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    Combined centrifugation assembly
    1.
    发明授权
    Combined centrifugation assembly 失效
    组合离心组装

    公开(公告)号：US06234948B1

    公开(公告)日：2001-05-22

    申请号：US09509361

    申请日：2000-03-24

    申请人： Michael Yavilevich

    发明人： Michael Yavilevich

    IPC分类号： B04B502

    CPC分类号： B01L3/5021 ,  B01L2400/0633 ,  B04B5/0421

    摘要： A centrifugation assembly and a method for rapid separation of phases of a liquid, for example for blood phase separation, which comprises a rotor (10) with a holding member (12) pivotable with respect to the rotor about a pivoting axis and containing a tube (16) with a blood sample (18). The assembly comprises a device for rotating the rotor about the rotor axis and a displacing mechanism (24) to displace the common center of gravity of the holding member with the sample with respect to the pivoting axis. A stopping mechanism (22) is provided to retain the degree of inclination of the holding member during the first phase of separation. After completing the first phase of separation, the holding member takes a horizontal position to enable alignment of centrifugal force with the walls of the tube. The centrifugation assembly may have a removing device (172) for removing the caps (168) from the tubes (16) residing within the holder (102).

    摘要翻译： 离心组件和用于快速分离液相（例如用于血液分离）的方法，其包括具有保持构件（12）的转子（10），所述保持构件（12）可相对于所述转子围绕枢转轴线枢转并且包含管 （16）与血液样本（18）。 组件包括用于围绕转子轴线旋转转子的装置和移动机构（24），以使样品相对于枢转轴线移动保持构件的共同重心。 提供止动机构（22）以在分离的第一阶段期间保持保持构件的倾斜度。 在完成分离的第一阶段之后，保持构件处于水平位置，以使离心力与管的壁对准。 离心组件可以具有用于从位于保持器（102）内的管（16）移除帽（168）的移除装置（172）。

    MULTI DECK AIRCRAFT
    2.
    发明申请
    MULTI DECK AIRCRAFT 审中-公开
    多架飞机

    公开(公告)号：US20100187352A1

    公开(公告)日：2010-07-29

    申请号：US12526784

    申请日：2008-01-29

    申请人： Michael Yavilevich

    发明人： Michael Yavilevich

    IPC分类号： B64C3/00 ,  B64D11/06 ,  B64D47/00 ,  B64D37/04 ,  B64C1/22 ,  B64D45/00 ,  B64D13/02 ,  B64C1/06

    CPC分类号： B64C1/061 ,  B64C1/062 ,  B64C2001/0027 ,  B64C2001/0036 ,  B64C2001/0072 ,  B64D9/00 ,  B64D11/00 ,  B64D37/04 ,  Y02T50/43 ,  Y02T50/44 ,  Y02T50/46

    摘要： The invention relates to multi deck passenger aircraft, having passenger cabins and/or service facilities arranged on the upper and lower deck and inner load bearing cell structure provided within aircraft body. The present invention is also directed toward methods for manufacturing derivative multi deck aircrafts. Energy absorbing, floatable cargo containers (24) attached to fuselage belly. External fuel tanks (26) displaced on the top of fuselage. Center wing region of the fuselage is using for arranging rows of seats and service facilities. Addition seating configuration for narrow and wide bodied aircraft is provided. Multi deck seating configuration significantly reduces per passenger operating cost over existing technology. Less fuel per passenger is required since there is less airframe weight and wetted area per passenger. Due to the lower overall cost per passenger seat within the multi deck seating structure, the net profit and return on investment in the aircraft are also increased.

    摘要翻译： 本发明涉及多层乘客机，其具有布置在飞机机体内的上下甲板和内承重单元结构的客舱和/或服务设施。 本发明还涉及制造衍生多层飞机的方法。 能量吸收，可浮动的货物集装箱（24），附在机身的腹部。 外部燃料箱（26）在机身顶部移动。 机身的中心翼区域用于排列座椅和服务设施。 提供了狭窄和宽体积飞机的增加座椅配置。 多层座椅配置大大降低了乘客运营成本，超过现有技术。 需要较少的乘客燃料，因为每个乘客的机身重量和湿润面积较小。 由于多座位座椅结构中乘客座位的总体成本较低，飞机的净利润和投资回报率也有所增加。