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1. 发明授权

US08353306B2 Fuel divider system for gas turbine engine 有权
标题翻译：燃气轮机发动机燃油分配器系统
公开(公告)号：US08353306B2
公开(公告)日：2013-01-15
申请号：US12190312
申请日：2008-08-12
申请人： Paul Futa , David Tuttle , David Lawrence
发明人： Paul Futa , David Tuttle , David Lawrence
IPC分类号： G05D11/00 , F02C7/22 , F02C7/26 , F02C9/26
CPC分类号： F02C7/228 , Y10T137/265 , Y10T137/2663
摘要： A fuel divider system includes a housing assembly and a flow passage network having an inlet, a primary outlet, and a secondary outlet. A fuel divider piston is slidably disposed within the housing assembly and movable between a flow biasing position and a flow equalizing position. A control chamber is fluidly coupled to the flow passage network and fluidly communicates with the piston. An inlet chamber, at least partially defined by the piston and the housing assembly, is fluidly coupled to the inlet. At least one channel is provided through the piston and configured to cooperate with the flow passage network to port the FD control chamber to: (i) the fuel pressure at the secondary outlet when the FD piston is in the flow biasing position, and (ii) the fuel pressure within the inlet chamber when the FD piston is in the flow equalizing position.
摘要翻译：燃料分配器系统包括壳体组件和具有入口，主出口和次级出口的流动通道网络。燃料分配器活塞可滑动地设置在壳体组件内并可在流动偏置位置和流动平衡位置之间移动。控制室流体地联接到流动通道网络并与活塞流体连通。至少部分地由活塞和壳体组件限定的入口室流体地联接到入口。通过活塞提供至少一个通道，并且构造成与流动通道网络配合以将FD控制腔室连接到：（i）当FD活塞处于流动偏置位置时在次级出口处的燃料压力，和（ii ）当FD活塞处于流动平衡位置时，入口室内的燃料压力。

2. 发明申请

US20100132368A1 ECOLOGY VALVE FUEL RETURN SYSTEM OPERABLE IN FLUID ISOLATION DURING GAS TURBINE ENGINE SHUT-DOWN 有权
标题翻译：在气体发动机关闭期间的流体分离中生产的阀门燃油返回系统
公开(公告)号：US20100132368A1
公开(公告)日：2010-06-03
申请号：US12327480
申请日：2008-12-03
申请人： David Lawrence , Paul Futa , Larry Portolese
发明人： David Lawrence , Paul Futa , Larry Portolese
IPC分类号： F02C9/26
CPC分类号： F02C7/232 , F02C7/236 , F02C9/26 , F05D2220/50 , F05D2260/85
摘要： In one embodiment, an ecology valve (EV) fuel return system includes a housing assembly, an ecology valve, and a fuel routing assembly. The ecology valve includes an EV piston slidably disposed within the housing assembly for movement between a fuel storage position and a fuel return position, a fuel storage chamber defined by the EV piston and the housing assembly, and an EV control chamber defined by the EV piston and the housing assembly. The fuel routing assembly, which is fluidly coupled to the EV control chamber and to the fuel storage chamber, is configured to route fuel: (i) from the fuel storage chamber to a fuel supply system when a gas turbine engine (GTE) is in a start-up mode, and (ii) from the first fuel manifold and from the EV control chamber to the fuel storage chamber when the GTE is in a shut-down mode.
摘要翻译：在一个实施例中，生态阀（EV）燃料返回系统包括壳体组件，生态阀和燃料路线组件。生态阀包括可滑动地设置在壳体组件内用于在燃料储存位置和燃料返回位置之间运动的EV活塞，由EV活塞和壳体组件限定的燃料储存室以及由EV活塞限定的EV控制室和壳体组件。流体耦合到EV控制室和燃料储存室的燃料路由组件被构造成在燃气涡轮发动机（GTE）处于燃料涡轮发动机（GTE）时将燃料（i）从燃料储存室路向燃料供应系统启动模式，以及（ii）当GTE处于关闭模式时，从第一燃料歧管和从EV控制室到燃料存储室。

3. 发明申请

US20070234732A1 Gas turbine engine fuel control system having a transfer valve and a shutoff valve and a common controller therefor 失效
标题翻译：燃气涡轮发动机燃料控制系统具有转换阀和截止阀及其公共控制器
公开(公告)号：US20070234732A1
公开(公告)日：2007-10-11
申请号：US11399421
申请日：2006-04-07
申请人： Jeffrey Shelby , Paul Futa , Matthew Arend , Per Danzl
发明人： Jeffrey Shelby , Paul Futa , Matthew Arend , Per Danzl
IPC分类号： F02C7/22
CPC分类号： F02C7/232 , F02C9/263 , F05D2260/406
摘要： A fuel control system for a gas turbine engine includes a metering valve for metering a flow of fuel, a throttling valve for maintaining a pressure drop across the metering valve, the throttling valve being shiftable between an open state and a shutoff state blocking an outlet of the metering valve, a primary control pressure supply for supplying a primary control pressure to the metering valve for controlling the position of the metering valve, a backup control pressure supply, a transfer valve shiftable between a first position connecting the primary control pressure to supply to the metering valve and a second position connecting the backup control pressure to the metering valve, and an electrohydraulic servovalve (EHSV) operably connected to the throttling valve and the transfer valve and controlling the state of the transfer valve and the position of the throttling valve. Also a method for controlling a transfer valve and a throttling valve.
摘要翻译：用于燃气涡轮发动机的燃料控制系统包括用于计量燃料流量的计量阀，用于维持跨越计量阀的压降的节流阀，所述节流阀可以在打开状态和关闭状态之间移动，计量阀，用于向计量阀提供初级控制压力以控制计量阀的位置的主控制压力供应源，备用控制压力供应器，可在连接主控制压力的第一位置之间转换以供应至计量阀和将备用控制压力连接到计量阀的第二位置以及可操作地连接到节流阀和转换阀并且控制转换阀的状态和节流阀的位置的电动液压伺服阀（EHSV）。也是用于控制转换阀和节流阀的方法。

4. 发明申请

US20070199301A1 Gas turbine engine fuel control system having start / back up check valve (sbuc) providing a main fuel check valve function 有权
标题翻译：燃气涡轮发动机燃料控制系统具有启动/后备止回阀（sbuc），其提供主燃料止回阀功能
公开(公告)号：US20070199301A1
公开(公告)日：2007-08-30
申请号：US11362004
申请日：2006-02-27
申请人： Jeffrey Shelby , Paul Futa , George Wieger
发明人： Jeffrey Shelby , Paul Futa , George Wieger
IPC分类号： F02C9/00
CPC分类号： F02C9/263 , F02C7/232 , F02C7/236 , Y02T50/671 , Y10T137/86815
摘要： A fuel control system (10) for a gas turbine engine includes a main fuel inlet line (18), an auxiliary fuel inlet line (20) and an engine fuel outlet line (16). A first flow path extends from the main fuel inlet line (18) to the engine fuel outlet line (16) and a second flow path extends from the auxiliary fuel inlet line (20) to the engine fuel outlet line (16). A check valve (22) in the first flow path allows fuel flow through the first flow path in a direction from the main fuel inlet line (18) to the engine fuel outlet line (16) and substantially prevents fuel flow through the first flow path in a direction from the engine fuel outlet line (16) to the main fuel inlet line (18). The check valve (22) is shiftable between a first position connecting the auxiliary fuel inlet (20) to the engine fuel outlet (16) and a second position blocking the second flow path. Also a method of controlling fuel flow in a fuel control system of a gas turbine engine.
摘要翻译：用于燃气涡轮发动机的燃料控制系统（10）包括主燃料入口管线（18），辅助燃料入口管线（20）和发动机燃料出口管线（16）。第一流路从主燃料入口管线（18）延伸到发动机燃料出口管线（16），并且第二流动路径从辅助燃料入口管线（20）延伸到发动机燃料出口管线（16）。第一流路中的止回阀（22）允许燃料沿着从主燃料入口管线（18）到发动机燃料出口管线（16）的方向流过第一流动路径，并且基本上防止燃料流过第一流动路径在从发动机燃料出口管线（16）到主燃料入口管线（18）的方向上。止回阀（22）可在连接辅助燃料入口（20）与发动机燃料出口（16）的第一位置与阻挡第二流动路径的第二位置之间移动。还有一种控制燃气涡轮发动机的燃料控制系统中的燃料流量的方法。

5. 发明申请

US20070023093A1 Latchable electrohydraulic servovalve 有权
标题翻译：可锁定电液伺服阀
公开(公告)号：US20070023093A1
公开(公告)日：2007-02-01
申请号：US11492845
申请日：2006-07-26
申请人： Jeffrey Shelby , Paul Futa , Matthew Arend
发明人： Jeffrey Shelby , Paul Futa , Matthew Arend
IPC分类号： F15B13/043
CPC分类号： F15B13/0436 , F15B20/002 , Y10T137/86606 , Y10T137/86614 , Y10T137/8663
摘要： An electro-hydraulic servovalve (EHSV) (10) that includes a nozzle (16), a motor (12) operably connected to the nozzle (16) for controlling the position of the nozzle (16) based on current provided to the motor (12), a spool (18) having first and second ends (22,26) slidably mounted in a sleeve (34) having first and second ends (31,33) and a first land (21) near the first end (22), a first passage (40) extending from near the nozzle (16) to the first end (31) of the sleeve (34), a second passage (42) extending from near the nozzle (16) to the second end (33) of the sleeve (34), the spool (18) shifting to a first fail-safe position when the current is below a first predetermined level and latching in a second fail-safe position different than the first fail-safe position when the current exceeds a second predetermined level greater than the first predetermined level.
摘要翻译：一种电动液压伺服阀（EHSV）（10），包括喷嘴（16），可操作地连接到喷嘴（16）的马达（12），用于基于提供给马达的电流来控制喷嘴（16）的位置具有可滑动地安装在套筒（34）中的第一和第二端（22,26）的卷轴（18）具有在第一端（22）附近的第一和第二端（31,33）和第一平台（21），从喷嘴（16）附近延伸到套筒（34）的第一端（31）的第一通道（40），从喷嘴（16）附近延伸到第二端（33）的第二通道（42）当电流低于第一预定水平时，阀芯（18）转换到第一故障安全位置，并且当电流超过第一故障安全位置时锁定在与第一故障安全位置不同的第二故障安全位置大于第一预定水平的第二预定水平。

6. 发明申请

US20130199630A1 GAS TURBINE ENGINE FUEL RETURN VALVE AND SYSTEM 有权
标题翻译：燃气涡轮发动机燃油返回阀和系统
公开(公告)号：US20130199630A1
公开(公告)日：2013-08-08
申请号：US13364895
申请日：2012-02-02
申请人： Paul Futa , Steven Alan Lewis , Larry Portolese
发明人： Paul Futa , Steven Alan Lewis , Larry Portolese
IPC分类号： F16K21/18
CPC分类号： F02C7/232 , Y10T137/7287 , Y10T137/7761 , Y10T137/777 , Y10T137/86582 , Y10T137/86702 , Y10T137/86815
摘要： A fuel return valve and system includes a flow-level select and shut-off valve and a servo control valve. The flow-level select and shut-off valve includes a first fuel inlet, a second fuel inlet, a return-to-tank fuel outlet, and a valve element movable between a shut-off position, a mid-flow position, and a max-flow position. The servo control valve is coupled to the flow-level select and shut-off valve and is configured to control relative fluid pressures therein to selectively move the valve element to the shut-off position, the mid-flow position, and the max-flow position.
摘要翻译：燃油回流阀和系统包括流量选择和截止阀和伺服控制阀。流量选择和关闭阀包括第一燃料入口，第二燃料入口，回油罐燃料出口和可在关闭位置，中流动位置和第二燃料入口最大流量位置。伺服控制阀连接到流量选择和关闭阀，并且被配置为控制其中的相对流体压力以选择性地将阀元件移动到关闭位置，中流位置和最大流量位置。

7. 发明授权

US08122699B2 Ecology valve fuel return system operable in fluid isolation during gas turbine engine shut-down 有权
标题翻译：在燃气涡轮发动机关闭期间可在液体隔离中操作的生态阀燃料返回系统
公开(公告)号：US08122699B2
公开(公告)日：2012-02-28
申请号：US12327480
申请日：2008-12-03
申请人： David Lawrence , Paul Futa , Larry Portolese
发明人： David Lawrence , Paul Futa , Larry Portolese
IPC分类号： F02G3/00
CPC分类号： F02C7/232 , F02C7/236 , F02C9/26 , F05D2220/50 , F05D2260/85
摘要： An ecology valve (EV) fuel return system includes a housing assembly, an ecology valve, and a fuel routing assembly. The ecology valve includes an EV piston slidably disposed within the housing assembly for movement between a fuel storage position and a fuel return position, a fuel storage chamber defined by the EV piston and the housing assembly, and an EV control chamber defined by the EV piston and the housing assembly. The fuel routing assembly, which is fluidly coupled to the EV control chamber and to the fuel storage chamber, is configured to route fuel: (i) from the fuel storage chamber to a fuel supply system when a gas turbine engine (GTE) is in a start-up mode, and (ii) from the first fuel manifold and from the EV control chamber to the fuel storage chamber when the GTE is in a shut-down mode.
摘要翻译：生态阀（EV）燃料回收系统包括壳体组件，生态阀和燃料路线组件。生态阀包括可滑动地设置在壳体组件内用于在燃料储存位置和燃料返回位置之间运动的EV活塞，由EV活塞和壳体组件限定的燃料储存室以及由EV活塞限定的EV控制室和壳体组件。流体耦合到EV控制室和燃料储存室的燃料路由组件被构造成在燃气涡轮发动机（GTE）处于燃料涡轮发动机（GTE）时将燃料（i）从燃料储存室路向燃料供应系统启动模式，以及（ii）当GTE处于关闭模式时，从第一燃料歧管和从EV控制室到燃料存储室。

8. 发明申请

US20060081222A1 Method to control starter / generator cooling fuel flow during engine starting 有权
标题翻译：在发动机启动期间控制起动器/发电机冷却燃油流量的方法
公开(公告)号：US20060081222A1
公开(公告)日：2006-04-20
申请号：US11040745
申请日：2005-01-21
申请人： Chris Eick , Paul Futa , Mitchell Laidlaw , Anthony Libera , Donald Purcell
发明人： Chris Eick , Paul Futa , Mitchell Laidlaw , Anthony Libera , Donald Purcell
IPC分类号： F02M31/20 , F02M37/00
CPC分类号： F02M31/20 , F02D33/006 , F02M37/0023 , Y02T10/126 , Y10T137/0396 , Y10T137/7762 , Y10T137/88062
摘要： The present invention provides a relatively simple way to automatically turn on and off the fuel to a starter/generator cooling system during engine start. The present invention takes advantage of a fuel pressure rise provided by an engine fuel boost pump during the period from engine start to engine idle conditions. This pressure rise is used to stroke a shutoff valve in a fuel return to tank valve (FRTTV), which shuts off the starter generator cooling fuel flow. This shutoff occurs automatically with no other external input from, for example, an engine controller. A check valve is also included that prevents back flow through the FRTTV in the event of an engine start with no aircraft pumps running.
摘要翻译：本发明提供了一种在发动机起动期间自动将燃料打开和关闭到起动/发电机冷却系统的相对简单的方法。本发明利用了从发动机起动到发动机怠速状态期间由发动机燃料增压泵提供的燃料压力上升。该压力升高用于冲击回油阀（FRTTV）的截止阀，该阀关闭起动发电机冷却燃料流。没有其他来自例如引擎控制器的外部输入自动发生关闭。还包括一个止回阀，防止发动机起动时没有飞机泵运行，通过FRTTV回流。

9. 发明申请

US20060053796A1 Method and apparatus for adding a secondary fluid flow to a gas turbine engine control fuel line 审中-公开
标题翻译：将二次流体流添加到燃气涡轮发动机控制燃料管线的方法和装置
公开(公告)号：US20060053796A1
公开(公告)日：2006-03-16
申请号：US11193334
申请日：2005-08-01
申请人： Dugan Shelby , Paul Futa
发明人： Dugan Shelby , Paul Futa
IPC分类号： F02C7/232
CPC分类号： F02C7/22 , F02C7/232 , F02C9/26 , F05D2270/301
摘要： A gas turbine engine fuel system (10) that includes a fuel line, a pressurizing valve (14) in the fuel line having a burn fuel outlet (16) to a burn fuel line (18) providing burn fuel to the engine (20) and a control fuel outlet (22) to a control fuel line (24) providing pressure for controlling an engine system (26), the pressurizing valve (14) being shiftable between a closed position blocking fuel flow to the burn fuel line (18) and to the control fuel line (24) and a second position, and a secondary flow valve (30) having a first end (44, 64) in fluid communication with the burn fuel line (18) downstream of the pressurizing valve (14) and a second end (64, 66) in fluid communication with the control fuel line (24) downstream of the pressurizing valve (14), the secondary flow valve (30) controlling the addition of a secondary fluid flow from a secondary fluid line (32) to the control fuel line (24), the secondary flow valve (30) substantially preventing the secondary flow from reaching the secondary flow valve first end (44, 64). Also a method of adding a secondary fluid flow to a control fuel line (24).
摘要翻译：一种燃气轮机发动机燃料系统（10），其包括燃料管线，燃料管路中的加压阀（14）具有燃烧燃料出口（16），燃烧燃料管线（18）向发动机（20）提供燃烧燃料，和控制燃料出口（22）连接到提供用于控制发动机系统（26）的压力的控制燃料管线（24），所述加压阀（14）能够在封闭位置阻挡燃料流到燃烧燃料管线（18）之间移动，以及具有与加压阀（14）下游的燃烧燃料管路（18）流体连通的第一端（44,64）的控制燃料管路（24）和第二位置的二次流量阀（30）和与加压阀（14）下游的控制燃料管线（24）流体连通的第二端（64,66），所述二级流量阀（30）控制从次级流体管线（ 32）连接到控制燃料管线（24），二次流量阀（30）密封防止二次流到达二次流量阀第一端（44,64）。还有一种将二次流体流加入到控制燃料管线（24）中的方法。

10. 发明授权

US09234465B2 Fuel flow divider and ecology system for a gas turbine engine fuel flow control system 有权
标题翻译：用于燃气涡轮发动机燃油流量控制系统的燃油分流器和生态系统
公开(公告)号：US09234465B2
公开(公告)日：2016-01-12
申请号：US13085107
申请日：2011-04-12
申请人： Paul Futa , Brad McRoberts , Greg Lafferty
发明人： Paul Futa , Brad McRoberts , Greg Lafferty
IPC分类号： F02C9/26 , F02C7/232
CPC分类号： F02C9/263 , F02C7/228 , F02C7/232 , F02C9/34 , Y10T137/2524
摘要： A flow divider valve for a gas turbine engine fuel supply system is provided. The flow divider valve is configured, whenever fuel pressure at its inlet port is between a first predetermined pressure and a second predetermined pressure, to supply the fuel to a start nozzle manifold outlet port at a substantially constant flow rate, and to direct any fuel flow in excess of the substantially constant flow rate to a run nozzle manifold outlet port.
摘要翻译：提供了一种用于燃气涡轮发动机燃料供应系统的分流阀。分流阀被构造成每当其入口处的燃料压力处于第一预定压力和第二预定压力之间时，以基本上恒定的流量将燃料供应到起始喷嘴歧管出口，并且引导任何燃料流超过流速喷嘴歧管出口的基本上恒定的流速。

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