Abstract: A drainage device for letting out a fluid that is present between the exterior skin and the interior lining of an aircraft, wherein the drainage device comprises a collecting vessel and an outlet line. The collecting vessel is designed to collect the fluid that is present between the exterior skin and the interior lining and the outlet line is connected to the collecting vessel and is designed to let out the collected fluid.

Abstract: A water deflector includes a water-diverting area and an attachment area for attachment to a seal profile. The water-diverting area and the attachment area are connected to one another via a connection area, which is elastically deformable in such a way that when force acts on the water-diverting area, it is movable in relation to the attachment area. The water deflector can be used in the area of a door, wherein the water deflector deforms when the door is closed and comes to rest in a cavity between the seal profile and the door outer skin, and assumes its starting shape again when the door is opened.

Abstract: An aircraft door includes an outer skin configured as a panel structure; and a rear body structure configured as an integral cast structure and operatively connected to the panel structure so as to provide rigidity.

Abstract: A conjunction for mounting a cross beam to a structure part of an aircraft fuselage by means of at least one conjunction device wherein the conjunction device defines a circular path on which loads acting on the cross beam are applied in the structure element.

Abstract: The present invention relates to a connecting device two curved ribs (1, 2) of an aircraft or spacecraft, with: a coupling element (5) which can be connected by means of predetermined coupling sections (6, 7) to respective connecting sections (V1, V2) of the two ribs (1, 2); wherein at least the predetermined coupling sections (6, 7) of the coupling element (5) are rectilinear Iy designed; and in that at least the respective connecting sections (Vi, V2) of the two ribs (1, 2) each have rectilinearly running inner belt regions (15) for a respective rectilinear connection of the predetermined coupling sections 16, 7) of the coupling element (5).

Abstract: According to an exemplary embodiment of the present invention, a frame member for an aircraft is provided comprising a clip region and a frame region. According to an aspect of this exemplary embodiment of the present invention, the clip region, shear web region and the frame region are integrated into the frame member and be formed from an extrusion mold by a milling process. Advantageously, this allows for a reduced number of individual elements for forming a frame member and provides the flexibility of variation of the forms and dimensions of a frame member for an aircraft.

Abstract: A drainage device for letting out a fluid that is present between the exterior skin and the interior lining of an aircraft, wherein the drainage device comprises a collecting vessel and an outlet line. The collecting vessel is designed to collect the fluid that is present between the exterior skin and the interior lining and the outlet line is connected to the collecting vessel and is designed to let out the collected fluid.

Abstract: A water deflector includes a water-diverting area and an attachment area for attachment to a seal profile. The water-diverting area and the attachment area are connected to one another via a connection area, which is elastically deformable in such a way that when force acts on the water-diverting area, it is movable in relation to the attachment area. The water deflector can be used in the area of a door, wherein the water deflector deforms when the door is closed and comes to rest in a cavity between the seal profile and the door outer skin, and assumes its starting shape again when the door is opened.

Abstract: According to an exemplary embodiment of the present invention, a frame member for an aircraft is provided comprising a clip region and a frame region. According to an aspect of this exemplary embodiment of the present invention, the clip region, shear web region and the frame region are integrated into the frame member and be formed from an extrusion mold by a milling process. Advantageously, this allows for a reduced number of individual elements for forming a frame member and provides the flexibility of variation of the forms and dimensions of a frame member for an aircraft.

Abstract: An aircraft passenger door is opened and closed by at least one door operating mechanism including a drive motor and a transmission unit that is rotatably arranged on the motor shaft and engages a toothed rack. The transmission unit includes first and second actuator gears respectively connected by first and second transmission shafts to first and second driven gears that are driven, preferably in opposite rotation directions, by a motor gear on the motor shaft. Thereby, the motor drives the actuator gears in opposite directions. The actuator gears engage the rack from opposite sides, with the rack extending between the actuator gears. Preferably, two racks are provided along the two side edges of the doorway opening, and four operating mechanisms are arranged in the door (two at each side edge thereof).

Abstract: A foot board for an aircraft passenger door has an elongated nearly quadrilateral single piece construction with an inner and an outer longitudinal edge fastened by screw bolts to an aircraft door sill structure. The foot board is constructed as a one piece or integral milled component, extending over the entire width of the door sill, with an outward slope for drainage into a drainage collecting channel that receives any water from individual drainage channels feeding into the collecting channel running along the outer longitudinal edge of the foot board, and a rib is arranged between each of two neighboring drainage channels extending perpendicularly to the collecting channel. Each of the two ends of the collecting channel empties into a collecting basin having an outlet opening for collected liquids.