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    • 1. 发明授权
    • Power transmission gearbox presenting a modifiable speed of rotation at its outlet, and a corresponding method of operation
    • 动力传动齿轮箱在其出口处呈现可改变的旋转速度,以及相应的操作方法
    • US08027772B2
    • 2011-09-27
    • US12393220
    • 2009-02-26
    • Michel Vialle
    • Michel Vialle
    • F16H37/02B64C27/12G06F19/00
    • F16H37/065B60W10/06B60W10/113B60W30/19B64C27/12B64D35/08F16H3/006Y10T74/19051Y10T477/79
    • A power transmission gearbox for rotorcraft for transmitting rotary movement from at least two engine members to a main shaft, wherein the gearbox presents at least two transmission systems for imparting rotary movement to the main shaft, each of the transmission systems including: an inlet shaft designed to be driven in rotation by an engine member; at least two reduction stages presenting different reduction ratios; a first gearwheel connected to the inlet shaft via a declutchable freewheel, the gearwheel meshing with a first toothed wheel secured to an intermediate shaft defining at least a first reduction stage; a second gearwheel connected to the inlet shaft via a simple freewheel, the second gearwheel meshing with a second toothed wheel secured to the intermediate shaft defining the second reduction stage; a main freewheel mounted on the intermediate shaft to rotate a complementary toothed wheel secured to the main shaft; and a clutch mechanism for the declutchable freewheel.
    • 用于将旋转运动从至少两个发动机构件传递到主轴的用于旋转航空器的动力传动齿轮箱,其中所述变速箱具有至少两个用于向主轴施加旋转运动的传动系统,每个传动系统包括:设计的入口轴 由发动机构件旋转驱动; 至少两个具有不同减速比的减速阶段; 第一齿轮通过可离合的自由轮连接到入口轴,所述齿轮与固定到至少限定第一减速级的中间轴的第一齿轮啮合; 第二齿轮通过简单的自由轮连接到入口轴,第二齿轮与固定到中间轴的第二齿轮啮合,第二齿轮限定第二减速台; 安装在所述中间轴上的主自由轮,以旋转固定到所述主轴的互补齿轮; 以及用于可离合的自由轮的离合器机构。
    • 2. 发明授权
    • Transmission mechanism between accessories and engine members for driving the rotor of a rotorcraft
    • 用于驱动旋翼航空器转子的附件和发动机构件之间的传动机构
    • US07418888B2
    • 2008-09-02
    • US11145928
    • 2005-06-07
    • Michel Vialle
    • Michel Vialle
    • F16H37/06B64C27/00
    • F16H1/22B64C27/14Y10T74/19126Y10T74/19135Y10T74/19647
    • A transmission mechanism between at least one accessory and engine members for driving the rotor of a rotorcraft, the transmission therebetween being selectively either in isolation or in combination. An intermediate shaft is interposed between a main drive shaft for the rotor and a secondary drive shaft for the accessory, for driving the accessory from an engine member allocated to driving it. This intermediate shaft engages directly on the main shaft and meshes with an accessory drive gear via freewheels to enable the gear to be driven either by the engine member or from the main shaft in the position for combined drive together with the rotor, the rotor being driven by the other engine member or autorotation in the event of both engine members failing.
    • 用于驱动旋翼航空器的转子的至少一个附件和发动机构件之间的传动机构,其间的传动是选择性地或者是组合的。 中间轴介于用于转子的主驱动轴和用于附件的辅助驱动轴之间,用于从分配给其驱动的发动机构件驱动附件。 该中间轴直接接合在主轴上,并通过单向离合器与辅助驱动齿轮啮合,以使齿轮能够由发动机构件或主轴与转子一起驱动的位置驱动,转子被驱动 在发动机构件发生故障的情况下,由另一个发动机构件或自动调整。
    • 6. 发明授权
    • Packet length indication for a facsimile system
    • 传真机系统的分组长度指示
    • US06934045B1
    • 2005-08-23
    • US09696562
    • 2000-10-25
    • Jerome Michel VialleMichael Clement WhitfieldRemy Gauguey
    • Jerome Michel VialleMichael Clement WhitfieldRemy Gauguey
    • G06K1/00H04J3/16H04M11/00H04N1/00
    • H04N1/00209
    • A facsimile system is disclosed for transferring a facsimile using a Transmission Control Protocol/Internet Protocol (TCP/IP) network. The facsimile system comprises a first communication processing system and a second communication processing system. The first communication processing system converts the facsimile into application packets that indicate individual application packet lengths. The first communication processing system then converts the application packets into TCP/IP packets and transfers the TCP/IP packets to the TCP/IP network. The second communication processing system receives the transferred TCP/IP packets from the TCP/IP network and converts the transferred TCP/IP packets into transferred application packets. The second communication processing system converts the transferred application packets into the facsimile using the individual application packet lengths.
    • 公开了一种用于使用传输控制协议/因特网协议(TCP / IP)网络传送传真的传真系统。 该传真系统包括第一通信处理系统和第二通信处理系统。 第一通信处理系统将传真转换为指示各个应用分组长度的应用分组。 第一通信处理系统然后将应用分组转换成TCP / IP分组,并将TCP / IP分组传送到TCP / IP网络。 第二通信处理系统从TCP / IP网络接收传送的TCP / IP分组,并将传送的TCP / IP分组转换成转移的应用分组。 第二通信处理系统使用各个应用分组长度将传送的应用分组转换成传真。
    • 7. 发明申请
    • ROTARY WING AIRCRAFT PROVIDED WITH PROPULSION MEANS, AND A METHOD APPLIED BY SAID AIRCRAFT
    • 旋转式飞机提供推进手段,以及适用于飞机的方法
    • US20120068007A1
    • 2012-03-22
    • US13230965
    • 2011-09-13
    • Michel Vialle
    • Michel Vialle
    • B64C27/04B64D35/00
    • B64C27/14B64C27/28B64D35/04
    • An aircraft (200) provided with a power plant (300) driving a rotary wing (60) and at least one propulsion means (7, 7′) possessing a propeller (6, 6′), said power plant (300) including at least one engine (1, 1′) having an outlet shaft (2, 2′) driving a drive train (400) in order to drive said rotary wing (60). The aircraft includes one coupling member (8, 8′) per engine (1, 1′) provided with a drive shaft (4, 4′) and with a first toothed wheel (13) that are coupled together by a clutch (15) and by a main controllable freewheel (25) arranged in parallel with the clutch, said drive shaft (4, 4′) driving at least one propulsion means (7, 7′) provided with brake means (9, 9′) for braking its propeller (6, 6′), said first toothed wheel (13) meshing with said drive train (400).
    • 具有驱动旋翼(60)的动力装置(300)和具有螺旋桨(6,6')的至少一个推进装置(7,7')的飞机(200),所述发电厂(300)包括: 具有驱动传动系(400)的驱动所述旋转翼(60)的出口轴(2,2')的至少一个发动机(1,1')。 该飞行器包括一个每个发动机(1,1')的一个连接件(8,8'),每个发动机(1,1')设置有一个驱动轴(4,4')和一个通过离合器(15)联接在一起的第一齿轮(13) 并且通过与离合器平行布置的主可控自由轮(25),所述驱动轴(4,4')驱动至少一个具有制动装置(9,9')的推进装置(7,7'),用于制动其 螺旋桨(6,6'),所述第一齿轮(13)与所述传动系(400)啮合。
    • 9. 发明申请
    • POWER TRANSMISSION GEARBOX PRESENTING A MODIFIABLE SPEED OF ROTATION AT ITS OUTLET, AND A CORRESPONDING METHOD OF OPERATION
    • 电力传动齿轮箱在其出口处呈现可转换的转速,以及相应的操作方法
    • US20090222178A1
    • 2009-09-03
    • US12393220
    • 2009-02-26
    • Michel VIALLE
    • Michel VIALLE
    • F16H37/06B60W10/04B60W30/18G06F19/00
    • F16H37/065B60W10/06B60W10/113B60W30/19B64C27/12B64D35/08F16H3/006Y10T74/19051Y10T477/79
    • A power transmission gearbox for rotorcraft for transmitting rotary movement from at least two engine members to a main shaft, wherein the gearbox presents at least two transmission systems for imparting rotary movement to the main shaft, each of the transmission systems including: an inlet shaft designed to be driven in rotation by an engine member; at least two reduction stages presenting different reduction ratios; a first gearwheel connected to the inlet shaft via a declutchable freewheel, the gearwheel meshing with a first toothed wheel secured to an intermediate shaft defining at least a first reduction stage; a second gearwheel connected to the inlet shaft via a simple freewheel, the second gearwheel meshing with a second toothed wheel secured to the intermediate shaft defining the second reduction stage; a main freewheel mounted on the intermediate shaft to rotate a complementary toothed wheel secured to the main shaft; and a clutch mechanism for the declutchable freewheel.
    • 用于将旋转运动从至少两个发动机构件传递到主轴的用于旋转航空器的动力传动齿轮箱,其中所述变速箱具有至少两个用于向主轴施加旋转运动的传动系统,每个传动系统包括:设计的入口轴 由发动机构件旋转驱动; 至少两个具有不同减速比的减速阶段; 第一齿轮通过可离合的自由轮连接到入口轴,所述齿轮与固定到至少第一减速级的中间轴的第一齿轮啮合; 第二齿轮通过简单的自由轮连接到入口轴,第二齿轮与固定到中间轴的第二齿轮啮合,第二齿轮限定第二减速台; 安装在所述中间轴上的主自由轮,以旋转固定到所述主轴的互补齿轮; 以及用于可离合的自由轮的离合器机构。