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    • 105. 发明申请
    • FLOW CONTROL DEVICE
    • 流量控制装置
    • US20110297254A1
    • 2011-12-08
    • US13131459
    • 2009-12-04
    • Frazer GeddesAtul B. SoodGilbert Alexander Anderson
    • Frazer GeddesAtul B. SoodGilbert Alexander Anderson
    • F16K15/00
    • E21B34/14E21B34/101E21B2034/007Y10T137/7904
    • A flow control device typically for protecting a seal (20) in a valve, wherein a body portion (5) has an orifice (8) allowing fluid flow, and the valve has a control portion (10) to allow and restrict fluid flow through the orifice. The flow control device has a fluid flow controller (30) between the body portion and the control portion in the form of at least one annular ring (35), disposed in a recess in one of the body portion and the control portion (10). The fluid flow controller (30) defines a leak path through the device that is opened and closed by a pressure differential acting across the annular member. Typically the application of a pressure differential across the fluid flow controller moves the ring(s) to one end of the recess and reduces the cross sectional area of the leak path available to the fluid, thereby diffusing the fluid flow through the orifice (8).
    • 一种通常用于保护阀门中的密封件(20)的流量控制装置,其中主体部分(5)具有允许流体流动的孔口(8),并且所述阀门具有控制部分(10),以允许和限制流体流过 孔口。 所述流量控制装置在所述主体部分和所述控制部分之间具有设置在所述主体部分和所述控制部分(10)之一中的凹部中的至少一个环形环(35)形式的流体流量控制器(30) 。 流体流量控制器(30)限定穿过该装置的泄漏路径,其通过作用在环形构件上的压差来打开和关闭。 通常,跨越流体流量控制器的压力差的应用将环移动到凹部的一端,并减小了可用于流体的泄漏路径的横截面面积,从而使流体流动通过孔口(8)扩散, 。
    • 109. 发明申请
    • FUEL FEED DEVICE FOR AVIATION ENGINE
    • 用于航空发动机的燃料送料装置
    • US20110253231A1
    • 2011-10-20
    • US13087745
    • 2011-04-15
    • Bastien DORELoïc Pora
    • Bastien DORELoïc Pora
    • F16K15/00
    • F02C9/263F01D21/02F02C7/232F05D2260/601Y10T137/7837
    • A jet pump (14) is inserted between the low-pressure pump and a high-pressure fuel pump (16). A fuel metering unit (20) includes a metering valve (22) which delivers a regulated fuel flow to a feed line (30), and a bypass valve (24) which diverts to a primary intake (14a) of the jet pump the excess fuel flow supplied by the high-pressure pump. An overspeed protection unit (50) includes a control element (54) of the bypass valve (24) which causes said to fully open in the event of an overspeed of the engine. A shutoff and pressurization checkvalve (42) is mounted on the feed line and controlled by a servo-valve (44) having a high-pressure port (44a) brought to the high fuel pressure, a low-pressure port brought to the pressure of the primary intake (14a) of the jet pump and an output setting the pressure in a control chamber (42a) of the shutoff valve (42) to a value between those prevailing at the high pressure and low pressure ports. In the event of overspeed, the restriction imposed by the jet pump causes a pressure rise at the primary intake of the jet pump, hence a pressure rise in the control chamber of the shutoff valve (42), favoring the closing thereof.
    • 喷射泵(14)插入在低压泵和高压燃料泵(16)之间。 燃料计量单元(20)包括计量阀(22),其将调节的燃料流输送到进料管线(30),以及旁路阀(24),其转移到喷射泵的初级进料口(14a) 由高压泵供应的燃料流量。 超速保护单元(50)包括旁通阀(24)的控制元件(54),其在发动机超速的情况下使其完全打开。 一个关闭和加压止回阀(42)安装在进料管上,由一个带有高压油口(44a)的伺服阀(44)控制,达到高燃油压力, 喷射泵的初级进气口(14a)和将截流阀(42)的控制室(42a)中的压力设定为高压和低压口处的压力之间的值的输出。 在超速的情况下,喷射泵施加的限制导致喷射泵的初级进气口处的压力上升,从而在截止阀(42)的控制室中的压力升高,有利于其关闭。
    • 110. 发明授权
    • Backflow preventer
    • 回流防止器
    • US08037899B2
    • 2011-10-18
    • US12387250
    • 2009-04-30
    • Masaharu MatsubaraYuichi Takeda
    • Masaharu MatsubaraYuichi Takeda
    • F16K15/00
    • F16K15/026F16K17/085Y10T137/3331Y10T137/7838Y10T137/7939Y10T137/87917Y10T137/88054
    • A first check valve has a narrow flow path portion (68) formed between an arcuate portion (46) of the outer periphery (45) of a support member and a second enlarged-diameter portion (11) of a casing. The narrow flow path portion (first portion of an intermediate flow path) is in fluidic communication with a back-pressure chamber (50) defined in the support member at the rear of the top of a valving element through a communicating passage (67) including a gap (66) between the outer periphery of the valving element and the inner periphery of a large-diameter portion (38) and grooves (27) on the rear surface of the top of the valving element. Thus, a low static pressure of fluid flowing through the narrow flow path portion is introduced into the back-pressure chamber to move the valving element by a large differential pressure during the supply of fluid, thereby allowing the valve opening to become larger than in the conventional apparatus and enabling a reduction of pressure losses. An intermediate chamber has a pressure chamber (130) defined therein by using a rigid partition. A high-pressure chamber (131) of the pressure chamber is in communication with the upstream side of the first check valve, and a low-pressure chamber (132) thereof is in communication with the narrow flow path portion. Thus, a valving element (136) is acted upon by a force larger than the differential pressure between the upstream side and an internal flow path (106) of the intermediate chamber, thereby allowing a relief valve (135) to be surely kept closed.
    • 第一止回阀具有形成在支撑构件的外周(45)的圆弧部(46)和壳体的第二扩径部(11)之间的窄流路部(68)。 窄流路部分(中间流路的第一部分)通过连通通道(67)与限定在阀元件顶部后部的支撑构件中的背压室(50)流体连通,该连通通道包括 阀元件的外周与大直径部分(38)的内周之间的间隙(66)和阀元件顶部的后表面上的槽(27)。 因此,流过窄流路部分的流体的低静压被引入到背压室中,以在供给流体期间以较大的压差移动阀元件,从而允许阀开度变大 常规装置并且能够减少压力损失。 中间室具有通过使用刚性隔板限定在其中的压力室(130)。 压力室的高压室(131)与第一止回阀的上游侧连通,低压室(132)与窄流路部连通。 因此,通过大于中间室的上游侧和内部流路(106)之间的压差的力作用阀元件(136),从而允许安全阀(135)可靠地保持关闭。