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    THRUST GENERATING DEVICE
    2.
    发明公开
    THRUST GENERATING DEVICE 审中-公开

    公开(公告)号：US20240067328A1

    公开(公告)日：2024-02-29

    申请号：US18455903

    申请日：2023-08-25

    申请人： HONDA MOTOR CO., LTD.

    发明人： Yuji Ishitsuka

    IPC分类号： B64C11/00 ,  F01D15/02

    CPC分类号： B64C11/001 ,  F01D15/02 ,  B64C29/0008 ,  F05D2220/30 ,  F05D2220/90

    摘要： A thrust generating device includes a propeller unit including a propeller and a duct covering the periphery of the propeller. The duct includes a cylinder disposed around the propeller, a hub disposed inside the cylinder, and a plurality of duct stators extending radially from the hub to the cylinder. The hub and each of the duct stators are disposed rearward of the propeller.

    Apparatus and method for controlling power generation system
    7.
    发明授权
    Apparatus and method for controlling power generation system 有权
    用于控制发电系统的装置和方法

    公开(公告)号：US09506405B2

    公开(公告)日：2016-11-29

    申请号：US13485129

    申请日：2012-05-31

    申请人： David W. Vos

    发明人： David W. Vos

    IPC分类号： F02C9/00 ,  B60K6/42 ,  F01D15/02

    CPC分类号： F02C9/00 ,  B60K6/42 ,  F01D15/02 ,  F05D2270/051

    摘要： A vehicle includes at least one propulsion member and a power generation system. The power generation system includes a power source and a transmission configured to provide torque to the at least one propulsion member. The power generation system further includes a control apparatus comprising an input device and a processor. The processor is configured to receive signals indicative of a power output command, a plurality of detected ambient air conditions, and a plurality of detected power generation system parameters. The processor is also configured to determine a plurality of power generation system control settings for improving efficiency of the vehicle based on at least one of signals indicative of the power output command, the signals indicative of the plurality of detected ambient air conditions, and the signals indicative of a plurality of power generation system parameters.

    摘要翻译： 车辆包括至少一个推进构件和发电系统。 发电系统包括电源和配置成向至少一个推进构件提供扭矩的变速器。 发电系统还包括包括输入装置和处理器的控制装置。 处理器被配置为接收指示功率输出命令，多个检测到的环境空气条件和多个检测到的发电系统参数的信号。 处理器还被配置为基于指示功率输出命令的信号，指示多个检测到的环境空气条件的信号和信号中的至少一个来确定用于改善车辆效率的多个发电系统控制设置 指示多个发电系统参数。

    AIRCRAFT PROPULSION ASSEMBLY COMPRISING AN AIR FLOW VALVE WITH A VARIABLE FLOW RATE
    8.
    发明申请
    AIRCRAFT PROPULSION ASSEMBLY COMPRISING AN AIR FLOW VALVE WITH A VARIABLE FLOW RATE 有权
    包括具有可变流量的空气流量阀的飞机推进组件

    公开(公告)号：US20150292352A1

    公开(公告)日：2015-10-15

    申请号：US14634212

    申请日：2015-02-27

    申请人： Airbus Operations (S.A.S.)

    发明人： Jacques Hervé Marche

    IPC分类号： F01D25/12 ,  B64D33/08 ,  F01D15/02 ,  F01D17/00 ,  F01D1/02 ,  F01D9/02

    CPC分类号： F01D25/12 ,  B64D33/08 ,  F01D1/02 ,  F01D9/02 ,  F01D15/02 ,  F01D17/00 ,  F01D17/148 ,  F02C6/08 ,  F02C7/143 ,  F02C7/185 ,  F02K3/06 ,  F02K3/115 ,  F05D2220/30 ,  F05D2260/213 ,  Y02T50/675

    摘要： A propulsion assembly having a heat exchanger and a system for supplying cold air including an air inlet in a stream of air, an air duct connecting the air inlet fluidly to the exchanger, and an air flow valve with a variable flow rate inside the duct, the valve including a hub having blades projecting radially from the hub forming a helix, each blade having a root mounted rotatably on the hub, the valve comprising an electric motor to drive the hub by a motor shaft, and structure for varying pitch angle of the blades, the extremity of each blade being flush with a wall of the duct, the valve controllable to a closed configuration where pitch angle of the blades is 0° and the valve prevents passage of air, an open configuration where pitch angle is 90°, and/or a charge configuration where pitch angle is between 0° and 90°.

    摘要翻译： 具有热交换器和用于供应冷空气的系统的推进组件，所述冷空气包括空气流中的空气入口，将空气入口流体连接到交换器的空气管道和在管道内具有可变流量的空气流量阀， 所述阀包括具有从所述毂径向突出形成螺旋形的叶片的毂，每个叶片具有可旋转地安装在所述轮毂上的根部，所述阀包括用于通过马达轴驱动所述轮毂的电动马达，以及用于改变所述桨叶角度的结构 叶片的每个叶片的末端与管道的壁齐平，该阀可控制到关闭构造，其中叶片的俯仰角为0°，并且阀阻止空气通过，俯仰角为90°的打开构造， 和/或俯仰角在0°和90°之间的电荷构型。

    EXHAUST-GAS POWER-RECOVERY TURBINE FOR A TURBO COMPOUND SYSTEM
    10.
    发明申请
    EXHAUST-GAS POWER-RECOVERY TURBINE FOR A TURBO COMPOUND SYSTEM 审中-公开
    用于涡轮复合系统的排气功率恢复涡轮机

    公开(公告)号：US20120297770A1

    公开(公告)日：2012-11-29

    申请号：US13305935

    申请日：2011-11-29

    申请人： Thomas Figler ,  Markus Kley

    发明人： Thomas Figler ,  Markus Kley

    IPC分类号： F02B41/00

    CPC分类号： F16C19/54 ,  F01D15/02 ,  F01D25/16 ,  F01D25/166 ,  F02C6/12 ,  F05D2220/40 ,  F05D2240/53 ,  F05D2260/4031 ,  F16C17/18 ,  F16C21/00 ,  F16C27/02 ,  F16C27/045 ,  F16C2360/00 ,  Y02T10/163

    摘要： The invention concerns an exhaust-gas power-recovery turbine for a turbo compound system, in particular of a motor vehicle, including: a turbine shaft, which at the first end thereof or in the area of the first end carries a rotor to be impinged by the exhaust gas flow of an internal combustion engine, in order to convert exhaust gas energy into drive power; and which at the second end thereof carries a pinion, which is designed to be brought into a driving connection with the crankshaft of the internal combustion engine, in order to transmit the drive power to the crankshaft. The invention is characterised in that that the turbine shaft is supported in the area of the rotor by means of a radial plain bearing and in the area of the pinion by means of a radial rolling-element bearing.

    摘要翻译： 本发明涉及一种用于涡轮复合系统，特别是机动车辆的废气动力回收涡轮机，包括：涡轮轴，其在其第一端处或在第一端的区域中承载要撞击的转子 通过内燃机的废气流，将废气能转换成驱动力; 并且其在其第二端处承载有被设计成与内燃机的曲轴进行驱动连接的小齿轮，以将驱动力传递到曲轴。 本发明的特征在于，涡轮轴通过径向滑动轴承支撑在转子的区域中，并且通过径向滚动元件轴承支撑在小齿轮的区域中。