Abstract:
A shower drainage outlet for a shower tub in an aircraft is stated, which shower drainage outlet comprises three parts that can be displaced, angled or rotated in relation to one another. In this way horizontal, vertical and angular tolerances can be compensated for. Furthermore, the shower drainage outlet is designed to be inserted through an opening in the floor region of the aircraft.
Abstract:
A device to diagnose a vacuum system comprises a pipe with a first opening that can be closed by a hingeable cover, and a second opening that is designed to establish a pressure-proof connection to the vacuum system. The diagnostic device may be operated in a volume-flow mode in which the cover is open in order to determine a volume flow in the base body, and in a negative-pressure mode in which the cover is closed so as to allow to draw conclusions about the available pressure difference.
Abstract:
The present invention relates to an arrangement of line connections for installations in an aircraft passenger cabin. The arrangement comprises a line connection element for accommodating several line connections; wherein the line connection element has a fixed position in the floor grid; wherein the line connections are adaptable to system lines of aircraft systems; and wherein the installations are adaptable by way of flexible inlet lines on the line connection element.
Abstract:
A closing device for a vacuum user system or vacuum toilet system of an aircraft that makes it possible to quickly open and close a pipe connection piece in a vacuum user system or in a vacuum toilet system of an aircraft. The closing device comprises a cover; a closing element that can be inserted into the pipe connection piece and is connected to the cover by a spacer and is designed such that it substantially fully covers a cross section of the pipe connection piece; a sealing bellows located between the cover and the closing element and that at least partly encloses the spacer, wherein the sealing bellows comprises a sealing face; and an element that is movable in relation to the cover, which element is movable from a first position to a second position, wherein the movable element engages the sealing bellows such that the sealing face of the sealing bellows in the second position has a greater extension in a plane across the spacer than it does in the first position.