Abstract: A luggage compartment arrangement for an aircraft has a base carrier which can be attached in the aircraft and a luggage compartment which is mounted so as to be pivotable about a pivot axis relative to the base carrier and/or so as to be movable translationally along a displacement path. The luggage compartment arrangement further has a spindle drive for pivoting and/or displacing the luggage compartment about the pivot axis. The spindle drive has a motor block with a rotatable spindle and a motor for driving the spindle. Via a spindle nut, at connection points, which are each radially remote from the pivot axis in the case of pivoting, the motor block is attached to the base carrier, and the spindle nut is at least indirectly attached to the luggage compartment, or vice versa.

Abstract: An apparatus for closing a locker, which can be lowered, of a baggage compartment, in particular of an overhead baggage compartment in an aircraft, wherein the locker is connected in an actuating element (5) which is held on a frame (1) such that it can rotate or pivot, and is connected to a gas compression spring (18) in order to assist a closing movement of the locker. In order to allow a completely automatic closing movement, the invention proposes that an electromechanical hybrid drive is provided in order to drive the actuating element (5) and, in addition to the mechanical component of the gas compression spring (18), has an electrical drive apparatus (12) as an electrical component.

Abstract: An apparatus for closing a locker, which can be lowered, of a baggage compartment, in particular of an overhead baggage compartment in an aircraft, wherein the locker is connected in an actuating element (5) which is held on a frame (1) such that it can rotate or pivot, and is connected to a gas compression spring (18) in order to assist a closing movement of the locker. In order to allow a completely automatic closing movement, the invention proposes that an electromechanical hybrid drive is provided in order to drive the actuating element (5) and, in addition to the mechanical component of the gas compression spring (18), has an electrical drive apparatus (12) as an electrical component.