An example floor panel for a flooring system in a passenger vehicle includes a top sheet, a bottom sheet, a body situated between the top sheet and the bottom sheet, and an interlocking feature that extends outward from the body for slidably engaging an adjacent floor panel. An example flooring system in a passenger vehicle includes a first set of floor panels including panels rigidly attached to a structure of the passenger vehicle, and a second set of floor panels and each floor panel of the second set of floor panels has an interlocking feature for slidably engaging an adjacent floor panel and for enabling lateral relative motion to occur and restricting vertical relative motion between panels of the second set of floor panels and a respective adjacent floor panel.

A floor fixing assembly for releasable fixing of a leg of a frame to a vehicle floor comprises at least one retaining peg which can be fixed to the vehicle floor. The floor fixing assembly furthermore comprises a frame fixing element, which is configured to be connected to the leg of the frame and comprises at least one receiving space for receiving the retaining peg. A clamping device is configured to be introduced into the receiving space of the frame fixing element in order to connect the frame fixing element to the retaining peg by form fit.

A floor fixing assembly for releasable fixing of a leg of a frame to a vehicle floor comprises at least one retaining peg which can be fixed to the vehicle floor. The floor fixing assembly furthermore comprises a frame fixing element, which is configured to be connected to the leg of the frame and comprises at least one receiving space for receiving the retaining peg. A clamping device is configured to be introduced into the receiving space of the frame fixing element in order to connect the frame fixing element to the retaining peg by form fit.

A device for attaching an object to an attachment rail, particularly a seat rail, in an aircraft or spacecraft. A base part has a support surface to be placed onto an outer surface of the rail, and a locking element to partially protrude from the support surface along a line of protrusion. The base part and locking element are coupled or configured to be coupled wherein the locking element can be moved relative to the base part along the line of protrusion and rotated with respect to the base part. An end section of the locking element has a tip portion shaped in a dovetail-type manner. The device includes a tensioning arrangement for tensioning the locking element with respect to the rail. An arrangement includes such a device as well as an attachment rail with a rail main body and a plurality of bushes. A method for attaching an object, and a seat rail are disclosed.

An aircraft fuselage assembly includes a primary structure with first and second rows of support elements extending parallel to a longitudinal axis and into an interior space of the fuselage where they have a free end. The free ends of the first and second rows are spaced from one another to from a free space below a common plane of the free ends and extending to the primary structure. A cargo floor assembly with at least one first cargo floor element is fixedly connected to the free ends of the first row in the common plane and at least one second cargo floor element fixedly connected to the free ends of the second row in the common plane. At least one central cargo floor element is arranged between the first and second lines and is releasably connected to the support elements of the first and second rows.

An aircraft fuselage assembly includes a primary structure with first and second rows of support elements extending parallel to a longitudinal axis and into an interior space of the fuselage where they have a free end. The free ends of the first and second rows are spaced from one another to from a free space below a common plane of the free ends and extending to the primary structure. A cargo floor assembly with at least one first cargo floor element is fixedly connected to the free ends of the first row in the common plane and at least one second cargo floor element fixedly connected to the free ends of the second row in the common plane. At least one central cargo floor element is arranged between the first and second lines and is releasably connected to the support elements of the first and second rows.

A cargo module swapping system for an electronic short take-off and landing aerial vehicle, including an autonomously driven robotic vehicle for transporting and swapping cargo modules on an autonomous electric aircraft. The robotic vehicle has two or more robotic arms for controlled material handling and manipulation, each configured to install, remove, and replace cargo bins directly onto the aft end of a forward portion of a central fuselage of an electric short take-off and landing (ESTOL) aircraft. The cargo bins are configured to function as the aft portion of the aircraft central fuselage.

A cargo module swapping system for an electronic short take-off and landing aerial vehicle, including an autonomously driven robotic vehicle for transporting and swapping cargo modules on an autonomous electric aircraft. The robotic vehicle has two or more robotic arms for controlled material handling and manipulation, each configured to install, remove, and replace cargo bins directly onto the aft end of a forward portion of a central fuselage of an electric short take-off and landing (ESTOL) aircraft. The cargo bins are configured to function as the aft portion of the aircraft central fuselage.

An apparatus for securing a raceway assembly within an aircraft, which includes a clip assembly associated with the raceway assembly, which secures the raceway assembly to a seat rail. The apparatus further includes a floor panel positioned in overlying relationship to the raceway assembly and the clip assembly.

An apparatus for securing a raceway assembly within an aircraft, which includes a clip assembly associated with the raceway assembly, which secures the raceway assembly to a seat rail. The apparatus further includes a floor panel positioned in overlying relationship to the raceway assembly and the clip assembly.