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    High-Speed Airplane Deicing Installation Systems and Methods
    81.
    发明申请
    High-Speed Airplane Deicing Installation Systems and Methods 审中-公开

    公开(公告)号：US20150360799A1

    公开(公告)日：2015-12-17

    申请号：US14833564

    申请日：2015-08-24

    Applicant: Valentin Luca

    Inventor： Valentin Luca

    IPC: B64F5/00

    CPC classification number: B64F5/23 ,  B05B7/08 ,  B05B12/02 ,  B05B12/04 ,  B05B13/005 ,  B05B13/0431 ,  B05B13/0436 ,  B64D15/00 ,  B64D15/02 ,  B64D15/06 ,  B64D15/10 ,  B64F5/20 ,  Y02P70/585

    Abstract: The present disclosure provides an airplane ground deicing installation that minimizes the impact of deicing operations on the airport during icing conditions. The installation does not require alteration of a normal taxi pattern and can be performed as quickly as the average separation time between take-offs. The installation allows modification of its shape to adapt to the contour of almost all types of commercial passengers airplanes operating from major airports, and simultaneously deices large surfaces of the airplane. Deicing and anti-icing fluids are applied to airplane surfaces from nozzles positioned in close proximity to the airplane's surface. Speed and adaptability to different types of airplanes, combined with a design that allows rapid relocation of the installation, are key features that make it possible to place the installation on the taxiway, close to the head of the runway it serves, such that the taxi pattern and the separation in between takeoffs are not altered as compared to the normal operations of the airport.

    High-Speed Airplane Deicing Installation Systems and Methods
    83.
    发明申请
    High-Speed Airplane Deicing Installation Systems and Methods 审中-公开
    高速飞机除冰安装系统及方法

    公开(公告)号：US20150298826A1

    公开(公告)日：2015-10-22

    申请号：US14690087

    申请日：2015-04-17

    Applicant: Valentin Luca

    Inventor： Valentin Luca

    IPC: B64F5/00

    CPC classification number: B64F5/23 ,  B05B7/08 ,  B05B12/02 ,  B05B12/04 ,  B05B13/005 ,  B05B13/0431 ,  B05B13/0436 ,  B64D15/00 ,  B64D15/02 ,  B64D15/06 ,  B64D15/10 ,  B64F5/20 ,  Y02P70/585

    Abstract: The present disclosure provides an airplane ground deicing installation that minimizes the impact of deicing operations on the airport during icing conditions. The installation does not require alteration of a normal taxi pattern and can be performed as quickly as the average separation time between take-offs. The installation allows modification of its shape to adapt to the contour of almost all types of commercial passengers airplanes operating from major airports, and simultaneously deices large surfaces of the airplane. Deicing and anti-icing fluids are applied to airplane surfaces from nozzles positioned in close proximity to the airplane's surface. Speed and adaptability to different types of airplanes, combined with a design that allows rapid relocation of the installation, are key features that make it possible to place the installation on the taxiway, close to the head of the runway it serves, such that the taxi pattern and the separation in between takeoffs are not altered as compared to the normal operations of the airport.

    Abstract translation: 本公开提供一种飞机地面除冰装置，其在结冰条件期间最小化除冰操作对机场的影响。 安装不需要更改常规的出租车模式，可以像起飞之间的平均间隔时间一样快速地进行。 该装置允许修改其形状以适应几乎所有类型的从主要机场运行的商用乘客飞机的轮廓，并且同时设计飞机的大表面。 来自位于飞机表面附近的喷嘴的除冰和防冰流体应用于飞机表面。 不同类型的飞机的速度和适应性，以及允许快速重新安装设备的设计，是使安装在滑行道上，靠近其所提供的跑道头部成为可能的关键特征，使得出租车 与机场的正常运行相比，起飞之间的距离不会改变。

    Method and system for mixing reactor feed
    84.
    发明授权
    Method and system for mixing reactor feed 有权
    混合反应器进料的方法和系统

    公开(公告)号：US09033259B2

    公开(公告)日：2015-05-19

    申请号：US12977515

    申请日：2010-12-23

    Applicant: Krishnakumar Venkatesan ,  Ertan Yilmaz ,  Ali Ergut

    Inventor： Krishnakumar Venkatesan ,  Ertan Yilmaz ,  Ali Ergut

    IPC: B05B7/06 ,  F23D1/00 ,  B05B7/04 ,  B05B7/08 ,  C10J3/50

    CPC classification number: F23D1/005 ,  B05B7/0408 ,  B05B7/061 ,  B05B7/08 ,  B05B7/0815 ,  C10J3/50 ,  C10J2300/0959 ,  C10J2300/0976 ,  C10J2300/1653 ,  C10J2300/1678 ,  F23D1/00 ,  F23D2201/10 ,  F23D2201/30 ,  F23D2214/00 ,  Y02E20/18

    Abstract: A method and system of feeding fuel into a gasifier are provided. The feed injector system includes a first injector port assembly including a plurality of annular channels substantially concentric about a longitudinal axis that define corresponding fluid flow paths that direct a flow of fluid substantially axially therethrough from a respective source to a reaction zone and a second injector port assembly including a flow port surrounded by a plurality of auxiliary ports spaced about a circumference of the flow port, the plurality of auxiliary ports communicatively coupled to a toroidal passage configured to receive a flow of fluid and channel the flow of fluid to the auxiliary ports such that the flow of fluid is discharged from the auxiliary ports having an axial flow component, a radially inward flow component, and a circumferential flow component.

    Abstract translation: 提供了将燃料供给气化器的方法和系统。 所述进料喷射器系统包括第一喷射器端口组件，所述第一喷射器端口组件包括围绕纵向轴线基本上同心的多个环形通道，所述多个环形通道限定相应的流体流动路径，所述流体流动路径基本上从相应的源引导到反应区域， 组件包括由围绕流动端口的圆周间隔开的多个辅助端口围绕的流动端口，所述多个辅助端口可通信地联接到环形通道，该环形通道被构造成接收流体流并将流体流引导到辅助端口， 流体的流动从具有轴向流动分量，径向向内流动分量和周向流动分量的辅助端口排出。

    FUEL INJECTION NOZZLE AND METHOD OF MANUFACTURING THE SAME
    86.
    发明申请
    FUEL INJECTION NOZZLE AND METHOD OF MANUFACTURING THE SAME 有权
    燃油喷射喷嘴及其制造方法

    公开(公告)号：US20140367495A1

    公开(公告)日：2014-12-18

    申请号：US13916767

    申请日：2013-06-13

    Applicant: General Electric Company

    Inventor： James Christopher Monaghan ,  Thomas Edward Johnson ,  Heath Michael Ostebee

    IPC: F02M55/00 ,  F23R3/28

    CPC classification number: F02M55/008 ,  B05B7/04 ,  B05B7/08 ,  F02M2200/80 ,  F23R3/10 ,  F23R3/28 ,  F23R3/286 ,  Y10T29/494

    Abstract: A fuel injection head for use in a fuel injection nozzle comprises a monolithic body portion comprising an upstream face, an opposite downstream face, and a peripheral wall extending therebetween. A plurality of pre-mix tubes are integrally formed with and extend axially through the body portion. Each of the pre-mix tubes comprises an inlet adjacent the upstream face, an outlet adjacent the downstream face, and a channel extending between the inlet and the outlet. Each pre-mix tube also includes at least one fuel injector that at least partially extends outward from an exterior surface of the pre-mix tube, wherein the fuel injector is integrally formed with the pre-mix tube and is configured to facilitate fuel flow between the body portion and the channel.

    Abstract translation: 一种用于燃料喷射喷嘴的燃料喷射头包括一个整体主体部分，包括一个上游面，一个相对的下游面以及一个在其间延伸的周壁。 多个预混合管一体地形成并且轴向地穿过主体部分。 每个预混合管包括邻近上游面的入口，邻近下游面的出口和在入口和出口之间延伸的通道。 每个预混合管还包括至少一个燃料喷射器，其至少部分地从预混合管的外表面向外延伸，其中燃料喷射器与预混合管一体地形成，并且构造成促进燃料在 身体部分和通道。

    CARBON DIOXIDE SNOW EJECTING DEVICE
    87.
    发明申请
    CARBON DIOXIDE SNOW EJECTING DEVICE 审中-公开
    二氧化碳喷出装置

    公开(公告)号：US20130341427A1

    公开(公告)日：2013-12-26

    申请号：US14003618

    申请日：2012-03-05

    Applicant: Tadashi Ukawa ,  Shunichi Magome ,  Shinpei Iwamoto

    Inventor： Tadashi Ukawa ,  Shunichi Magome ,  Shinpei Iwamoto

    IPC: B05B7/14

    CPC classification number: B05B7/1486 ,  B05B7/08 ,  B05B7/0815 ,  B08B7/0092 ,  B24C1/003 ,  B24C7/0046

    Abstract: A carbon dioxide snow ejecting device is provided to achieve efficient cleaning by widely ejecting carbon dioxide snow while suppressing consumption loss of carbon dioxide gas. The device includes a carbon dioxide gas supply source for generating carbon dioxide snow, a straightened-flow gas supply source for supplying straightened-flow gas for propelling the carbon dioxide snow, a carbon dioxide snow ejection port 1, and first straightened-flow gas discharge ports 3 incliningly opposing to each other so that the carbon dioxide snow ejection port 1 is located therebetween. The device forms the ejected carbon dioxide snow in a flat shape by the effects of the straightened-flow gas. Thus, unlike conventional techniques, neither loss nor generation of particles will not be caused by the carbon dioxide snow collides the internal surface of a nozzle. Therefore, it is able to prevent situations where loss of carbon dioxide gas and poor cleaning.

    Abstract translation: 提供一种二氧化碳喷雪装置，通过在抑制二氧化碳气体的消耗损失的同时广泛喷射二氧化碳雪来实现有效的清洗。 该装置包括用于产生二氧化碳雪的二氧化碳气体供应源，用于供应用于推进二氧化碳雪的直流气体的直流气体供应源，二氧化碳排雪口1和第一直流气体排出 端口3彼此倾斜地相对，使得二氧化碳排雪口1位于它们之间。 该装置通过直流气体的作用形成平坦形状的喷出的二氧化碳雪。 因此，与常规技术不同，二氧化碳雪不会引起喷嘴的内表面的损失和产生颗粒。 因此，能够防止二氧化碳气体的损失和清洁不良的情况。

    Multipurpose Sequential Droplet Applicator
    89.
    发明申请
    Multipurpose Sequential Droplet Applicator 有权
    多用途顺序滴灌机

    公开(公告)号：US20110250103A1

    公开(公告)日：2011-10-13

    申请号：US12758771

    申请日：2010-04-12

    Applicant: Thomas Robert McCarthy

    Inventor： Thomas Robert McCarthy

    IPC: B01D11/04

    CPC classification number: B05B12/04 ,  B05B7/08 ,  B05B7/24 ,  B05B12/06 ,  B05B12/18

    Abstract: Embodiments of this device or method repeatedly apply droplets of two or more liquids in an alternate or sequential manner to a target location on a surface for removing material from the surface, adding material to the surface, or using the surface to catalyze a reaction of components of the liquids. The droplets have essentially no contact with one another before reaching the surface (FIG. 12A thru 13H). The effect of the droplets on the target surface can be modified by a continuous or interrupted flow of air or other gas to the target surface (FIG. 27A thru 29H), or by application of radiations such as sonic or ultrasonic radiation, or various frequencies of electromagnetic radiation, to the target surface, or some combination of these. Means may be included for adjusting the temperature of the liquids and gasses.

    Abstract translation: 该装置或方法的实施方案以交替或顺序的方式将两种或更多种液体的液滴重复地施加到表面上的目标位置，以从表面去除材料，向表面添加材料，或者使用该表面催化组分 的液体。 液滴在到达表面之前基本上没有彼此接触（图12A至13H）。 液滴对目标表面的影响可以通过连续或间断的空气或其他气体流向目标表面（图27A至29H）或通过施加诸如声波或超声波辐射或各种频率 的电磁辐射，到目标表面，或这些的一些组合。 可以包括用于调节液体和气体的温度的装置。

    Strand orientation alignment in strand coating systems and methods
    90.
    发明授权
    Strand orientation alignment in strand coating systems and methods 有权
    绞线涂布系统和方法中的绞线取向对准

    公开(公告)号：US07771786B2

    公开(公告)日：2010-08-10

    申请号：US11079663

    申请日：2005-03-14

    Applicant: M. Steve Lessley ,  Rico R. Valentin ,  Edward W. Bolyard

    Inventor： M. Steve Lessley ,  Rico R. Valentin ,  Edward W. Bolyard

    IPC: B05D5/10

    CPC classification number: B05B13/0207 ,  A61F13/15593 ,  B05B7/08 ,  B05C5/0241

    Abstract: A strand coating system and method including drawing (710) a strand having major and minor dimensions past an adhesive dispensing nozzle, orienting (720) at least a portion of the strand so that the major dimension of the strand is substantially parallel to a direction in which adhesive is dispensed from the adhesive dispensing nozzle as the portion of the strand is drawn past the adhesive dispensing nozzle, and applying (730) adhesive to the strand as the strand is drawn past the adhesive dispensing nozzle.

    Abstract translation: 一种股线涂布系统和方法，包括将具有主要和次要尺寸的股线绘制（710）通过粘合剂分配喷嘴，使股线的至少一部分定向（720），使得股线的主要尺寸基本上平行于 当股线的一部分被拉过粘合剂分配喷嘴时，粘合剂从粘合剂分配喷嘴分配，并且当股线被拉过粘合剂分配喷嘴时，将（730）粘合剂施加到股线上。

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