ENGINE-DRIVEN WORKING MACHINE
    3.
    发明公开
    ENGINE-DRIVEN WORKING MACHINE 审中-公开
    发动机驱动工作机

    公开(公告)号:EP3219951A1

    公开(公告)日:2017-09-20

    申请号:EP17152867.2

    申请日:2017-01-24

    Abstract: An engine-driven working machine capable of reducing an opening of an outer case to be small, and decreasing the number of components is provided. An engine-driven working machine 10 is a generator in which an inverter 27 is provided at a suction side of a cooling fan 17, and a fuel tank 25 is provided over the inverter 27. The generator 10 includes an intake port 36 that is formed in an outer case 12, and a first air guide passage 61 that is formed by a tank bottom portion 38 of the fuel tank 25. The intake port 36 is formed in a lower side part 12b of a tank front wall 37, in the outer case 12. The first air guide passage 61 is formed by the tank bottom portion 38 that is inclined with a falling gradient toward the inverter 27 from the intake port 36.

    Abstract translation: 提供一种能够将外壳的开口减小并且减少部件数量的发动机驱动式作业机械。 发动机驱动式作业机械10是在冷却风扇17的吸入侧设置逆变器27,在该逆变器27的上方设置燃料箱25的发电机。发电机10具有: 在外壳12内,由燃料箱25的箱底部38形成的第一空气引导通道61.吸入口36形成在箱前壁37的下侧部12b, 壳体12.第一导风路61由从进气口36朝向逆变器27倾斜成倾斜的罐底部38形成。

    AUXILIARY POWER UNIT WITH COMBINED COOLING OF GENERATOR
    5.
    发明公开
    AUXILIARY POWER UNIT WITH COMBINED COOLING OF GENERATOR 审中-公开
    HILFSTRIEBWERK MIT KOMBINIERTERKÜHLUNGEINES发电机

    公开(公告)号:EP3133266A1

    公开(公告)日:2017-02-22

    申请号:EP16183260.5

    申请日:2016-08-08

    Abstract: An auxiliary power unit (10) for an aircraft, including an internal combustion engine (12) having a liquid coolant system, a generator (64) drivingly engaged to the internal combustion engine (12) and having a liquid coolant system distinct from the liquid coolant system of the internal combustion engine (12), a first heat exchanger (66) in fluid communication with the liquid coolant system of the internal combustion engine (12), a second heat exchanger (68) in fluid communication with the liquid coolant system of the generator (64), an exhaust duct (70) in fluid communication with air passages (66b, 68b) of the heat exchangers (66, 68), and a fan (78) received in the exhaust duct (70) and rotatable by the internal combustion engine (12) for driving a cooling air flow through the air passages (66b, 68b). The liquid coolant system of the engine (12) may be distinct from fuel and lubricating systems of the auxiliary power unit (10).

    Abstract translation: 一种用于飞行器的辅助动力单元(10),包括具有液体冷却剂系统的内燃机(12),与所述内燃机(12)驱动接合并具有不同于所述液体的液体冷却剂系统的发电机(64) 内燃机(12)的冷却剂系统,与内燃机(12)的液体冷却剂系统流体连通的第一热交换器(66),与液体冷却剂系统流体连通的第二热交换器 ,与所述热交换器(66,68)的空气通道(66b,68b)流体连通的排气管道(70)和容纳在所述排气管道(70)中的可旋转的风扇(78) 通过用于驱动通过空气通道(66b,68b)的冷却空气流的内燃机(12)。 发动机(12)的液体冷却剂系统可以不同于辅助动力单元(10)的燃料和润滑系统。

    MODULE SYSTEM FOR FORMATION OF A RADIATOR DEVICE, AND CHARGE AIR COOLER AND RADIATOR LIQUID COOLER FORMED BY SUCH A MODULE SYSTEM
    6.
    发明公开
    MODULE SYSTEM FOR FORMATION OF A RADIATOR DEVICE, AND CHARGE AIR COOLER AND RADIATOR LIQUID COOLER FORMED BY SUCH A MODULE SYSTEM 审中-公开
    用于形成加热装置和系统的冷却器和加热冷水机组模块化系统,模块化系统的组成

    公开(公告)号:EP2652282A4

    公开(公告)日:2017-01-25

    申请号:EP11849127

    申请日:2011-11-28

    Applicant: SCANIA CV AB

    Abstract: Module system for formation of a radiator device (1''') for a motor vehicle comprising a basic module (10) and two or more supplementary modules (40, 40') which are connectable to the basic module. Each module comprises an inlet tank (11, 41), an outlet tank (12, 42) and a radiator element (13, 43) which extends between the inlet tank and the outlet tank. The first inlet tank (11) of the basic module is provided with a first connecting outlet at an upper end and a second connecting outlet at a lower end, each of which outlets is connectable to the second inlet of the inlet tank (41) of respective supplementary modules. The first outlet tank (12) of the basic module is similarly provided with a first connecting inlet at an upper end and a second connecting inlet at a lower end, each of which connecting inlets is connectable to the outlet of the outlet tank (42) of respective supplementary modules.

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