Abstract: A system for mounting aircraft system components in the crown area of an aircraft comprising a first longitudinal carrier element, a second longitudinal carrier element and a bridging element which connects the first longitudinal carrier element to the second longitudinal carrier element. The system is mountable in the crown area of an aircraft in such a way that the first and the second longitudinal carrier elements extend substantially parallel to the longitudinal axis of the aircraft. A plurality of cable ducts for accommodating electrical lines is provided on the first and/or the second longitudinal carrier elements.

Abstract: A sealing device for mounting a monument on a structural element of an aircraft and for providing a seal between the sealing device and the floor of the aircraft is provided. The sealing device comprises a cylindrical element with a pin for attaching the sealing device to the structural element and a recess for receiving another pin of a mounting device to which the monument is attached. The sealing device may have a smaller diameter than a mounting block of the mounting device such that the seal cannot be damaged by trolley wheels.

Abstract: A system for mounting aircraft system components in the crown area of an aircraft comprising a first longitudinal carrier element, a second longitudinal carrier element and a bridging element which connects the first longitudinal carrier element to the second longitudinal carrier element. The system is mountable in the crown area of an aircraft in such a way that the first and the second longitudinal carrier elements extend substantially parallel to the longitudinal axis of the aircraft. A plurality of cable ducts for accommodating electrical lines is provided on the first and/or the second longitudinal carrier elements.

Abstract: A modular seat system for a passenger compartment of a vehicle includes at least one seat, which has a seat unit with a seating element and a seat back and a seat frame with at least one pair of essentially vertical support elements, at whose upper end a bearing structure is arranged on which the seat unit rests, a fixing structure in the floor of the passenger compartment with at least two longitudinal rails, which have a predetermined spacing from one another, for accommodating the lower ends of the support elements, and an adapter plate for the fixing of the support elements, which adapter plate is fitted to the lower end of the support elements, and is fitted in a mobile fashion to at least one support element, so that the spacing of the support elements from one another is variable independently of the width of the seat unit.

Abstract: A sealing device for mounting a monument on a structural element of an aircraft and for providing a seal between the sealing device and the floor of the aircraft is provided. The sealing device comprises a cylindrical element with a pin for attaching the sealing device to the structural element and a recess for receiving another pin of a mounting device to which the monument is attached. The sealing device may have a smaller diameter than a mounting block of the mounting device such that the seal cannot be damaged by trolley wheels.

Abstract: A mirror arrangement (10) for monitoring a passenger cabin of an aircraft is disclosed, comprising at least one mirror element (40) for reflecting light and a mirror mount (20) for fastening the at least one mirror element (40) inside the passenger cabin, the mirror mount (20) comprising a holder (22), to which the at least one mirror element (40) is fastenable and which is displaceable relative to the passenger cabin.

Abstract: The present invention relates to a mirror arrangement (10) for monitoring a passenger cabin of an aircraft, comprising at least one mirror element (40) for reflecting light and a mirror mount (20) for fastening the at least one mirror element (40) inside the passenger cabin, the mirror mount (20) comprising a holder (22), to which the at least one mirror element (40) is fastenable and which is displaceable relative to the passenger cabin.

Abstract: A passenger seat unit comprises modular designed elements, such as at least one seat, and shield elements in the head and foot region. The shield elements are formed by seat dividers that are arranged opposite each other, which seat dividers comprise laterally arranged limbs of the partition wall. One side of the limbs of the partition wall encloses a wall element and forms a closed longitudinal side. The other side of the limbs of the partition wall forms a second longitudinal side which frames an access opening. The longitudinal sides comprise means for length adjustment. It is particularly advantageous if the passenger seat unit according to the invention makes possible more flexible and more economical use of the existing cabin area in passenger aircraft. Flexible adaptation to various cabin lengths is possible without effort.

Abstract: A passenger seat unit comprises modular designed elements, such as at least one seat, and shield elements in the head and foot region. The shield elements are formed by seat dividers that are arranged opposite each other, which seat dividers comprise laterally arranged limbs of the partition wall. One side of the limbs of the partition wall encloses a wall element and forms a closed longitudinal side. The other side of the limbs of the partition wall forms a second longitudinal side which frames an access opening. The longitudinal sides comprise means for length adjustment. It is particularly advantageous if the passenger seat unit according to the invention makes possible more flexible and more economical use of the existing cabin area in passenger aircraft. Flexible adaptation to various cabin lengths is possible without effort.