MIXED FLOW FAN
    103.
    发明公开
    MIXED FLOW FAN 审中-公开
    混流式风扇

    公开(公告)号:EP3242037A1

    公开(公告)日:2017-11-08

    申请号:EP17169590.1

    申请日:2017-05-04

    摘要: A mixed flow fan and a method of manufacturing a mixed flow fan. The method may include molding a fan wheel with a plurality of blades and a plurality of apertures. The plurality of blades extends radially outward from an axis of rotation and a plurality of apertures arranged with one aperture positioned between each pair of adjacent blades. The method also includes molding a plug having a conical shape. The plug includes a plurality of plugging members arranged circumferentially, where the number of the plurality of plugging members corresponds to the number of the plurality of apertures in the fan wheel. The method further includes welding together the fan wheel and the plug, where each of the plurality of apertures of the fan wheel is sealed by one of the plurality of plugging members of the plug to form a continuous surface.

    摘要翻译: 一种混流风扇和一种制造混流风扇的方法。 该方法可以包括用多个叶片和多个孔模制风扇叶轮。 多个叶片从旋转轴线径向向外延伸,并且多个孔布置成具有位于每对相邻叶片之间的一个孔。 该方法还包括模制具有圆锥形状的塞子。 插头包括多个沿周向布置的插塞构件,其中多个插塞构件的数量对应于风扇轮中的多个孔的数量。 该方法进一步包括将风扇叶轮和塞子焊接在一起,其中风扇叶轮的多个孔中的每一个都被塞子的多个塞子中的一个密封,以形成连续表面。

    FAN ASSEMBLY AND FAN WHEEL ASSEMBLIES
    106.
    发明公开
    FAN ASSEMBLY AND FAN WHEEL ASSEMBLIES 有权
    风扇组件和风扇轮组件

    公开(公告)号:EP2959167A1

    公开(公告)日:2015-12-30

    申请号:EP13712011.9

    申请日:2013-03-06

    IPC分类号: F04D17/06 F04D29/28 F04D29/38

    摘要: Fan assemblies, and in particular fan wheels and stator assemblies for fan assemblies, are disclosed. In one embodiment, the fan wheel includes a wheel back having an outer surface forming one of a curved dome-shape and a truncated cone-shape. The fan wheel may also include a plurality of fan blades radially spaced about and mounted to the outer surface of the wheel back. In one embodiment, each of the fan blades is formed from a segment of an airfoil-shaped aluminum extrusion defining at least one internal cavity. The fan blade first ends can be provided with a compound cut profile with at least one curved cut such that the first end of the blade is mounted flush to the wheel back outer surface. The stator assembly can also be provided with a plurality of stator blades formed from airfoil-shaped aluminum extrusion segments and provided with compound cut profiles.

    摘要翻译: 公开了风扇组件,特别是用于风扇组件的风扇轮和定子组件。 在一个实施例中,风扇轮包括具有形成弯曲圆顶形状和截头圆锥形状之一的外表面的轮背。 风扇叶轮还可以包括多个风扇叶片,所述风扇叶片围绕轮背的外表面径向间隔开并安装到轮背的外表面。 在一个实施例中,每个风扇叶片由限定至少一个内腔的翼型铝挤压件的一段形成。 风扇叶片第一端部可以设有具有至少一个弯曲切口的复合切割轮廓,使得叶片的第一端部安装成与轮背部外表面齐平。 定子组件还可以设置有多个由翼型铝挤压段形成并具有复合切割轮廓的定子叶片。

    Kompakter Diagonallüfter
    107.
    发明公开
    Kompakter Diagonallüfter 审中-公开
    紧凑型斜流式风扇

    公开(公告)号:EP1538340A3

    公开(公告)日:2005-07-13

    申请号:EP04027609.9

    申请日:2004-11-20

    申请人: MINEBEA CO., LTD.

    IPC分类号: F04D25/08 F04D17/06

    CPC分类号: F04D17/06 F04D25/0606

    摘要: Die Erfindung betrifft einen Diagonallüfter mit einem Gehäuse (10), einem durch einen Elektromotor (11) angetriebenen Laufrad (14), dessen Nabe (12) zusammen mit einem das Laufrad umgebenden Luftführungsmantel (17) einen im wesentlichen ringförmigen Strömungskanal (18) mit einer Lufteintrittöffnung (19) und einer Luftaustrittsöffnung (20) definiert. Die Nabe (12) ist als ein sich zur Luftaustrittöffnung (20) hin verbreiternder Kegelstumpf ausgebildet, wobei der Luftführungsmantel (17) im wesentlichen profiliert ausgebildet ist, wobei der Elektromotor (11) mittels im wesentlichen radial nach außen verlaufenden Stegen (16) im Gehäuse (10) gehalten ist. Die Erfindung zeichnet sich dadurch aus, dass die Stege (16) zur Befestigung des Motors im Bereich der Lufteintrittsöffnung (19) des Strömungskanals (18) angeordnet sind.

    VORTEX COMPRESSOR.
    108.
    发明公开
    VORTEX COMPRESSOR. 失效
    涡流压缩机。

    公开(公告)号:EP0646728A4

    公开(公告)日:1995-08-02

    申请号:EP94905268

    申请日:1993-12-27

    IPC分类号: F04D23/00 F04D29/16 F04D17/06

    CPC分类号: F04D23/008 F04D29/161

    摘要: A vortex compressor comprises a housing (1) which is provided with an annular operating channel, an inlet port (2) and a discharge port (3) connected to the annular operating channel, and a cut-off (4) situated between the inlet port (2) and the discharge port (3). The disk (5) of the operating wheel mounted in the housing (1) is provided with a vane rim (6) accomodated in the annular operating channel. The housing (1) and cut-off (4) are provided with interconnnecting openings (7 and 8) which are arch-shaped and eequidistant from the vane rim (6). The inlet and outlet edges of the vane rim (6) are arranged coaxially at the edge of the lateral face of the disk (5). The inlet port (2) is in the form of an opening which is bow shaped and equidistant from the vane rim (6) and situated towards the inlet edges of the vanes, while the opening (7) in the housing (1) and the opening (8) in the cut-off (4) are situated towards the outlet edges of the vanes. The opening (7), the opening of the inlet port (2) and the cut-off are arranged in three segments on a plane perpendicular to the axis of rotation of the disk (5). The segment of the opening of the inlet port (2) is adjacent to the segment of the cut-off (4). Part of the segment of the cut-off (4) coincides with the segment of the opening in the housing, and the opening (8) in the cut-off (4) is situated in the part of the segment of the opening (7) of the housing (1) which coincides with segment of the cut-off (4).

    Mixed-flow compressor
    110.
    发明公开
    Mixed-flow compressor 失效
    对角Verdichter。

    公开(公告)号:EP0446900A1

    公开(公告)日:1991-09-18

    申请号:EP91103850.3

    申请日:1991-03-13

    申请人: HITACHI, LTD.

    IPC分类号: F04D29/44 F04D17/06 F04D29/62

    摘要: A compressor is disclosed wherein a diffuser flow path is curved in a radial direction in the vicinity of an outlet of a mixed-flow turbine (1), and guide vanes (7) each having a height larger than a maximum radius (r b ) at the outlet of the mixed-flow turbine (1) are arranged in the form of a circular wing row at the curved portion on a flow path surface of the diffuser plate (4) located toward a side plate. Thus, it is possible to keep uniform the flow within the diffuser (6) and to enhance the performance of the compressor. In addition, the axial length of the compressor may be shortened to thereby make the compressor compact in size.

    摘要翻译: 公开了一种压缩机,其中扩散器流动路径在混合流动涡轮机(1)的出口附近在径向方向上弯曲,并且每个具有大于最大半径(rb)的高度的导叶(7) 混流式涡轮机(1)的出口在朝向侧板的扩散板(4)的流路表面上的弯曲部分处以圆形翼列的形式布置。 因此,可以使扩散器(6)内的流量保持均匀并且增强压缩机的性能。 此外,可以缩短压缩机的轴向长度,从而使压缩机的尺寸更小。