公开(公告)号：WO2009082702A1

公开(公告)日：2009-07-02

申请号：PCT/US2008/087764

申请日：2008-12-19

Applicant: CATERPILLAR INC. ,  STOCKNER, Alan ,  SHAFER, Scott

Inventor： STOCKNER, Alan ,  SHAFER, Scott

IPC: F02M59/02

CPC classification number: F02M59/442 ,  F02M59/44 ,  F02M63/027 ,  F04B1/0404 ,  F04B1/0421 ,  F04B53/16

Abstract: A pumping element (900) for pressurizing a fluid within a fluid pump (100) has a fuel pump housing (904) disposed around the pumping element (900). A plunger (908) reciprocates within a bore (906) defined in a barrel (122), which define a pressurization chamber (910) into which fluid is pressurized. A flow (409) path is defined between the plunger (908) and the bore (906). The flow (409) path permitting fluid to pass from the pressurization chamber (910) during pressurization of fluid. A collection chamber formed between the plunger (908) and the bore (906) is disposed adjacent to the bore (906). At least one weep opening defined in the barrel (122) is fluidly connected to the collection chamber, and n annular reservoir (306) defined between the barrel (122) and the fuel pump housing (904) is disposed to receive fluid via the at least one weep opening.

Abstract translation: 用于对流体泵（100）内的流体加压的泵送元件（900）具有设置在泵送元件（900）周围的燃料泵壳体（904）。 柱塞（908）在界定在筒体（122）中的孔（906）内往复运动，该孔限定了加压腔（910），流体被加压到该加压室中。 在柱塞（908）和孔（906）之间限定流动（409）路径。 流体（409）允许流体在流体加压期间从加压室（910）通过。 形成在柱塞（908）和孔（906）之间的收集室邻近孔（906）设置。 限定在筒体（122）中的至少一个流体开口流体地连接到收集室，并且限定在筒体（122）和燃料泵壳体（904）之间的n个环形容器（306）被设置成经由管 至少一个哭泣开幕。

公开(公告)号：WO2009058337A1

公开(公告)日：2009-05-07

申请号：PCT/US2008/012329

申请日：2008-10-31

Applicant: CATERPILLAR INC. ,  SHAFER, Scott, F. ,  STOCKNER, Alan, R.

Inventor： SHAFER, Scott, F. ,  STOCKNER, Alan, R.

IPC: F02M59/44 ,  F02M63/00

CPC classification number: F02M59/442 ,  F02M63/0001 ,  Y10T137/85978

Abstract: Mixing a pumped fluid with a lubrication fluid within a pump can undermine the lubricity of the lubrication fluid. In order to reduce mixing of fluids within a pump of the present disclosure, a pump is provided that comprises a housing, a piston, a first annulus, and a second annulus. The housing includes an inlet for the pumped fluid, an inlet for the lubrication fluid provided at a first pressure, and a piston bore fluidly coupled to the inlet for the pumped fluid. The piston is moveable within the piston bore. The first annulus is fluidly coupled to the inlet for the lubrication fluid. The second annulus is configured to be fluidly coupled to a drain circuit provided at a second pressure less than the first pressure. The first annulus and the second annulus are located along the length of the piston bore.

Abstract translation: 将泵送的液体与泵内的润滑液混合可能会破坏润滑液的润滑性。 为了减少本公开的泵内的流体的混合，提供了包括壳体，活塞，第一环和第二环的泵。 壳体包括用于泵送流体的入口，用于在第一压力下提供的润滑流体的入口以及与泵送流体的入口流体耦合的活塞孔。 活塞可在活塞孔内移动。 第一环与流体连接到用于润滑流体的入口。 第二环状结构被配置为流体耦合到在小于第一压力的第二压力下提供的排水回路。 第一环和第二环沿着活塞孔的长度定位。

公开(公告)号：WO2006093596A1

公开(公告)日：2006-09-08

申请号：PCT/US2006/002577

申请日：2006-01-23

Applicant: CATERPILLAR INC. ,  STOCKNER, Alan, R.

Inventor： STOCKNER, Alan, R.

IPC: F16K17/04 ,  F16K15/04

CPC classification number: F02M63/0225 ,  F02M63/0012 ,  F02M63/005 ,  F02M63/025 ,  F16K15/044 ,  F16K17/0406 ,  Y10T137/2582

Abstract: A pressure relief valve (20) includes a valve body (22) defining an inlet (44) configured to receive fluid from a fluid system (10), a pressure control orifice (46) ending in a valve seat (50), and a guideway (52) extending from the valve seat. The pressure relief valve further includes a valve closing member (66) configured to abut the valve seat in a closed position and to be displaced from the valve seat in an open position, thereby releasing pressure from the fluid system. The pressure relief valve also includes a flow member (68) including a stem (70) and a flow plate (74). The stem is operably associated with the valve closing member and is configured to reciprocate within the guideway. The pressure relief valve further includes a valve spring (78) operably associated with the valve body.

Abstract translation: 减压阀（20）包括限定入口（44）的阀体（22），所述入口（44）构造成从流体系统（10）接收流体，结束于阀座（50）的压力控制孔（46） 从阀座延伸的导轨（52）。 压力释放阀还包括阀关闭构件（66），其构造成在关闭位置抵靠阀座并且在打开位置从阀座移位，从而从流体系统释放压力。 减压阀还包括包括杆（70）和流动板（74）的流动构件（68）。 杆与阀关闭构件可操作地相关联并且构造成在导轨内往复运动。 减压阀还包括可操作地与阀体相关联的阀弹簧（78）。

公开(公告)号：WO2011153118A3

公开(公告)日：2012-01-26

申请号：PCT/US2011038487

申请日：2011-05-31

Applicant: CATERPILLAR INC ,  COLDREN DANA ,  STOCKNER ALAN

Inventor： COLDREN DANA ,  STOCKNER ALAN

IPC: F02M55/02 ,  F02M59/44 ,  F02M61/10 ,  F02M61/16

CPC classification number: F02M47/027 ,  F02M45/08 ,  F02M57/023 ,  F02M57/025 ,  F02M63/0033 ,  F02M63/0045 ,  F02M63/0064 ,  F02M63/0225

Abstract: A fuel system (12) includes a plurality of fuel injectors (30) each defining a nozzle supply passage (48), a nozzle outlet (50) and a low pressure space (54). The fuel system (12) includes a plurality of mechanically actuated pressure intensifiers (70) each including a tappet (32) and being positioned partially within one of the fuel injectors (30), and a common rail (44) fluidly connecting with each of the fuel injectors (30). Each of the fuel injectors (30) further includes an injection pressure control mechanism (80) having an injection pressure control valve (82). Each injection pressure control valve (82) blocks the corresponding pressure intensifier (70) from the common rail (44) and fluidly connects the pressure intensifier (80) with the low pressure space (54) at a first position, and fluidly connects the pressure intensifier (80) with the common rail (44) and blocks the pressure intensifier (70) from the low pressure space (54) at a second position. Injecting fuel via operating the fuel system (12) may include operating the fuel system(12) in a low leakage mode where the pressure intensifier (70) displaces fuel at a low pressure, between high pressure injections.

Abstract translation: 燃料系统（12）包括多个燃料喷射器（30），每个燃料喷射器限定喷嘴供应通道（48），喷嘴出口（50）和低压空间（54）。 燃料系统（12）包括多个机械致动的压力增压器（70），每个包括挺杆（32）并且部分地位于燃料喷射器（30）之一内;以及共轨（44），其与 燃料喷射器（30）。 每个燃料喷射器（30）还包括具有喷射压力控制阀（82）的喷射压力控制机构（80）。 每个喷射压力控制阀（82）从共轨（44）阻挡相应的增压器（70）并在第一位置将压力增强器（80）与低压空间（54）流体连接，并将压力 增压器（80）和共轨（44），并且在第二位置处从低压空间（54）阻止增压器（70）。 通过操作燃料系统（12）来注入燃料可以包括以低泄漏模式操作燃料系统（12），其中增压器（70）在高压喷射之间以低压替代燃料。

公开(公告)号：WO2009058283A1

公开(公告)日：2009-05-07

申请号：PCT/US2008/012249

申请日：2008-10-29

Applicant: CATERPILLAR INC. ,  GIBSON, Dennis, H. ,  STOCKNER, Alan, R.

Inventor： GIBSON, Dennis, H. ,  STOCKNER, Alan, R.

IPC: F02M55/00 ,  F02M55/02 ,  F02M61/14

CPC classification number: F02M55/02 ,  F02M55/005 ,  F02M61/14 ,  F02M63/0225

Abstract: A fuel system (12) for an engine (10) is disclosed. The fuel system includes a common rail (34), and a cylinder head (20) having a first bore (46) and a second bore (52) intersecting the first bore. A fuel injector (32) is coupled to the cylinder head and at least partially received within the first bore. The fuel system also includes a one-piece hollow tube (48), extending linearly from the common rail to the fuel injector through the second bore. The one-piece hollow tube is configured to communicate high pressure fuel from the common rail to the fuel injector.

Abstract translation: 公开了一种用于发动机（10）的燃料系统（12）。 燃料系统包括共轨（34）和具有与第一孔相交的第一孔（46）和第二孔（52）的气缸盖（20）。 燃料喷射器（32）联接到气缸盖并且至少部分地容纳在第一孔内。 燃料系统还包括一体式中空管（48），其通过第二孔线从共轨线性地延伸到燃料喷射器。 一体式中空管构造成将来自共轨的高压燃料与燃料喷射器相通。

公开(公告)号：WO2008005384A3

公开(公告)日：2008-01-10

申请号：PCT/US2007/015233

申请日：2007-06-29

Applicant: CATERPILLAR INC ,  BARTLEY, Bradley, E. ,  STOCKNER, Alan, R. ,  MACK, David, C.

Inventor： BARTLEY, Bradley, E. ,  STOCKNER, Alan, R. ,  MACK, David, C.

IPC: F02M59/10 ,  F02M59/44 ,  F02M59/48

Abstract: In one aspect, the present disclosure is directed to a tappet assembly (22) for a machine. The assembly (22) may include a tappet body (24), a pin (26) fixedly mounted in the tappet body (22), and a substantially cylindrical roller (28) mounted about the pin (26). The roller (28) may have a substantially cylindrical outer surface (30) with a circumferential dimension and a width dimension, the width dimension being defined by two lateral edges (31). The roller (26) may be configured to provide rolling contact between the outer surface (30) of the roller (28) and a cam lobe (20). The outer surface (30) of the roller (28) may be crowned such that at maximum operational loading conditions of the machine a footprint of contact pressure from the cam lobe (20) is spread substantially the full width of outer cylindrical surface (30) of the roller (28).

公开(公告)号：WO1983000581A1

公开(公告)日：1983-02-17

申请号：PCT/US1981001076

申请日：1981-08-10

Applicant: CATERPILLAR TRACTOR CO. ,  CEMENSKA, Richard, A. ,  STOCKNER, Alan, R.

Inventor： CATERPILLAR TRACTOR CO.

IPC: H01F07/08

CPC classification number: H01F7/1653

Abstract: La présente invention élimine les désavantages du solénoïde hélicoïdal de l'art antérieur en proposant un agencement unique d'un enroulement de bobine et une construction de noyau modulaire qui non seulement permettent un assemblage rapide et économique de solénoïde de diverses dimensions produisant des forces d'intensité différente mais éliminent la tendance de l'induit à tourner par rapport au noyau. Le solénoïde à réponse rapide (10) comprend un premier et un second organe magnétisables (12, 14) montés de manière télescopique avec un mouvement axial rotatif. Le premier organe interne (12) comprend un nombre sélectionnable de sections modulaires identiques individuelles (16) qui définissent d'une manière collective une pluralité de fentes circulaires espacées longitudinalement (18). Le second organe externe (14) est formé en deux moitiés (14a, 14b) et comprend une pluralité de projections en forme d'anneaux espacées longitudinalement (20) qui s'étendent respectivement dans les fentes (18). On fait tourner certaines de ces sections (16) de 180o pendant l'assemblage de manière à générer des flux de courants dirigés en sens opposés dans les portions d'enroulement (38) des sections adjacentes (16).

公开(公告)号：WO2011153118A2

公开(公告)日：2011-12-08

申请号：PCT/US2011/038487

申请日：2011-05-31

Applicant: CATERPILLAR INC. ,  COLDREN, Dana ,  STOCKNER, Alan

Inventor： COLDREN, Dana ,  STOCKNER, Alan

IPC: F02M55/02 ,  F02M61/10 ,  F02M61/16 ,  F02M59/44

CPC classification number: F02M47/027 ,  F02M45/08 ,  F02M57/023 ,  F02M57/025 ,  F02M63/0033 ,  F02M63/0045 ,  F02M63/0064 ,  F02M63/0225

Abstract: A fuel system (12) includes a plurality of fuel injectors (30) each defining a nozzle supply passage (48), a nozzle outlet (50) and a low pressure space (54). The fuel system (12) includes a plurality of mechanically actuated pressure intensifiers (70) each including a tappet (32) and being positioned partially within one of the fuel injectors (30), and a common rail (44) fluidly connecting with each of the fuel injectors (30). Each of the fuel injectors (30) further includes an injection pressure control mechanism (80) having an injection pressure control valve (82). Each injection pressure control valve (82) blocks the corresponding pressure intensifier (70) from the common rail (44) and fluidly connects the pressure intensifier (80) with the low pressure space (54) at a first position, and fluidly connects the pressure intensifier (80) with the common rail (44) and blocks the pressure intensifier (70) from the low pressure space (54) at a second position. Injecting fuel via operating the fuel system (12) may include operating the fuel system(12) in a low leakage mode where the pressure intensifier (70) displaces fuel at a low pressure, between high pressure injections.

Abstract translation: 燃料系统（12）包括多个燃料喷射器（30），每个燃料喷射器限定喷嘴供应通道（48），喷嘴出口（50）和低压空间（54）。 燃料系统（12）包括多个机械致动的压力增压器（70），每个包括挺杆（32）并且部分位于燃料喷射器（30）之一内;以及共轨（44），其与每个 燃料喷射器（30）。 每个燃料喷射器（30）还包括具有喷射压力控制阀（82）的喷射压力控制机构（80）。 每个喷射压力控制阀（82）从共轨（44）阻挡相应的增压器（70）并在第一位置将压力增强器（80）与低压空间（54）流体连接，并将压力 增压器（80）和共轨（44），并且在第二位置处从低压空间（54）阻止增压器（70）。 通过操作燃料系统（12）来注入燃料可以包括以低泄漏模式操作燃料系统（12），其中增压器（70）在高压喷射之间以低压替代燃料。

公开(公告)号：WO2010129090A2

公开(公告)日：2010-11-11

申请号：PCT/US2010/026594

申请日：2010-03-09

Applicant: CATERPILLAR INC. ,  LEWIS, Stephen, R. ,  STOCKNER, Alan, R. ,  GRANT, Marion, B. ,  GIBSON, Dennis, H. ,  MANUBOLU, Avinash, R.

Inventor： LEWIS, Stephen, R. ,  STOCKNER, Alan, R. ,  GRANT, Marion, B. ,  GIBSON, Dennis, H. ,  MANUBOLU, Avinash, R.

IPC: F02M61/16 ,  F02M61/18 ,  F02M55/02

CPC classification number: C21D10/005 ,  F02M55/02 ,  F02M61/168 ,  F02M61/18 ,  F02M2200/8053 ,  F02M2200/9061 ,  Y10T29/479 ,  Y10T29/49401 ,  Y10T29/49428

Abstract: A metallic fuel system component (14, 50) includes an internal surface (52, 90) and an external surface (54, 92). The metallic fuel system component (14, 50) is made by inducing compressive residual stress in only a portion of the internal surface (52, 90) of the metallic fuel system (10) component by transmitting a laser shock wave (146) through the metallic fuel system (10) component from the external surface (54, 92) to the internal surface (52, 90).

Abstract translation: 金属燃料系统部件（14,50）包括内表面（52,90）和外表面（54,92）。 金属燃料系统部件（14,50）通过在金属燃料系统（10）部件的内表面（52,90）的一部分中仅通过将激光冲击波（146）穿过所述金属燃料系统部件 金属燃料系统（10）组件从外表面（54,92）到内表面（52,90）。

公开(公告)号：WO2008027146A2

公开(公告)日：2008-03-06

申请号：PCT/US2007/017094

申请日：2007-07-31

Applicant: CATERPILLAR INC. ,  STOCKNER, Alan, R. ,  COX, Glenn, B. ,  CHEN, Qiang ,  MCCLURE, Thomas, R. ,  MILLER, Robert, L. ,  WILEY, Stephen, M. ,  GONG, Xiaohui

Inventor： STOCKNER, Alan, R. ,  COX, Glenn, B. ,  CHEN, Qiang ,  MCCLURE, Thomas, R. ,  MILLER, Robert, L. ,  WILEY, Stephen, M. ,  GONG, Xiaohui

IPC: F01N3/025 ,  F02M43/04 ,  F02M61/16

CPC classification number: F01N3/0253 ,  F01N3/2066 ,  F01N3/30 ,  F01N2610/08 ,  F01N2610/1453 ,  F01N2610/1493 ,  F02M43/04 ,  F02M61/162 ,  F02M67/02 ,  F02M69/08 ,  Y02T10/24

Abstract: A fluid injector (42) for an exhaust treatment device (40) is disclosed. The fluid injector may have a housing (70) at least partially forming a fluid chamber (98). The housing may have a central axis (90), and a fluid passageway (80) configured to supply fluid to the fluid chamber. The supply of fluid may be in a tangential direction relative to the central axis.

Abstract translation: 公开了一种用于废气处理装置（40）的流体注射器（42）。 流体注射器可以具有至少部分地形成流体室（98）的壳体（70）。 壳体可以具有中心轴线（90）和被配置为向流体室供应流体的流体通道（80）。 流体的供应可以相对于中心轴线处于切向方向。