Shower drainage outlet in aircraft
    11.
    发明申请
    Shower drainage outlet in aircraft 有权
    飞机淋浴排水口

    公开(公告)号:US20070204397A1

    公开(公告)日:2007-09-06

    申请号:US11699222

    申请日:2007-01-29

    CPC classification number: B64D11/02 E03C1/20 E03C1/264 Y10S4/14

    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 translation: 说明了一种用于飞机上的淋浴盆的淋浴排水口,哪个淋浴排水口包括可相对于彼此移动,成角度或旋转的三个部分。 这样可以补偿水平,垂直和角度公差。 此外,淋浴排水出口设计成通过飞机地板区域中的开口插入。

    DEVICE AND METHOD TO DIAGNOSE VACUUM SYSTEMS
    12.
    发明申请
    DEVICE AND METHOD TO DIAGNOSE VACUUM SYSTEMS 有权
    诊断真空系统的设备和方法

    公开(公告)号:US20070199139A1

    公开(公告)日:2007-08-30

    申请号:US11627178

    申请日:2007-01-25

    CPC classification number: E03F1/006 B64F5/60

    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 translation: 用于诊断真空系统的装置包括具有可由可铰接盖封闭的第一开口的管和设计成建立与真空系统的耐压连接的第二开口。 诊断装置可以在其中盖打开的体积流动模式下操作,以便确定基体中的体积流量,并且在封闭盖的负压模式中,以便得出结论 关于可用的压力差。

    Closing device for a vacuum user system of an aircraft
    14.
    发明申请
    Closing device for a vacuum user system of an aircraft 有权
    飞机真空用户系统关闭装置

    公开(公告)号:US20080179561A1

    公开(公告)日:2008-07-31

    申请号:US12008981

    申请日:2008-01-15

    CPC classification number: B64D11/02 F16K7/20

    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.

    Abstract translation: 用于飞机的真空用户系统或真空吸尘器系统的关闭装置,其能够快速地打开和关闭真空用户系统或飞机的真空马桶系统中的管道连接件。 关闭装置包括盖子; 封闭元件,其可以插入到管连接件中并且通过间隔件连接到盖,并且被设计成使得其基本上完全覆盖管连接件的横截面; 密封波纹管,其位于所述盖和所述封闭元件之间并且至少部分地包围所述间隔件,其中所述密封波纹管包括密封面; 以及可相对于所述盖移动的元件,所述元件可从第一位置移动到第二位置,其中所述可移动元件与所述密封波纹管接合,使得所述密封波纹管在所述第二位置的密封面具有更大的延伸 在跨越间隔物的平面上,而不是在第一位置。

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