Locking element

1. A locking element for securing containers or similar freight on a cargo bay floor of an aircraft in a vertical direction (z) perpendicular to the cargo bay floor and in a transverse direction (y) perpendicular to the longitudinal direction (x) of the aircraft, comprising:

a frame including a guide extending along a longitudinal direction of the locking element,

mounting devices for fixing the frame to the cargo bay floor, and

at least one lock attached to the frame, the lock including a claw for securing containers or similar freight in the transverse direction (y; −y) to surround and hold a part section of the container, wherein the lock is selectively movable along the guide in a longitudinal direction of the locking element which corresponds to the transverse direction (y; −y), and a releasable fixing device for selectively fixing the lock to the guide and for allowing the lock to be selectively movable in the longitudinal direction along the guide with respect to the frame to a desired longitudinal position with respect to the frame,

wherein the releasable fixing device comprises a swivel shaft with a swivel axis about which the lock is swivellable from a raised working position to a lowered loading position while the swivel axis remains in the same longitudinal position with respect to the frame.

2. The locking element according to claim 1 , wherein the fixing device comprises catch elements for securing the lock and counter-catch elements at defined positions in the frame.

3. The locking element according to claim 1 , wherein the fixing device is formed springily such that the lock can be moved against a spring force in the transverse direction (y; −y).

4. The locking element according to claim 3 , wherein the fixing device comprises catch slides guided in the frame and spring-loaded as counter-catch elements.

5. The locking element according to claim 1 , wherein the lock comprises a travel slide in which the claw is swivellably mounted and which can be moved and fixed in the guide.

6. The locking element according to claim 1 , wherein the swivel shaft comprises a journal mounted displaceable against spring force to release the lock from the frame for movement along the guide.

7. The locking element according to claim 1 , wherein the mounting devices are connected with the frame mobile in the longitudinal direction (x), wherein preferably parts of the mounting devices are arranged in the region of and preferably centrally to longitudinal ends of side rails of the frame running in the transverse direction (y; −y).

8. The locking element according to claim 1 , wherein load-holding devices are provided.

9. The locking element according to claim 7 , wherein the load-holding devices are arranged removably on the frame.

10. The locking element according to claim 1 , wherein the lock on at least one side has chamfered surfaces to move the lock from the working position to the loading position when a container passes over the lock in a direction which is not the same as a holding direction of the lock.

11. A cargo bay floor of an aircraft wherein the cargo bay floor comprises: rails which are attached to the cargo bay floor in the longitudinal direction of the aircraft (x), and at least one locking element according to claim 1 , which is attached to the rails.

12. The cargo bay floor according to claim 11 , wherein the at least one locking element is attached between two adjacent rails.

13. A method of configuring a cargo bay of an aircraft for containers or similar freight of different sizes, comprising the following steps:

mounting of rails in the cargo bay of the aircraft;

fixing of at least one locking element according to claim 1 to the rails or cargo bay floor of the aircraft;

adjusting the distance between two locks of two locking elements to standard sizes of containers or similar freight by moving and fixing at least one lock along the transverse direction (y).

14. The locking element of claim 1 , wherein the swivel shaft forms the part of the fixing device via which forces occurring during holding are transferred to the frame.

15. A locking element for securing a container or similar freight on a cargo bay floor of an aircraft in a vertical direction (z) perpendicular to the cargo bay floor and in a transverse direction (y) perpendicular to the longitudinal direction (x) of the aircraft, the locking element comprising:

a frame adapted to be mounted to the cargo bay floor, the frame including an elongate guide extending longitudinally with respect to the frame,

a first lock including a swivel shaft coupled to the frame, the swivel shaft of the first lock including a swivel axis about which the first lock is swivellable between a raised working position and a lowered loading position, the swivel shaft of first lock being selectively movable along the guide with respect to the frame to a desired position,

a second lock including a swivel shaft coupled to the frame, the swivel shaft of the second lock including a swivel axis about which the second lock is swivellable between a raised working position and a lowered loading position, the swivel shaft of the second lock being selectively movable along the guide with respect to the frame to a desired position, wherein the first lock and the second lock are selectively movable along the guide independently of one another.

16. A cargo bay floor of an aircraft, the cargo bay floor including:

a first rail and a second rail extending along a longitudinal direction (x) of the aircraft, and

a locking element for securing containers or similar freight to the cargo bay floor, the locking element including a frame, a first mounting device for fixing the frame to the first rail, a second mounting device for fixing the frame to the second rail, a first lock and a second lock attached to the frame, the first lock and the second lock each including a claw for securing containers or similar freight in the transverse direction (y) of the aircraft to surround and hold a part section of the container, the first lock being movable independently of the second lock, wherein a guide is provided in the frame for moving the first lock along a longitudinal direction of the locking element which corresponds to the transverse direction (y) of the aircraft, the first lock including a releasable fixing device for selectively fixing the first lock to the guide and for allowing the first lock to be selectively movable along the guide with respect to the frame to a desired position with respect to the frame,

wherein the releasable fixing device of the first lock comprises a swivel shaft with a swivel axis about which the first lock is swivellable from a raised working position to a lowered loading position, the second lock having a raised working position, the claw of the second lock facing in the opposite direction as the claw of the first lock when the first and second locks are in the raised working positions.