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公开(公告)号：US09303563B2
公开(公告)日：2016-04-05
申请号：US13654645
申请日：2012-10-18
CPC分类号： F02C7/232 , F23K5/147 , F23N1/002 , F23N2005/185 , F23N2035/16 , F23N2037/02
摘要： A fluid flow valve includes a movable valve piston positioned in a valve body, the valve piston configured to flow a fluid therethrough. A metering window is interactive with the movable valve piston to meter flow through the movable valve piston. A flow meter is positioned at the valve piston to measure a flow rate of fluid through the valve piston. A valve controller is operable connected to the flow meter and the movable valve piston to control position of the valve piston based on flow rate measured at the flow meter.
摘要翻译： 流体流动阀包括定位在阀体中的可动阀活塞，阀活塞构造成使流体流过其中。 计量窗口与可移动阀活塞交互，以计量通过可移动阀活塞的流量。 流量计定位在阀活塞处以测量通过阀活塞的流体的流速。 阀控制器可操作地连接到流量计和可移动阀活塞，以基于在流量计测量的流量来控制阀活塞的位置。
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公开(公告)号：US09212608B2
公开(公告)日：2015-12-15
申请号：US13902104
申请日：2013-05-24
CPC分类号： F02C9/263 , F02C7/232 , Y10T137/0318 , Y10T137/86517
摘要： A method of metering fuel with a fuel valve. The method includes arranging a spool within to a sleeve along an axis, wherein the spool includes four seal lands. The sleeve includes a fuel inlet aperture, a fuel outlet aperture, and a shutoff port. A first cavity and a second cavity are defined between the spool, the sleeve, and subsets of the seal lands. The fuel inlet port and the fuel outlet port abut one such cavity. Sliding the spool along the axis results in the fuel outlet aperture extending longitudinally beyond the second seal land in the upstream direction.
摘要翻译： 一种用燃料阀计量燃料的方法。 该方法包括将线轴沿着轴线布置在套筒内，其中线轴包括四个密封接合面。 套筒包括燃料入口孔，燃料出口孔和关闭端口。 第一腔和第二腔被限定在阀芯，套管和密封垫的子集之间。 燃料入口和燃料出口邻接一个这样的空腔。 沿着轴线滑动线轴导致燃料出口孔在上游方向上纵向延伸超过第二密封台肩。
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公开(公告)号：US09194302B2
公开(公告)日：2015-11-24
申请号：US13880997
申请日：2011-10-14
申请人： Bruno Robert Gaully , Cecile Marot
发明人： Bruno Robert Gaully , Cecile Marot
摘要： A control of a fuel metering device for a turbine engine as a function of a weight flow rate setpoint includes responding to at least one validity criterion to select a weight flow rate from among: a weight flow rate calculated as a function of a position signal; a weight flow rate calculated as a function of the position signal and of at least one temperature measurement signal; a weight flow rate calculated as a function of the position signal and of at least one permittivity measurement signal; a weight flow rate calculated as a function of the position signal, of at least one temperature measurement signal, and of at least one permittivity measurement signal; and a weight flow rate calculated as a function of a temperature measurement signal, of a permittivity measurement signal, and of a volume flow rate measurement signal.
摘要翻译： 作为重量流量设定点的函数的用于涡轮发动机的燃料计量装置的控制包括响应至少一个有效性标准，以从以下各项中选择重量流量：根据位置信号计算的重量流量; 作为位置信号和至少一个温度测量信号的函数计算的重量流量; 作为位置信号和至少一个介电常数测量信号的函数计算的重量流量; 至少一个温度测量信号和至少一个介电常数测量信号的作为位置信号的函数计算的重量流量; 以及作为温度测量信号，介电常数测量信号和体积流量测量信号的函数计算的重量流量。
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公开(公告)号：US20150330311A1
公开(公告)日：2015-11-19
申请号：US14278888
申请日：2014-05-15
CPC分类号： F02C7/232 , F02C9/263 , F02M59/34 , F02M59/366 , F02M63/0015 , F02M63/004 , F02M63/0078 , F16K31/0651 , F16K31/0693
摘要： A fuel metering valve includes a main flow path extending axially between an inlet and an outlet. Also included is a plunger disposed around a portion of a plunger guide, the plunger and the plunger guide configured to translate between an open position and a closed position to selectively distribute a fuel flowing through the main flow path to the outlet of the fuel metering valve. Further included is a solenoid coil disposed between a solenoid outer body and a solenoid inner body, the solenoid coil configured to magnetically attract the plunger to the open position. Yet further included is a secondary flow path for routing a stagnant volume of fuel upon translation of the plunger from the closed position to the open position.
摘要翻译： 燃料计量阀包括在入口和出口之间轴向延伸的主流路。 还包括设置在柱塞引导件的一部分周围的柱塞，柱塞和柱塞导向器构造成在打开位置和关闭位置之间平移，以选择性地将流过主流路的燃料分配到燃料计量阀的出口 。 进一步包括设置在螺线管外部主体和螺线管内部主体之间的螺线管线圈，螺线管线圈构造成将柱塞磁吸引到打开位置。 还包括二次流动路径，用于在柱塞从关闭位置平移到打开位置时路由停滞的燃料量。
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公开(公告)号：US20150315981A1
公开(公告)日：2015-11-05
申请号：US14268605
申请日：2014-05-02
摘要： A fuel supply system includes a fuel line path configured to route a fuel to a combustion inlet region. Also included is a flow manipulation member disposed proximate the fuel line path, the flow manipulation member comprising a piezoelectric material configured to cyclically manipulate a mass flow pressure of the fuel being routed through the fuel line path.
摘要翻译： 燃料供给系统包括配置成将燃料路由到燃烧入口区域的燃料路径路径。 还包括设置在燃料管线路径附近的流动操作构件，流动操纵构件包括压电材料，该压电材料构造成循环地操纵经过燃料管线路径被路由的燃料的质量流量压力。
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公开(公告)号：US09133771B2
公开(公告)日：2015-09-15
申请号：US13576634
申请日：2011-02-01
申请人： Hideki Ogata , Kazuhiko Ohyama , Tomoyuki Hatano , Akihiro Shimizu , Touya Miwa
发明人： Hideki Ogata , Kazuhiko Ohyama , Tomoyuki Hatano , Akihiro Shimizu , Touya Miwa
CPC分类号： F02C7/232 , F02C7/228 , F02C9/34 , F23K5/06 , F23K5/147 , F23K2301/206 , F23N1/007 , F23N2035/24 , F23N2037/02 , F23N2037/10 , F23R3/28 , F23R3/343 , Y02T50/672
摘要： A fuel supply device of a gas turbine engine is provided. The fuel supply device includes a fuel divider which divides fuel supplied from a collecting fuel passage to feed the fuel to a pilot fuel passage and to a main fuel passage. The fuel divider includes a movable member which is movable according to fuel pressure at the fuel entrance and opens and closes pilot ports and main ports according to a distance of the movement of the movable member. When the fuel pressure at the fuel entrance is not higher than a predetermined value, the fuel is supplied only to the pilot fuel passage, while when the fuel pressure at the fuel entrance is higher than the predetermined value, the fuel is supplied to the pilot fuel passage and to the main fuel passage.
摘要翻译： 提供燃气轮机的燃料供给装置。 燃料供给装置包括燃料分配器，该燃料分配器将从收集燃料通道供应的燃料分配以将燃料供给到先导燃料通道和主燃料通道。 燃料分配器包括可根据燃料入口处的燃料压力移动的可动构件，并根据可移动构件的运动距离打开和关闭先导口和主端口。 当燃料入口处的燃料压力不高于预定值时，仅将燃料供给到先导燃料通道，而当燃料入口处的燃料压力高于预定值时，燃料被供给到飞行员 燃料通道和主燃料通道。
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公开(公告)号：US09038397B2
公开(公告)日：2015-05-26
申请号：US14247575
申请日：2014-04-08
IPC分类号： F02C1/00 , F02C7/06 , F02K99/00 , F02C7/12 , F02C3/08 , F02C7/224 , F02C7/232 , F02C9/48 , G05B15/02 , G05D7/06
CPC分类号： F02C7/12 , F01D25/12 , F02C3/08 , F02C7/06 , F02C7/08 , F02C7/14 , F02C7/224 , F02C7/232 , F02C9/00 , F02C9/48 , F05D2220/32 , F05D2260/213 , G05B15/02 , G05D7/06 , Y02T50/675
摘要： A gas turbine engine according to an exemplary embodiment of this disclosure, among other possible things includes a fan. A geared architecture is configured for driving the fan. A turbine section is configured for driving the geared architecture. A thermal management system that includes a first fluid circuit and a second fluid circuit that manage heat generated in at least a portion of the gas turbine engine. A first heat exchanger is incorporated into each of the first fluid circuit and the second fluid circuit. A second heat exchanger is incorporated into the first fluid circuit. A valve controls an amount of a first fluid that is communicated to the first heat exchanger and the second heat exchanger. A controller is configured to control a positioning of the valve. The amount of the first fluid communicated to the first heat exchanger is based on a first characteristic of a second fluid and the amount of the first fluid communicated to the second heat exchanger is based on a second characteristic of the second fluid. A method and a system are also disclosed.
摘要翻译： 根据本公开的示例性实施例的燃气涡轮发动机以及其它可能的事情包括风扇。 齿轮架构配置为驱动风扇。 涡轮机部分被配置用于驱动齿轮架构。 一种热管理系统，其包括第一流体回路和第二流体回路，其管理在燃气涡轮发动机的至少一部分中产生的热量。 第一热交换器被并入到第一流体回路和第二流体回路的每一个中。 第二热交换器被并入到第一流体回路中。 阀门控制与第一热交换器和第二热交换器连通的第一流体的量。 控制器被配置为控制阀的定位。 与第一热交换器连通的第一流体的量基于第二流体的第一特性，并且与第二热交换器连通的第一流体的量基于第二流体的第二特性。 还公开了一种方法和系统。
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公开(公告)号：US09022056B2
公开(公告)日：2015-05-05
申请号：US13750034
申请日：2013-01-25
CPC分类号： F17D3/00 , F02C7/232 , F02C9/38 , F05D2270/3015 , Y10T137/2496 , Y10T137/2564 , Y10T137/6579
摘要： A device includes a first hot fuel bleed, a second cold fuel bleed, a fuel pressure regulator including a fuel inlet line, a fuel outlet line and a fuel pressure set point line, the pressure of the outlet line being set by the regulator to a fixed divergence from the pressure of the set point line, a first connector to connect the first bleed to the inlet line of the regulator and the second bleed to the set point line of the regulator, when a first pressure of the first bleed is greater than or equal to a second pressure of the second bleed and to connect the first bleed to the set point line of the regulator and the second bleed to the inlet line of the regulator when the first pressure is lower than the second pressure, and a second connector.
摘要翻译： 一种装置包括第一热燃料泄放，第二冷燃料泄放，包括燃料入口管线的燃料压力调节器，燃料出口管线和燃料压力设定点线，出口管线的压力由调节器设定为 与设定点线的压力固定偏离，第一连接器，用于将第一渗液连接到调节器的入口管线，并且第二泄放到调节器的设定点线，当第一次流出的第一压力大于 或等于所述第二泄放的第二压力，并且当所述第一压力低于所述第二压力时，将所述第一泄漏与所述调节器的设定点线连接并且将所述第二泄放连接到所述调节器的入口管线，以及第二连接器 。
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99.发明申请公开(公告)号：US20150089953A1
公开(公告)日：2015-04-02
申请号：US14396459
申请日：2013-04-26
IPC分类号： F02C7/22
CPC分类号： F02C7/222 , F02C7/232 , F05D2260/602 , Y02T50/671
摘要： Systems and methods for preventing fuel leakage in a gas turbine engine are provided. A fuel accumulation system includes a control valve section fluidly coupled to a fuel manifold passage and an accumulator valve section fluidly coupled at a first side to the control valve section. The control valve section is configured to control expansion of a fluid flowing in the fuel manifold passage. The accumulator valve section is configured to receive fluid expanded in the fuel manifold passage via the control valve section.
摘要翻译： 提供了用于防止燃气涡轮发动机中的燃料泄漏的系统和方法。 燃料积存系统包括流体耦合到燃料歧管通道的控制阀部分和在第一侧处流体耦合到控制阀部分的蓄能器阀部分。 控制阀部分构造成控制在燃料歧管通道中流动的流体的膨胀。 蓄能阀部分构造成接收经由控制阀部分在燃料歧管通道中膨胀的流体。
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公开(公告)号：US08991152B2
公开(公告)日：2015-03-31
申请号：US13012471
申请日：2011-01-24
申请人： Steven A. Heitz
发明人： Steven A. Heitz
CPC分类号： F02C7/22 , F02C7/232 , F02C7/236 , F05D2260/601 , F05D2260/604 , Y10T137/86019
摘要： An aircraft fuel system is provided and includes a metering valve having inlet and outlet sides to monitor fuel flow from the inlet to the outlet side, a check valve that, when opened, allows fuel to flow toward the inlet side during start and climb conditions and, when closed, prevents such fuel flow and an ejector pump, which is operably disposed between the check valve and the metering valve, and which, with the check valve closed, pumps fuel toward the inlet side during idle conditions.
摘要翻译： 提供飞机燃料系统并且包括计量阀，该计量阀具有入口和出口侧以监测从入口到出口侧的燃料流量;止回阀，当打开时允许燃料在起动和爬升条件期间朝向入口侧流动， 当关闭时，防止这种燃料流动，并且喷射器泵可操作地设置在止回阀和计量阀之间，并且在单向阀关闭的情况下，在空转条件下将燃料泵送到入口侧。
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