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公开(公告)号：WO2016160510A1
公开(公告)日：2016-10-06
申请号：PCT/US2016/024014
申请日：2016-03-24
Applicant: DRESSER-RAND COMPANY
Inventor： WIEDERIEN, Richard J. , MAIER, William C. , SOROKES, James , KUZDZAL, Mark J.
CPC classification number: F04D29/462 , F04D29/668 , F05D2250/51
Abstract: An inlet guide vane assembly for a compressor is provided. The inlet guide vane assembly may include a hub configured to be disposed in an inlet of the compressor, and an inlet guide vane extending from the hub. The inlet guide vane may include a stationary section configured to be coupled with the inlet and a mobile section disposed adjacent the stationary section. The mobile section may include a rod configured to extend through an opening formed in the inlet. The inlet guide vane assembly may also include at least one biasing member disposed about the rod and configured to exert a biasing force on the mobile section to urge the mobile section radially outward.
Abstract translation: 提供了一种用于压缩机的入口导叶组件。 入口引导叶片组件可以包括构造成设置在压缩机的入口中的轮毂和从轮毂延伸的入口导向叶片。 入口引导叶片可以包括构造成与入口联接的固定部分和邻近固定部分设置的移动部分。 移动部分可以包括构造成延伸穿过形成在入口中的开口的杆。 入口引导叶片组件还可以包括围绕杆布置的至少一个偏置构件，其构造成在移动部分上施加偏置力以将径向向外推动移动部件。
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公开(公告)号：WO2016160489A1
公开(公告)日：2016-10-06
申请号：PCT/US2016/023925
申请日：2016-03-24
Applicant: DRESSER-RAND COMPANY
Inventor： LARDY, Pascal , SOROKES, James , KUZDZAL, Mark J.
CPC classification number: F04D29/30 , F04D25/06 , F04D29/058 , F04D29/284 , F04D29/4213 , F04D29/462 , F05D2250/51
Abstract: An impeller includes a hub mountable to a rotary shaft and configured to rotate about a center axis. The impeller may include a plurality of main blades and splitter blades arranged equidistantly and circumferentially about the center axis. A splitter blade having a leading edge and a trailing edge may be positioned between first and second adjacent main blades and canted such that the leading edge is displaced from a blade position equidistant the first and second adjacent main blades a first percentage amount of one half an angular distance between the first and second adjacent main blades. The trailing edge may be displaced from the blade position equidistant the first and second adjacent main blades a second percentage amount of one half the angular distance between the first and second adjacent main blades. The second percentage amount may be greater or less than the first percentage amount.
Abstract translation: 叶轮包括可安装到旋转轴并构造成围绕中心轴线旋转的轮毂。 叶轮可以包括围绕中心轴线等距并且周向布置的多个主叶片和分流叶片。 具有前缘和后缘的分流叶片可以位于第一和第二相邻主叶片之间并且倾斜，使得前缘从与第一和第二相邻主叶片等距离的叶片位置移位，第一百分比量为一半 第一和第二相邻主叶片之间的角距离。 后边缘可以从第一和第二相邻主叶片等距离的叶片位置移位第二和第二相邻主叶片之间的角距离的一半的第二百分比量。 第二百分比量可以大于或小于第一百分比量。
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公开(公告)号：WO2016160480A1
公开(公告)日：2016-10-06
申请号：PCT/US2016/023908
申请日：2016-03-24
Applicant: DRESSER-RAND COMPANY
Inventor： PEER, David J. , TAYLOR, David Andrew , MASSEY, Brian David , LUPKES, Kirk Ryan , WISLER, Scott D. , SOROKES, James , KUZDZAL, Mark J.
CPC classification number: F04D29/5853 , F04D29/0516 , F04D29/284
Abstract: A compressor may include a casing defining a discharge cavity and a seal cavity. A rotary shaft may be disposed in the casing, and a shaft seal assembly may be disposed in the seal cavity and about the rotary shaft. An impeller may be coupled with and configured to be driven by the rotary shaft. A balance piston may be integral with the impeller and may define the discharge cavity and the seal cavity. A balance piston seal may be disposed about the balance piston such that the balance piston seal and the balance piston define a radial clearance therebetween. The radial clearance may be configured to provide fluid communication from the impeller to the discharge cavity. A heat shield may be disposed in the discharge cavity, and may be configured to prevent the conduction of heat from the discharge cavity to the seal cavity via the casing.
Abstract translation: 压缩机可以包括限定排出腔和密封腔的壳体。 旋转轴可以设置在壳体中，并且轴密封组件可以设置在密封腔中并且围绕旋转轴。 叶轮可以与旋转轴联接并构造成由旋转轴驱动。 平衡活塞可以与叶轮成一体，并且可以限定排出腔和密封腔。 平衡活塞密封件可以围绕平衡活塞设置，使得平衡活塞密封件和平衡活塞在其间限定径向间隙。 径向间隙可以被配置为提供从叶轮到排出腔的流体连通。 隔热罩可以设置在排放腔中，并且可以被配置为防止热量经由壳体从排出腔传导到密封腔。
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4.发明申请
公开(公告)号：WO2016160393A1
公开(公告)日：2016-10-06
申请号：PCT/US2016/023388
申请日：2016-03-21
Applicant: DRESSER-RAND COMPANY
Inventor： SOROKES, James , KUZDZAL, Mark J. , BROWN, Paul Morrison , SARETTO, Silvano R. , SRINIVASAN, Ravichandra , SAILER, Logan
CPC classification number: F04D29/444 , F04D17/10 , F05D2250/52
Abstract: A diffuser for a compressor includes an annular diffuser passageway defined by a hub wall and a shroud wall of a housing of the compressor. The annular diffuser passageway may be fluidly coupled with a centrifugal impeller configured to rotate with a rotary shaft of the compressor about a center axis. The diffuser may also include a plurality of low solidity diffuser vanes extending into the annular diffuser passageway from the hub wall or the shroud wall and arranged annularly about the center axis. The diffuser may further include a plurality of high solidity diffuser vanes disposed radially outward from the plurality of low solidity diffuser vanes and extending into the annular diffuser passageway from the hub wall or the shroud wall and arranged annularly about the center axis.
Abstract translation: 用于压缩机的扩散器包括由毂壁和压缩机的壳体的护罩壁限定的环形扩散器通道。 环形扩散器通道可以与配置成围绕中心轴线与压缩机的旋转轴一起旋转的离心式叶轮流体耦合。 扩散器还可以包括多个低固体扩散器叶片，其从轮毂壁或护罩壁延伸到环形扩散器通道中并围绕中心轴线环状布置。 扩散器还可以包括从多个低固体扩散器叶片径向向外设置并从毂壁或护罩壁延伸到环形扩散器通道中并且围绕中心轴线环状布置的多个高固体扩散器叶片。
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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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Patent Agency Ranking
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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公开(公告)号：WO2020106279A1
公开(公告)日：2020-05-28
申请号：PCT/US2018/062033
申请日：2018-11-20
Applicant: DRESSER-RAND COMPANY
Inventor： MOHR, Byron L. , BARNES, Tristen , KUZDZAL, Mark J. , GUERRA, Christopher , MILLER, Harry Francis
Abstract: A bearing and/or seal assembly (10) where pressurized gas (e.g., air) may be arranged to produce a contact-free bearing and/or seal is provided. The assembly includes a permeable body (12) including structural features (13) selectively engineered to convey a pressurized gas (Ps) from an inlet side (20) side of the permeable body to an outlet side (22) of the permeable body to form an annular film of the pressurized gas relative to the rotatable shaft. Disclosed embodiments may be produced by way of three-dimensional (3D) Printing/Additive Manufacturing (AM) technologies with practically no manufacturing variability; and may also cost-effectively and reliably benefit from the relatively complex geometries and the features and/or conduits that may be involved to, for example, form the desired distribution pattern or impart a desired directionality to the pressurized gas conveyed through the permeable body of the bearing and/or seal assembly.
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公开(公告)号：WO2019199318A1
公开(公告)日：2019-10-17
申请号：PCT/US2018/027488
申请日：2018-04-13
Applicant: DRESSER-RAND COMPANY
Inventor： KUZDZAL, Mark J.
IPC: F04D25/06 , F04D17/12 , F04D29/058
Abstract: Single-and multi-stage compressors independently drive impellers in each compressor stage with one or more electric motors that are incorporated in the compressor casing. In multi-stage embodiments, impellers in respective compressor stages are capable of being driven at different rotational speeds. In some embodiments, the electric motor is a ring-type electric motor, where the rotor is coupled to a circumscribing impeller. The rotor in turn circumscribes the stator. In other embodiments, the electric motor is a flat or pancake-type electric motor, where its rotor is coupled to an axial sidewall of the impeller, and its stator is disposed axially outboard of and in opposed relationship with the rotor body. In some embodiments, the compressor stage incorporates a pair of flat or pancake-type electric motors. In some embodiments, rotors of the electric motors have permanent magnet-type rotor magnets, while in other embodiments the rotor magnets are electromagnetic rotor magnets.
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公开(公告)号：WO2019160550A1
公开(公告)日：2019-08-22
申请号：PCT/US2018/018361
申请日：2018-02-15
Applicant: DRESSER-RAND COMPANY
Inventor： SOROKES, James M. , KUZDZAL, Mark J. , EL GHAZZANI, El Mostafa , LARDY, Pascal
Abstract: Compressors achieve in a single stage a high-pressure ratio ( r ) of greater than or equal to 2.5:1 on a process fluid having a molecular weight of 12-20, such as natural gas. Two or more of the compressor stages are combined serially to increase overall pressure ratio. Each single-stage includes respective inlet and outlet passages and an unshrouded, centrifugal impeller that includes a plurality of impeller blades. Process fluid is discharged from trailing edges of the impeller blades at a rotational velocity greater than or equal to 1400 feet/second into a diffuser passage of the outlet. Dimension ranges of the annular diffuser passage, the centrifugal impeller, and the diffuser vanes vary as a function of pressure ratio ( r ) and/or the flow coefficient (φ) of the process fluid flowing between the inlet and the outlet.
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