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    GROUND SUPPORT SYSTEM FOR AN AIRCRAFT HAVING A TURBINE ENGINE
    22.
    发明授权
    GROUND SUPPORT SYSTEM FOR AN AIRCRAFT HAVING A TURBINE ENGINE 有权

    公开(公告)号：EP3079986B1

    公开(公告)日：2018-10-24

    申请号：EP14815910.6

    申请日：2014-12-10

    申请人： Duinmaaijer B.V.

    发明人： MOES, Pieter Jacob ,  LAMMERS, Jan Willem ,  HETTEMA, Robert Raymond

    IPC分类号： B64F1/34 ,  B64F1/36 ,  B64F5/00 ,  F02B63/04 ,  F02B63/06 ,  B64F5/60

    CPC分类号： B64F1/364 ,  B64F1/34 ,  B64F5/60 ,  F02B63/04 ,  F02B63/06 ,  F04D25/04

    摘要： A ground support system (1) for an aircraft having a turbine engine, which ground support system comprises; an intermittent combustion engine (2), a generator (3) which is driven by the combustion engine to supply electrical power with a constant frequency, an electricity cable (4) to transport the electrical power to the aircraft, an air pump (5) which is driven by the combustion engine to supply pressurised air, an air duct (6) to transport the pressurised air to the aircraft, a control unit (7) to control the operation of the ground support system (1), which control unit (7) communicates with the combustion engine (2) to let the combustion engine run at a predetermined engine rotational speed, and wherein the air pump (5) is driven by the combustion engine (2) via an adjustable transmission (16) to adjust an air flow rate of the pressurised air supplied by the air pump (5), while the combustion engine (2) remains running at the predetermined engine rotational speed.

    Enhanced canopy for mobile ground power unit
    23.
    发明公开
    Enhanced canopy for mobile ground power unit 有权
    VERBESSERTE HAUBEFÜREINE MOBILE BODENVERSORGUNSEINHEIT

    公开(公告)号：EP3006347A1

    公开(公告)日：2016-04-13

    申请号：EP14188501.2

    申请日：2014-10-10

    申请人： Illinois Tool Works Inc.

    发明人： Tindall, Leslie

    IPC分类号： B64F1/34

    CPC分类号： B64F1/364 ,  B64F1/34 ,  H02K5/20 ,  H02K5/24 ,  H02K7/1815

    摘要： The invention relates to a mobile ground power unit (1) for supplying power to an aircraft parked on the ground, the ground power unit (1) comprising an engine (10), which is preferably a combustion engine, and
    - an electric generator (20), whereby the electric generator (20) is configured to be driven by the engine,
    - a housing (30) whereby the engine (10) and the electric generator (20) are disposed within the housing (30), wherein the housing features as a component (31) a canopy (31.1) having an outer wall (33) facing outside the housing (30), wherein the outer wall (33) is having at least one area consisting of a single piece that is covering an (preferably all the) upper side of the engine (10) (and generator) and that extends downwards along at least two (preferably three) different vertical sides of the ground power unit (1), wherein the canopy (31.1) comprises an inner wall (32) facing inside the housing (30), wherein the inner wall (32) and the outer wall (33) 'define a hollow space (34) between each other.
    The invention further relates to a canopy as a component (31) of a housing (30) for a ground power unit (1).

    摘要翻译： 本发明涉及一种用于向搁置在地面上的飞行器供电的移动地面动力装置（1），该地面动力装置（1）包括优选内燃机的发动机（10），以及 - 发电机 20），由此所述发电机（20）构造成由所述发动机驱动， - 壳体（30），由此所述发动机（10）和所述发电机（20）设置在所述壳体（30）内，其中所述壳体 特征为组件（31）具有面向外壳（30）外侧的外壁（33）的顶篷（31.1），其中外壁（33）具有至少一个区域，该区域由单件构成，该单件覆盖（ 优选地是所有的发动机（10）的上侧（和发电机），并且沿着地面动力单元（1）的至少两个（优选三个）不同的垂直侧向下延伸，其中，顶盖（31.1）包括内壁 （32）面向所述壳体（30）的内​​部，其中所述内壁（32）和所述外壁（33） w空间（34）之间。 本发明还涉及作为用于地面动力单元（1）的壳体（30）的部件（31）的顶盖。

    Electric power supply system for an aircraft, aircraft and airport power supply system
    24.
    发明公开
    Electric power supply system for an aircraft, aircraft and airport power supply system 有权
    电力供应系统的飞机，飞机和飞机供电系统

    公开(公告)号：EP2720340A1

    公开(公告)日：2014-04-16

    申请号：EP12188512.3

    申请日：2012-10-15

    申请人： Airbus Operations GmbH

    发明人： Brombach, Johannes ,  Schulz, Detlef

    IPC分类号： H02J4/00 ,  B64F1/34

    CPC分类号： H02J4/00 ,  B64D2221/00 ,  B64F1/34 ,  Y02T50/54 ,  Y02T50/82

    摘要： The present invention relates to an electric power supply system for an aircraft having a transformer-less HVDC architecture, the system comprising: at least one multiphase engine generator in a star configuration which provides a multiphase alternating (AC) voltage; a converting circuit for converting the multiphase AC voltage into a corresponding direct (DC) voltage for supplying at least one aircraft load; an electric power supply interface (27) for connection with a standardized GPU plug (50) of an external GPU (28), the electric power supply interface (27) comprising a supply voltage output terminal coupled to a self-contained power source (55) for providing a low voltage control signal for driving a GPU internal switching circuit (54) wherein the power source is decoupled from the AC voltage and DC voltage. The present invention further relates to an aircraft and an airport power supply system.

    摘要翻译： 本发明涉及在电力供给系统，用于飞机上具有无变压器的HVDC架构，该系统包括：至少一个在星形配置，其提供的多相交流（AC）电压的多相位发动机驱动型发电机; 一个变换电路，用于将多相交流电压转换成相应的直流（DC）电压为提供至少一种飞行器负载; 电力供应接口（27），用于与外部GPU（28），所述电力供应接口（27）包括耦合到一个独立的电源的电源电压输出端的标准化GPU栓（50）的连接（55的 ）用于驱动worin电源的GPU内部的开关电路（54）提供的低电压的控制信号被从AC电压和DC电压去耦。 本发明还涉及飞机在机场和供电系统。

    PENDULAR CARGO DISPLACER
    25.
    发明公开
    PENDULAR CARGO DISPLACER 审中-公开

    公开(公告)号：EP2164791A1

    公开(公告)日：2010-03-24

    申请号：EP08758247.4

    申请日：2008-06-25

    申请人： Vestergaard, Martin

    发明人： Vestergaard, Martin

    IPC分类号： B66F9/18 ,  B64F1/34 ,  B64F1/32 ,  B66F9/02

    CPC分类号： B66F9/181 ,  B64F1/32 ,  B64F1/368 ,  B66F9/02

    摘要： Loading device using a pendular movement for the displacement of cargo. The loading device consists of a pole (2) and a cable (6), which may be attached to a winch (5). The pole may be telescopic enabling the loading device to obtain different heights.

    摘要翻译： 装载装置使用摆动运动来移动货物。 装载装置包括可连接到绞车（5）的杆（2）和缆绳（6）。 杆可以是伸缩式的，使得加载装置能够获得不同的高度。

    Variable regulator for pneumatic airplane starters
    26.
    发明公开
    Variable regulator for pneumatic airplane starters 失效
    变量调节器fneumzechen Flugzeuganlasser。

    公开(公告)号：EP0473530A1

    公开(公告)日：1992-03-04

    申请号：EP91500101.0

    申请日：1991-08-23

    申请人： Lorente Arcas, Ambrosio

    发明人： Lorente Arcas, Ambrosio

    IPC分类号： F02N7/14 ,  B64F1/34

    CPC分类号： F02N7/14

    摘要： The regulator makes it possible to start different types of airplanes with a single starter, providing it the pressure and air flow required.
    Upon the operator selecting the start step corresponding to the plane to start, the convenient rating of the turbine is set by operating a simple control that controls the flow of fuel to the combustion chamber, using the indications of a sensor that indicates to it the rotation speed achieved by the turbine. When the operation so requires, in order to obtain the pressure and air flow that the airplane needs to start, the system also activates different mechanisms.
    As an alternative, by means of a microprocessor the start step corresponding to the plane to start can be chosen automatically, using the indications of pressure and flow at the inlet of the airplane.

    摘要翻译： 调节器可以使用单个启动器启动不同类型的飞机，为其提供所需的压力和空气流量。 在操作者选择与该平面相对应的开始步骤开始时，通过使用控制向燃烧室的燃料流动的简单控制来设定涡轮机的便利等级，该指示使用向其指示旋转的传感器 涡轮机达到的速度。 当操作需要时，为了获得飞机需要启动的压力和空气流量，系统还激活不同的机制。 作为替代，通过微处理器，可以使用飞机入口处的压力和流量的指示来自动选择与启动平面相对应的起始步骤。

    Self-propelled, electricity generating, hybrid tractor for airport services, for checking the on-board aircraft equipment and for starting-up the aircraft engines
    27.
    发明公开
    Self-propelled, electricity generating, hybrid tractor for airport services, for checking the on-board aircraft equipment and for starting-up the aircraft engines 失效
    自行车，电力生产，机场服务混合拖拉机，用于检查机上飞机设备和启动飞机发动机

    公开(公告)号：EP0350615A3

    公开(公告)日：1991-07-03

    申请号：EP89110119.8

    申请日：1989-06-05

    申请人： SIMAI S.p.A.

    发明人： Garegnani, Luigino

    IPC分类号： B60L11/12 ,  B64F1/34

    CPC分类号： B64F1/34 ,  B60L11/123 ,  F02B3/06 ,  Y02T10/6217 ,  Y02T10/646 ,  Y02T10/7005 ,  Y02T10/7077

    摘要： Electricity generating tractor for various airport services, constituted by an electric-drive car on whose platform a driver's cabin is positioned in its front side, which driver's cabin is provided with control and check instruments, and in its rear side a generator is installed, which consists of a Diesel engine driving a three-phase alternator equipped with a suitable rectifier in order to supply the direct current necessary for causing said car to move, for checking the on-board aircraft instruments from ground level, and for starting up the turbine engines of the aircrafts. Alongside said generator groups of electrical batteries are installed, which are automatically connected with said generator in order to act as back-up batteries; said back-up batteries are suitable for directly powering the car drive motors, and for supplying the necessary electrical energy for starting up the turbine engines of the aircrafts, and for carrying out the on-­board checks in all cases of stopping of said generator.

    摘要翻译： 用于各种机场服务的发电拖拉机，由驾驶室的驾驶室构成，其驾驶室位于其前侧，驾驶室设有控制和检查工具，并在其后侧安装有发电机，其中 由配备有合适的整流器的三相交流发电机驱动的柴油发动机组成，以便提供使所述轿厢移动所需的直流电流，用于从陆地检查机载飞机仪表，以及启动涡轮发动机 的飞机。 在所述发电机组的电池旁安装有与所述发电机自动连接以便用作备用电池的发电机组; 所述备用电池适用于直接为汽车驱动电机供电，并且用于提供用于启动飞行器的涡轮发动机的必需电能，并且用于在所有发生器停止的所有情况下进行车载检查。