公开(公告)号：US5862897A

公开(公告)日：1999-01-26

申请号：US662413

申请日：1996-06-10

申请人： John Martin Allport ,  David William Henry Tennant

发明人： John Martin Allport ,  David William Henry Tennant

IPC分类号： F16F15/173 ,  F16F7/10

CPC分类号： F16F15/173

摘要： A torsional vibration damper has a rotational axis and an annular housing having inner and outer members. The housing has an annular channel in which an inertia member is received. The channel has axially extending walls and is closed by an annular cover plate to retain the inertia member The inner edge of the cover plate is received in a rabbet in the inner channel wall and is joined to the wall by means of a weld. The inner and outer members are connected by an annular weld at a central hub. The weld may extend between two radial extremes which are separated by a distance substantially greater than the thickness of weld. The damper is easier to manufacture and assemble and has greater structural integrity.

摘要翻译： 扭转振动阻尼器具有旋转轴线和具有内部和外部构件的环形壳体。 壳体具有环形通道，容纳惯性构件。 通道具有轴向延伸的壁，并且由环形盖板封闭以保持惯性构件。盖板的内边缘被容纳在内通道壁中的滚珠内，并且通过焊接接合到壁。 内部和外部构件通过环形焊接在中心毂处连接。 焊缝可以在两个径向极限之间延伸，这两个极限极限远远大于焊缝的厚度。 阻尼器更容易制造和组装，并具有更大的结构完整性。

公开(公告)号：US07798774B2

公开(公告)日：2010-09-21

申请号：US12321190

申请日：2009-01-16

申请人： John Martin Allport ,  Georgina Chiu ,  Clive Robert Martin

发明人： John Martin Allport ,  Georgina Chiu ,  Clive Robert Martin

IPC分类号： F04D29/42

CPC分类号： F02C6/12 ,  F01D9/026 ,  F02B37/025 ,  Y02T10/144 ,  Y10S415/915

摘要： A turbine housing (13) for a radial flow turbine, particularly a turbine used in an exhaust gas turbocharger. The housing has a general volute shape with a substantially annular part extending around the turbine axis and an inlet duct (20) extending therefrom. The inlet duct (20) has a first wall facing part of the outer surface of the annular part of the housing, a pair of spaced webs (44) extending from the outer surface of the circular part of the housing to the first wall, the webs defining a valley (45) therebetween. The arrangement renders the housing stiffer and less prone to fatigue cracking.

摘要翻译： 用于径向流动涡轮机的涡轮机壳体（13），特别是用于排气涡轮增压器中的涡轮机。 壳体具有一般的蜗壳形状，具有围绕涡轮机轴线延伸的大致环形部分和从其延伸的入口管道（20）。 入口管道（20）具有面对壳体的环形部分的外表面的一部分的第一壁，一对隔开的腹板（44），其从壳体的圆形部分的外表面延伸到第一壁， 腹板在其间限定一个谷（45）。 该装置使壳体更硬，并且不容易发生疲劳开裂。

公开(公告)号：US20090238689A1

公开(公告)日：2009-09-24

申请号：US12322351

申请日：2009-01-30

申请人： Zahir Jamil ,  John Martin Allport

发明人： Zahir Jamil ,  John Martin Allport

IPC分类号： F04D29/056 ,  F16C33/10 ,  G06F17/50 ,  B21D53/10

CPC分类号： F01D25/166 ,  F02C6/12 ,  F05D2220/40 ,  F05D2260/96 ,  F16C17/02 ,  F16C17/18 ,  F16C17/26 ,  F16C33/1045 ,  F16C2360/24 ,  Y10T29/49647

摘要： A turbocharger shaft is supported for rotation about its axis in a bearing housing by a pair of floating ring bearings disposed between the shaft and the bearing housing. The floating ring bearings are penetrated in a substantially radial direction by a plurality of apertures to allow the passage of lubricating oil between inner and outer surfaces of the ring. The apertures are arranged at irregular angular intervals around the ring so as to prevent the generation of sub-synchronous vibrations that occur during rotation of the turbocharger shaft. This reduces turbocharger noise and increases life.

摘要翻译： 涡轮增压器轴被支撑成通过设置在轴和轴承壳体之间的一对浮动环轴承围绕其轴线在轴承壳体中旋转。 浮动环轴承通过多个孔径向贯穿大致径向，以允许润滑油在环的内表面和外表面之间通过。 孔围绕环布置成不规则的角度间隔，以防止在涡轮增压器轴旋转期间产生副同步振动。 这样可以降低涡轮增压器的噪音并延长使用寿命。

公开(公告)号：US06955252B2

公开(公告)日：2005-10-18

申请号：US10475250

申请日：2002-04-08

申请人： John Martin Allport

发明人： John Martin Allport

IPC分类号： F16D3/12 ,  F16F15/12 ,  F16F15/124 ,  F16H55/36 ,  F16D3/34

CPC分类号： F16H55/36 ,  F16D3/12 ,  F16F15/12 ,  F16F15/124 ,  F16H2055/366

摘要： The present invention relates to a device for isolating torque fluctuations of a rotary drive shaft. The device comprises a first member (2) for connection to the drive shaft, a second member (3) for connection to a driven member and an intermediate member (21) interposed between the first and second members. The intermediate member comprises a radially outer ring (22) connected to the first member, a radially inner ring (24) connected to the second member and at least one resilient rolling element (32) in a cavity between the inner and outer rings. The cavity is defined by alignment of at least one pair of recesses (26, 29), one recess being on the radially inner surface of the outer ring and the other recess being on the outer surface of the inner ring, each recess having a ramped surface. Relative rotation of the first and second members causes relative rotation of the inner and outer rings so that the rolling element rotates and compresses.

摘要翻译： 本发明涉及用于隔离旋转驱动轴的转矩波动的装置。 该装置包括用于连接到驱动轴的第一构件（2），用于连接到从动构件的第二构件（3）和插入在第一构件和第二构件之间的中间构件（21）。 中间构件包括连接到第一构件的径向外环（22），连接到第二构件的径向内环（24）和在内圈和外圈之间的空腔中的至少一个弹性滚动元件（32）。 空腔由至少一对凹槽（26,29）的对准限定，一个凹槽位于外圈的径向内表面上，另一个凹槽位于内圈的外表面上，每个凹槽具有斜坡 表面。 第一和第二构件的相对旋转引起内环和外环的相对旋转，使得滚动体旋转并压缩。

公开(公告)号：US20090129920A1

公开(公告)日：2009-05-21

申请号：US12321190

申请日：2009-01-16

申请人： John Martin Allport ,  Georgina Chiu ,  Clive Robert Martin

发明人： John Martin Allport ,  Georgina Chiu ,  Clive Robert Martin

IPC分类号： F04D29/42 ,  B22D23/00

CPC分类号： F02C6/12 ,  F01D9/026 ,  F02B37/025 ,  Y02T10/144 ,  Y10S415/915

摘要： A turbine housing (13) for a radial flow turbine, particularly a turbine used in an exhaust gas turbocharger. The housing has a general volute shape with a substantially annular part extending around the turbine axis and an inlet duct (20) extending therefrom. The inlet duct (20) has a first wall facing part of the outer surface of the annular part of the housing, a pair of spaced webs (44) extending from the outer surface of the circular part of the housing to the first wall, the webs defining a valley (45) therebetween. The arrangement renders the housing stiffer and less prone to fatigue cracking.

摘要翻译： 用于径向流动涡轮机的涡轮机壳体（13），特别是用于排气涡轮增压器中的涡轮机。 壳体具有一般的蜗壳形状，具有围绕涡轮机轴线延伸的大致环形部分和从其延伸的入口管道（20）。 入口管道（20）具有面对壳体的环形部分的外表面的一部分的第一壁，一对隔开的腹板（44），其从壳体的圆形部分的外表面延伸到第一壁， 腹板在其间限定一个谷（45）。 该装置使壳体更硬，并且不容易发生疲劳开裂。