DIESEL ENGINE VEHICLE CONFIGURATIONS FOR EVACUATION OF ENGINE AND/OR EXHAUST SYSTEM HEAT
    1.
    发明申请
    DIESEL ENGINE VEHICLE CONFIGURATIONS FOR EVACUATION OF ENGINE AND/OR EXHAUST SYSTEM HEAT 审中-公开
    用于发动机和/或排气系统加热的柴油发动机车辆配置

    公开(公告)号:US20080115989A1

    公开(公告)日:2008-05-22

    申请号:US11943124

    申请日:2007-11-20

    Abstract: The diesel engine vehicle has a passenger area, and a substantially vertically oriented ventilated chamber separate from the passenger area. The ventilated chamber can be in air flow communication with an engine compartment to evacuate heat therefrom. A heat-emitting exhaust treatment unit can be housed in the ventilated chamber and connected between the diesel engine and an exhaust outlet in an exhaust system of the vehicle.

    Abstract translation: 柴油发动机车辆具有乘客区域和与乘客区域分离的基本垂直定向的通风室。 通风室可以与发动机室进行气流连通以从其排出热量。 发热排气处理单元可以容纳在通风室中并且连接在柴油发动机和车辆的排气系统中的排气出口之间。

    EXHAUST GAS DIFFUSER
    2.
    发明申请
    EXHAUST GAS DIFFUSER 有权
    排气歧管

    公开(公告)号:US20080116005A1

    公开(公告)日:2008-05-22

    申请号:US11943148

    申请日:2007-11-20

    Applicant: Francois MATTE

    Inventor: Francois MATTE

    CPC classification number: F01N13/082 F01N2590/08

    Abstract: The diffuser can be used at an end of a vehicle exhaust system. The diffuser can have a generally hollow body with an inlet for receiving exhaust gasses from a substantially vertically-extending component of the vehicle exhaust system, and a substantially flat outlet grate through which the exhaust gasses are to be released to the atmosphere, the outlet grate being configured and adapted for use in a roof of the vehicle, in an aligned position therewith, with the hollow body of the diffuser positioned inside the vehicle and below the outlet grate.

    Abstract translation: 扩散器可用于车辆排气系统的末端。 扩散器可以具有大致中空的主体,其具有用于从车辆排气系统的基本垂直延伸的部件接收废气的入口,以及基本上平坦的出口格栅,废气将通过该排气排放到大气中,出口格栅 被配置和适于在与其对准的位置的车辆的屋顶中使用,扩散器的空心体位于车辆内部和出口格栅下方。

    WING FLAPPING MECHANISM AND METHOD
    3.
    发明申请
    WING FLAPPING MECHANISM AND METHOD 审中-公开
    WING FLAPPING机制与方法

    公开(公告)号:US20140263826A1

    公开(公告)日:2014-09-18

    申请号:US14216381

    申请日:2014-03-17

    Applicant: Francois MATTE

    Inventor: Francois MATTE

    CPC classification number: B64C33/02 A63H27/008 B64C2201/025

    Abstract: The wing flapping mechanism (100) includes a main frame (110), a pair of opposite wings (120) laterally projecting from the main frame (110), and a linkage arrangement to convert rotation of a motor (150) into a three-dimensional cyclic wing motion of each of the wings (120). The linkage arrangement includes torque-transmitting couplings extending from inside the main frame (110) into the wing structures (122) to transmit an alternating pivoting motion, created as a result of the rotation of the motor (150), to the distal end of a corresponding third torsion-responsive tube (140, 144′″). Each torque-transmitting coupling extends inside a shoulder joint (130), a first torsion-responsive tube (132, 144′), an elbow joint (134), a second torsion-responsive tube (136, 144″), a wrist joint (138) and the third torsion-responsive tube (140, 144′″) of the corresponding wing structure (122).

    Abstract translation: 机翼拍动机构(100)包括主框架(110),从主框架(110)侧向突出的一对相对的翼片(120),以及将马达(150)的旋转转换成三维 每个翼(120)的三维循环翼运动。 联动装置包括从主框架(110)内部延伸到机翼结构(122)中的扭矩传递联接件,以将由马达(150)的旋转产生的交替的枢转运动传递到电动机(150)的远端 相应的第三扭转响应管(140,144'“)。 每个扭矩传递联接件在肩关节(130),第一扭转响应管(132,144'),肘关节(134),第二扭转响应管(136,144“),腕关节 (138)和相应翼结构(122)的第三扭转响应管(140,144'“)。

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