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    Plant Watering Device
    3.
    发明申请
    Plant Watering Device 审中-公开

    公开(公告)号：US20170265405A1

    公开(公告)日：2017-09-21

    申请号：US15459370

    申请日：2017-03-15

    申请人： Robert Sandoval

    发明人： Robert Sandoval

    IPC分类号： A01G27/02 ,  A01G25/00

    CPC分类号： A01G27/02 ,  A01G25/00 ,  A01G25/14

    摘要： A plant watering device. The plant watering device includes an outer container having a plurality of apertures on a lower portion of a first sidewall, an inner container having a second sidewall defining and open upper end and an open lower end, wherein the second sidewall of the inner container is secured to an interior surface of the first sidewall of the outer container via a fastener; and an apron encircling an outer side of the first sidewall. The plant watering device is securable to the ground via a stake. In use, water is poured into the inner container, flows through the open lower end of the inner container to the outer container interior volume, and then exits the apertures of the outer container. This allows the water to gently diffuse around an area where a plant is planted, while the apron prevents soil erosion and damage to the plant.

    Components for gas turbine engines
    4.
    发明授权
    Components for gas turbine engines 有权
    燃气涡轮发动机部件

    公开(公告)号：US08157514B2

    公开(公告)日：2012-04-17

    申请号：US12407534

    申请日：2009-03-19

    申请人： Victor Reyes ,  Christopher Urwiller ,  Robert Sandoval ,  John Best

    发明人： Victor Reyes ,  Christopher Urwiller ,  Robert Sandoval ,  John Best

    IPC分类号： F04D29/18

    CPC分类号： F01D5/34 ,  F01D5/10 ,  F01D5/26 ,  F05D2270/114

    摘要： A component for a gas turbine engine having an engine axis includes a rotor disk and a plurality of airfoils. The rotor disk comprises a web and a rim. The web has a first outer surface at least partially defining a plurality of holes and a plurality of slots. Each of the plurality of slots extends from a corresponding one of the plurality of holes and forms a first angle with the engine axis at the point of intersection with the corresponding one of the plurality of holes. The rim has a second outer surface also at least partially defining the plurality of slots. Each of the plurality of slots forms a second angle with the engine axis at the second outer surface, the second angle being different from the first angle. Each of the plurality of airfoils extends from the second outer surface.

    摘要翻译： 具有发动机轴的燃气轮机的部件包括转子盘和多个翼型件。 转子盘包括腹板和轮缘。 幅材具有至少部分地限定多个孔和多个槽的第一外表面。 多个槽中的每一个从多个孔中的对应的一个孔延伸，并且在与多个孔中的相应一个孔的交叉点处与发动机轴线形成第一角度。 轮辋具有至少部分地限定多个槽的第二外表面。 所述多个槽中的每一个在所述第二外表面与所述发动机轴形成第二角度，所述第二角度与所述第一角度不同。 多个翼型件中的每一个从第二外表面延伸。

    Secondary flow, high pressure turbine module cooling air system for recuperated gas turbine engines
    5.
    发明申请
    Secondary flow, high pressure turbine module cooling air system for recuperated gas turbine engines 失效
    二次流量，高压汽轮机模块冷却空气系统，用于回收燃气轮机

    公开(公告)号：US20060123796A1

    公开(公告)日：2006-06-15

    申请号：US11011367

    申请日：2004-12-13

    申请人： Larry Aycock ,  John Barrett ,  Howard Becker ,  Michael Durden ,  Robert Kime ,  Brian Koch ,  Robert Sandoval

    发明人： Larry Aycock ,  John Barrett ,  Howard Becker ,  Michael Durden ,  Robert Kime ,  Brian Koch ,  Robert Sandoval

    IPC分类号： F02C6/08 ,  F02C7/10

    CPC分类号： F01D9/065 ,  F01D25/12 ,  F02C7/08 ,  F02C7/18

    摘要： A secondary flow, turbine cooling air system for the uniform cooling of high pressure turbine module components such as the turbine shroud, turbine blade tips, turbine nozzle, transion liner, and turbine bearing support housing in a recuperated gas turbine engine is provided. The secondary flow turbine cooling system provides uniform cooling air having a similar pressure and temperature in a recuperated gas turbine engine as the compressor discharge air of a non-recuperated gas turbine engine. A method for uniform cooling of high pressure turbine module components using the secondary flow turbine cooling air system is also provided.

    摘要翻译： 提供了一种二次流动的涡轮冷却空气系统，用于在再生燃气涡轮发动机中均匀冷却高压涡轮机模块部件，例如涡轮机罩，涡轮叶片尖端，涡轮喷嘴，换向衬套和涡轮轴承支撑壳体。 次级涡轮机冷却系统提供具有类似的压力和温度的均匀的冷​​却空气，其在经过再生的燃气涡轮发动机中作为压缩机排出未燃还原燃气涡轮发动机的空气。 还提供了使用二次涡轮机冷却空气系统来均匀冷却高压涡轮机组件部件的方法。

    COMPONENTS FOR GAS TURBINE ENGINES
    6.
    发明申请
    COMPONENTS FOR GAS TURBINE ENGINES 有权
    气体涡轮发动机组件

    公开(公告)号：US20100239422A1

    公开(公告)日：2010-09-23

    申请号：US12407534

    申请日：2009-03-19

    申请人： Victor Reyes ,  Christopher Urwiller ,  Robert Sandoval ,  John Best

    发明人： Victor Reyes ,  Christopher Urwiller ,  Robert Sandoval ,  John Best

    IPC分类号： F01D5/02

    CPC分类号： F01D5/34 ,  F01D5/10 ,  F01D5/26 ,  F05D2270/114

    摘要： A component for a gas turbine engine having an engine axis includes a rotor disk and a plurality of airfoils. The rotor disk comprises a web and a rim. The web has a first outer surface at least partially defining a plurality of holes and a plurality of slots. Each of the plurality of slots extends from a corresponding one of the plurality of holes and forms a first angle with the engine axis at the point of intersection with the corresponding one of the plurality of holes. The rim has a second outer surface also at least partially defining the plurality of slots. Each of the plurality of slots forms a second angle with the engine axis at the second outer surface, the second angle being different from the first angle. Each of the plurality of airfoils extends from the second outer surface.

    摘要翻译： 具有发动机轴的燃气轮机的部件包括转子盘和多个翼型件。 转子盘包括腹板和轮缘。 幅材具有至少部分地限定多个孔和多个槽的第一外表面。 多个槽中的每一个从多个孔中的对应的一个孔延伸，并且在与多个孔中的相应一个孔的交叉点处与发动机轴线形成第一角度。 轮辋具有至少部分地限定多个槽的第二外表面。 所述多个槽中的每一个在所述第二外表面与所述发动机轴形成第二角度，所述第二角度与所述第一角度不同。 多个翼型件中的每一个从第二外表面延伸。