FUNCTIONAL ENHANCEMENT MODULE FOR AIRCRAFT

    公开(公告)号:US20210263546A1

    公开(公告)日:2021-08-26

    申请号:US17254878

    申请日:2019-06-27

    Abstract: A functional enhancement module is for vehicles and for enhancing a functional module which is supplied with electric power via a power supply bus. The functional enhancement module is configured to be supplied with the electric power via the power supply bus. The functional enhancement module includes: a controller having a power specification for a maximum power flow of the functional module and being configured to detect a current power flow at a reference point; and a power controller configured to control a power take-up of the functional enhancement module. The controller is configured to control the power controller in accordance with the detected power flow, such that a combined power take-up of the functional module and the functional enhancement module does not exceed the power specification.

    ELECTRONIC HOUSING FOR AIRCRAFT
    2.
    发明申请

    公开(公告)号:US20210229816A1

    公开(公告)日:2021-07-29

    申请号:US17264855

    申请日:2019-08-06

    Abstract: An electronic housing houses electronics for an aircraft. The electronic housing has an outer wall surrounding an electronic receiving compartment; and fasteners on one side of the outer wall on an outer side. The fasteners are configured to engage in a snap-fit connection to a predefined raceway configured for the attachment of a cover by a snap-fit connection.

    Functional enhancement module for aircraft

    公开(公告)号:US11353906B2

    公开(公告)日:2022-06-07

    申请号:US17254878

    申请日:2019-06-27

    Abstract: A functional enhancement module is for vehicles and for enhancing a functional module which is supplied with electric power via a power supply bus. The functional enhancement module is configured to be supplied with the electric power via the power supply bus. The functional enhancement module includes: a controller having a power specification for a maximum power flow of the functional module and being configured to detect a current power flow at a reference point; and a power controller configured to control a power take-up of the functional enhancement module. The controller is configured to control the power controller in accordance with the detected power flow, such that a combined power take-up of the functional module and the functional enhancement module does not exceed the power specification.

    HOLDER FOR AN OPERATING CONSOLE IN AN AIRCRAFT SEAT
    4.
    发明申请
    HOLDER FOR AN OPERATING CONSOLE IN AN AIRCRAFT SEAT 审中-公开
    在飞机座椅上的操作控制台的持有人

    公开(公告)号:US20150021961A1

    公开(公告)日:2015-01-22

    申请号:US14382216

    申请日:2013-03-20

    Abstract: The invention relates to a holder for a control console or a display device on an aircraft seat, the holder being arranged in an armrest, backrest or the trim of the aircraft seat. The control console is removable from the holder. The holder comprises a support arm, by means of which the control console or display device can be supported, and the control console or display device which is supported on the support arm can be fixed in the holder in a secured position. The control console or display device which is supported on the support arm can be moved out of the secured position into a display position, and the control console or display device can only be removed from the support arm in the display position. The control console or display device can be pivoted about at least one pivot axis in the display position.

    Abstract translation: 本发明涉及一种用于飞机座椅上的控制台或显示装置的支架,该支架设置在飞机座椅的扶手,靠背或装饰件中。 控制台可从支架上拆下。 保持器包括支撑臂,通过该支撑臂可以支撑控制台或显示装置,并且支撑在支撑臂上的控制台或显示装置可以固定在保持器中的固定位置。 支撑在支撑臂上的控制台或显示装置可以从固定位置移动到显示位置,并且控制台或显示装置只能在显示位置从支撑臂移除。 控制台或显示装置可围绕显示位置的至少一个枢转轴线枢转。

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