Mixing container and method of filling
    1.
    发明公开
    Mixing container and method of filling 有权
    MischbehälterundFüllverfahren

    公开(公告)号:EP2025621A1

    公开(公告)日:2009-02-18

    申请号:EP08161164.2

    申请日:2008-07-25

    Inventor: Helou, Elie Jr.

    CPC classification number: B65D81/3222

    Abstract: A mixing container (10) having an outer vessel (12) with an open mouth (20) and an inner vessel (24) also with an open mouth (28) separately stores two liquids (48,50) for automatic mixing when the container (10) is opened. Upon assembly, an interior seal between the open mouth (28) of the inner vessel (24) and the bottom (16) of the outer vessel (12) is effected through placement of a closure (34) in the open mouth (20) of the outer vessel (12). The inner vessel (24) is received by a socket (40) mounted in the closure (10) which provides a resilient bias on the inner vessel (24) to force the open mouth (28) of the inner vessel (24) against the bottom (16). A method for filling the mixing container (10) includes a filling of the inner vessel (24), placement of the outer vessel (12) over the inner vessel (24), immersing at least the open mouth (20) of the outer vessel (12) into a second liquid (50) and evacuating the outer vessel (12). The mixing container (10) may then be closed to resiliently bias the open mouth (28) of the inner vessel (24) against the bottom (16) of the outer vessel (12) to effect the interior seal.

    Abstract translation: 具有具有开口(20)的外容器(12)和也具有开口(28)的内容器(24)的混合容器(10)分别存储两个用于自动混合的液体(48,50),当液体 (10)打开。 在组装时,内容器(24)的开口(28)和外容器(12)的底部(16)之间的内部密封通过将闭合件(34)放置在开口(20)中而实现, 的外部容器(12)。 内容器(24)由安装在封闭件(10)中的插座(40)容纳,该插座(40)在内容器(24)上提供弹性偏压,以迫使内容器(24)的开口(28)抵靠 底部(16)。 填充混合容器(10)的方法包括内容器(24)的填充,将外容器(12)放置在内容器(24)上,至少浸入外容器(20)的开口(20) (12)进入第二液体(50)并抽空外部容器(12)。 然后可以将混合容器(10)关闭以将内部容器(24)的开口(28)弹性地偏压抵靠外部容器(12)的底部(16),以实现内部密封。

    METHODS FOR FUEL-EFFICIENT TRANSPORTATION OF CARGO BY AIRCRAFT
    2.
    发明公开
    METHODS FOR FUEL-EFFICIENT TRANSPORTATION OF CARGO BY AIRCRAFT 有权
    VERFAHREN ZUM KRAFTSTOFFSPARENDEN FRACHTTRORTSPORT DURCH FLUGZEUGE

    公开(公告)号:EP2205484A2

    公开(公告)日:2010-07-14

    申请号:EP08848221.1

    申请日:2008-10-07

    Inventor: Helou, Elie Jr.

    Abstract: A fuel-efficient method for transporting cargo to a desired location via an aircraft. The method comprises determining the weight of the cargo capable of being transported in a single container, selecting a container having a sufficient weight capacity to support the cargo based on the determined weight of the cargo, and filing the selected container with the cargo. The filled container is loaded onto a location on the aircraft beam relative to the aircraft's CG based on the weight of the filled container to stay within the acceptable CG range for the aircraft. The filled containers having the greater weight are positioned on the beam at or adjacent to the aircraft's CG and the filled containers having lower weight are positioned farther from the aircraft's CG. The containers provide strength and rigidity to the beam to sustain the bending and torsional loads in flight.

    Abstract translation: 一种用于通过飞行器将货物运送到所需位置的节省燃料的方法。 该方法包括确定能够在单个容器中运输的货物的重量,选择具有足够重量容量的容器以基于确定的货物重量来支撑货物,以及用货物填充所选择的容器。 填充的容器基于填充的容器的重量而相对于飞机的CG装载在飞行器梁上的位置上,以保持在飞行器的可接受的CG范围内。 具有较大重量的填充容器位于飞机的CG处或邻近飞机的CG处,并且具有较小重量的填充的容器定位成远离飞行器的CG。 容器为梁提供强度和刚度,以维持飞行中的弯曲和扭转载荷。

    CARGO AIRCRAFT
    4.
    发明公开
    CARGO AIRCRAFT 有权
    FRACHTFLUGZEUG

    公开(公告)号:EP1833721A2

    公开(公告)日:2007-09-19

    申请号:EP05857018.5

    申请日:2005-11-22

    Inventor: Helou, Elie Jr.

    Abstract: In one embodiment, an aircraft for transporting at least one cargo container is disclosed. The aircraft comprises a forward fuselage, an empennage, a beam structure, and mounts to detachably and structurally engage the at least one cargo container with the beam structure. The beam structure is disposed between the forward fuselage and the empennage and the beam structure configured to receive the at least one cargo container. The beam structure and structurally engaged cargo container provide sufficient structural rigidity to support the aircraft in flight.

    Abstract translation: 在一个实施例中,公开了一种运送至少一个货物集装箱的飞机。 飞行器包括前机身,尾翼,梁结构,以及可拆卸地和结构地接合具有梁结构的至少一个货物集装箱的安装件。 梁结构设置在前机身和尾翼之间,梁结构构造成接收至少一个货物集装箱。 梁结构和结构上接合的货物集装箱提供足够的结构刚度以支持飞行中的飞机。

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