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    HOME APPLIANCE DOOR AND HOME APPLIANCE
    51.
    发明公开
    HOME APPLIANCE DOOR AND HOME APPLIANCE 审中-公开

    公开(公告)号：EP3159636A4

    公开(公告)日：2018-02-28

    申请号：EP16805957

    申请日：2016-07-14

    申请人： LG ELECTRONICS INC

    发明人： YI MYEONGHA ,  KIM NAMI

    IPC分类号： F25D23/02 ,  A47F3/04 ,  F25B11/00 ,  F25D11/00 ,  F25D21/04 ,  F25D23/06

    CPC分类号： F25D21/04 ,  A47F3/043 ,  A47F3/0434

    摘要： The present invention provides a door for a home appliance including a panel assembly including a front panel defining at least a portion of a front appearance of the door, a rear panel disposed behind the front panel, and a spacer disposed between a peripheral portion of the front panel and a peripheral portion of the rear panel so as to maintain a spacing between the front panel and the rear panel, a frame assembly for supporting the panel assembly, the frame assembly including a side frame disposed along a side surface of the door, the side frame contacting outside air, and a heat transfer structure for transferring heat of outside air from the side frame to an interior region defined between the front panel and the rear panel and between the spacer and a side end of the door, and a home appliance including the same.

    A COOLING DEVICE
    55.
    发明公开
    A COOLING DEVICE 有权
    冷却装置

    公开(公告)号：EP2035758A1

    公开(公告)日：2009-03-18

    申请号：EP07786886.7

    申请日：2007-06-28

    申请人： Arçelik Anonim Sirketi

    发明人： KERPICCI, Husnu ,  KURTULUS, Tolga

    IPC分类号： F25B11/00 ,  F25B11/02 ,  F04F11/02

    CPC分类号： F25B11/02 ,  F04B41/06 ,  F04D25/04 ,  F04F13/00 ,  F25B1/10

    摘要： The present invention relates to a cooling device (1) wherein the refrigerant pressure at the compressor (2) is increased by means of a supercharging device (6) that is connected between the pump-out side of the compressor (2) and the suction side of the compressor (2) and wherein capacity increase of the compressor (2) is provided by decreasing the power required for compression in the compressor (2) and the piston leaks occurring during compression.

    摘要翻译： 本发明涉及一种冷却装置（1），其中压缩机（2）处的制冷剂压力借助于增压装置（6）增加，该增压装置（6）连接在压缩机（2）的泵出侧和吸入口 通过减小压缩机（2）中压缩所需的功率和压缩期间发生的活塞泄漏来提供压缩机（2）的容量增加。

    COLD AIR REFRIGERATING SYSTEM AND TURBOEXPANDER TURBINE FOR THIS SYSTEM
    56.
    发明授权
    COLD AIR REFRIGERATING SYSTEM AND TURBOEXPANDER TURBINE FOR THIS SYSTEM 有权
    冷空调冷和膨胀涡轮该系统

    公开(公告)号：EP1243878B1

    公开(公告)日：2007-11-07

    申请号：EP00989064.1

    申请日：2000-12-27

    申请人： Panin, Alexandr Andreevich

    发明人： PANIN, Alexandr Andreevich ,  PESHKOV, Alexandr Alexeevich ,  RAVIKOVICH, Jury Alexandrovich

    IPC分类号： F25B11/00 ,  F01D5/04 ,  B64D13/06

    CPC分类号： B64D13/06 ,  F01D5/048 ,  F05D2230/90 ,  F05D2240/31 ,  F05D2250/182 ,  F05D2250/61 ,  F25B9/004 ,  F25B9/06 ,  F25B11/04 ,  F25B2341/0014 ,  Y02T50/673

    摘要： The cold air refrigerating system comprises a compressor (1), a dual-chamber heat exchanger (2), a turboexpander (6) and a refrigerating chamber (3), with a fan (5) and air cooler (4) installed therein. The fan (7) is mounted on the same shaft with the turboexpander (6). The front chambers of the heat exchangers (9 and 2), a moisture separator (8) and the second chamber of the heat exchanger (2) are connected. In another embodiment, the system contains a compressor (44) and a turboexpander (49) a dual-chamber heat exchanger (45), a refrigerating chamber (46), with a fan (48) and an air cooler (47) installed therein, a dual-chamber evaporation heat exchanger (51) and a moisture separator (50). The front chambers of the evaporation heat exchangers (51 and 45), the moisture separator (50), turboexpander (49) an air cooler (47) and the second chamber of the heat exchanger (45) are connected in tandem with an inlet of the compressor(44). A bearing disc (67) of a turbine (66) is embodied with interblade bores (69) conjugated through chamfers (70) with the meridian surface of the disk (67). Longitudinal micro-chamfers (71) are made on the surfaces of the chamfers (69). A radius (Rk) of the cross-section of the micro-chamfer (71) constitutes 0.1 - 1.0 of the radius (Rch)of the chamfer (70), the pitch (t) between the micro-chamfers (71) does not exceed two radii (Rk), and the height (h) of the micro-chamfer (71) constitutes (0.2 - 1.0) of the radius (Rk).

    COLD AIR REFRIGERATING SYSTEM AND TURBOEXPANDER TURBINE FOR THIS SYSTEM
    57.
    发明公开
    COLD AIR REFRIGERATING SYSTEM AND TURBOEXPANDER TURBINE FOR THIS SYSTEM 有权
    冷空调冷和膨胀涡轮该系统

    公开(公告)号：EP1243878A4

    公开(公告)日：2005-01-12

    申请号：EP00989064

    申请日：2000-12-27

    申请人： PANIN ALEXANDR ANDREEVICH

    发明人： PANIN ALEXANDR ANDREEVICH ,  PESHKOV ALEXANDR ALEXEEVICH ,  RAVIKOVICH JURY ALEXANDROVICH

    IPC分类号： F25B11/00 ,  B64D13/06 ,  F01D5/04 ,  F25B9/00 ,  F25B9/06 ,  F25B11/04

    CPC分类号： B64D13/06 ,  F01D5/048 ,  F05D2230/90 ,  F05D2240/31 ,  F05D2250/182 ,  F05D2250/61 ,  F25B9/004 ,  F25B9/06 ,  F25B11/04 ,  F25B2341/0014 ,  Y02T50/673

    摘要： An air-cooling device comprises compressor (1). Double cavity heat exchanger (2), turbo expander (6) and the freezing chamber (3) containing fan (5) and air cooler (4). Fan (7) is mounted on the same shaft with the turbo expander (6). The first cavities of the heat exchangers (9 and 2), moist separator (8) and the second cavity of the heat exchanger (2) are connected with the compressor (1) input in sequence. In the other appearance the device comprises compressor (44) and turbo expander (49), double cavity heat exchanger (45), freezing chamber (46) containing fan (48) and air cooler (47), double cavity vaporization heat exchanger (51) and moist separator (50). The first cavities of the vaporization heat exchangers (51 and 45), moist separator (50, turbo expander (49), air cooler (47) and the second cavity of the heat exchanger (45) are in sequence connected with the compressor input (44). The bearing disk (67) of the turbine wheel (66) is constructed with inter blade canals (69) co0njugates by means of the flutes (70) with the meridional disk surface (67). The canal surface (69) contain longitudinal micro canal (71). The radius of the micro canal (71) cross cut IS 0.1 - 1.0 of the radius (Rf) of the flute (70), the pitch (t) between the micro canals (71) is not more than the double radius (Rk) and the height (h) of the micro canal (710 is about 0.2 - 1.0 of the radius (Rk).

    COLD AIR REFRIGERATING SYSTEM AND TURBOEXPANDER TURBINE FOR THIS SYSTEM
    58.
    发明公开
    COLD AIR REFRIGERATING SYSTEM AND TURBOEXPANDER TURBINE FOR THIS SYSTEM 有权
    卡特彼勒食品有限公司

    公开(公告)号：EP1243878A2

    公开(公告)日：2002-09-25

    申请号：EP00989064.1

    申请日：2000-12-27

    申请人： Panin, Alexandr Andreevich

    发明人： PANIN, Alexandr Andreevich ,  PESHKOV, Alexandr Alexeevich ,  RAVIKOVICH, Jury Alexandrovich

    IPC分类号： F25B11/00 ,  F01D5/04

    CPC分类号： B64D13/06 ,  F01D5/048 ,  F05D2230/90 ,  F05D2240/31 ,  F05D2250/182 ,  F05D2250/61 ,  F25B9/004 ,  F25B9/06 ,  F25B11/04 ,  F25B2341/0014 ,  Y02T50/673

    摘要： An air-cooling device comprises compressor (1). Double cavity heat exchanger (2), turbo expander (6) and the freezing chamber (3) containing fan (5) and air cooler (4). Fan (7) is mounted on the same shaft with the turbo expander (6). The first cavities of the heat exchangers (9 and 2), moist separator (8) and the second cavity of the heat exchanger (2) are connected with the compressor (1) input in sequence. In the other appearance the device comprises compressor (44) and turbo expander (49), double cavity heat exchanger (45), freezing chamber (46) containing fan (48) and air cooler (47), double cavity vaporization heat exchanger (51) and moist separator (50). The first cavities of the vaporization heat exchangers (51 and 45), moist separator (50, turbo expander (49), air cooler (47) and the second cavity of the heat exchanger (45) are in sequence connected with the compressor input (44). The bearing disk (67) of the turbine wheel (66) is constructed with inter blade canals (69) co0njugates by means of the flutes (70) with the meridional disk surface (67). The canal surface (69) contain longitudinal micro canal (71). The radius of the micro canal (71) cross cut IS 0.1 - 1.0 of the radius (Rf) of the flute (70), the pitch (t) between the micro canals (71) is not more than the double radius (Rk) and the height (h) of the micro canal (710 is about 0.2 - 1.0 of the radius (Rk).

    摘要翻译： 空气冷却装置包括压缩机（1）。 双腔热交换器（2），涡轮膨胀机（6）和包含风扇（5）和空气冷却器（4）的冷冻室（3）。 风扇（7）与涡轮膨胀机（6）安装在同一轴上。 热交换器（9和2）的第一空腔，湿分离器（8）和热交换器（2）的第二腔室依次与压缩机（1）输入连接。 在另一个外观中，该装置包括压缩机（44）和涡轮膨胀机（49），双腔热交换器（45），包含风扇（48）和空气冷却器（47）的冷冻室（46），双腔蒸发热交换器 ）和湿分离器（50）。 蒸发热交换器（51和45），湿分离器（50，涡轮膨胀机49），空气冷却器（47）和热交换器（45）的第二空腔的第一空腔与压缩机输入端 涡轮叶轮（66）的轴承盘（67）由具有子午盘表面（67）的凹槽（70）共同构成的叶片间槽（69）构成，运河表面（69）包含 纵向微管（71），微通道（71）的半径与沟槽（70）的半径（Rf）交叉切割0.1-1.0，微通道（71）之间的间距（t）不大于 比微管的双半径（Rk）和高度（h）（710为半径的大约0.2-1.0）（Rk）。

    Vorrichtung zum gleichzeitigen Erzeugen von Wärme und Kälte
    59.
    发明公开
    Vorrichtung zum gleichzeitigen Erzeugen von Wärme und Kälte 失效
    同时生产热和冷的设备

    公开(公告)号：EP0367057A3

    公开(公告)日：1991-02-06

    申请号：EP89119595.0

    申请日：1989-10-22

    申请人： FRAUNHOFER-GESELLSCHAFT ZUR FÖRDERUNG DER ANGEWANDTEN FORSCHUNG E.V.

    发明人： Heitland, Herbert, Prof. Dr. Ing. ,  Boy, Elmar, Dipl.-Ing.

    IPC分类号： F25B29/00 ,  F25B11/00 ,  F02C3/36 ,  F02C6/04 ,  F02C6/18

    CPC分类号： F02C6/04 ,  F02C3/36 ,  F02C6/18 ,  F25B9/004 ,  F25B11/00

    摘要： Beschrieben wird eine Vorrichtung zum gleichzeitigen Er­zeugen von Wärme und Kälte auf einem oberhalb und einem unterhalb der Temperatur eines Reservoirs gelegenen Tempe­raturniveau,
    - mit einem ersten Kompressor (KI), der ein Arbeitsmedium mit der Temperatur des Reservoirs verdichtet, und einer Brennkammer (BK), in der ein erster Teil des aus dem ersten Kompressor (KI) austretenden Arbeitsmediums eintritt und isobar erwärmt wird, und die austritts­seitig mit einer ersten Turbine (TI) verbunden ist, die den Kompressor (KI) antreibt, und der austrittsseitig das Arbeitsmedium mit einer höheren Temperatur als der Temperatur des Reservoirs entnehmbar ist,
    - mit einem zweiten Kompressor (KII), in den der zweite Teil des aus dem ersten Kompressor (KI) austretenden Arbeitsmediums eintritt, und der austrittsseitig über einen Wärmetauscher (WTII), der mit einem Wärmeaus­tausch-Medium mit der Temperatur des Reservoirs gekühlt wird, mit der Eintrittsseite einer zweiten Turbine (TII) verbunden ist, die den zweiten Kompressor (KII) antreibt, und der austrittsseitig ein nutzbares kaltes Arbeitsmedium mit einer niedrigeren Temperatur als der Temperatur des Reservoirs entnehmbar ist.

    摘要翻译： 给出了一种用于在位于高于和低于储存器温度的温度水平的温度水平上同时产生热和冷的装置的描述， - 具有第一压缩机（KI），其中工作介质的温度为 储存器被压缩，并且燃烧室（BK），其中从第一压缩机（KI）出来的工作介质的第一部分进入并被等压加热，并且在出口侧连接到第一涡轮机（TI） ，其驱动压缩机（KI），并且工作介质可以在出口侧以比储存器的温度高的温度从出口侧排出， - 具有第二压缩机（KII），其中第二部分工作 从第一压缩机（KI）出来的介质经由热交换器（WTII）在出口侧连接，热交换器（WTII）在储存器的温度下被热交换介质冷却到第二涡轮机的入口侧 （TII），其驱动第二压缩机（KII），并且可以在比储存器的温度低的温度下在出口侧从其中取出有用的冷加工介质。