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    • 1. 发明授权
    • Compact, modularized air conditioning system that can be mounted upon an airplane ground support equipment cart
    • 紧凑的模块化空调系统,可安装在飞机地面支撑设备推车上
    • US08117864B2
    • 2012-02-21
    • US12250504
    • 2008-10-13
    • Jeffrey E. MontminyKyta InsixiengmayJames W. Mann, IIIBenjamin E. NewellTy A. Newell
    • Jeffrey E. MontminyKyta InsixiengmayJames W. Mann, IIIBenjamin E. NewellTy A. Newell
    • F25D17/06
    • B64F1/364
    • A modular and compact air conditioning system is designed to be conveyed by a ground support equipment cart and to occupy minimal space within the cart. The system is constructed within a rectangular frame supporting top, bottom, left side, right side, front side, and back side panels. The top and back side panels contain thin air conditioner condensers. One of the left and right side panels contain an air outlet, and the other contains an air inlet and a duct that may be connected to an airplane to provide cooling air to the airplane. A condenser fan is mounted within the rectangular frame and is arranged to draw outside air in through the condensers and to blow the air out through the air outlet. First and second air conditioners are mounted within the rectangular frame, each including a compressor, an expansion valve, and evaporator coils, with each compressor pumping refrigerant through one of the condensers, through one of the expansion valves, and through one of the evaporator coils and back to the compressor. One of the two evaporator coils is mounted over the air inlet, and the other is mounted over the duct. A variable speed blower is mounted within the rectangular frame adjacent the air inlet, and an enclosed air passage routes air from the air inlet through one of the evaporator coils, the air passage narrowing and routing the air through the blower, the passage then widening and curving around and routing the air through the other of the evaporator coils and through the duct.
    • 模块化和紧凑型空调系统设计为由地面支撑设备推车输送并占据车内最小的空间。 该系统构造在支撑顶部,底部,左侧,右侧,前侧和后侧面板的矩形框架内。 顶部和背面板包含薄型空调冷凝器。 左侧板和右侧板中的一个包含空气出口,另一个包含空气入口和可以连接到飞机以向飞机提供冷却空气的管道。 冷凝器风扇安装在矩形框架内,并布置成通过冷凝器抽吸外部空气并将空气吹出空气出口。 第一和第二空调安装在矩形框架内,每个包括压缩机,膨胀阀和蒸发器盘管,每个压缩机通过一个膨胀阀将制冷剂泵送通过一个冷凝器,并通过一个蒸发器盘管 并回到压缩机。 两个蒸发器盘管中的一个安装在空气入口上,另一个安装在管道上。 变速鼓风机安装在与空气入口相邻的矩形框架内,封闭的空气通道将空气从空气入口通过一个蒸发器盘管,空气通道变窄并使空气通过鼓风机,通道然后变宽, 绕过并绕过空气通过另一个蒸发器盘管并通过管道。
    • 2. 发明申请
    • COMPACT, MODULARIZED AIR CONDITIONING SYSTEM THAT CAN BE MOUNTED UPON AN AIRPLANE GROUND SUPPORT EQUIPMENT CART
    • 紧凑的,可以安装在AIRPLANE地面支持设备上的模块化空调系统
    • US20090107160A1
    • 2009-04-30
    • US12250504
    • 2008-10-13
    • Jeffrey E. MontminyKyta InsixiengmayJames W. Mann, IIIBenjamin E. NewellTy A. Newell
    • Jeffrey E. MontminyKyta InsixiengmayJames W. Mann, IIIBenjamin E. NewellTy A. Newell
    • B60H1/32F25D17/06F25B1/00F25D21/00
    • B64F1/364
    • A modular and compact air conditioning system is designed to be conveyed by a ground support equipment cart and to occupy minimal space within the cart. The system is constructed within a rectangular frame supporting top, bottom, left side, right side, front side, and back side panels. The top and back side panels contain thin air conditioner condensers. One of the left and right side panels contain an air outlet, and the other contains an air inlet and a duct that may be connected to an airplane to provide cooling air to the airplane. A condenser fan is mounted within the rectangular frame and is arranged to draw outside air in through the condensers and to blow the air out through the air outlet. First and second air conditioners are mounted within the rectangular frame, each including a compressor, an expansion valve, and evaporator coils, with each compressor pumping refrigerant through one of the condensers, through one of the expansion valves, and through one of the evaporator coils and back to the compressor. One of the two evaporator coils is mounted over the air inlet, and the other is mounted over the duct. A variable speed blower is mounted within the rectangular frame adjacent the air inlet, and an enclosed air passage routes air from the air inlet through one of the evaporator coils, the air passage narrowing and routing the air through the blower, the passage then widening and curving around and routing the air through the other of the evaporator coils and through the duct.
    • 模块化和紧凑型空调系统设计为由地面支撑设备推车输送并占据车内最小的空间。 该系统构造在支撑顶部,底部,左侧,右侧,前侧和后侧面板的矩形框架内。 顶部和背面板包含薄型空调冷凝器。 左侧板和右侧板中的一个包含空气出口,另一个包含空气入口和可以连接到飞机以向飞机提供冷却空气的管道。 冷凝器风扇安装在矩形框架内,并布置成通过冷凝器抽吸外部空气并将空气吹出空气出口。 第一和第二空调安装在矩形框架内,每个包括压缩机,膨胀阀和蒸发器盘管,每个压缩机通过一个膨胀阀将制冷剂泵送通过一个冷凝器,并通过一个蒸发器盘管 并回到压缩机。 两个蒸发器盘管中的一个安装在空气入口上,另一个安装在管道上。 变速鼓风机安装在与空气入口相邻的矩形框架内,封闭的空气通道将空气从空气入口通过一个蒸发器盘管,空气通道变窄并使空气通过鼓风机,通道然后变宽, 绕过并绕过空气通过另一个蒸发器盘管并通过管道。
    • 3. 发明授权
    • Refractive index sensor using internally reflective light beams
    • 折射率传感器使用内部反射光束
    • US07271883B2
    • 2007-09-18
    • US11168151
    • 2005-06-28
    • Benjamin E. NewellTy A. Newell
    • Benjamin E. NewellTy A. Newell
    • G01N21/00
    • G01N21/43
    • A sensor system comprised of a diffuse light source and a sensor mounted on a transparent layer of material that is adjacent to a fluid. The refractive index of the transparent layer is greater than the refractive index of the fluid, causing a portion of the diffuse light source to be reflected from the interface of the transparent layer and the adjacent fluid. A sensor is placed at a location to intercept the reflected light. The diffuse light source and the sensor are optically coupled to the transparent layer with a transparent material wit a refractive index greater than that of the fluid. A light absorbing coating is placed ante surface of the transparent layer in order to absorb extraneous light from internal scattering of light from the fluid and light external to the sensor system.
    • 传感器系统,包括漫射光源和安装在与流体相邻的透明材料层上的传感器。 透明层的折射率大于流体的折射率,导致漫射光源的一部分从透明层和相邻流体的界面反射。 将传感器放置在一个位置以拦截反射光。 漫射光源和传感器以透明材料光学耦合到透明层,折射率大于流体的折射率。 将光吸收涂层放置在透明层的前表面上,以便吸收来自流体的光的内部散射和传感器系统外部的光的外来光。
    • 4. 发明授权
    • Adjustable air conditioning control system for a universal airplane ground support equipment cart
    • 可调式空调控制系统,用于通用飞机地面支撑设备推车
    • US08037714B2
    • 2011-10-18
    • US12250503
    • 2008-10-13
    • James W. Mann, IIIJeffrey E. MontminyBenjamin E. NewellTy A. Newell
    • James W. Mann, IIIJeffrey E. MontminyBenjamin E. NewellTy A. Newell
    • F25B41/00
    • B64F1/364
    • A ground support equipment air conditioning system detachably connects to a port on an airplane. An air conduit connects an air intake and filter to a coupling that is adapted to be connected to one end of an air duct or hose the other end of which is adapted to be connected to an airplane's port. A variable speed blower in the air conduit has its speed varied by a controller to regulate the pressure supplied to an airplane. This controller receives as inputs the pressure sensed by a pressure sensor connected to the air conduit adjacent the coupling to sense the pressure of air passing into the airplane and also a setpoint pressure which can be varied to match the requirements of different types or classes of airplane. First and second air conditioners each include a circular refrigerant conduit channeling refrigerant through a compressor, a condenser, an expansion valve, and an evaporator. The evaporators are positioned in the air conduit with the first air conditioner's evaporator preceding the blower and the second air conditioner's evaporator following the blower in the air conduit. A condenser cooling fan drives air through the two condensers and is controlled by a controller responsive to one or more pressures or temperatures measured in one of the air or refrigerant conduits or in the surrounding air.
    • 地面支持设备空调系统可拆卸地连接到飞机上的端口。 空气管道将进气口和过滤器连接到适于连接到空气管道或软管的一端的联接器,其另一端适于连接到飞机的端口。 空气管道中的变速鼓风机的速度由控制器变化,以调节供应给飞机的压力。 该控制器接收由连接到邻近联接器的空气管道的压力传感器感测的压力,以感测通过飞机的空气的压力,以及可以根据不同类型或类别的飞机的要求进行变化的设定点压力 。 第一和第二空调每个包括通过压缩机,冷凝器,膨胀阀和蒸发器引导制冷剂的圆形制冷剂管道。 蒸发器定位在空气管道中,第一空调器的蒸发器在鼓风机之前,第二空调器的蒸发器跟随空气管道中的鼓风机。 冷凝器冷却风扇通过两个冷凝器驱动空气,并且由控制器控制,响应于在空气或制冷剂管道之一或周围空气中测量的一个或多个压力或温度。
    • 5. 发明申请
    • ADJUSTABLE AIR CONDITIONING CONTROL SYSTEM FOR A UNIVERSAL AIRPLANE GROUND SUPPORT EQUIPMENT CART
    • 用于通用飞机地面支持设备的可调节空调控制系统
    • US20090107159A1
    • 2009-04-30
    • US12250503
    • 2008-10-13
    • James W. Mann, IIIJeffrey E. MontminyBenjamin E. NewellTy A. Newell
    • James W. Mann, IIIJeffrey E. MontminyBenjamin E. NewellTy A. Newell
    • B60H1/32F25B7/00F25D17/06F25B41/00
    • B64F1/364
    • A ground support equipment air conditioning system detachably connects to a port on an airplane. An air conduit connects an air intake and filter to a coupling that is adapted to be connected to one end of an air duct or hose the other end of which is adapted to be connected to an airplane's port. A variable speed blower in the air conduit has its speed varied by a controller to regulate the pressure supplied to an airplane. This controller receives as inputs the pressure sensed by a pressure sensor connected to the air conduit adjacent the coupling to sense the pressure of air passing into the airplane and also a setpoint pressure which can be varied to match the requirements of different types or classes of airplane. First and second air conditioners each include a circular refrigerant conduit channeling refrigerant through a compressor, a condenser, an expansion valve, and an evaporator. The evaporators are positioned in the air conduit with the first air conditioner's evaporator preceding the blower and the second air conditioner's evaporator following the blower in the air conduit. A condenser cooling fan drives air through the two condensers and is controlled by a controller responsive to one or more pressures or temperatures measured in one of the air or refrigerant conduits or in the surrounding air.
    • 地面支持设备空调系统可拆卸地连接到飞机上的端口。 空气管道将进气口和过滤器连接到适于连接到空气管道或软管的一端的联接器,其另一端适于连接到飞机的端口。 空气管道中的变速鼓风机的速度由控制器变化,以调节供应给飞机的压力。 该控制器接收由连接到邻近联接器的空气管道的压力传感器感测的压力,以感测通过飞机的空气的压力,以及可以根据不同类型或类别的飞机的要求进行变化的设定点压力 。 第一和第二空调每个包括通过压缩机,冷凝器,膨胀阀和蒸发器引导制冷剂的圆形制冷剂管道。 蒸发器定位在空气管道中,第一空调器的蒸发器在鼓风机之前,第二空调器的蒸发器跟随空气管道中的鼓风机。 冷凝器冷却风扇通过两个冷凝器驱动空气,并且由控制器控制,响应于在空气或制冷剂管道之一或周围空气中测量的一个或多个压力或温度。