The invention relates to a latch unit for use in an aircraft cargo hold to secure freight. The latch unit includes a claw that can be depressed out of an elevated, position in which an item of freight can be brought into an immobilizing engagement with the claw, into a resting position in which an item of freight can travel over the latch unit. The latch unit is constructed to engage freight that approaches in a direction leading out of the cargo hold and allows freight to freely move when the freight approaches from all other directions. In addition, the latch unit allows freight to rotate while in the door region, while at the same time prevents freight from accidentally rolling out of the cargo hold.
1. A latch unit for an aircraft cargo hold loading system that includes roller and ball units that are provided on a floor of the cargo hold, the latch unit comprising:
a claw that can be depressed from an operating position in which an item of freight can be brought into an immobilizing engagement with the claw, into a resting position in which the item of freight can travel over the latch unit, and
a mechanical actuator which causes a lowering movement when the actuator is encountered by the approaching item of freight, the actuator being positioned in front of a cargo hold door and constructed such that when the item of freight approaches the latch unit in a direction leading out through the cargo hold door, the claw remains in the operating position, whereas when the latch unit is approached from all other directions the claw is depressed into the resting position; and
a locking mechanism for retaining the claw in a retracted position wherein when the claw is retracted out of the operating position, the claw is positioned lower than the resting position until the locking mechanism is released.
2. A latch unit as claimed in claim 1 wherein the claw defines an engagement surface and comprises a hinged joint disposed opposite to the engagement surface, the surface and joint are each so arranged that the engagement surface can be lowered against the force of a spring-loading in a movement substantially tangential to the hinge joint from the operating position into the resting position.
3. A latch unit as claimed in claim 2 , wherein an upper surface of the claw defines a substantially rectangular contour with sloping portions that incline upwardly toward a middle region of an upper edge of the engagement surface from outside edges of the claw.
4. A latch unit as claimed in claim 1 , comprising the locking mechanism for retaining the claw in the retracted position wherein the claw is at least as depressed as in the resting position.
5. A latch unit for an aircraft cargo hold loading system that includes roller and ball units that are provided on a floor of the cargo hold, the latch unit comprising:
a claw that can be depressed from an operating position in which an item of freight can be brought into an immobilizing engagement with the claw, into a resting position, in which the item of freight can travel over the latch unit;
a mechanical actuator which causes a lowering movement when the actuator is encountered the approaching item of freight, the actuator being adapted to be positioned in a region of a cargo hold door and so constructed such that when the item of freight approaches the latch unit in a direction leading out through the cargo hold door, the claw remains in the operating position, whereas when the latch unit is approached from all other directions the claw is depressed into the resting position; and
a locking mechanism for retaining the claw in a retracted position wherein the claw is at least as depressed as in the resting position wherein the locking mechanism is so constructed, and the latch unit can be attached to the floor of the cargo hold in such a way that the claw comes into engagement with the locking mechanism whenever the claw is depressed out of the operating position into a position lower by a predetermined amount than the resting position, and is thereafter retained by the locking mechanism until the locking mechanism is released.