Fully-featured minimalist backpack

    公开(公告)号:US11406170B1

    公开(公告)日:2022-08-09

    申请号:US16054117

    申请日:2018-08-03

    IPC分类号: A45F3/04 A45F3/14

    摘要: A fully-featured minimalist backpack including a back portion having at least one main pocket, a thoracic strap extending from a bottom of the back portion, and two shoulder straps extending from a top of the back portion. The shoulder straps may each be connected to a front portion of the thoracic strap. The thoracic strap may have one or more pockets. A slot for a personal electronic device may be included in the main pocket. Various configurations for retaining eyeglasses and earphone cables may be included. The thoracic strap may have distal ends that are magnetically attachable to each other. An elastic band may be located between the shoulder straps. One or more secondary or hidden pockets may be included.

    Elements of stretched false ceiling, use of same for producing false walls and false ceilings
    9.
    发明授权
    Elements of stretched false ceiling, use of same for producing false walls and false ceilings 失效
    拉伸虚假天花板的元素,使用相同的产生假墙和假天花板

    公开(公告)号:US06880302B1

    公开(公告)日:2005-04-19

    申请号:US09979246

    申请日:2000-05-20

    申请人: Marc Fontaine

    发明人: Marc Fontaine

    摘要: The invention concerns a false wall element comprising a stretched fabric in a frame with lateral edge provided with means catching the edges of said fabric, said lateral edge comprising a rigid profiled section forming a free edge curved in the plane, with curvature corresponding to that of a part of the edge of said fabric fastened on said curved edge. Said false wall elements are used for making curved stretched suspended false ceilings and stretched false walls with curved profile.

    摘要翻译: 本发明涉及一种假壁元件,其包括在框架中的拉伸织物,其侧边设置有抓住所述织物边缘的装置,所述侧边缘包括形成在平面中弯曲的自由边缘的刚性成型部分,其曲率对应于 所述织物的边缘的一部分紧固在所述弯曲边缘上。 所述假壁元件用于制造弯曲拉伸的悬浮假天花板和具有弯曲轮廓的拉伸假壁。

    System for supplying fuel to an aircraft engine
    10.
    发明授权
    System for supplying fuel to an aircraft engine 失效
    向飞机发动机供油的系统

    公开(公告)号:US4686825A

    公开(公告)日:1987-08-18

    申请号:US839545

    申请日:1986-03-14

    摘要: This invention relates to a system for supplying fuel to an aircraft engine, wherein an electronic computer subdivides the stroke of the throttle lever into a plurality of zones, in each of which the thrust of the engine varies between a maximum value and a minimum value. The computer ensures a modulation of the thrust about the value corresponding to that displayed by the position of said throttle lever. No mechanical link is provided between the lever and the fuel admission valve.

    摘要翻译: 本发明涉及一种用于向飞机发动机供应燃料的系统,其中电子计算机将节气门杆的行程分为多个区域,每个区域中发动机的推力在最大值和最小值之间变化。 计算机确保对与由所述节流杆的位置显示的值相对应的值的推力的调制。 在杠杆和燃油入口阀之间没有提供机械连杆。