The invention relates to an overhead luggage compartment for aircraft, comprising: a tray for accommodating pieces of luggage, which tray can be pivoted about an axis of rotation between a closed position and an open position; and comprising a housing, which encloses the tray in the closed position and which has devices arranged thereon for fastening to a supporting structure of the aircraft and has a suspension device for a passenger service unit; and comprising a closure element for holding the tray in the closed position. The housing is formed by two frame parts arranged lateral to the tray, which frame parts are connected to each other by means of cross-braces, and the fastening devices and the suspension device for the passenger service unit and at least one stop element for limiting the open position of the tray are arranged on the frame parts.

An aircraft includes a cabin wall defining a cabin and a convertible monument in the cabin adjacent the cabin wall. The convertible monument has a plurality of monument walls defining sides, a front and a rear of the monument surrounding a chamber defined by the monument walls. The convertible monument has a closet component positioned in the chamber for supporting non-perishable items in the chamber. The chamber has a convertible area convertible between a cooling compartment and an uncooled compartment. A chiller is positioned in the chamber proximate the convertible area. The chiller is configured to supply cool air to the cooling compartment when operated for cooling perishable items stowed in the cooling compartment. The convertible area is used as an uncooled compartment for stowing non-perishable items when the chiller is inactive.

A vehicle body includes a primary vehicle structure and interior vehicle fittings as well as a coupling device for fastening the interior vehicle fittings to the primary vehicle structure. The coupling device is configured to generate a magnetic field, so as to fasten the interior vehicle fittings to the primary vehicle structure without contact. Methods for assembling a vehicle body as well as an edifice are also described.

An aircraft ceiling liner element comprises a load-bearing carrier platform, configured to form a part of an aircraft ceiling liner, and a mounting mounted on the carrier platform, connectable to a primary structure of the aircraft. An electrical connection mounted on the carrier platform is connectable to an electrical supply network of the aircraft. Furthermore, the aircraft ceiling liner element comprises a mechanical interface mounted on the carrier platform, configured to attach various interchangeable modular units detachably and in a load-transferring manner to the carrier platform, and an electrical interface mounted on the carrier platform, which interface is configured to create an electrical connection between the modular unit and the carrier platform.

A storage compartment for the overhead region of a passenger cabin of a passenger aircraft has a carrier which can be mounted in the passenger aircraft, and a pivoting part for receiving a storage item. The pivoting part is mounted on the carrier so as to be pivotable about a pivot axis in a pivoting region between an open position and a closing position. The storage compartment further contains a closing force module. The closing force module contains a switching module by which the closing force module can be brought into an active state or into a passive state. In the active state, a greater closing moment is brought about in the direction of the closing position on the pivoting part by the closing force module, at least in a partial region of the pivoting region, than in the passive state. The closing force module is configured free from electricity with respect to the generation of the closing moment and/or with respect to the switching over between the active state and passive state.

An aircraft storage bin that includes an upper housing, and a bucket pivotally connected to the upper housing that cooperates with the upper housing to define a bin interior. The bucket includes a bottom, a front edge, first and second opposing side walls extending upwardly from the bottom and a center of gravity. The bucket pivots about a pivot axis with respect to the upper housing between an open position and a closed position. The center of gravity of the bucket is positioned below the pivot axis when the bucket is in the closed position.

A tension-only member for a truss structure and a method of operating a vehicle with tension-only members is provided. Tension-only members readily deform when a compressive load is applied. The tension-only members may be a leaf spring, a strap, a cable, or a rope between two connector ends. The tension-only members are placed diagonally in a truss such that the tension-only members support a load applied in one direction but deflect when a load is applied in an opposite direction. A truss structure with such tension-only members can be flexible to enable a vehicle frame to which it is attached to flex.

An arrangement in a cabin of an aircraft includes a plurality of passenger seats, which create seat rows arranged between at least one aisle and a cabin wall. At least one first section has at least one row with a first number of passenger seats and at least one second section has at least one seat row with a second number of passenger seats, that is below the first number, are created. The at least one seat row of the first section and the at least one seat row of the second section directly border on the at least one aisle. In the second section between a passenger seat facing the cabin wall and the respective cabin wall a stowage compartment is arranged, which is positionable on a cabin floor.

A control system and method of controlling access to storage bins in a vehicle. The system includes a lock configured to be selectively movable between a locked position to prevent access to an interior of the storage bins and an unlocked position to allow access to the interior of the storage bins. A switch is positioned in a cabin of the vehicle. A control circuit is configured to determine an operational status of the vehicle and selectively position the locks. The control circuit can also receive an override signal from the switch and unlock the locks in certain situations.

In a preferred embodiment, an aircraft monument is adapted for being mounted against an aft-facing bulkhead of the aircraft. The monument may have an aisle-accessible compartment that includes comestible item dispensers and lower footwell regions to accommodate the passengers seated immediately aft of the monument. The monument may also include an aft-facing wall that is readily removal during a maintenance operation so as to facilitate servicing of a heater or chiller unit disposed inside the monument.