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    • 1. 发明授权
    • Airplane ground support equipment cart having extractable modules and a generator module that is seperable from power conversion and air conditioning modules
    • 具有可抽出模块的飞机地面支撑设备车和与电力转换和空调模块分离的发电机模块
    • US08047555B2
    • 2011-11-01
    • US12250489
    • 2008-10-13
    • James W. Mann, IIIJeffrey E. Montminy
    • James W. Mann, IIIJeffrey E. Montminy
    • B62B3/04
    • B64F1/34B64F1/364
    • A ground support equipment cart contains one or more removable equipment modules. The cart contains a rectangular module containing airplane air conditioning components mounted upon the cart and extending the width of the cart but occupying substantially less than half of the cart's length. The cart also contains one or more rectangular equipment modules removably mounted upon the cart, one or two of the removable modules containing electrical power converting components. And the cart contains a rectangular module containing power generating components mounted upon the cart and occupying substantially the remainder of the cart. The cart separates into two parts, one part containing the module containing power generating components. The cart also contains a control module having a display and controls for, and that is networked to, the other modules. One or more of the removable modules slide out on a tray and may be locked in position.
    • 地面支持设备车包含一个或多个可移动设备模块。 该推车包含一个矩形模块,其中包含安装在推车上的飞机空调部件,并延伸推车的宽度,但占据大约小于推车长度的一半。 该推车还包括一个或多个矩形设备模块,其可拆卸地安装在推车上,一个或两个可拆卸模块包含电力转换部件。 并且该推车包含一个矩形模块,其中包含安装在推车上的发电部件,并基本上占据该车的剩余部分。 推车分为两部分,一部分包含包含发电部件的模块。 该购物车还包含控制模块,该控制模块具有对其他模块的显示和控制,并与其连接。 一个或多个可移动模块在托盘上滑出并且可以被锁定就位。
    • 2. 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。
    • 3. 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。
    • 4. 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。
    • 5. 发明授权
    • Maintenance and control system for ground support equipment
    • 地面支援设备维护和控制系统
    • US08055388B2
    • 2011-11-08
    • US12250506
    • 2008-10-13
    • James W. Mann, IIIJeffrey E. MontminySteven E. BivensDavid Wayne Leadingham
    • James W. Mann, IIIJeffrey E. MontminySteven E. BivensDavid Wayne Leadingham
    • G01M1/38
    • B64F1/34B64F1/364
    • Ground support equipment for servicing an airplane includes a ground support equipment cart upon which are mounted at least two equipment modules and a control module. A first equipment module mounted upon the cart contains ground support equipment for servicing an airplane and also has a network connection, and at least one additional equipment module mounted upon the cart contains additional ground support equipment and also has a network connection. The control module has a user display and user controls that are connected to a control processor which has a network connection. The user display and the user controls serve as a shared control panel for the ground support equipment contained in the modules mounted upon the cart. In response the control processor sends over the network to one or more of the other modules information defining what particular services the selected type or class of airplane requires of the modules.
    • 用于维修飞机的地面支撑设备包括地面支撑设备车,其上安装有至少两个设备模块和控制模块。 安装在推车上的第一设备模块包含用于维修飞机的地面支撑设备,并且还具有网络连接,并且安装在推车上的至少一个附加设备模块包含附加的地面支撑设备并且还具有网络连接。 控制模块具有连接到具有网络连接的控制处理器的用户显示和用户控制。 用户显示器和用户控件用作用于包含在安装在推车上的模块中的地面支撑设备的共享控制面板。 作为响应,控制处理器通过网络向一个或多个其他模块发送信息,该信息定义了所选择的类型或类别的飞机对模块的需求。
    • 6. 发明申请
    • MAINTENANCE AND CONTROL SYSTEM FOR GROUND SUPPORT EQUIPMENT
    • 地面支持设备的维护和控制系统
    • US20090112368A1
    • 2009-04-30
    • US12250506
    • 2008-10-13
    • James W. Mann, IIIJeffrey E. MontminySteven E. BivensDavid Wayne Leadingham
    • James W. Mann, IIIJeffrey E. MontminySteven E. BivensDavid Wayne Leadingham
    • B62B3/10F25D17/06G05B15/00F02B63/00
    • B64F1/34B64F1/364
    • Ground support equipment for servicing an airplane includes a ground support equipment cart upon which are mounted at least two equipment modules and a control module. A first equipment module mounted upon the cart contains ground support equipment for servicing an airplane and also has a network connection, and at least one additional equipment module mounted upon the cart contains additional ground support equipment for servicing an airplane and also has a network connection. The control module has a user display and user controls that are connected to a control processor which has a network connection. The user display and the user controls serve as a shared control panel for the ground support equipment contained in the modules mounted upon the cart. A network interconnects the network connections of the modules mounted upon the cart. The control processor can cause the user display to present a menu listing various types or classes of airplanes for selection by a user. In response to user selection of a type or class of airplane, the control processor sends over the network to one or more of the other modules information defining what particular services the selected type or class of airplane requires of the modules.
    • 用于维修飞机的地面支撑设备包括地面支撑设备车,其上安装有至少两个设备模块和控制模块。 安装在推车上的第一设备模块包含用于维修飞机的地面支撑设备,并且还具有网络连接,并且安装在推车上的至少一个附加设备模块包含用于维修飞机的附加地面支撑设备,并且还具有网络连接。 控制模块具有连接到具有网络连接的控制处理器的用户显示和用户控制。 用户显示器和用户控件用作用于包含在安装在推车上的模块中的地面支撑设备的共享控制面板。 网络将安装在购物车上的模块的网络连接互连。 控制处理器可以使用户显示器呈现列出用于用户选择的各种类型的飞机的菜单。 响应于用户选择飞机类​​型或类别,控制处理器通过网络向一个或多个其他模块发送信息,该信息定义了所选择的类型或类别的飞机对模块的需求。
    • 7. 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。
    • 9. 发明申请
    • A MULTI-VOLTAGE POWER SUPPLY FOR A UNIVERSAL AIRPLANE GROUND SUPPORT EQUIPMENT CART
    • 通用飞机地面支持设备的多电源电源
    • US20090121552A1
    • 2009-05-14
    • US12250265
    • 2008-10-13
    • James W. Mann, IIIDavid Wayne Leadingham
    • James W. Mann, IIIDavid Wayne Leadingham
    • H02J4/00
    • H02M5/458B64F1/364H02M7/217H02M7/48H02M2001/008Y10T307/658Y10T307/664Y10T307/675Y10T307/696
    • An airplane ground support system includes a multi-voltage power supply. This system includes an air conditioning module and a control module having a display and a processor, the display and processor presenting an airplane type or class selection menu to airplane support technicians and responding to the selection of a type or class of airplane by generating a power output selection signal designating the type of power needed by the selected type or class of airplane. The system also includes a power supply module which has an A.C. power input, at least one power output, and which receives the power output selection signal as an incoming signal. A power conversion system within the power supply module connects to the A.C. power input and supplies converted and voltage regulated power to the at least one power output. This power conversion system also receives the power conversion control signal as an input signal. A control system within the power conversion module receives measurements of the voltage at the power supply module's at least one power output and also receives the control module's power output selection signal. This control system generates the power conversion system's power conversion control signal and adjusts it to regulate the power module's output to a predetermined preset voltage level as mandated by the power output selection signal.
    • 飞机地面支撑系统包括多电压电源。 该系统包括空调模块和具有显示器和处理器的控制模块,所述显示器和处理器向飞机支持技术人员提供飞机类型或类别选择菜单,并通过产生功率来响应对类型或类别的飞机的选择 输出选择信号指定所选类型或类别的飞机所需的功率类型。 该系统还包括具有交流输入功率,至少一个功率输出并且接收功率输出选择信号作为输入信号的电源模块。 电源模块内的电源转换系统连接到交流电源输入端,并将转换和调压功率提供给至少一个电源输出。 该电力转换系统还接收功率转换控制信号作为输入信号。 电力转换模块内的控制系统接收电源模块的至少一个电力输出端的电压测量,并且还接收控制模块的功率输出选择信号。 该控制系统产生电力转换系统的电力转换控制信号,并根据功率输出选择信号强制调整功率模块的输出到预定的预设电压电平。
    • 10. 发明授权
    • Multi-voltage power supply for a universal airplane ground support equipment cart
    • 用于通用飞机地面支撑设备推车的多电压电源
    • US08030801B2
    • 2011-10-04
    • US12250265
    • 2008-10-13
    • James W. Mann, IIIDavid Wayne Leadingham
    • James W. Mann, IIIDavid Wayne Leadingham
    • H02J4/00
    • H02M5/458B64F1/364H02M7/217H02M7/48H02M2001/008Y10T307/658Y10T307/664Y10T307/675Y10T307/696
    • An airplane ground support system includes a multi-voltage power supply. This system includes an air conditioning module and a control module having a display and a processor, the display and processor presenting an airplane type or class selection menu to airplane support technicians and responding to the selection of a type or class of airplane by generating a power output selection signal designating the type of power needed by the selected type or class of airplane. The system also includes a power supply module which has an A.C. power input, at least one power output, and which receives the power output selection signal as an incoming signal. A power conversion system within the power supply module connects to the A.C. power input and supplies converted and voltage regulated power to the at least one power output. This power conversion system also receives the power conversion control signal as an input signal. A control system within the power conversion module receives measurements of the voltage at the power supply module's at least one power output and also receives the control module's power output selection signal. This control system generates the power conversion system's power conversion control signal and adjusts it to regulate the power module's output to a predetermined preset voltage level as mandated by the power output selection signal.
    • 飞机地面支撑系统包括多电压电源。 该系统包括空调模块和具有显示器和处理器的控制模块,所述显示器和处理器向飞机支持技术人员提供飞机类型或类别选择菜单,并通过产生功率来响应对类型或类别的飞机的选择 输出选择信号指定所选类型或类别的飞机所需的功率类型。 该系统还包括具有交流输入功率,至少一个功率输出并且接收功率输出选择信号作为输入信号的电源模块。 电源模块内的电源转换系统连接到交流电源输入端,并将转换和调压功率提供给至少一个电源输出。 该电力转换系统还接收功率转换控制信号作为输入信号。 电力转换模块内的控制系统接收电源模块的至少一个电力输出端的电压测量,并且还接收控制模块的功率输出选择信号。 该控制系统产生电力转换系统的电力转换控制信号,并根据功率输出选择信号强制调整功率模块的输出到预定的预设电压电平。