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公开(公告)号：WO1996033358A1
公开(公告)日：1996-10-24
申请号：PCT/GB1996000940
申请日：1996-04-22
Applicant: DRESSER-RAND COMPANY , HOLDCROFT, James, Gerald , AUBER, Philippe, Jacques , RABUTEAU, Michel, Emile, Marie
Inventor： DRESSER-RAND COMPANY , HOLDCROFT, James, Gerald
IPC: F16J15/34
CPC classification number: F16J15/3464 , Y10S277/91
Abstract: The present invention relates to a shaft seal (1) comprising a sealing element (14) mounted co-axially to a rotary sealing ring (10) to form a primary seal between opposed faces thereof to substantially prevent fluid flow across the primary seal. The sealing ring (10) is mounted about the shaft (2) on an inner sleeve (11). The inner sleeve is fixed to the shaft to be axially and rotationally fast. The sealing ring (10) is connected to the inner sleeve (11) by half-moon shaped locking members (12) extending through the inner sleeve (11) outwardly into the sealing ring (10). The locking members (12) lock the sealing ring (10) rotationally and axially fast on the inner sleeve (11).
Abstract translation: 本发明涉及一种轴密封件（1），其包括与旋转密封环（10）同轴安装的密封元件（14），以在其相对的面之间形成主密封件，以基本上防止流体流过主密封件。 密封环（10）围绕轴（2）安装在内套筒（11）上。 内套筒固定在轴上以便轴向和旋转地快速。 密封环（10）通过从内套筒（11）向外延伸到密封环（10）中的半月形锁定件（12）连接到内套筒（11）。 锁定构件（12）在内套筒（11）上旋转地和轴向地快速地锁定密封环（10）。
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公开(公告)号：WO1996033357A1
公开(公告)日：1996-10-24
申请号：PCT/GB1996000939
申请日：1996-04-22
Applicant: DRESSER-RAND COMPANY , HOLDCROFT, James, Gerald , AUBER, Philippe, Jacques
Inventor： DRESSER-RAND COMPANY , HOLDCROFT, James, Gerald
IPC: F16J15/34
CPC classification number: F16J15/3464
Abstract: The present invention relates to a shaft seal (1) comprising a sealing element (14) mounted co-axially to a rotary sealing ring (10) to form a primary seal between opposed faces thereof to substantially prevent fluid flow across the primary seal. The sealing element (14) is urged axially towards the rotary ring (10) by a springs (15) acting between a pusher sleeve (15) connected to the sealing element (14) and a seal housing (19). A secondary seal formed between the pusher sleeve (15) and the housing (19) by a sealing member (20) located in a channel (21) in the pusher sleeve (15).
Abstract translation: 本发明涉及一种轴密封件（1），其包括与旋转密封环（10）同轴安装的密封元件（14），以在其相对的面之间形成主密封件，以基本上防止流体流过主密封件。 通过作用在连接到密封元件（14）的推动器套筒（15）和密封壳体（19）之间的弹簧（15），密封元件（14）被轴向推向旋转环（10）。 通过位于推动套筒（15）中的通道（21）中的密封构件（20）在推动器套筒（15）和壳体（19）之间形成的二次密封。
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公开(公告)号：WO1996022854A1
公开(公告)日：1996-08-01
申请号：PCT/US1996000361
申请日：1996-01-11
Applicant: DRESSER-RAND COMPANY
IPC: B23K15/00
CPC classification number: B23K15/0073 , B23K26/22 , B23K26/242 , B23K26/28
Abstract: Two components (42, 44) are bonded together by placing a layer of braze filler metal between and in contact with the faying surfaces, and then directing a high energy beam (46) through one of the components, through the faying surfaces and the layer of brazer filler metal, and into the second component so as to form a melt-through weld bond (53) centrally located between two braze bonds (54, 55). Relative movement between the high energy beam and the components can be provided so that the high energy beam is always perpendicular to the portion of the faying surfaces in which the weld bond is currently being formed. The two components can be an impeller disc and an impeller cover.
Abstract translation: 两个部件（42,44）通过将一个钎焊填充金属层放置在接合表面之间并与接合表面接触而接合在一起，然后通过其中一个部件引导高能束（46）穿过接合表面和层 的钎焊填料金属，并且进入第二组分，以便形成位于两个钎焊键（54,55）之间的中心位置的熔融熔接焊接（53）。 可以提供高能量束和组件之间的相对运动，使得高能束总是垂直于当前正在形成焊接接合部的接合面的部分。 这两个部件可以是叶轮盘和叶轮盖。
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公开(公告)号：WO1993005357A1
公开(公告)日：1993-03-18
申请号：PCT/US1992007617
申请日：1992-09-09
Applicant: DRESSER-RAND COMPANY
Inventor： DRESSER-RAND COMPANY , SOROKES, James, M.
IPC: G01B01/00
CPC classification number: G01B5/004
Abstract: A device for measuring three-dimensional coordinate position of a blade to validate the position on an impeller having a main guide track (24) with a mounting collar (26) on one end with a secondary guide track securably received on the main guide track. The secondary guide track (46) has an arm member that includes a vertically extending rod. The lower end of the rod is used to contact the coordinate points to be measured on the face of the blade. The X, Y, and Z coordinate measurements of each point along the face of the blade is read from scale indicia located along the main guide track, the secondary guide track and the rod extending down from the secondary guide track.
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公开(公告)号：WO2020251530A1
公开(公告)日：2020-12-17
申请号：PCT/US2019/036319
申请日：2019-06-10
Applicant: DRESSER-RAND COMPANY
Inventor： SANFORD, Joel T.
Abstract: An improved inlet valve system for a cylinder chamber of a reciprocating compressor and a method for utilizing a high pressure gas source to control an inlet valve system for a cylinder chamber of a reciprocating compressor is disclosed. The inlet valve system may include an unloader, a valve assembly including a cylindrical valve body circumferentially disposed about a central axis of the inlet valve system, and a control valve actuator including a control valve body. The valve assembly may include a plurality of inlet valve elements disposed respectively in valve element ports fluidly connected to a control valve passage. A high pressure gas source is utilized to hold open and close the inlet valve elements via the control valve passage in order to control the capacity of the reciprocating compressor.
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Patent Agency Ranking
公开(公告)号：WO2019013898A1
公开(公告)日：2019-01-17
申请号：PCT/US2018/035526
申请日：2018-06-01
Applicant: DRESSER-RAND COMPANY
Inventor： KERTH, Jason M.
Abstract: A pumped heat energy storage (PHES) system (100) including a charging circuit and a discharging circuit effective to balance or split a total heat rejection of the PHES system between the charging circuit and the discharging circuit. The charging circuit may include thermal storage vessels (102, 104) to store thermal energy generated from a first compressor (110). A first heat rejection system (128) is fluidly coupled with the thermal storage vessels to remove thermal energy from the charging circuit. The discharging circuit may include a first turbine (146) fluidly coupled with the thermal storage vessels to extract thermal energy stored in the thermal storage vessels and convert the thermal energy to mechanical energy via an expansion of a second working fluid. A second heat rejection system (156) is fluidly coupled with the thermal storage vessels and the first turbine to remove thermal energy from the discharging circuit.
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公开(公告)号：WO2018034765A1
公开(公告)日：2018-02-22
申请号：PCT/US2017/042488
申请日：2017-07-18
Applicant: DRESSER-RAND COMPANY
Inventor： MOLL, Randall W. , FLURSCHUTZ, Daniel , LUCAS, George M.
Abstract: A drainage system for a stage of a turbine. The drainage system includes at least one annular recess (148) defined in the inner surface (150) of the casing (104) of the turbine and configured to accumulate liquid therein. An axial slot (142) and a radial slot (156) are formed in a diaphragm (112) of the turbine, the axial slot (142) extending between the upstream and downstream faces (134,138) of the diaphragm. The drainage system further includes a tubular member (162) including an axially extending tubular portion (164) disposed in the axial slot (142) and a radially extending tubular portion (166) disposed in the radial slot (156). The radially extending tubular portion (166) is sized and configured to fluidly couple the at least one annular recess (148) and the axially extending tubular portion (164), such that liquid in the at least one annular recess is drained therefrom and discharged from the stage of the turbine via the axially extending tubular portion (164).
Abstract translation:
涡轮机级的排水系统。 排水系统包括至少一个环形凹槽（148），该环形凹槽限定在涡轮的壳体（104）的内表面（150）中，并构造成在其中积聚液体。 在涡轮机的隔膜（112）中形成轴向槽（142）和径向槽（156），轴向槽（142）在隔膜的上游面和下游面（134,138）之间延伸。 排水系统还包括管状构件（162），该管状构件包括设置在轴向槽（142）中的轴向延伸管状部分（164）和设置在径向槽（156）中的径向延伸管状部分（166）。 径向延伸的管状部分（166）的尺寸和结构设计成流体地连接至少一个环形凹槽（148）和轴向延伸的管状部分（164），使得至少一个环形凹槽中的液体从其排出并从 通过轴向延伸的管状部分（164）的涡轮机级。
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公开(公告)号：WO2016160506A1
公开(公告)日：2016-10-06
申请号：PCT/US2016/023989
申请日：2016-03-24
Applicant: DRESSER-RAND COMPANY
Inventor： PEER, David J. , WIEDERIEN, Richard J. , BROWN, Paul Morrison , SOROKES, James , KUZDZAL, Mark J.
CPC classification number: F04D29/0516 , F04D29/284
Abstract: A balance piston seal assembly for a balance piston of a compressor is provided. The balance piston seal assembly may include a balance piston seal, a stationary support, and a gripping assembly disposed between the balance piston seal and the stationary support. The balance piston seal may be configured to be disposed about the balance piston such that an inner radial surface of the balance piston seal and an outer radial surface of the balance piston define a radial clearance therebetween. The stationary support may be configured to be coupled or integral with a casing of the compressor. The gripping assembly may be configured to secure the balance piston seal with the stationary support and to maintain concentricity between the balance piston seal and the balance piston during thermal radial expansion of the balance piston seal relative to the balance piston.
Abstract translation: 提供了一种用于压缩机的平衡活塞的平衡活塞密封组件。 平衡活塞密封组件可包括平衡活塞密封件，固定支撑件和设置在平衡活塞密封件和固定支撑件之间的夹紧组件。 平衡活塞密封件可以构造成围绕平衡活塞设置，使得平衡活塞密封件的内部径向表面和平衡活塞的外径向表面在其间限定径向间隙。 固定支撑件可以被构造成与压缩机的壳体联接或一体。 夹持组件可以被配置为在平衡活塞密封件相对于平衡活塞的热径向膨胀期间将平衡活塞密封件固定在固定支撑件上并且在平衡活塞密封件和平衡活塞之间保持同心度。
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公开(公告)号：WO2016160419A1
公开(公告)日：2016-10-06
申请号：PCT/US2016/023568
申请日：2016-03-22
Applicant: DRESSER-RAND COMPANY
Inventor： LARDY, Pascal , SOROKES, James , KUZDZAL, Mark J. , BROWN, Paul Morrison , SARETTO, Silvano R. , SRINIVASAN, Ravichandra
CPC classification number: F04D13/06 , F04D1/00 , F04D27/0292 , F04D29/441
Abstract: A supersonic compressor including an inlet configured to receive and flow therethrough a process fluid. The supersonic compressor may further include a rotary shaft and a centrifugal impeller coupled therewith. The centrifugal impeller may be configured to impart energy to the process fluid received and to discharge the process fluid therefrom in at least a partially radial direction at an exit absolute Mach number of about one or greater. The supersonic compressor may further include a static diffuser circumferentially disposed about the centrifugal impeller and configured to receive the process fluid therefrom and convert the energy imparted. The supersonic compressor may further include a collector fluidly coupled to and configured to collect the process fluid exiting the diffuser, such that the supersonic compressor is configured to provide a compression ratio of at least about 8:1.
Abstract translation: 一种超音速压缩机，其包括被配置为接收和流过其中的过程流体的入口。 超音速压缩机还可以包括旋转轴和与其连接的离心式叶轮。 离心式叶轮可以被配置为向所接收的过程流体赋予能量，并且在至少部分径向方向上以大约一个或更大的退出绝对马赫数排出其处理流体。 超音速压缩机还可以包括围绕离心式叶轮周向设置的静态扩散器，并被配置为从其接收工艺流体并转换所赋予的能量。 超音速压缩机还可以包括流体耦合到并被构造成收集离开扩散器的工艺流体的收集器，使得超音速压缩机被配置成提供至少约8:1的压缩比。
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公开(公告)号：WO2016160414A1
公开(公告)日：2016-10-06
申请号：PCT/US2016/023545
申请日：2016-03-22
Applicant: DRESSER-RAND COMPANY
Inventor： SOROKES, James , KUZDZAL, Mark J.
CPC classification number: F04D29/102 , F04D13/043 , F04D13/06 , F04D17/10 , F04D25/045 , F04D25/06 , F04D29/0413 , F04D29/0416 , F04D29/043 , F04D29/046 , F04D29/0513 , F04D29/0516 , F04D29/056 , F04D29/083 , F04D29/106 , F04D29/22 , F04D29/284 , F04D29/42
Abstract: A balance piston for a compressor is provided. The balance piston may include an annular body and a seal extending from an axial surface of the annular body. The annular body may be configured to be disposed about and coupled with a rotary shaft of the compressor. The seal may be configured to form a sealing engagement with at least one component of the compressor to prevent a flow of a process fluid from an impeller of the compressor to a seal cavity of the compressor.
Abstract translation: 提供了一种用于压缩机的平衡活塞。 平衡活塞可以包括环形体和从环形体的轴向表面延伸的密封件。 环形体可以被配置为围绕压缩机的旋转轴设置并与其连接。 密封件可以被配置成与压缩机的至少一个部件形成密封接合，以防止工艺流体从压缩机的叶轮流到压缩机的密封腔。
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