AZIMUTHAL ALIGNMENT OF THREE PARTS OF A COMPRESSOR VOLUTE
    2.
    发明公开
    AZIMUTHAL ALIGNMENT OF THREE PARTS OF A COMPRESSOR VOLUTE 有权
    三个压缩机螺旋壳体部分的方位角对准

    公开(公告)号:EP2800905A1

    公开(公告)日:2014-11-12

    申请号:EP12820946.7

    申请日:2012-12-21

    IPC分类号: F04D29/44 F04D29/62 F01D9/02

    摘要: A compressor housing (1) includes a scroll member (2), a shroud member (4), and an annular member (6). The scroll member (2) has a first positioning portion (31), which contacts the shroud member (4) to determine the position of the shroud member (4) in relation to the scroll member (2) in the circumferential direction of the impeller (8), and a second positioning portion (32), which contacts the annular member (6) to determine the position of the annular member (6) in relation to the scroll member (2) in the circumferential direction of the impeller (8). The first positioning portion (31) and the second positioning portion (32) are formed at the same position in the circumferential direction of the impeller (8).

    COMPRESSOR HOUSING FOR TURBOCHARGER AND METHOD FOR MANUFACTURING THE SAME

    公开(公告)号:EP3572674A1

    公开(公告)日:2019-11-27

    申请号:EP19175601.4

    申请日:2019-05-21

    申请人: OTICS Corporation

    IPC分类号: F04D29/42 F04D29/62 F04D29/44

    摘要: A compressor housing 1 for a turbocharger, which is composed of a scroll piece 20, a shroud piece 30, and an outer-circumferential annular piece 40. The scroll piece 20 includes a through part 22 constituting a discharge port 13, a first intermediate wall surface 23 extended from an intake-side wall surface 21 of a scroll chamber 12 and smoothly connected with the discharge port 13, and a scroll outer-circumferential part 24. The outer-circumferential annular piece 40 includes an outer-circumferential annular press-fit part 44 press fitted into the scroll outer-circumferential part 24, and a protruding part 42 bent from an outer-circumference-side wall surface 41 of the scroll chamber 12. The protruding part 42 is inserted into the through part 22 to form an inner wall surface 14a of an intermediate part 14 that communicates the discharge port 13 with the scroll chamber 12. Then, the compressor housing 1 is fixed to a center housing 2 that is made of iron with high rigidity through joining parts 25 provided at the scroll piece 20.

    METHOD FOR PRODUCING COMPRESSOR HOUSING
    4.
    发明公开
    METHOD FOR PRODUCING COMPRESSOR HOUSING 有权
    制造压缩机壳体的方法

    公开(公告)号:EP3173627A1

    公开(公告)日:2017-05-31

    申请号:EP16193708.1

    申请日:2016-10-13

    申请人: OTICS Corporation

    IPC分类号: F04D29/02 F04D29/42 F04D29/62

    摘要: A compressor housing is constructed by assembling a scroll piece and a shroud piece. The scroll piece includes an inlet cylindrical portion 21, a front side wall section 22, and an outlet cylindrical portion 23 in which the inner wall surface of the outlet communicating section is curved to connect an inner wall surface of a scroll chamber and that of an outlet port. Fabrication of the scroll piece includes a die casting step that uses a back mold 4 having a first projecting portion 41 and a front mold 5 having a second projecting portion 51 projecting toward the back side to form an intermediate formed body 20 wherein both the first 41 and second projecting portions 51 are disposed within the outlet cylindrical portion 23, and a cutting and removal step that removes residue portions in the intermediate formed body 20 by cutting.

    摘要翻译: 压缩机壳体通过组装涡旋件和罩件而构成。 涡旋件包括入口圆筒部分21,前侧壁部分22和出口圆筒部分23,出口连通部分的内壁表面弯曲成连接涡旋室的内壁表面和 出口端口。 涡旋件的制造包括压铸步骤,该压铸步骤使用具有第一突出部41的后模4和具有朝向后侧突出的第二突出部51的前模5形成中间成形体20,其中第一41 第二突出部51配置在出口圆筒部23的内部,通过切削除去中间成形体20的残渣部的切断除去工序。

    METHOD FOR PRODUCING COMPRESSOR HOUSING
    7.
    发明授权
    METHOD FOR PRODUCING COMPRESSOR HOUSING 有权
    制造压缩机壳体的方法

    公开(公告)号:EP3173627B1

    公开(公告)日:2018-03-21

    申请号:EP16193708.1

    申请日:2016-10-13

    申请人: OTICS Corporation

    IPC分类号: F04D29/02 F04D29/42 F04D29/62

    摘要: A compressor housing is constructed by assembling a scroll piece and a shroud piece. The scroll piece includes an inlet cylindrical portion 21, a front side wall section 22, and an outlet cylindrical portion 23 in which the inner wall surface of the outlet communicating section is curved to connect an inner wall surface of a scroll chamber and that of an outlet port. Fabrication of the scroll piece includes a die casting step that uses a back mold 4 having a first projecting portion 41 and a front mold 5 having a second projecting portion 51 projecting toward the back side to form an intermediate formed body 20 wherein both the first 41 and second projecting portions 51 are disposed within the outlet cylindrical portion 23, and a cutting and removal step that removes residue portions in the intermediate formed body 20 by cutting.

    COMPRESSOR STRUCTURE FOR TURBOCHARGERS
    8.
    发明公开
    COMPRESSOR STRUCTURE FOR TURBOCHARGERS 有权
    VERDICHTERSTRUKTURFÜRTURBOLADER

    公开(公告)号:EP3015716A1

    公开(公告)日:2016-05-04

    申请号:EP15188949.0

    申请日:2015-10-08

    申请人: OTICS Corporation

    IPC分类号: F04D29/42 F04D29/62

    摘要: A compressor structure for turbochargers (1) including a scroll piece (20), a shroud piece 30 and a seal plate (40) assembled with each other in an axial direction (Y). The scroll piece (20) includes a penetration part (22) penetrating in the axial direction (Y) so as to constitute a discharge port (13) and a first intermediate wall surface (23) smoothly extending from an intake-side wall surface (21) to the discharge port (13). The shroud piece (30) includes an inner circumferential side wall surface (32), and the seal plate (40) includes a protruding part (42) provided with a second intermediate wall surface (43) extending from an outer circumferential side wall surface (41) and facing the first intermediate wall surface (23) so as to constitute an inner wall surface (14a) of an intermediate part (14) through which the discharge port (13) and the scroll chamber (12) are communicated with each other.

    摘要翻译: 一种用于涡轮增压器(1)的压缩机结构,其包括在轴向(Y)上彼此组装的涡旋件(20),护罩片30和密封板(40)。 涡旋件(20)包括沿轴向(Y)贯穿的贯通部(22),以构成排出口(13)和从进气侧壁面平滑地延伸的第一中间壁面(23) 21)连接到排出口(13)。 所述护罩片30具有内周侧壁面32,所述密封板40具有突出部42,所述突出部42具有从外周侧壁面43延伸的第二中间壁面43, 41)并且面向第一中间壁面(23),以构成中间部分(14)的内壁表面(14a),排出口(13)和涡旋室(12)通过该内壁表面彼此连通 。

    Turbocharger
    9.
    发明公开
    Turbocharger 有权
    Turbolader

    公开(公告)号:EP2796687A1

    公开(公告)日:2014-10-29

    申请号:EP14165656.1

    申请日:2014-04-23

    申请人: OTICS Corporation

    IPC分类号: F02C6/12 F02C7/30 F02C6/08

    摘要: A turbocharger 1 includes a compressor housing 2 and a bearing housing 3. The compressor housing 2 has a shroud surface 221 and a diffuser surface 222. The bearing housing 3 has an opposite surface 311 facing the diffuser surface 222. An adhesion preventing part 4 is provided on at least one of the diffuser surface 222 and the opposite surface 311. The turbocharger 1 is configured so that compressed air spouts out from the adhesion preventing part 4 to the diffuser passage 15 by an ejector effect caused when compressed air passes through the diffuser passage 15.

    摘要翻译: 涡轮增压器1包括压缩机壳体2和轴承壳体3.压缩机壳体2具有护罩表面221和扩散器表面222.轴承壳体3具有面向扩散器表面222的相对表面311.防粘附部分4是 设置在扩散器表面222和相对表面311中的至少一个上。涡轮增压器1构造成使得当压缩空气通过扩散器时,压缩空气通过喷射器效应从防附着部分4喷出到扩散通路15 第15段。