Abstract: A Galley container (1) for use in an aircraft, includes at least two container sidewalls (6), a container floor element (7) and a container ceiling element (8), forming a hollow inner shell casing (2) with a circumferential first rim (12) and a circumferential second rim (12?). The composite tape (11) is spun around the inner shell casing and along the circumference of the rims, forming at least part of a construction layer (5) of the galley container. The composite tape includes at least one fiber and a matrix material.

Abstract: A trolley for accommodating objects includes a housing. The housing includes a bottom wall; two upright side walls and a top wall arranged substantially parallel to the bottom wall and transversely between the side walls. Each side wall extends from the bottom wall, and at least one side wall includes a panel with a core covered on either side with an inner layer and an outer layer, respectively, and at least one outer edge with a plastic rim forming a shock-absorbing edge. The plastic rim is molded onto said outer edge such that the plastic rim surrounds the outer edge of the panel.

Abstract: A device for accommodating objects, in particular for use in an airplane, comprises at least one panel. The panel has at least one outer edge which is provided with a rim in order to form a shock-absorbing edge. The rim comprises plastic that is integrally molded onto the outer edge of the panel. The device can be an airplane trolley, folding trolley, container or galley.

Abstract: A Galley container (1) for use in an aircraft, includes at least two container sidewalls (6), a container floor element (7) and a container ceiling element (8), forming a hollow inner shell casing (2) with a circumferential first rim (12) and a circumferential second rim (12?). The composite tape (11) is spun around the inner shell casing and along the circumference of the rims, forming at least part of a construction layer (5) of the galley container. The composite tape includes at least one fibre and a matrix material.

Abstract: A device (1) for accommodating objects, in particular for use in an airplane, includes a housing (5) and a door (18) which is pivotable about a pivot axis (PA) between an open position and a closed position. The door (18) is movable in a direction which extends substantially parallel to the pivot axis (PA) between a locked position and an unlocked position. The door (18) includes a locking edge (182) and the housing (5) includes a door post (101), wherein the locking edge (182) engages with the door post (101) in the locked position to lock the door in its closed position and allow movement of the door (18) in the direction which extends substantially parallel to the pivot axis (PA) between the locked and the unlocked position.

Abstract: A device for accommodating objects, in particular for use in an airplane, comprising a housing, which has an access opening, as well as a door which is connected to the housing by at least one hinge so as to be pivotable between an open position and a closed position. The hinge defines a pivot axis for pivoting the door. The access opening is at least partially clear in the open position of the door and the access opening is at least partially closed off by the door in the closed position of the door. The door is lockable relative to the housing in its closed position. The door, in its closed position, is movable in a direction which extends substantially parallel to the pivot axis between a locked position and an unlocked position. The door, in its locked position, is locked relative to the housing, and the door, in its unlocked position, is pivotable about the pivot axis.

Abstract: A catering assembly for use with an aircraft or train includes a wall (1) provided with a multiplicity of slots (2) running in the vertical direction with undercuts as well as a multiplicity of essentially block-shaped modules (6) with runners (14) on the rear that can be accommodated in the undercut slots (2), the cross-sectional shape of which, viewed in the horizontal plane, corresponds to the cross-sectional shape of the undercut slots (2), viewed in the horizontal plane. The catering assembly furthermore includes lifting elements for raising or lowering the module (6), the runners (14) of which have been accommodated in a the undercut slot (2), over the wall. It is preferable if the slots (2) are widened in places (15) such that a runner (14) can be inserted here in the horizontal direction so as then to hook into the undercut slot (2) after being moved vertically.

Abstract: A cooling unit (1) for a service trolley for use in an aircraft or train. The cooling unit (1) includes a drawer. The drawer contains a layer of heat-insulating material (29) and one or more Peltier elements (42) located in the layer (29) with a warm side (43) facing the one side of the heat-insulating layer (29) and a cold side (44) facing the other side of the heat-insulating layer (29). First fans (32) are provided on the cold side (44) of the heat-insulating layer (29) and second fans (33) are provided on the warm side (43) of the heat-insulating layer (29). The invention furthermore relates to a service trolley provided with a cooling unit (1) according to the invention as well as to a rack (60) for a multiplicity of cooling units (1) according to the invention. Finally, the invention relates to an aircraft or train containing a cooling unit or service trolley according to the invention.

Abstract: A device for accommodating objects, in particular for use in an airplane, comprising a housing, which has an access opening, as well as a door which is connected to the housing by at least one hinge so as to be pivotable between an open position and a closed position. The hinge defines a pivot axis for pivoting the door. The access opening is at least partially clear in the open position of the door and the access opening is at least partially closed off by the door in the closed position of the door. The door is lockable relative to the housing in its closed position. The door, in its closed position, is movable in a direction which extends substantially parallel to the pivot axis between a locked position and an unlocked position. The door, in its locked position, is locked relative to the housing, and the door, in its unlocked position, is pivotable about the pivot axis.

Abstract: A device for accommodating objects, in particular for use in an airplane, comprises at least one panel. The panel has at least one outer edge which is provided with a rim in order to form a shock-absorbing edge. The rim comprises plastic that is integrally molded onto the outer edge of the panel. The device can be an airplane trolley, folding trolley, container or galley.

Abstract: The invention relates to a drawer comprising a bottom surface (11), two opposing side walls (12,13) and a top surface (14). The side walls are each provided at the top with a recess (15) that extends over the entire side wall, is open towards the outside of the drawer and is delimited from above by a support body (16). Viewed in the vertical direction, the recesses are a recess distance (x) away from the top surface. Viewed in the horizontal direction, the outsides of the support bodies have an external support body spacing (v). The sidewalls are each provided with a supporting foot (17) that extends along the entire sidewall. Viewed in the vertical direction, the supporting foot extends to a supporting foot depth (y) below the bottom surface. Viewed horizontally, the insides of the supporting feet have an internal supporting foot spacing (w).

Abstract: A wheel assembly provided with a bracket (1), a wheel (5) which is mounted in the bracket (1) it such a manner that it can rotate about an axle (4), a brake member (7) which can move with respect to the wheel (5) and has a brake pin (8) provided with a screw thread, around the brake pin a displaceable brake disc (9) provided with a complementary screw thread, and a locking disc (11) for fixing the position of the brake disc (9) along the screw thread. The locking disc (11) is provided with at least one pawl (12) which is positioned radially with respect to the brake pin and can be displaced substantially in the axial direction of the brake pin (8). The brake disc (9) comprises at least one radial slot (10) for accommodating the pawl (12) in order to block the displacement of the brake disc (9) along the axis of the brake pin (8).