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公开(公告)号：US20130343939A1
公开(公告)日：2013-12-26
申请号：US13532783
申请日：2012-06-26
Applicant: Kenneth John Stoddard , Cameron Snow Andersen , Garth L. Mason , Jared M. Mangum
Inventor： Kenneth John Stoddard , Cameron Snow Andersen , Garth L. Mason , Jared M. Mangum
IPC: F15B13/042 , F04B45/04 , F04B7/02
CPC classification number: F15B9/08 , F04B9/105 , F04B9/1056 , F04B53/10 , F15B15/1476 , F15B15/204 , Y10T137/8663
Abstract: A two-step hydraulic valve is described. In an implementation, a two-step hydraulic valve with retrograde spool action has a pilot spool that controls hydraulic force applied to a main spool to switch a rod of a hydraulic actuator back-and-forth between extension and retraction. The main spool is hydraulically driven in retrograde motion to the pilot spool, providing improved reliability and switching action for the valve. The pilot spool also has an overtravel feature that can be used to hyperextend the rod for various purposes. In an example system, the two-step hydraulic valve controls a hydraulic actuator connected to drive a submersible reciprocating pump, such as a diaphragm pump.
Abstract translation: 描述了两步液压阀。 在一个实施方案中，具有逆向阀芯作用的两级液压阀具有先导阀芯，其控制施加到主阀芯的液压力，以在延伸和缩回之间来回切换液压致动器的杆。 主阀芯以逆向运动液压驱动到先导阀芯，为阀门提供改进的可靠性和开关动作。 导向阀芯还具有超行程特征，可以用于将杆伸出以用于各种目的。 在示例系统中，两级液压阀控制连接以驱动潜水往复泵（例如隔膜泵）的液压致动器。
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公开(公告)号：US08827205B2
公开(公告)日：2014-09-09
申请号：US12463207
申请日：2009-05-08
Applicant: Garth L. Mason
Inventor： Garth L. Mason
CPC classification number: B64C25/18 , B64C25/22 , B64C25/30 , Y10T74/18592
Abstract: An electromechanical linear actuator includes a pneumomechanical back-up system to ensure extension of retractable landing gear for landing an aircraft. Structurally, the linear actuator includes a stator forming a channel for receiving a ball screw. Further, the actuator includes a ball screw housing forming a chamber for receiving the ball screw. Specifically, the ball screw and the housing are in threaded engagement to translate rotation of the ball screw into axial extension of the housing. To power electromechanical extension of the actuator, the ball screw is selectively engaged to a motor with a gear train. Importantly, fluid communication between the ball screw housing and a pressurized fluid is selectively provided by a valve. If electromechanical extension of the actuator fails, the gear train is disconnected from the ball screw and the pressurized fluid is introduced into the chamber to drive pneumomechanical extension.
Abstract translation: 机电线性致动器包括气动机械备用系统，以确保用于着陆飞机的可伸缩起落架的延伸。 在结构上，线性致动器包括形成用于接收滚珠丝杠的通道的定子。 此外，致动器包括形成用于容纳滚珠丝杠的腔室的滚珠丝杠壳体。 具体地，滚珠丝杠和壳体是螺纹接合的，以将滚珠丝杠的旋转转移到壳体的轴向延伸。 为了对致动器的机电延伸进行动力，滚珠丝杠选择性地与具有齿轮系的马达接合。 重要的是，滚珠丝杠壳体和加压流体之间的流体连通由阀选择性地提供。 如果执行机构的机电延伸器故障，齿轮系与滚珠丝杠断开，加压流体被引入腔室，以驱动气力机械延伸。
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Patent Agency Ranking
公开(公告)号：US09416885B2
公开(公告)日：2016-08-16
申请号：US13481241
申请日：2012-05-25
Applicant: Cameron Andersen , Jared Mangum , Garth L. Mason , Kenneth John Stoddard , Tyson R. Messick
Inventor： Cameron Andersen , Jared Mangum , Garth L. Mason , Kenneth John Stoddard , Tyson R. Messick
CPC classification number: F16K15/033 , F16K17/0413 , F16K27/0209 , Y10T137/0491 , Y10T137/7922
Abstract: Low profile valves are described. In an embodiment, a tubular member for fluid transport has a valve constructed within a wall of the tubular member for controlling a radial flow of fluid, such as water, oil, or gas, through the wall without impeding the flow of fluid or tools through the tubular member or near the exterior of the tubular member. The low profile valve may be used, for example, in the oil and gas industries as a pressure relief valve or check valve. When used as a pressure relief valve, a load member such as a spring, strap, or rocker arm maintains a backpressure on the valve. Example low profile valves can provide flow control from within a very thin annulus between other components.
Abstract translation: 描述了低通阀。 在一个实施例中，用于流体输送的管状构件具有构造在管状构件的壁内的阀，用于控制通过壁的流体（例如水，油或气体）的径向流动，而不阻碍流体或工具的流动通过 管状构件或管状构件的外部附近。 低压阀可以用于例如石油和天然气工业中作为减压阀或止回阀。 当用作减压阀时，诸如弹簧，带子或摇臂的负载构件在阀上保持背压。 示例性低剖面阀可以在其他部件之间的非常薄的环形空间内提供流量控制。
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公开(公告)号：US08256710B2
公开(公告)日：2012-09-04
申请号：US11855342
申请日：2007-09-14
Applicant: Garth L. Mason , Lane G. Taylor , Daniel E. Cooney
Inventor： Garth L. Mason , Lane G. Taylor , Daniel E. Cooney
Abstract: A trim tab is disclosed for use on an aerodynamic foil that has first and second surfaces which extend between a leading edge and a trailing edge. Structurally, the trim tab includes a tab member that is bounded by slits formed through each surface to extend from the trailing edge toward the leading edge. Also, the tab member is bounded by a slot formed between the slits on the second surface to establish a flange between the slot and the trailing edge. Further, the trim tab includes an actuator that is mounted on the foil between the slot and the leading edge. The actuator includes an actuator arm that is connected to the flange. As a result, extension and retraction of the actuator moves the tab member about a hinge-less tab that is created on the first surface.
Abstract translation: 公开了一种在空气动力学箔上使用的修剪突片，其具有在前缘和后缘之间延伸的第一和第二表面。 在结构上，修剪突片包括突出部件，该突出部件由通过每个表面形成的狭缝限定，以从后缘朝向前缘延伸。 此外，突片构件由形成在第二表面上的狭缝之间的槽限定，以在槽和后缘之间建立凸缘。 此外，修剪片包括安装在插槽和前缘之间的箔上的致动器。 致动器包括连接到凸缘的致动器臂。 结果是，致动器的延伸和缩回使得突片构件围绕在第一表面上形成的无铰链的突片移动。
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公开(公告)号：US20090072085A1
公开(公告)日：2009-03-19
申请号：US11855342
申请日：2007-09-14
Applicant: Garth L. Mason , Lane G. Taylor , Daniel E. Cooney
Inventor： Garth L. Mason , Lane G. Taylor , Daniel E. Cooney
Abstract: A trim tab is disclosed for use on an aerodynamic foil that has first and second surfaces which extend between a leading edge and a trailing edge. Structurally, the trim tab includes a tab member that is bounded by slits formed through each surface to extend from the trailing edge toward the leading edge. Also, the tab member is bounded by a slot formed between the slits on the second surface to establish a flange between the slot and the trailing edge. Further, the trim tab includes an actuator that is mounted on the foil between the slot and the leading edge. The actuator includes an actuator arm that is connected to the flange. As a result, extension and retraction of the actuator moves the tab member about a hinge-less tab that is created on the first surface.
Abstract translation: 公开了一种在空气动力学箔上使用的修剪突片，其具有在前缘和后缘之间延伸的第一和第二表面。 在结构上，修剪突片包括突出部件，该突出部件由通过每个表面形成的狭缝限定，以从后缘朝向前缘延伸。 此外，突片构件由形成在第二表面上的狭缝之间的槽限定，以在槽和后缘之间建立凸缘。 此外，修剪片包括安装在插槽和前缘之间的箔上的致动器。 致动器包括连接到凸缘的致动器臂。 结果是，致动器的延伸和缩回使得突片构件围绕在第一表面上形成的无铰链的突片移动。
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公开(公告)号：US20130312851A1
公开(公告)日：2013-11-28
申请号：US13481241
申请日：2012-05-25
Applicant: Cameron Andersen , Jared Mangum , Garth L. Mason , Kenneth John Stoddard , Tyson R. Messick
Inventor： Cameron Andersen , Jared Mangum , Garth L. Mason , Kenneth John Stoddard , Tyson R. Messick
CPC classification number: F16K15/033 , F16K17/0413 , F16K27/0209 , Y10T137/0491 , Y10T137/7922
Abstract: Low profile valves are described. In an embodiment, a tubular member for fluid transport has a valve constructed within a wall of the tubular member for controlling a radial flow of fluid, such as water, oil, or gas, through the wall without impeding the flow of fluid or tools through the tubular member or near the exterior of the tubular member. The low profile valve may be used, for example, in the oil and gas industries as a pressure relief valve or check valve. When used as a pressure relief valve, a load member such as a spring, strap, or rocker arm maintains a backpressure on the valve. Example low profile valves can provide flow control from within a very thin annulus between other components.
Abstract translation: 描述了低通阀。 在一个实施例中，用于流体输送的管状构件具有构造在管状构件的壁内的阀，用于控制通过壁的流体（例如水，油或气体）的径向流动，而不阻碍流体或工具的流动 管状构件或管状构件的外部附近。 低压阀可以用于例如石油和天然气工业中作为减压阀或止回阀。 当用作减压阀时，诸如弹簧，带子或摇臂的负载构件在阀上保持背压。 示例性低剖面阀可以在其他部件之间的非常薄的环形空间内提供流量控制。
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公开(公告)号：US20100282901A1
公开(公告)日：2010-11-11
申请号：US12463207
申请日：2009-05-08
Applicant: Garth L. Mason
Inventor： Garth L. Mason
CPC classification number: B64C25/18 , B64C25/22 , B64C25/30 , Y10T74/18592
Abstract: An electromechanical linear actuator includes a pneumomechanical back-up system to ensure extension of retractable landing gear for landing an aircraft. Structurally, the linear actuator includes a stator forming a channel for receiving a ball screw. Further, the actuator includes a ball screw housing forming a chamber for receiving the ball screw. Specifically, the ball screw and the housing are in threaded engagement to translate rotation of the ball screw into axial extension of the housing. To power electromechanical extension of the actuator, the ball screw is selectively engaged to a motor with a gear train. Importantly, fluid communication between the ball screw housing and a pressurized fluid is selectively provided by a valve. If electromechanical extension of the actuator fails, the gear train is disconnected from the ball screw and the pressurized fluid is introduced into the chamber to drive pneumomechanical extension.
Abstract translation: 机电线性致动器包括气动机械备用系统，以确保用于着陆飞机的可伸缩起落架的延伸。 在结构上，线性致动器包括形成用于接收滚珠丝杠的通道的定子。 此外，致动器包括形成用于容纳滚珠丝杠的腔室的滚珠丝杠壳体。 具体地，滚珠丝杠和壳体是螺纹接合的，以将滚珠丝杠的旋转转移到壳体的轴向延伸。 为了对致动器的机电延伸进行动力，滚珠丝杠选择性地与具有齿轮系的马达接合。 重要的是，滚珠丝杠壳体和加压流体之间的流体连通由阀选择性地提供。 如果执行机构的机电延伸器故障，齿轮系与滚珠丝杠断开，加压流体被引入腔室，以驱动气力机械延伸。
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