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    Top deck surface coating of engine block
    4.
    发明授权
    Top deck surface coating of engine block 有权
    发动机缸体顶板表面涂层

    公开(公告)号：US09353702B2

    公开(公告)日：2016-05-31

    申请号：US14473627

    申请日：2014-08-29

    Applicant: CATERPILLAR INC.

    Inventor： Robert E. Sharp ,  Adam William Ostein ,  Curtis John Graham ,  Jarrod David Moss ,  Bharat Kumar Meduru

    IPC: C23C4/00 ,  F02F7/00 ,  F02F1/00 ,  F02F1/02 ,  C23C4/12

    CPC classification number: F02F7/0095 ,  C23C4/00 ,  C23C4/01 ,  C23C4/02 ,  C23C4/08 ,  C23C4/131 ,  C23C4/18 ,  C23C14/028 ,  C23C14/042 ,  F02F1/004 ,  F02F1/02 ,  F02F7/0002 ,  F02F7/0085

    Abstract: A method of manufacturing an engine block is disclosed. In one embodiment, the method includes providing an engine block including a cylinder bore and a top deck with a head face including a predetermined surface roughness. The method also includes masking the cylinder bore with a masking plug, the masking plug being located at a predetermined insertion distance measured from a masking plug outer surface to the head face. The method further includes applying a corrosion resistant coating to the top deck over the head face and machine finishing the engine block including the coating to the engine block specifications.

    Abstract translation: 公开了一种制造发动机缸体的方法。 在一个实施例中，该方法包括提供包括气缸孔的发动机缸体和具有包括预定表面粗糙度的头部面的顶板。 该方法还包括用掩蔽塞屏蔽气缸孔，掩蔽塞位于从掩蔽塞外表面到头面测量的预定插入距离处。 该方法还包括将抗腐蚀涂层施加到头部表面上的顶部甲板上，以及将包括涂层的发动机缸体整理到发动机缸体规格的机器。

    High-pressure rotating fitting
    5.
    发明授权
    High-pressure rotating fitting 有权

    公开(公告)号：US12163606B2

    公开(公告)日：2024-12-10

    申请号：US17521537

    申请日：2021-11-08

    Applicant: Caterpillar Inc.

    Inventor： Curtis John Graham ,  Christopher Anthony Kinney ,  Robert E. Sharp ,  Ryan Dean Macy

    IPC: F16L27/08 ,  F16C19/06

    Abstract: A fitting has a first housing including a first body and a second body. The first body defines a first channel and a second channel, and second body defines a third channel that is co-planar with the first channel and a fourth channel that is co-planar with the first channel. First bearings are disposed within the first channel and the third channel, where the first bearings rotatably coupled the first housing to the second housing. Additionally, second bearings are disposed within the second channel and the fourth channel, the second bearings rotatably coupling the first housing to the second housing. A plug couples to the first housing, a gasket is disposed between the plug and the first housing, and a passage is defined at least in part by the first housing, the second housing, and the plug.

    INSERT FOR TURBOCHARGER SUPPORT HOUSING
    6.
    发明申请
    INSERT FOR TURBOCHARGER SUPPORT HOUSING 审中-公开
    插入涡轮增压器支撑壳

    公开(公告)号：US20160369657A1

    公开(公告)日：2016-12-22

    申请号：US14740446

    申请日：2015-06-16

    Applicant: Caterpillar Inc.

    Inventor： Robert E. Sharp ,  Jacob P. Fabrizius ,  Jeremiah Keltner ,  Timothy S. Graham ,  Bharat K. Meduru

    IPC: F01D25/28

    CPC classification number: F02B67/10 ,  F02B39/00

    Abstract: An insert for a turbocharger support housing is provided. The insert includes a main body having a first surface and a second surface. The first and second surfaces define a thickness of the main body therebetween. The main body is configured to mate with a wear prone surface of the turbocharger support housing. The insert also includes a plurality of projections extending from the second surface. Each of the plurality of projections has an opening communicating with the first surface and a bottom end of the projection, such that each of the plurality of projections is configured to correspond with a mounting bore on the wear prone surface.

    Abstract translation: 提供了一种用于涡轮增压器支撑壳体的插入件。 插入件包括具有第一表面和第二表面的主体。 第一和第二表面限定其间的主体的厚度。 主体构造成与涡轮增压器支撑壳体的易磨损表面相配合。 插入件还包括从第二表面延伸的多个突起。 多个突起中的每一个具有与突起的第一表面和底端连通的开口，使得多个突起中的每一个被构造成对应于易磨损表面上的安装孔。

    TOP DECK SURFACE COATING
    7.
    发明申请
    TOP DECK SURFACE COATING 有权
    顶层表面涂料

    公开(公告)号：US20160061143A1

    公开(公告)日：2016-03-03

    申请号：US14473627

    申请日：2014-08-29

    Applicant: CATERPILLAR INC.

    Inventor： Robert E. Sharp ,  Adam William Ostein ,  Curtis John Graham ,  Jarrod David Moss ,  Bharat Kumar Meduru

    IPC: F02F7/00 ,  F02F1/02 ,  C23C4/12 ,  F02F1/00

    CPC classification number: F02F7/0095 ,  C23C4/00 ,  C23C4/01 ,  C23C4/02 ,  C23C4/08 ,  C23C4/131 ,  C23C4/18 ,  C23C14/028 ,  C23C14/042 ,  F02F1/004 ,  F02F1/02 ,  F02F7/0002 ,  F02F7/0085

    Abstract: A method of manufacturing an engine block is disclosed. In one embodiment, the method includes providing an engine block including a cylinder bore and a top deck with a head face including a predetermined surface roughness. The method also includes masking the cylinder bore with a masking plug, the masking plug being located at a predetermined insertion distance measured from a masking plug outer surface to the head face. The method further includes applying a corrosion resistant coating to the top deck over the head face and machine finishing the engine block including the coating to the engine block specifications.

    Abstract translation: 公开了一种制造发动机缸体的方法。 在一个实施例中，该方法包括提供包括气缸孔的发动机缸体和具有包括预定表面粗糙度的头部面的顶板。 该方法还包括用掩蔽塞屏蔽气缸孔，掩蔽塞位于从掩蔽塞外表面到头面测量的预定插入距离处。 该方法还包括将抗腐蚀涂层施加到头部表面上的顶部甲板上，以及将包括涂层的发动机缸体整理到发动机缸体规格的机器。

    System and method for determining wear of a worn surface
    8.
    发明授权
    System and method for determining wear of a worn surface 有权
    确定磨损表面磨损的系统和方法

    公开(公告)号：US09404843B2

    公开(公告)日：2016-08-02

    申请号：US14510330

    申请日：2014-10-09

    Applicant: Caterpillar Inc.

    Inventor： Jacob P. Fabrizius ,  Trent A. Simpson ,  Robert E. Sharp ,  Benjamin J. Rasmussen ,  Jarrod D. Moss

    IPC: G01B11/28 ,  G01N3/56 ,  G01M15/04 ,  G01B11/22

    CPC classification number: G01N3/56 ,  G01B11/22 ,  G01M5/0033 ,  G01M15/02 ,  G01M15/042 ,  G01N21/9515 ,  G01N2201/103

    Abstract: A method of determining wear of a worn surface of a machine component includes providing a scanning device at a distance from the worn surface. The method also includes moving at least one of the scanning device and the worn surface relative to the other and generating a set of data points via the scanning device. Each data point of the set of data points is indicative of a depth of a corresponding point on the worn surface relative to a reference plane. The method further includes determining a maximum depth of the worn surface based on the set of data points and comparing the maximum depth to a reference value to determine a next step in a remanufacturing process of the machine component.

    Abstract translation: 确定机器部件的磨损表面的磨损的方法包括提供距磨损表面一定距离的扫描装置。 该方法还包括相对于另一扫描装置和磨损表面中的至少一个移动并经由扫描装置产生一组数据点。 数据点集合中的每个数据点表示磨损表面上相对于参考平面的对应点的深度。 该方法还包括基于该组数据点确定磨损表面的最大深度，并将最大深度与参考值进行比较，以确定机器部件的再制造过程中的下一步骤。

    METHOD OF MANUFACTURING AN ENGINE BLOCK
    9.
    发明申请
    METHOD OF MANUFACTURING AN ENGINE BLOCK 有权
    制造发动机块的方法

    公开(公告)号：US20140165955A1

    公开(公告)日：2014-06-19

    申请号：US13713266

    申请日：2012-12-13

    Applicant: CATERPILLAR INC.

    Inventor： Curtis J. Graham ,  Adam W. Ostein ,  Christian E. Sabotta ,  Robert E. Sharp ,  Trent A. Simpson

    IPC: F02F7/00 ,  B23P6/02

    CPC classification number: F02F7/0021 ,  B23P6/02 ,  F02B2075/025 ,  F02F7/0007 ,  F02F7/0012 ,  F02F7/0053 ,  F05C2201/021 ,  F16J10/00 ,  Y10T29/49233

    Abstract: A method for manufacturing an engine block includes removing material from the top deck of the engine block surrounding a first opening to create a first recessed area, placing a first seal within the first recessed area, positioning a first insert within the first recessed area and against the first seal. The method may also include removing material from the top deck of the engine block surrounding a second opening to create a second recessed area that at least partially overlaps the first recessed area, placing a second seal in the second recessed area and positioning a second insert within the second recessed area and against the second seal.

    Abstract translation: 一种用于制造发动机缸体的方法，包括从围绕第一开口的发动机缸体的顶板移除材料，以形成第一凹陷区域，将第一密封件放置在第一凹陷区域内，将第一嵌件定位在第一凹陷区域内并抵靠 第一印。 该方法还可以包括从围绕第二开口的发动机块的顶板移除材料，以产生至少部分地与第一凹陷区域重叠的第二凹陷区域，将第二密封件放置在第二凹陷区域中并将第二插入件定位在 第二凹陷区域和第二密封件。

    HIGH-PRESSURE ROTATING FITTING
    10.
    发明公开
    HIGH-PRESSURE ROTATING FITTING 审中-公开

    公开(公告)号：US20230143692A1

    公开(公告)日：2023-05-11

    申请号：US17521537

    申请日：2021-11-08

    Applicant: Caterpillar Inc.

    Inventor： Curtis John Graham ,  Christopher Anthony Kinney ,  Robert E. Sharp ,  Ryan Dean Macy

    IPC: F16L27/08 ,  F16C19/06

    CPC classification number: F16L27/0828 ,  F16C19/06 ,  F16L27/0812 ,  F16L27/0841

    Abstract: A fitting has a first housing including a first body and a second body. The first body defines a first channel and a second channel, and second body defines a third channel that is co-planar with the first channel and a fourth channel that is co-planar with the first channel. First bearings are disposed within the first channel and the third channel, where the first bearings rotatably coupled the first housing to the second housing. Additionally, second bearings are disposed within the second channel and the fourth channel, the second bearings rotatably coupling the first housing to the second housing. A plug couples to the first housing, a gasket is disposed between the plug and the first housing, and a passage is defined at least in part by the first housing, the second housing, and the plug.

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