second lock rod portion telescopically moves the second lock rod portion. This lock bar assembly is configured such that an angle of about 45° is established between the handle and a generally horizontal plane when in the first position to enhance ergonomic operation of the bar lock assembly.

A bar lock assembly including a lock rod having first and second lock rod portions and defines a rotational axis. A second lock rod portion section telescopically extends from the first lock rod portion when the bar lock assembly is in a first condition. The second lock rod portion is substantially retracted within the first lock rod portion when the bar lock assembly is in a second condition. An elongated handle having opposed ends extends from the first lock rod portion. One handle end is pivotally connected to the first lock rod about a fixed axis. Linkage between the handle and the second lock rod portion telescopically moves the second lock rod portion. This lock bar assembly is configured such that an angle of about 45° is established between the handle and a generally horizontal plane when in the first position to enhance ergonomic operation of the bar lock assembly.

A latch feature for a door is disclosed herein. The latch feature includes an input body that is operable to move linearly between first and second positions relative to the door. The latch feature also includes an output body. The output body is coupled to the input body by a pivot member that is configured to pivot relative to the output body and the input body to allow the output body to move linearly toward the input body from an outboard position to an inboard position as the input body moves from the first position to the second position.

A latch feature for a door is disclosed herein. The latch feature includes an input body that is operable to move linearly between first and second positions relative to the door. The latch feature also includes an output body. The output body is coupled to the input body by a pivot member that is configured to pivot relative to the output body and the input body to allow the output body to move linearly toward the input body from an outboard position to an inboard position as the input body moves from the first position to the second position.

A latch mechanism is configured to be shifted between a closed state in which a glove door is held on a compartment body at a closed position and an open state in which the glove door is not held on the compartment body. An operation lever is operated to shift the lock mechanism from the closed state to the open state. When the latch mechanism is shifted to the closed state, the first engaging member is engaged with the engagement hole. When the latch mechanism is shifted to the open state, the first engaging member is disengaged from the engagement hole. The compartment body includes an operation restriction wall that restricts operation of the first engaging member from the side surface of an instrument panel or the side surface of the compartment body so that the first engaging member is not disengaged from the engagement hole.

A latch mechanism is configured to be shifted between a closed state in which a glove door is held on a compartment body at a closed position and an open state in which the glove door is not held on the compartment body. An operation lever is operated to shift the lock mechanism from the closed state to the open state. When the latch mechanism is shifted to the closed state, the first engaging member is engaged with the engagement hole. When the latch mechanism is shifted to the open state, the first engaging member is disengaged from the engagement hole. The compartment body includes an operation restriction wall that restricts operation of the first engaging member from the side surface of an instrument panel or the side surface of the compartment body so that the first engaging member is not disengaged from the engagement hole.

There is provided herein an aircraft including at least one aircraft galley container and a controller. Each one of the at least one aircraft galley container includes a safety feature having a first mode and a second mode, and a controller for automatically selecting one of the first mode and second mode of the safety feature and placing the safety feature in the selected mode. The automatic selection of the mode is dependent on a condition of the aircraft satisfying or failing to satisfy a predetermined condition. There is also provided a method of operating a safety feature of an aircraft galley container.

There is provided herein an aircraft including at least one aircraft galley container and a controller. Each one of the at least one aircraft galley container includes a safety feature having a first mode and a second mode, and a controller for automatically selecting one of the first mode and second mode of the safety feature and placing the safety feature in the selected mode. The automatic selection of the mode is dependent on a condition of the aircraft satisfying or failing to satisfy a predetermined condition. There is also provided a method of operating a safety feature of an aircraft galley container.

A low profile actuating window lock for casement windows having a longitudinal slot in a sidewall of the casing for the lock, wherein an actuator including a fork component translates within the slot in a direction opposite movement of the handle, the handle pivotable about a restrictor arm that pivots relative to the casing, allowing the handle to rotate from the locked position to the unlocked position with low clearance from the window frame. The pivot points of the handle and restrictor arm configuration allow for an over center linkage that prevents back driving the casement window lock.