Whole blood control sample
    2.
    发明授权
    Whole blood control sample 失效
    全血控制样品

    公开(公告)号:US4731330A

    公开(公告)日:1988-03-15

    申请号:US880696

    申请日:1986-07-01

    IPC分类号: G01N33/96 G01N31/00 G01N33/86

    摘要: A whole blood control sample and a method of preparing the sample are disclosed. The method comprises collecting a whole blood sample from one or more donor, separating each sample into red blood cells and plasma, fixing the red blood cells, mixing the fixed red blood cells with plasma from the same or a different donor to produce a suspension, quick-freezing the suspension before the red blood cells can settle, and lyophilizing the frozen suspension. The control sample therefore comprises a lyophilized mixture of fixed red blood cells and plasma solids.

    摘要翻译: 公开了全血对照样品和制备样品的方法。 该方法包括从一个或多个供体收集全血样品,将每个样品分成红细胞和血浆,固定红细胞,将固定的红细胞与来自相同或不同供体的血浆混合以产生悬浮液, 在红细胞可以沉淀之前快速冷冻悬浮液,并冻结冷冻悬浮液。 因此,对照样品包含固定的红细胞和血浆固体的冻干混合物。

    Fail safe electrical brake control system for aircraft
    3.
    发明授权
    Fail safe electrical brake control system for aircraft 有权
    飞机失效安全电气制动控制系统

    公开(公告)号:US06183051B2

    公开(公告)日:2001-02-06

    申请号:US09241182

    申请日:1999-02-01

    IPC分类号: B60T886

    摘要: A brake-by-wire control system for aircraft brakes is presented. The system includes a hardware based discrete component control path and a software control path, the two operating in parallel. Each of the paths monitors the same input, with the hardware path being configured to enable the shutoff valve driver and the software path being configured to inhibit the shutoff valve driver, depending upon the status of the inputs. As a consequence, a failure in a single path in the braking system cannot enable the brake system so as to allow for inadvertent braking.

    摘要翻译: 提出了一种用于飞机制动器的线控制动控制系统。 该系统包括基于硬件的离散组件控制路径和软件控制路径,两者并行运行。 每个路径监视相同的输入,硬件路径被配置为使得切断阀驱动器和软件路径被配置为根据输入的状态来禁止截止阀驱动器。 因此,制动系统中的单个路径中的故障不能使制动系统能够无意制动。

    Razor and blade
    5.
    发明授权
    Razor and blade 失效
    剃须刀和刀片

    公开(公告)号:US5848475A

    公开(公告)日:1998-12-15

    申请号:US839260

    申请日:1997-04-17

    IPC分类号: A45D27/24 B26B21/16

    CPC分类号: B26B21/16 A45D27/24

    摘要: The invention provides a razor having a retaining mechanism adapted to receive a blade longer than the mechanism for retaining the blade so that one or both wings of the blade extend past the retaining mechanism to provide a small straight razor. Additionally, the blade is positionable within the retaining mechanism so that its wing can be extended from one or the other side of the retaining mechanism. The retaining mechanism for the blade has a pivotably-attached handle to allow ergonomic adjustment of the shaving angle. The blade and retaining mechanism have associated mechanisms for retaining and aligning the blade in the retaining mechanism.

    摘要翻译: 本发明提供了一种具有保持机构的剃刀,该保持机构适于容纳比用于保持刀片的机构更长的刀片,使得刀片的一个或两个翼片延伸超过保持机构以提供小的直的剃须刀。 此外,刀片可定位在保持机构内,使得其翼可以从保持机构的一侧或另一侧延伸。 叶片的保持机构具有可枢转地附接的手柄,以允许剃须角度的人体工程学调节。 刀片和保持机构具有用于保持和对准保持机构中的刀片的相关机构。

    Razor and blade
    6.
    发明授权
    Razor and blade 失效
    剃须刀和刀片

    公开(公告)号:US06247234B1

    公开(公告)日:2001-06-19

    申请号:US09633929

    申请日:2000-08-08

    IPC分类号: B26B2114

    CPC分类号: B26B21/28 B26B21/22

    摘要: The invention provides a razor having a retaining mechanism assembly adapted to receive more than one blade with one of the blades being capable of lateral movement beyond the confines of the retaining mechanism assembly into a straight razor configuration. The retaining mechanism assembly has components for retaining and aligning the blades both within and beyond its confines. The retaining mechanism assembly has a pivotally attached handle to allow ergonomic adjustments to the shaving angle.

    摘要翻译: 本发明提供了一种具有保持机构组件的剃刀,该保持机构组件适于容纳多于一个的叶片,其中一个叶片能够横向移动超过保持机构组件的边界直线剃须轮廓。 保持机构组件具有用于在其范围内和之外保持和对准叶片的部件。 保持机构组件具有枢转地附接的手柄,以允许对剃须角进行人体工程学调节。

    Coking tar impregnated refractory products
    8.
    发明授权
    Coking tar impregnated refractory products 失效
    焦油沥青耐火制品

    公开(公告)号:US5011802A

    公开(公告)日:1991-04-30

    申请号:US468167

    申请日:1990-01-22

    IPC分类号: C04B35/01 C04B35/101

    CPC分类号: C04B35/101 C04B35/013

    摘要: A coking process in which tar impregnated refractory products are heated in a muffle within a furnace to a temperature sufficient to cause emission or release of the volatile constituents in the tars and pitches used for impregnation, whether by decomposition or distillation, for a time which is sufficient to remove substantially all of such constituents from the products, characterized by heating the refractory products in a muffle within the furnace while maintaining a positive pressure within the muffle during the emission of the volatile constituents, and thereafter cooling the refractories in a substantially nonoxidizing atmosphere. After the temperature of the refractory products is low enough to avoid any thermal shocking of the brick the brick are removed from the furnace and the muffle.

    摘要翻译: 将焦油浸渍的耐火产品在炉内的马弗管中加热到足以引起用于浸渍的焦油和沥青中的挥发性成分的排放或释放的温度的焦化方法,无论是通过分解还是蒸馏,时间是 足以从产品中基本上除去所有这些成分,其特征在于在排出挥发性成分的同时在炉内加热马弗炉中的马弗炉中的耐火产品,同时保持马弗炉内的正压,然后在基本上非氧化气氛中冷却耐火材料 。 在耐火产品的温度足够低以避免砖的任何热冲击之后,将砖从炉和马弗炉中取出。

    Decentralized electric brake system
    9.
    发明授权
    Decentralized electric brake system 有权
    分散式电动制动系统

    公开(公告)号:US09227608B2

    公开(公告)日:2016-01-05

    申请号:US12539884

    申请日:2009-08-12

    摘要: An electric aircraft brake control system has a plurality of wheel and brake assemblies, each having a wheel, wheel speed transducer, brake assembly and a brake actuator. Electromechanical control units are uniquely associated with and connected to certain of the wheel and brake assemblies, and each of the electromechanical control units is provided with an antiskid system as an integral portion thereof. Brake data concentrators are provided for receiving data corresponding to various aircraft operational parameters, including brake pedal position, and provide operational signals to the electromechanical control unit as a function thereof. A controller for emergency and park braking is connected to the electromechanical actuator controllers through one of the brake data concentrators to effect emergency braking action on the brake assemblies, such emergency braking action having incident antiskid control. The system allows for a redundency in brake control circuitry and operation, which increases the dispatchability of an associated aircraft by ensuring continued effective operation of the aircraft even in view of a failure of one of the redundant circuits or systems. A reduction in weight is also achieve by reducing lengthy cable runs.

    摘要翻译: 电动飞机制动控制系统具有多个车轮和制动器组件,每个车轮和制动器组件具有车轮,车轮速度传感器,制动器组件和制动致动器。 机电控制单元与某些车轮和制动器组件独特地相关联并连接到其中,并且每个机电控制单元都设置有作为其整体部分的防滑系统。 提供制动数据集中器用于接收与各种飞行器操作参数对应的数据,包括制动踏板位置,并且作为其功能向机电控制单元提供操作信号。 用于紧急和停车制动的控制器通过一个制动数据集中器连接到机电致动器控制器,以对制动组件施加紧急制动作用,这种紧急制动动作具有事件防滑控制。 该系统允许在制动控制电路和操作中的冗余,其通过确保飞机的持续有效操作来增加相关飞行器的调度性,即使考虑到冗余电路或系统之一的故障。 通过减少长时间的电缆运行也可以减轻重量。

    DECENTRALIZED ELECTRIC BRAKE SYSTEM
    10.
    发明申请
    DECENTRALIZED ELECTRIC BRAKE SYSTEM 有权
    分散电动制动系统

    公开(公告)号:US20110040466A1

    公开(公告)日:2011-02-17

    申请号:US12539884

    申请日:2009-08-12

    IPC分类号: G06F17/00

    摘要: An electric aircraft brake control system has a plurality of wheel and brake assemblies, each having a wheel, wheel speed transducer, brake assembly and a brake actuator. Electromechanical control units are uniquely associated with and connected to certain of the wheel and brake assemblies, and each of the electromechanical control units is provided with an antiskid system as an integral portion thereof. Brake data concentrators are provided for receiving data corresponding to various aircraft operational parameters, including brake pedal position, and provide operational signals to the electromechanical control unit as a function thereof. A controller for emergency and park braking is connected to the electromechanical actuator controllers through one of the brake data concentrators to effect emergency braking action on the brake assemblies, such emergency braking action having incident antiskid control. The system allows for a redundency in brake control circuitry and operation, which increases the dispatchability of an associated aircraft by ensuring continued effective operation of the aircraft even in view of a failure of one of the redundant circuits or systems. A reduction in weight is also achieve by reducing lengthy cable runs.

    摘要翻译: 电动飞机制动控制系统具有多个车轮和制动器组件,每个车轮和制动器组件具有车轮,车轮速度传感器,制动器组件和制动致动器。 机电控制单元与某些车轮和制动器组件独特地相关联并连接到其中,并且每个机电控制单元都设置有作为其整体部分的防滑系统。 提供制动数据集中器用于接收与各种飞行器操作参数对应的数据,包括制动踏板位置,并且作为其功能向机电控制单元提供操作信号。 用于紧急和停车制动的控制器通过一个制动数据集中器连接到机电致动器控制器,以对制动组件施加紧急制动作用,这种紧急制动动作具有事件防滑控制。 该系统允许在制动控制电路和操作中的冗余,其通过确保飞机的持续有效操作来增加相关飞行器的调度性,即使考虑到冗余电路或系统之一的故障。 通过减少长时间的电缆运行也可以减轻重量。