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    SOLAR COOLING, HEATING AND POWER SYSTEM
    2.
    发明申请
    SOLAR COOLING, HEATING AND POWER SYSTEM 有权
    太阳能冷却，加热和电力系统

    公开(公告)号：US20140125060A1

    公开(公告)日：2014-05-08

    申请号：US14127310

    申请日：2012-06-04

    申请人： Michael K. Sahm

    发明人： Michael K. Sahm

    IPC分类号： F03G6/06 ,  F01D15/10 ,  F25B27/00

    CPC分类号： F03G6/06 ,  F01D15/10 ,  F03G6/001 ,  F03G6/065 ,  F03G6/067 ,  F22B1/006 ,  F25B27/002 ,  Y02B10/20 ,  Y02E10/46

    摘要： A solar energy driven power generation system includes a solar energy receiver configured to collect solar energy. A vapor generator is operably connected to the solar energy receiver. A vapor turbine is operably connected to the vapor generator and is configured to be driven by a flow of vapor from the vapor generator. An electrical power generator is operably connected to the vapor turbine and driven thereby. A thermal conditioning system is operably connected to the vapor turbine and is driven by a flow of output vapor or hot liquid from the vapor turbine. A method of power generation includes collecting solar thermal energy and generating vapor utilizing the solar thermal energy. A vapor turbine is driven by the vapor and electrical power is produced via the rotation of the vapor turbine. Output vapor from the vapor turbine is utilized to drive a thermal conditioning system.

    摘要翻译： 太阳能驱动发电系统包括被配置为收集太阳能的太阳能接收器。 蒸汽发生器可操作地连接到太阳能接收器。 蒸汽涡轮机可操作地连接到蒸汽发生器，并被构造成由蒸汽发生器的蒸气流驱动。 电力发电机可操作地连接到蒸气涡轮并由此驱动。 热调节系统可操作地连接到蒸汽涡轮机，并且由来自蒸汽涡轮机的输出蒸气或热液体的流动驱动。 一种发电方法包括利用太阳能热能收集太阳能热能并产生蒸气。 蒸汽涡轮机由蒸气驱动，并且通过蒸汽涡轮机的旋转产生电力。 来自蒸汽涡轮机的输出蒸汽用于驱动热调节系统。

    Vapor compression cycle environmental control system
    4.
    发明授权
    Vapor compression cycle environmental control system 有权
    蒸汽压缩循环环境控制系统

    公开(公告)号：US06663044B1

    公开(公告)日：2003-12-16

    申请号：US10251719

    申请日：2002-09-20

    申请人： Jules Ricardo Munoz ,  Luca Bertuccioli ,  Michael K. Sahm ,  Jay Fletcher ,  Charles E. Lents ,  Richard Welch ,  Steve Squier ,  Arthur Chris Becker

    发明人： Jules Ricardo Munoz ,  Luca Bertuccioli ,  Michael K. Sahm ,  Jay Fletcher ,  Charles E. Lents ,  Richard Welch ,  Steve Squier ,  Arthur Chris Becker

    IPC分类号： B64D1100

    CPC分类号： B64D13/06 ,  B64D2013/0607 ,  B64D2013/0618 ,  B64D2013/0644 ,  B64D2013/0648 ,  Y02T50/56

    摘要： The present invention relates to a vapor compression cycle environmental control system for use on aircraft. The system includes an environmental control subsystem which supplies pressurized ram air at a desired temperature to the aircraft's flight deck and/or cabin. The environmental control subsystem uses a vapor compression cycle subsystem to provide the ram air at the desired temperature. The system further includes an air turbine driven by engine bleed air to provide power to an aircraft mounted accessory drive and to provide heated air to an anti-ice system. The aircraft mounted accessory drive provides power to an air compressor which forms part of the environmental control subsystem and to a working fluid compressor which forms part of the vapor compression cycle subsystem.

    摘要翻译： 本发明涉及一种用于飞机上的蒸汽压缩循环环境控制系统。 该系统包括环境控制子系统，其将期望温度的加压冲压空气供应到飞行器的驾驶舱和/或舱室。 环境控制子系统使用蒸汽压缩循环子系统来提供在所需温度下的冲压空气。 该系统还包括由发动机排放空气驱动的空气涡轮机，以向飞机安装的附件驱动器提供动力，并将热空气提供给防冰系统。 飞机安装的附件驱动器为形成环境控制子系统的一部分的空气压缩机和形成蒸气压缩循环子系统的一部分的工作流体压缩机提供动力。

    Arrangement for controlling fluid jets injected into a fluid stream
    6.
    发明授权
    Arrangement for controlling fluid jets injected into a fluid stream 有权
    用于控制注入流体流中的流体射流的布置

    公开(公告)号：US08015827B2

    公开(公告)日：2011-09-13

    申请号：US12142957

    申请日：2008-06-20

    申请人： Fabio R. Bertolotti ,  David S. Liscinsky ,  Vincent C. Nardone ,  Daniel R. Sabatino ,  Michael K. Sahm ,  Bernd R. Noack

    发明人： Fabio R. Bertolotti ,  David S. Liscinsky ,  Vincent C. Nardone ,  Daniel R. Sabatino ,  Michael K. Sahm ,  Bernd R. Noack

    IPC分类号： F02C6/04

    CPC分类号： F02K1/28 ,  F01D5/145 ,  F02C6/08 ,  F02K1/38 ,  F02K1/46 ,  F23D14/583 ,  Y02T50/673 ,  Y10T137/0329

    摘要： In an air mixing arrangement wherein a primary fluid is introduced through an opening in a wall to be mixed with a secondary fluid flowing along the wall surface, the opening is airfoil shaped with its leading edge being orientated at an attack angle with respect to the secondary fluid flow stream so as to thereby enhance the penetration and dispersion of the primary fluid stream into the secondary fluid stream. The airfoil shaped opening is selectively positioned such that its angle of attack provides the desired lift to optimize the mixing of the two streams for the particular application. In one embodiment, a collar is provided around the opening to prevent the secondary fluid from contacting the surface of the wall during certain conditions of operation. Multiple openings maybe used such as the combination of a larger airfoil shaped opening with a smaller airfoil shaped opened positioned downstream thereof, or a round shaped opening placed upstream of an airfoil shaped opening. Pairs of openings and associated collars maybe placed in symmetric relationship so as to promote mixing in particular applications, and nozzles maybe placed on the inner side of wall to enhance the flow characteristics of the primary fluid.

    摘要翻译： 在空气混合装置中，其中主要流体通过壁中的开口引入以与沿着壁表面流动的次级流体混合，所述开口是翼型，其前缘相对于次级 流体流动，从而增强初级流体流进入次级流体流的渗透和分散。 翼型开口被选择性地定位成使得其迎角提供所需的升力以优化用于特定应用的两个流的混合。 在一个实施例中，围绕开口设置套环，以防止在某些操作条件下次要流体接触壁的表面。 可以使用多个开口，例如较大的翼型形状的开口与位于其下游的较小的翼型形状的组合，或者设置在翼型形状的开口的上游的圆形开口。 一对开口和相关的套环可以放置在对称关系中，以促进特定应用中的混合，并且喷嘴可以放置在壁的内侧以增强初级流体的流动特性。

    Electric power and cooling system for an aircraft
    8.
    发明授权
    Electric power and cooling system for an aircraft 有权
    飞机电力和冷却系统

    公开(公告)号：US06845630B2

    公开(公告)日：2005-01-25

    申请号：US10077281

    申请日：2002-02-14

    申请人： Louis J. Bruno ,  Charles E. Lents ,  Michael K. Sahm ,  Wayne A. Thresher

    发明人： Louis J. Bruno ,  Charles E. Lents ,  Michael K. Sahm ,  Wayne A. Thresher

    IPC分类号： B64D13/06 ,  F25D9/00 ,  B64D13/02

    CPC分类号： B64D13/06 ,  B64D2013/064 ,  B64D2013/0644 ,  Y02T50/56

    摘要： The present invention relates to an electrical power and cooling system for use in an aircraft having at least one engine. The electrical power and cooling system comprises a single shaft, a power turbine mounted on the shaft for receiving fresh pressurized air from the at least one engine, a cooling turbine mounted on the shaft and receiving the fresh pressurized air from the at least one engine, a generator mounted on the shaft, and a fan mounted on the shaft for creating a flow of cooling air. The system further has a condenser for removing moisture from the air exiting the cooling turbine and a mixing chamber for mixing the cooled dry air with recirculated cabin air. The electrical power and cooling system delivers conditioned air to a cabin and/or a flight deck onboard the aircraft and electrical power to the aircraft's electrical systems.

    摘要翻译： 本发明涉及一种用于具有至少一个发动机的飞行器中的电力和冷却系统。 电力和冷却系统包括单个轴，安装在轴上的动力涡轮机，用于接收来自至少一个发动机的新鲜加压空气;安装在轴上的冷却涡轮机，以及接收来自至少一个发动机的新鲜加压空气， 安装在轴上的发电机和安装在轴上的风扇，用于产生冷却空气流。 该系统还具有用于从离开冷却涡轮机的空气中除去水分的冷凝器和用于将冷却的干燥空气与再循环的机舱空气混合的混合室。 电力和冷却系统向飞机上的舱室和/或飞行甲板提供调节空气，并向飞机的电气系统提供电力。

    Aircraft architecture with a reduced bleed aircraft secondary power system
    9.
    发明授权
    Aircraft architecture with a reduced bleed aircraft secondary power system 有权
    飞机架构与减少飞机二次电力系统

    公开(公告)号：US06704625B2

    公开(公告)日：2004-03-09

    申请号：US10076898

    申请日：2002-02-14

    申请人： Jose Albero ,  Charles E. Lents ,  Michael K. Sahm ,  Richard C. Welch

    发明人： Jose Albero ,  Charles E. Lents ,  Michael K. Sahm ,  Richard C. Welch

    IPC分类号： B64B124

    CPC分类号： F02C7/32 ,  B64D13/06 ,  B64D2013/0611 ,  B64D2013/0618 ,  B64D2013/064 ,  B64D2013/0644 ,  Y02T50/54 ,  Y02T50/56

    摘要： The present invention relates to an improved architecture for an aircraft. The aircraft has a first engine, a first gearbox associated with the first engine, a first starter/generator associated with the gearbox, and a first motor drive connected to the first starter/generator for providing the starter/generator with electric power to start the first engine and to receive electric power from the starter/generator after the engine has been started to operate electrically driven systems onboard the aircraft. The aircraft preferably further has at least one other engine which has a gearbox and a starter/generator associated with it and at least a second motor drive connected to the starter/generator. The electrically driven systems operated by the motor drive(s) include an environmental control system, a wing anti-icing system, an aircraft control system, and the aircraft fuel system. The aircraft also includes an auxiliary power unit for supplying electrical power to at least the first motor drive for initiating operation of the first engine.

    摘要翻译： 本发明涉及一种用于飞机的改进的架构。 飞机具有第一发动机，与第一发动机相关联的第一变速箱，与变速箱相关联的第一起动/发电机，以及连接到第一起动器/发电机的第一电动机驱动器，用于向起动器/发电机提供电力以启动 第一发动机，并且在发动机起动之后从起动器/发电机接收电力来操作飞机上的电驱动系统。 飞机优选地还具有至少一个其它发动机，其具有齿轮箱和与其相关联的起动器/发电机以及连接到起动器/发电机的至少第二马达驱动器。 由电动机驱动器操作的电驱动系统包括环境控制系统，机翼防冰系统，飞机控制系统和飞机燃料系统。 该飞机还包括辅助动力单元，用于向至少第一马达驱动器提供电力以启动第一发动机的操作。

    Diffuser guide vanes for high-speed screw compressor
    10.
    发明授权
    Diffuser guide vanes for high-speed screw compressor 失效
    用于高速螺旋压缩机的扩散器导叶

    公开(公告)号：US06672856B1

    公开(公告)日：2004-01-06

    申请号：US10187165

    申请日：2002-06-28

    申请人： H. Ezzat Khalifa ,  Michael K. Sahm

    发明人： H. Ezzat Khalifa ,  Michael K. Sahm

    IPC分类号： F04C1816

    CPC分类号： F04C29/12 ,  F04C18/16 ,  F04C2240/10 ,  F04C2250/102

    摘要： A screw compressor includes a housing containing at least one rotor for generating a discharge flow in a discharge flow direction; a diffuser communicated with the housing and having a collecting portion for receiving the discharge flow, a diffuser throat and a diffuser portion, said diffuser extending from the housing in a diffuser direction; and at least one turning vane positioned in the collecting portion and adapted to guide flow from the discharge flow direction to the diffuser direction.

    摘要翻译： 螺杆式压缩机包括容纳至少一个用于在排出流动方向产生排放流的转子的壳体; 与所述壳体连通并具有用于接收排出流的收集部分的扩散器，扩散器喉部和扩散器部分，所述扩散器从所述壳体沿扩散器方向延伸; 以及至少一个转动叶片，其定位在收集部分中并且适于引导从排出流动方向到扩散器方向的流动。