公开(公告)号：US20160265539A1

公开(公告)日：2016-09-15

申请号：US14642390

申请日：2015-03-09

Applicant: CATERPILLAR INC.

Inventor： Richard E. ANNATI ,  Thomas J. WILLIAMS ,  David E. HARNADEK

IPC: F04D17/10 ,  F04D29/42

CPC classification number: F04D17/10 ,  F04D17/06 ,  F04D29/4206 ,  F04D29/441 ,  F04D29/444

Abstract: A compressor assembly is disclosed. The compressor assembly has a compressor housing. The compressor assembly may also have a compressor impeller disposed within the compressor housing. Further, the compressor assembly may have a bearing housing. The bearing housing may have a body portion and a web. The web may extend outward from the body portion. The bearing housing may also have a bearing housing flange extending radially outward from the web. The bearing housing flange may be configured to be attached to the compressor housing. In addition, the compressor assembly may have a shim disposed between the compressor housing and the bearing housing flange.

Abstract translation: 公开了一种压缩机组件。 压缩机组件具有压缩机壳体。 压缩机组件也可以具有设置在压缩机壳体内的压缩机叶轮。 此外，压缩机组件可以具有轴承壳体。 轴承壳体可以具有主体部分和腹板。 网可以从主体部分向外延伸。 轴承壳体还可以具有从腹板径向向外延伸的轴承壳体凸缘。 轴承壳体凸缘可被构造成附接到压缩机壳体。 此外，压缩机组件可以具有设置在压缩机壳体和轴承壳体凸缘之间的垫片。

公开(公告)号：US20160265549A1

公开(公告)日：2016-09-15

申请号：US14642110

申请日：2015-03-09

Applicant: Caterpillar Inc.

Inventor： Richard E. ANNATI ,  Jeffrey W. McCORMACK ,  Thomas J. WILLIAMS ,  Gary W. POWERS ,  David E. HARNADEK

IPC: F04D29/44 ,  F04D25/04 ,  F04D17/10

CPC classification number: F04D29/441 ,  F04D29/083 ,  F04D29/444 ,  F05D2220/40 ,  F05D2260/38 ,  F05D2300/50212

Abstract: A compressor assembly is disclosed. The compressor assembly may have a compressor housing, which may have an inner wall inclined at a first angle relative to a plane disposed generally orthogonal to a rotational axis of the compressor assembly. The compressor assembly may also have a compressor impeller disposed within the compressor housing. Further, the compressor assembly may have a bearing housing attached to the compressor housing. The bearing housing may have a body portion and a web that may extend outward from the body portion to a web end. The web may be inclined at a second angle relative to the plane. The compressor assembly may have a diffuser ring disposed between the inner wall and the web. The compressor assembly may also have a spring disposed between the web and the diffuser ring. The spring may be configured to apply a generally axial load on the diffuser ring.

Abstract translation: 公开了一种压缩机组件。 压缩机组件可以具有压缩机壳体，其可以具有相对于大致垂直于压缩机组件的旋转轴线设置的平面以第一角度倾斜的内壁。 压缩机组件也可以具有设置在压缩机壳体内的压缩机叶轮。 此外，压缩机组件可以具有附接到压缩机壳体的轴承壳体。 轴承壳体可以具有主体部分和可以从主体部分向腹板端延伸的腹板。 腹板可以相对于平面以第二角度倾斜。 压缩机组件可以具有设置在内壁和腹板之间的扩散器环。 压缩机组件还可以具有布置在卷材和扩散器环之间的弹簧。 弹簧可以构造成在扩散器环上施加大致轴向的载荷。

公开(公告)号：US20160265554A1

公开(公告)日：2016-09-15

申请号：US14642621

申请日：2015-03-09

Applicant: CATERPILLAR INC.

Inventor： Richard E. ANNATI ,  Gary W. POWERS ,  Jeffrey W. McCORMACK ,  Thomas J. WILLIAMS

IPC: F04D29/62 ,  F04D29/42 ,  F04D17/10

CPC classification number: F04D29/624 ,  F01D25/28 ,  F01D25/285 ,  F02C6/12 ,  F04D29/059 ,  F04D29/4206 ,  F05D2220/40 ,  F05D2230/68 ,  F05D2250/281 ,  F05D2260/31

Abstract: A housing for a turbocharger includes a first outer surface, a second outer surface opposite the first outer surface, and a mounting hole extending between the first outer surface and the second outer surface. The mounting hole includes a first end opposite a second end and a counterbore formed at the first end. The counterbore includes threads that are configured to engage with threads on a shank of a lifting device. The mounting hole also includes a throughbore extending from the counterbore to the second end and configured to receive a fastener for mounting the turbocharger housing. The counterbore forms a first opening through the first outer surface of the turbocharger housing, and the throughbore forms a second opening through the second outer surface of the turbocharger housing. The mounting hole is configured to receive only one fastener or shank at a time.

Abstract translation: 用于涡轮增压器的壳体包括第一外表面，与第一外表面相对的第二外表面，以及在第一外表面和第二外表面之间延伸的安装孔。 安装孔包括与第二端相对的第一端和形成在第一端的沉孔。 沉孔包括构造成与提升装置的柄上的螺纹接合的螺纹。 安装孔还包括从沉孔延伸到第二端的通孔，并且构造成容纳用于安装涡轮增压器壳体的紧固件。 沉孔形成通过涡轮增压器壳体的第一外表面的第一开口，并且通孔形成通过涡轮增压器壳体的第二外表面的第二开口。 安装孔被配置为一次仅接收一个紧固件或柄。