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    Surgical system having manifolds with integral pneumatic accumulators
    3.
    发明授权
    Surgical system having manifolds with integral pneumatic accumulators 有权
    外科系统具有集成式气动蓄能器

    公开(公告)号：US09180232B2

    公开(公告)日：2015-11-10

    申请号：US11455490

    申请日：2006-06-19

    Applicant: David L. Williams ,  Michael Bowman

    Inventor： David L. Williams ,  Michael Bowman

    IPC: A61M1/00 ,  A61F9/007

    CPC classification number: A61M1/0058 ,  A61F9/00736 ,  A61M2205/123

    Abstract: A surgical system having all of the various pneumatic control sub-systems or sub-manifolds integrally mounted on a common primary manifold. The various required control mechanisms such as valves are likewise integrally mounted to the common manifold and to the sub-manifolds. Within any or all of the sub-manifolds or primary manifolds, volumes of material not necessary for the operation of the manifold are carved or pocketed out and used to form integral accumulators for storing extra pressurized air. The volume of the accumulator can vary according to the pressurized air requirement of the particular manifold, or the overall pneumatic system.

    Abstract translation: 具有整体安装在公共主歧管上的所有各种气动控制子系统或子歧管的手术系统。 各种所需的控制机构（例如阀）同样整体地安装在公共歧管和子歧管上。 在任何一个或所有的子歧管或主歧管中，对于歧管的操作而言不必要的体积的体积被雕刻或者包装出来并用于形成用于存储额外的加压空气的整体式蓄能器。 蓄能器的体积可以根据特定歧管或整个气动系统的加压空气需求而变化。

    Surgical system having manifolds with integral pneumatic accumulators
    5.
    发明申请
    Surgical system having manifolds with integral pneumatic accumulators 有权
    外科系统具有集成式气动蓄能器

    公开(公告)号：US20070270735A1

    公开(公告)日：2007-11-22

    申请号：US11455490

    申请日：2006-06-19

    Applicant: David L. Williams ,  Michael Bowman

    Inventor： David L. Williams ,  Michael Bowman

    IPC: A61M1/00

    CPC classification number: A61M1/0058 ,  A61F9/00736 ,  A61M2205/123

    Abstract: A surgical system having all of the various pneumatic control sub-systems or sub-manifolds integrally mounted on a common primary manifold. The various required control mechanisms such as valves are likewise integrally mounted to the common manifold and to the sub-manifolds. Within any or all of the sub-manifolds or primary manifolds, volumes of material not necessary for the operation of the manifold are carved or pocketed out and used to form integral accumulators for storing extra pressurized air. The volume of the accumulator can vary according to the pressurized air requirement of the particular manifold, or the overall pneumatic system.

    Abstract translation: 具有整体安装在公共主歧管上的所有各种气动控制子系统或子歧管的手术系统。 各种所需的控制机构（例如阀）同样整体地安装在公共歧管和子歧管上。 在任何一个或所有的子歧管或主歧管中，对于歧管的操作而言不必要的体积的体积被雕刻或者包装出来并用于形成用于存储额外的加压空气的整体式蓄能器。 蓄能器的体积可以根据特定歧管或整个气动系统的加压空气需求而变化。

    Systems and methods of reducing NOx emissions in gas turbine systems and internal combustion engines
    6.
    发明申请
    Systems and methods of reducing NOx emissions in gas turbine systems and internal combustion engines 失效
    减少燃气轮机系统和内燃机NOx排放的系统和方法

    公开(公告)号：US20070220896A1

    公开(公告)日：2007-09-27

    申请号：US11388466

    申请日：2006-03-24

    Applicant: Balachandar Varatharajan ,  Chellappa Balan ,  Michael Bowman

    Inventor： Balachandar Varatharajan ,  Chellappa Balan ,  Michael Bowman

    IPC: F02C1/00

    CPC classification number: F02C1/002 ,  F02C3/20 ,  F05D2270/082 ,  Y02T50/677

    Abstract: A gas turbine systems of reducing NOx emissions and enhancing operability comprises a compressor; a combustor disposed downstream of and in fluid communication with the compressor; a turbine assembly disposed down stream of and in fluid communication with the combustor; an oxygen-enriched gas source disposed in selective fluid communication with the compressor, the combustor, or a combination of the foregoing, wherein the oxygen-enriched gas source is a pressure swing absorption system, an electrolyzer, or a membrane reactor.

    Abstract translation: 一种减少NO x排放和提高可操作性的燃气轮机系统包括压缩机; 设置在压缩机下游并与压缩机流体连通的燃烧器; 涡轮组件，其布置在燃烧器的下游并与燃烧器流体连通; 设置成与压缩机，燃烧器或前述的组合选择性流体连通的富氧气体源，其中富氧气体源是变压吸收系统，电解器或膜反应器。

    AIRCRAFT SECONDARY ELECTRIC LOAD CONTROLLING SYSTEM
    9.
    发明申请
    AIRCRAFT SECONDARY ELECTRIC LOAD CONTROLLING SYSTEM 审中-公开
    飞机二次电力负荷控制系统

    公开(公告)号：US20050006954A1

    公开(公告)日：2005-01-13

    申请号：US10604189

    申请日：2003-06-30

    Applicant: Michael Bowman ,  Farhad Nozari ,  Thomas Currier

    Inventor： Michael Bowman ,  Farhad Nozari ,  Thomas Currier

    IPC: B60L1/00 ,  B64D31/00 ,  B64D41/00 ,  H02J1/14 ,  H02J3/00

    CPC classification number: H02J1/14 ,  B64D41/00 ,  B64D2221/00 ,  Y02T50/44

    Abstract: A method of controlling electrical load power consumption during operation of an aircraft (12) includes determining current operating conditions of the aircraft (12). An engine secondary power extraction limit is determined in response to the current operating conditions. Engine secondary power extraction is determined. Multiple secondary loads (18) are operated in response to the engine secondary power extraction limit and the engine secondary power extraction.

    Abstract translation: 一种在飞行器（12）的操作期间控制电负载功率消耗的方法包括确定飞行器（12）的当前操作条件。 根据当前的运行条件确定发动机次级功率提取极限。 发动机二次电力提取确定。 多次次级负载（18）响应于发动机二级功率提取极限和发动机二级功率提取而运行。

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