公开(公告)号：US20080115989A1

公开(公告)日：2008-05-22

申请号：US11943124

申请日：2007-11-20

Applicant: Francois MATTE ,  Marc RIEDL

Inventor： Francois MATTE ,  Marc RIEDL

IPC: B60H1/03 ,  B60H1/26 ,  B60K11/06 ,  F01N3/023

CPC classification number: F01N3/021 ,  F01N13/082 ,  F01N2340/04 ,  F01N2590/08 ,  Y02T10/20

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。

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

IPC: F01N7/00

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。

公开(公告)号：US09216823B2

公开(公告)日：2015-12-22

申请号：US14216381

申请日：2014-03-17

Applicant: Francois Matte

Inventor： Francois Matte

IPC: B64C33/02 ,  A63H27/00

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'“）。

公开(公告)号：US20120187241A1

公开(公告)日：2012-07-26

申请号：US13010275

申请日：2011-01-20

Applicant: Francois Matte

Inventor： Francois Matte

IPC: B64C31/024 ,  B64C31/028

CPC classification number: B64C31/032

Abstract: The system includes a keel fitting that can be rigidly attached directly to the keel of the hang glider. It also includes two elongated frame members symmetrically mounted on opposite sides of the keel fitting. At least one electrical motor is mounted on each frame member and there are at least two propellers, each in driving engagement with a corresponding one of the electrical motors. The system further includes an electrical power unit mounted on the back of the pilot. The electrical power unit includes at least one battery and a pilot-actuated control circuit to vary the electrical power supplied to the electrical motors. The system gives the pilot the capability of taking off from a flat terrain. Once airborne, the system is not operated and the hang glider can then be used as an unpowered one.

Abstract translation: 该系统包括可以直接刚性连接到滑翔机龙骨的龙骨配件。 它还包括对称地安装在龙骨配件的相对侧上的两个细长的框架构件。 至少一个电动机安装在每个框架构件上，并且存在至少两个螺旋桨，每个螺旋桨与相应的一个电动机驱动接合。 该系统还包括安装在飞行员背部的电力单元。 电力单元包括至少一个电池和先导驱动的控制电路，以改变供应给电动机的电力。 该系统使飞行员能够从平坦的地形起飞。 一旦机载，系统不运行，然后滑翔机可以用作无动力的。

公开(公告)号：US08561936B2

公开(公告)日：2013-10-22

申请号：US13010275

申请日：2011-01-20

Applicant: Francois Matte

Inventor： Francois Matte

IPC: B64C31/024 ,  B64C31/028

CPC classification number: B64C31/032

Abstract: The system includes a keel fitting that can be rigidly attached directly to the keel of the hang glider. It also includes two elongated frame members symmetrically mounted on opposite sides of the keel fitting. At least one electrical motor is mounted on each frame member and there are at least two propellers, each in driving engagement with a corresponding one of the electrical motors. The system further includes an electrical power unit mounted on the back of the pilot. The electrical power unit includes at least one battery and a pilot-actuated control circuit to vary the electrical power supplied to the electrical motors. The system gives the pilot the capability of taking off from a flat terrain. Once airborne, the system is not operated and the hang glider can then be used as an unpowered one.

Abstract translation: 该系统包括可以直接刚性连接到滑翔机龙骨的龙骨配件。 它还包括对称地安装在龙骨配件的相对侧上的两个细长的框架构件。 至少一个电动机安装在每个框架构件上，并且存在至少两个螺旋桨，每个螺旋桨与相应的一个电动机驱动接合。 该系统还包括安装在飞行员背部的电力单元。 电力单元包括至少一个电池和先导驱动的控制电路，以改变供应给电动机的电力。 该系统使飞行员能够从平坦的地形起飞。 一旦机载，系统不运行，然后滑翔机可以用作无动力的。

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

IPC: B64C33/02

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'“）。