A galley system within an internal cabin of an aircraft includes one or more inboard cart compartments that are configured to removably retain one or more first galley carts, and one or more outboard cart compartments. The outboard cart compartment(s) are configured to removably retain one or more second galley carts. The inboard cart compartment(s) extend forwardly and/or rearwardly in relation to the outboard cart compartment(s).

Concepts and technologies are disclosed herein for a galley lift. In one embodiment, the galley lift includes an upper portion and a lower portion. The upper portion can have a lift platform and a lift platform ram extension. The lower portion can have a lift mechanism and a ram. In some embodiments, the lift platform ram extension is attached to the ram.

Concepts and technologies are disclosed herein for a galley lift. In one embodiment, the galley lift includes an upper portion and a lower portion. The upper portion can have a lift platform and a lift platform ram extension. The lower portion can have a lift mechanism and a ram. In some embodiments, the lift platform ram extension is attached to the ram.

An item of galley equipment is disclosed. The item includes an interior liner, a first and a second door, and a catch. The interior liner defines an interior (V) and an access mouth. The catch comprises a static part and a mobile part. The first door comprises a first part of the catch and is hingedly connected to a part of the galley equipment which is not the second door or supported on the second door. The first door may reversibly rotate about the hinge connection between an open position and a closed position. The second door comprises a second part of the catch and is hingedly connected to a part of the galley equipment which is not the first door or supported on the first door. The second door may reversibly rotate about the hinge connection between an open position and a closed position.

An item of galley equipment is disclosed. The item includes an interior liner, a first and a second door, and a catch. The interior liner defines an interior (V) and an access mouth. The catch comprises a static part and a mobile part. The first door comprises a first part of the catch and is hingedly connected to a part of the galley equipment which is not the second door or supported on the second door. The first door may reversibly rotate about the hinge connection between an open position and a closed position. The second door comprises a second part of the catch and is hingedly connected to a part of the galley equipment which is not the first door or supported on the first door. The second door may reversibly rotate about the hinge connection between an open position and a closed position.

A bump strip includes first and second end caps and an intermediate part that, together, define a length of the bump strip. The end caps having an end part and a connecting part, and whereby one or more fastening holes is provided through the end cap connecting parts and the intermediate part such that a single fastener passing through the fastening hole of an end cap and the intermediate part secures the bump strip to a surface to be protected.

An aircraft galley insert is disclosed. In one or more embodiments, the aircraft galley insert includes a control unit including a control unit housing. The aircraft galley insert further includes one or more electronic components at least partially contained within the control unit housing, wherein at least one electronic component of the one or more electronic components is coupled to the control unit housing. The aircraft galley insert further includes one or more operating load components electrically coupled to the at least one electronic component via one or more electrical lines. In one or more embodiments, the control unit housing is configured to provide a grounding path for radiated emissions produced by the at least one electronic component by transferring radiated emissions back to the at least one electronic component.

An aircraft galley insert is disclosed. In one or more embodiments, the aircraft galley insert includes a control unit including a control unit housing. The aircraft galley insert further includes one or more electronic components at least partially contained within the control unit housing, wherein at least one electronic component of the one or more electronic components is coupled to the control unit housing. The aircraft galley insert further includes one or more operating load components electrically coupled to the at least one electronic component via one or more electrical lines. In one or more embodiments, the control unit housing is configured to provide a grounding path for radiated emissions produced by the at least one electronic component by transferring radiated emissions back to the at least one electronic component.

An overhead bin in an aircraft includes a liner disposed on an underside of a cabin ceiling and a receptacle that protrudes through an opening in the liner. A bin has a top side with at least one attachment point that includes: a stud mechanically coupled to the top side and a screw disposed within the stud. The stud includes a rounded flange configured to insert into the receptacle for removably securing the bin beneath the liner. An installation method for an overhead bin in an aircraft includes raising the overhead bin to engage the stud with the receptacle, sliding the overhead bin outboard for inserting the stud into the receptacle, and turning a screw within the stud for tightening the stud within the receptacle for securing the overhead bin beneath the ceiling.

A galley monument for an aircraft has a shelf structure, a pull-out member supported on the shelf structure so as to be able to be moved between an insertion position and a deployment position and has a carrier plate, and a display device supported on the pull-out member and having a display. A first surface of the carrier plate in the deployment position of the pull-out member is located in a deployment plane and protrudes with respect to the shelf structure and is located in the insertion position at least partially inside the shelf structure. The display device in the deployment position of the pull-out member can be pivoted about a centre of rotation between a storage position, in which the display device extends parallel with the deployment plane, and a position for use, in which the display device extends transversely relative to the deployment plane.