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    • 46. 发明公开
    • Composite pressure vessel including fluid port with replaceable seal in composite sidewall structure and method of constructing such fluid port
    • 与具有在复合侧壁上的可移除密封件的流体开口,以及制造这种液体开口的方法由复合材料制成的压力容器中。
    • EP0239407A2
    • 1987-09-30
    • EP87302646.2
    • 1987-03-26
    • Pneumo Abex Corporation
    • Dirkin, William
    • F16J12/00F17C1/06
    • F16J12/00F15B15/149F17C1/16F17C2201/0119F17C2201/035F17C2203/0604F17C2203/0624F17C2203/0663F17C2203/067F17C2203/0673F17C2205/0305F17C2209/2154F17C2260/036F17C2270/0554F17C2270/0563
    • A composite pressure vessel (1) including a fluid port (22) extending through the composite sidewall structure (2) formed by providing a radial hole (26) through the sidewall structure (2) for receipt of an externally removable porting plug (24). The porting plug (24) is retained within the radial hole (26) by threaded engagement in an internally threaded grommet (28) which may either be incorporated into the composite windings (4, 6) of the sidewall structure (2) or held in place against the exterior surface of the sidewall structure (2) by local composite windings (30). At the inner end of the porting plug (24) is a seal groove (38) containing a ring seal (40) which is sized to form a fluid-tight seal around a porting hole (48) in a liner member (8) in the interior of the sidewall structure (2) to prevent fluid leakage between the porting plug (24) and liner member (8). The inner diameter of the seal groove (38) is formed by a reduced diameter end portion (36) at the inner end of the porting plug (24), whereas the outer diameter of the seal groove (38) is formed by a back-up ring (42) surrounding such reduced diameter end portion (36) in radial spaced relation therefrom. The back-up ring (42) is preloaded against the liner member (8) during threading of the porting plug (24) into the grommet (28) to ensure a tight fit between the back-up ring (42) and liner member (8).
    • 复合材料压力容器(1)包括一个流体出口(22)通过复合侧壁结构(2)延伸通过所述侧壁结构(2)用于接收从外部可移除移植插头提供的径向孔(26)(24)而形成 , 移植插头(24)被保持在径向孔(26)通过螺纹接合其可以是结合到所述复合绕组的内部护环螺纹(28)(4,6)的侧壁结构(2)或保持在内 放置靠在侧壁结构(2)由本地复合绕组(30)的外表面。 在移植塞的内端部(24)是含有一个环形密封件(40)的所有其尺寸,以形成围绕在衬套部件上的移植孔(48)以流体密封的密封件(8)的密封槽(38) 侧壁结构(2)的内部,以防止移植插头(24)和衬垫构件(8)之间的流体泄漏。 密封槽的内径(38)是通过在移植插头(24)的内端的直径减小的端部(36)形成,而所述密封槽的外径(38)由背FORMED 挡圈(42),从那里周围在径向间隔开的关系检查缩径端部(36)。 该支撑环(42)的移植插头(24)插入到护环(28)的纸期间靠在衬垫构件(8)预加载,以确保支撑环(42)和衬垫部件之间的紧密配合( 8)。
    • 48. 发明公开
    • Dual tandem composite cylinder assembly
    • Tandemzylinder aus Verbundwerkstoff。
    • EP0174117A1
    • 1986-03-12
    • EP85305777.6
    • 1985-08-14
    • Pneumo Abex Corporation
    • Dirkin, WilliamDouglass, DuaneTootle, James N.Benton, Terry L.
    • F15B15/14F16J10/02B29C63/00
    • F16C7/026B29C63/0021F15B11/0365F15B2215/305
    • Duel tandem composite cylinder assembly (1, 96) includes a cylinder (2) having circumferential or hoop stress windings (20,21) surrounding a pair of hydraulic chambers (3, 4) in series to react the circumferential loads and prevent diametrical expansion of the hydraulic chambers. Longitudinal tension windings (70) extend over substantially the entire length of the cylinder outwardly of the circumferential windings to react the axial loads which the cylinder must contain. Compressive cylinder composite windings (65, 95) are also provided for carrying compressive toads generated within the cylinder. The hydraulic chambers are desirably lined with removable liner members (22, 23) to facilitate changing of seals and refurbishment of the cylinder.
    • 决斗串联复合气缸组件(1,96)包括具有围绕一对液压室(3,4)的圆周或环向应力绕组(20,21)的气缸(2),所述液压室串联以反应所述圆周载荷并防止径向膨胀 液压室。 纵向张力绕组(70)在圆周绕组的基本上整个长度上延伸到圆周绕组外部,以使气缸必须包含的轴向负载反应。 还提供压缩气缸复合绕组(65,95)以承载气缸内产生的压缩载荷。 液压室理想地衬有可拆卸的衬套构件(22,23),以便于密封的更换和气缸的翻新。
    • 49. 发明公开
    • Servo actuator control/damping mechanism
    • Hydraulisch Betriebener Kontroll-oderDämpfungsmechanismus。
    • EP0136005A1
    • 1985-04-03
    • EP84305122.8
    • 1984-07-27
    • Pneumo Abex Corporation
    • Mason, James S.Foerster, David
    • F15B20/00
    • F15B18/00
    • A fluid servo actuator control/damping mechanism (10) and method which utilize and combine the functions of an electro-mechanically driven servo valve (26) to achieve ram (16) or actuator (12,14) fluid flow and load control even after loss of fluid power as well as the main ram position control function under normal operating conditions. The mechanism comprises a main control servo valve (26) including a positionable valve element (34) for selective application of fluid power to a ram (16), a sensor (88) connectable to the ram for providing ram load feedback information, and an electro-mechanical drive (78) operable independently of fluid power for selectively positioning the valve element (34) under normal operating conditions for controlled actuation of the same and, upon loss of fluid power, for providing variable orifices to controllably meter bypass fluid flow across the ram by utilizing the existing metering pattern of the servo valve (26) and modulating the valve element (34) thereof in response to feedback information received from the sensor (88), for actively controlled damping of the ram.
    • 一种流体伺服致动器控制/阻尼机构(10)和方法,其利用并组合机电驱动的伺服阀(26)的功能,以实现冲程(16)或致动器(12,14)即使在损失之后的流体流量和负载控制 的流体动力以及正常运行条件下的主压头位置控制功能。 该机构包括主控伺服阀(26),其包括用于选择性地向冲头(16)施加流体动力的可定位阀元件(34),可连接到压头的传感器(88),用于提供压头负载反馈信息,以及 电动机械驱动器(78)可独立于流体动力操作,用于在正常操作条件下选择性地定位阀元件(34)以便控制其启动,并且在流体动力损失时,用于提供可变孔口以可控地计量旁路流体流动 通过利用伺服阀(26)的现有计量模式并响应于从传感器(88)接收的反馈信息来调节其阀元件(34),以便主动控制压头的阻尼。
    • 50. 发明公开
    • Control actuation system including staged direct drive valve with fault control
    • Kontrollbetätigungssystenmit direkt angetriebenem Stufenventil und Fehlerkontrolle。
    • EP0115925A1
    • 1984-08-15
    • EP84300329.4
    • 1984-01-19
    • Pneumo Abex Corporation
    • Vanderlaan, Robert D.
    • F15B18/00
    • F15B18/00
    • A control actuation system (70) for an aircraft including an electro-mechanically controlled, hydraulically powered actuator (72) for driving a main control valve (26) of a dual hydraulic servo-actuator control system (10). The actuator includes a tandem piston (74) connected to the main control valve (26) which is controllably positioned by a staged valve (125) of relatively short stroke whereby a force motor (218) of minimum size and energy requirements may be used to directly drive the valve. The staged valve (125) includes a linearly movable valve plunger (184) for simultaneously controlling the differential application of fluid pressure from respective hydraulic system on opposed pressure surfaces (94, 96 and 98, 100) of respective piston sections (90, 92) to cause movement of the piston (74) in response to relatively short axial movement of the valve plunger as long as at least one hydraulic system remains operative. Also, the staged valve (125) includes a fault control valve sleeve (130) concentric with the valve plunger (184) which, upon shut-down or failure of both hydraulic systems, moves linearly to render the valve plunger inoperative and release fluid pressure from opposed, corresponding pressure surfaces (94, 96 and 98, 100) of the tandem piston to respective returns therefor through respective centering rate control orifices (118,120, 250, 252) in the fault control valve sleeve (130) as the piston in moved to a neutral position by a centering spring device (254) acting on the main control valve.
    • 一种用于飞行器的控制致动系统(70),其包括用于驱动双液压伺服致动器控制系统(10)的主控制阀(26)的电机械控制的液压动力致动器(72)。 致动器包括连接到主控制阀(26)的串联活塞(74),其通过相对较短行程的分级阀(125)可控地定位,由此可以使用最小尺寸和能量要求的力马达(218)来 直接驱动阀门。 分级阀125包括可直线运动的阀柱塞184,用于同时控制相应的液压系统在相应的活塞部分(90,92)的相对的压力表面(94,96和98,100)上差动地施加流体压力, 以便只要至少一个液压系统保持工作,响应于阀柱塞的相对短的轴向运动而引起活塞(74)的移动。 此外,分级阀125还包括与阀柱塞184同心的故障控制阀套管130,在两个液压系统关闭或故障时,该活塞阀线性移动,使得阀柱塞不起作用并释放流体压力 通过作为活塞的故障控制阀套(130)中的相应的对中速度控制孔(118,120,250,252),从串联活塞的相对的相应的压力表面(94,96和98,100)到相应的回程, 通过作用在主控制阀上的定心弹簧装置(254)移动到中立位置。