公开(公告)号：US20240200454A1

公开(公告)日：2024-06-20

申请号：US18541945

申请日：2023-12-15

Applicant: Danfoss Power Solutions GmbH & Co OHG

Inventor： Chris Shrive ,  Christian Feller ,  Matthias Liermann

IPC: F01B1/06 ,  F01B25/02

CPC classification number: F01B1/0686 ,  F01B1/0675 ,  F01B25/02

Abstract: A hydraulic control circuit for a hydraulic motor operable at least at two displacements, having a proportional speed control valve with a control valve spool continuously moveable by means of a force generated by a pilot pressure being controlled by a continuously, electrically adjustable pilot valve having an electrical actuator, wherein the control valve spool is moveable between a full-torque end position, a reduced-torque end position, and at least one intermediate position. A time related control current function is provided for controlling the current applied to the electrical actuator for controlling the pilot pressure including a pre-current portion with a constant non-zero current and a current ramp portion during which the current is raised or lowered continuously from a ramp starting current level to an intermediate current level. The current is changed abruptly to a switching current level at the end of the current ramp portion for allowing the movement of the speed control valve spool from one of the two end positions via the at least one intermediate switching position into the other end position.

公开(公告)号：US20220195872A1

公开(公告)日：2022-06-23

申请号：US17603366

申请日：2020-03-30

Applicant: CIRCLE DYNAMICS, INC.

Inventor： James Laurence DOYLE

IPC: F01B1/06 ,  F01B25/02

Abstract: A pneumatic motor for rotating an axle including: a. a housing including: b. an air intake port; c. an air exhaust port; d. at least two cylinders; each cylinder being positioned radially from the axle; e. at least two air channels in communication with each cylinder; f. at least two pistons, each piston attached to the axle by a connecting rod, each piston and respective connecting rod being radially aligned, each piston to be received in one of said at least two cylinders; each connecting rod being attached centrally offset in relation to a central axis of the axle; wherein when one connecting rod and piston are in power stroke, the other connecting rod and piston are in exhaust stroke.

公开(公告)号：US11306590B2

公开(公告)日：2022-04-19

申请号：US16962081

申请日：2019-01-11

Applicant: Graco Minnesota Inc.

Inventor： Martin P. McCormick ,  Benjamin J. Dauwalter ,  Kenneth C. Floer

IPC: F01B31/00 ,  F01B11/00 ,  F04B9/125 ,  F01B31/02 ,  F01B25/02

Abstract: An air motor assembly includes an exhaust block with an exhaust port that conveys exhaust air into an exhaust manifold. The exhaust port includes an expansion chamber that creates a pressure drop in the exhaust gas, thereby decreasing the temperature of the exhaust gas. The expansion chamber is defined between a first wall that is tangential to the air motor cylinder and a second wall that is transverse to an axis of the exhaust port. Poppet valves control actuation of a shuttle. The poppet valves are disposed on the exterior of the air motor assembly and are thermally insulated from the air motor assembly.

公开(公告)号：US10354897B2

公开(公告)日：2019-07-16

申请号：US15697834

申请日：2017-09-07

Applicant: Daifuku Co., Ltd.

Inventor： Takeshi Abe ,  Tadahiro Yoshimoto

IPC: B01D53/02 ,  H01L21/673 ,  H01L21/677 ,  H01L21/67 ,  F01D11/00 ,  F01B25/02

Abstract: A container storage facility has storage portions for storing containers, and supplies a purge gas to the interior of the containers. The container storage facility includes ejection portions that eject the purge gas, a gas supply device that controls the supply flow rate of the purge gas, a main pipe that conducts the purge gas output from the gas supply device, and branch pipes that are branched from the main pipe and are connected to the ejection portions. The ejection portions eject the purge gas regardless of whether or not containers are stored in the storage portions, and the gas supply device controls the supply flow rate of the purge gas so as to increase as the total number of containers stored in the storage portions decreases.

公开(公告)号：US09217396B2

公开(公告)日：2015-12-22

申请号：US12975983

申请日：2010-12-22

Applicant: Ko-Jen Wu

Inventor： Ko-Jen Wu

IPC: F02B33/44 ,  F02B47/08 ,  F01B25/02 ,  F02M25/07 ,  F02C6/12 ,  F01N3/10 ,  F02B29/04 ,  F02B37/00

CPC classification number: F02M25/0712 ,  F01N3/10 ,  F01N2340/06 ,  F02B29/0406 ,  F02B37/00 ,  F02C6/12 ,  F02M26/06 ,  F02M26/09 ,  F02M26/23 ,  F05D2270/082 ,  Y02T10/121

Abstract: According to one embodiment of the invention, a turbine housing includes a turbine inlet in fluid communication with a turbine volute configured to house a turbine wheel, the turbine inlet configured to direct an exhaust gas flow from an engine to the turbine wheel. The turbine housing also includes a turbine outlet in fluid communication with the turbine volute, the turbine outlet configured to direct the exhaust gas flow to an exhaust gas conduit and a first exhaust gas recirculation supply port located on and in fluid communication with the turbine outlet, the first exhaust gas recirculation supply port being configured to direct a portion of the exhaust gas flow to an exhaust gas recirculation supply conduit.

Abstract translation: 根据本发明的一个实施例，涡轮壳体包括与构造成容纳涡轮机叶轮的涡轮蜗壳流体连通的涡轮机入口，涡轮机入口被配置为将排气流从发动机引导到涡轮机叶轮。 涡轮机壳体还包括与涡轮蜗壳流体连通的涡轮机出口，涡轮机出口构造成将废气流引导到位于涡轮出口处并与涡轮机出口流体连通的排气管道和第一排气再循环供应口， 所述第一废气再循环供应端口被配置为将废气流的一部分引导到废气再循环供应管道。

公开(公告)号：US09194259B2

公开(公告)日：2015-11-24

申请号：US13485055

申请日：2012-05-31

Applicant: Douglas Robert Mitchell

Inventor： Douglas Robert Mitchell

IPC: F01B25/02 ,  F01D25/32

CPC classification number: F01D25/32 ,  F05D2220/31

Abstract: Solid particle erosion in a steam turbine is minimized by diverting through angled slots formed in appendages of outer rings of the diaphragms, a portion of the steam from the steam flow path thereby bypassing downstream rotating components. The slot through the first stage appendage lies in communication with a passage through a downstream outer ring of a following stage such that the diverted solid particle containing steam may be extracted from the steam flow path and passed to the feed water heater of the turbine. The slot in the second stage appendage diverts steam from between the first and second stages and about the second stage. Solid particle erosion in various regions, i.e., the trailing edge of the stator vanes, along the surfaces of the buckets and in the regions of the cover and its connection with the buckets as well as the sealing devices is thereby minimized.

Abstract translation: 通过在隔膜的外环的附属物中形成的成角度的槽转向蒸汽涡轮机中的固体颗粒侵蚀，一部分来自蒸汽流动路径的蒸汽绕过下游的旋转部件。 通过第一级附件的槽与通过下一级的下游外环的通道连通，使得含有蒸汽的转向固体颗粒可以从蒸汽流动路径中抽出并传递到涡轮机的给水加热器。 第二级附件中的槽从第一级和第二级之间以及第二级附近转移蒸汽。 因此，在各个区域（即，定子叶片的后缘）沿着桶的表面和盖的区域及其与桶的连接以及密封装置的固体颗粒侵蚀因此被最小化。

公开(公告)号：US09068474B2

公开(公告)日：2015-06-30

申请号：US13750291

申请日：2013-01-25

Applicant: GM GLOBAL TECHNOLOGY OPERATIONS LLC

Inventor： Joel Cowgill

IPC: F02B23/00 ,  F02B33/44 ,  F02B33/00 ,  F01B25/02 ,  F04D29/44 ,  F01D25/16 ,  F02C6/12 ,  F01D17/10 ,  F02B37/00 ,  F02B37/007 ,  F02B37/18

CPC classification number: F01D25/162 ,  F01D17/105 ,  F02B37/002 ,  F02B37/007 ,  F02B37/18 ,  F02C6/12 ,  F05D2220/40 ,  Y02T10/144

Abstract: A turbine housing comprises an exhaust port flange, a turbine discharge flange, a crossover flange, and a bearing support ring. The exhaust port flange is configured for mechanically coupling the turbine housing to a mating structure providing a source of working fluid. The turbine discharge flange is configured for mechanically coupling the turbine housing to an exhaust system. The crossover flange is configured for mechanically coupling the turbine housing to a crossover duct. The bearing support ring is configured for mechanically supporting a bearing, on which a turbine output shaft is supported. The turbine housing defines an inlet plenum, a turbine shroud, and a discharge vent. The exhaust port flange defines an inlet port configured to provide fluid communication between the inlet plenum and the source of working fluid. The turbine shroud defines a fluid expansion flow path for expansion of the stream of working fluid.

Abstract translation: 涡轮壳体包括排气口凸缘，涡轮排出凸缘，交叉凸缘和轴承支撑环。 排气口法兰被构造成将涡轮机壳体机械地联接到提供工作流体源的配合结构。 涡轮排出法兰被构造成将涡轮机壳体机械地联接到排气系统。 交叉法兰被配置为将涡轮机壳体机械地联接到交叉管道。 轴承支撑环被构造成用于机械地支撑支撑涡轮机输出轴的轴承。 涡轮壳体限定入口气室，涡轮罩和排气口。 排气口法兰限定入口端口，该入口端口被配置为提供入口通风室和工作流体源之间的流体连通。 涡轮机罩限定了用于膨胀工作流体流的流体膨胀流动路径。

公开(公告)号：US08851831B2

公开(公告)日：2014-10-07

申请号：US13564738

申请日：2012-08-02

Applicant: Zheng-Heng Sun

Inventor： Zheng-Heng Sun

IPC: F01B25/02 ,  F24F7/06 ,  H05K7/20

CPC classification number: F04D25/0613 ,  F04D25/105 ,  H05K7/20172 ,  Y10T137/7903

Abstract: An electronic device includes an air dam module. The air dam module includes a frame defining a vent, a first rotating member, a second rotating member, and two third rotating members. The first rotating member is rotatably connected to a surface bounding the vent, to vertically block a lower half of the vent by its gravity. The second rotating member is rotatably connected to the surface bounding the vent. The third rotating members are rotatably connected to opposite ends of the second rotating member. The second and third rotating members vertically block an upper half of the vent by their gravities.

Abstract translation: 电子设备包括一个空气坝模块。 空气坝模块包括限定通气口的框架，第一旋转构件，第二旋转构件和两个第三旋转构件。 第一旋转构件可旋转地连接到围绕通气口的表面，以通过其重力垂直地阻挡通气口的下半部。 第二旋转构件可旋转地连接到限定通气口的表面。 第三旋转构件可旋转地连接到第二旋转构件的相对端。 第二和第三旋转构件通过它们的重力垂直地阻挡通气孔的上半部。

公开(公告)号：US08696308B2

公开(公告)日：2014-04-15

申请号：US12899298

申请日：2010-10-06

Applicant: Tim Denholm ,  James Alexander McEwen ,  Tom J. Roberts ,  Robert L. Holroyd ,  Christopher Normington ,  Arun Vijayakumar ,  Stephen Edward Garrett

Inventor： Tim Denholm ,  James Alexander McEwen ,  Tom J. Roberts ,  Robert L. Holroyd ,  Christopher Normington ,  Arun Vijayakumar ,  Stephen Edward Garrett

IPC: F01B25/02 ,  F03D7/00 ,  F04D15/00

CPC classification number: F01D17/162 ,  F01D17/143 ,  F01D17/165 ,  F05D2220/40 ,  F05D2250/25 ,  F05D2250/314

Abstract: According to a first aspect of the present invention there is provided a variable geometry turbine comprising: a turbine wheel mounted for rotation about a turbine axis within a housing, the housing defining an annular inlet surrounding the turbine wheel and defined between first and second inlet sidewalls, the annular inlet being divided into at least two axially offset inlet portions; a cylindrical sleeve axially movable across the annular inlet to vary the size of a gas flow path through the inlet; and a guide for guiding the movement of the cylindrical sleeve, the guide being at least partially located within the inlet at a radially extent of the inlet portions, and extending in an axial direction parallel to the turbine axis.

Abstract translation: 根据本发明的第一方面，提供了一种可变几何涡轮机，其包括：涡轮机叶轮，其安装成围绕壳体内的涡轮机轴线旋转，壳体限定围绕涡轮机叶轮并限定在第一和第二入口侧壁之间的环形入口 所述环形入口被分成至少两个轴向偏移的入口部分; 圆柱形套筒可轴向移动穿过环形入口以改变通过入口的气体流动路径的尺寸; 以及用于引导所述圆柱形套筒的运动的引导件，所述引导件至少部分地位于所述入口的入口部分的径向范围内，并且在平行于所述涡轮机轴线的轴向方向上延伸。

公开(公告)号：US08452516B1

公开(公告)日：2013-05-28

申请号：US13446326

申请日：2012-04-13

Applicant: Becky E. Rose ,  Lisa I. Brilliant

Inventor： Becky E. Rose ,  Lisa I. Brilliant

IPC: G06F19/00 ,  G06G7/70 ,  F02C7/05 ,  B64D33/02 ,  F01D5/14 ,  F01D5/12 ,  F01D25/00 ,  F01D13/02 ,  F01D17/00 ,  F03D11/00 ,  F03B11/00 ,  F04D29/38 ,  F01B25/00 ,  F01B25/02

CPC classification number: B64D45/00 ,  B64D2033/022 ,  F01D17/162 ,  F02C7/05 ,  F02C9/20 ,  F04D27/0292 ,  F04D29/563 ,  F05D2270/114

Abstract: A method of protecting a gas turbine engine according an exemplary aspect of the present disclosure includes, among other things, the steps of determining at least one flight condition of an aircraft and comparing the at least one flight condition to a programmed condition. The method further includes the steps of moving a plurality of inlet vanes of a low pressure compressor from a first position to a second position if the step of comparing the at least one flight condition to the programmed flight condition determines the programmed flight condition are met and deflecting any foreign objects with the plurality of inlet vanes.

Abstract translation: 根据本公开的示例性方面的保护燃气涡轮发动机的方法包括确定飞机的至少一个飞行状况并将至少一个飞行状况与编程状态进行比较的步骤。 该方法还包括以下步骤：如果将至少一个飞行条件与编程的飞行条件进行比较的步骤确定已满足编程的飞行条件，则将低压压缩机的多个入口叶片从第一位置移动到第二位置， 用多个入口叶片偏转任何异物。