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1. 发明授权

US07607285B2 Four mode thermal recirculation throttle valve 有权
标题翻译：四模热循环节流阀
公开(公告)号：US07607285B2
公开(公告)日：2009-10-27
申请号：US10740651
申请日：2003-12-18
申请人： Paul W. Futa, Jr. , David J. Hauck , Gregory E. Kline , Steven A. Lewis , George S. Wieger
发明人： Paul W. Futa, Jr. , David J. Hauck , Gregory E. Kline , Steven A. Lewis , George S. Wieger
IPC分类号： F02C9/00 , F02G3/00
CPC分类号： F02C7/232 , Y02T50/671
摘要： A thermal recirculation throttle valve (1) for an aircraft fuel system includes a housing (11) having a throttling valve chamber; a cover (5) operatively engaging a first side of the housing (11); a power piston (6) within a power piston sleeve (7), the power piston (6) having a first (21) and second face (22) for control pressure to act upon, the power piston (6) and power piston sleeve (7) operatively engaged with the housing (11) within the throttling valve chamber; a Linear Variable Differential Transformer (15) for measuring a linear position of the power piston (6) within the housing (11); a throttling valve (8) within a throttling valve sleeve (9), the throttling valve (8) operatively engaged with the power piston (60) to transfer the linear movement of the piston (6) between a fully extended and a fully retracted operating position; and a flow deflector (10) engaged with the throttling valve (8) for protecting the housing (11) from flow erosion from fuel exiting flow windows (37). The throttling valve (8) includes a pair of fail-safe operating positions, a fully open operating position, a low leakage shutoff operating position, and a variety of variable flow operating positions between the shutoff and fully open operating positions.
摘要翻译：用于飞机燃料系统的热再循环节流阀（1）包括具有节流阀室的壳体（11）与所述壳体（11）的第一侧可操作地接合的盖（5）; 动力活塞（7）内的动力活塞（6），动力活塞（6）具有第一面（21）和第二面（22），用于控制压力作用在动力活塞（6）和动力活塞套（7），其在所述节流阀室内与所述壳体（11）可操作地接合; 用于测量所述壳体（11）内的所述动力活塞（6）的线性位置的线性可变差动变压器（15）; 在节流阀套（9）内的节流阀（8），节流阀（8）与动力活塞（60）可操作地接合，以将活塞（6）的线性运动传递到完全伸出和完全缩回的操作位置; 以及与所述节流阀（8）接合的导流器（10），用于保护所述壳体（11）免受来自流出窗口（37）的燃料的流动侵蚀。节流阀（8）包括一对故障保护操作位置，完全打开的操作位置，低泄漏关闭操作位置以及在关闭和完全打开的操作位置之间的各种可变流动操作位置。

2. 发明授权

US07296406B2 System for positioning a piston including a fail fixed valve for holding the piston in position during a power interruption and method of using same 有权
标题翻译：用于定位包括故障固定阀的活塞的系统，用于在电力中断期间将活塞保持在适当的位置以及使用它的方法
公开(公告)号：US07296406B2
公开(公告)日：2007-11-20
申请号：US11363323
申请日：2006-02-28
申请人： Paul W. Futa, Jr. , George S. Wieger , Steven A. Lewis , Gregory A. Lafferty , John C. Van Oosterum
发明人： Paul W. Futa, Jr. , George S. Wieger , Steven A. Lewis , Gregory A. Lafferty , John C. Van Oosterum
IPC分类号： F02C9/00 , F15B20/00
CPC分类号： F15B20/008 , F15B13/0438 , F15B2211/8633 , F15B2211/875
摘要： A controlled piston (20, 62, 102) having a first end (24, 64, 104) mounted in a controlled piston sleeve (22) and a spool (16) movably mounted in a spool sleeve (18), a first fluid passage (40, 66, 108) from the spool (16) to the controlled piston first end (24, 64, 104), the position of the spool (16) affecting a position of the controlled piston (20, 62, 102), an FFV (42, 68, 110) in an FFV sleeve (44, 70, 112) in the first fluid passage (40, 66, 108) having a first end section (46, 74, 116), a second end section (48, 78, 120) and a central section (50, 82, 126) having a third diameter less than the diameters of the first and second sections, the FFV (42, 68, 110) being shiftable between a first position blocking the first fluid passage (40, 66, 108) and a second position allowing fluid flow past the central section (50, 82, 126) to the controlled piston (20, 62, 102), and a second fluid passage (56, 88, 134) from the spool (16) to the FFV first end section (46, 74, 116). Shifting the spool (16) to a failsafe position shifts the FFV (42, 68, 110) to the first position to fix the controlled piston (20, 62, 102) in place.
摘要翻译：一个受控的活塞（20,62,102），其具有安装在受控的活塞套管（22）中的第一端（24,64,104）和可移动地安装在卷轴套管（18）中的阀芯（16），第一流体通道（40,66,108）从所述阀芯（16）到所述受控活塞第一端（24,64,104）的位置，所述阀芯（16）的位置影响所述受控活塞（20,62,102）的位置，在第一流体通道（40,66,108）中的FFV套筒（44,47,112）中的FFV（42,68,110）具有第一端部分（46,74,116），第二端部分 48，78，120）和具有小于第一和第二部分的直径的第三直径的中心部分（50,82,126），所述FFV（42,68,110）可在阻挡第一和第二部分的第一位置之间移动流体通道（40,66,108）和允许流体流过中央部分（50,82,126）到受控活塞（20,62,102）的第二位置，以及第二流体通道（56,88,134 ）从卷轴（16）到FFV 第一端部分（46,74,116）。将阀芯（16）移动到故障安全位置将FFV（42,68,110）移动到第一位置以将受控活塞（20,62,102）固定就位。

3. 发明授权

US5332233A Face seal means 失效
标题翻译：面密封装置
公开(公告)号：US5332233A
公开(公告)日：1994-07-26
申请号：US979091
申请日：1992-11-19
申请人： Paul W. Futa, Jr. , George S. Wieger
发明人： Paul W. Futa, Jr. , George S. Wieger
IPC分类号： F04C15/00 , F16J15/48 , F16L23/00
CPC分类号： F04C15/0023 , F04C15/0034 , F16J15/48
摘要： A seal for preventing leakage of pressurized fluid along a flow path along an engagement plane between a first and second members. The seal has a cylindrical body with a first elastomeric ring located on an end and a second elastomeric ring located on a peripheral surface of the cylindrical body. The cylindrical body is located in a passage in the second member. A spring urges the first elastomeric ring into engagement with a face on the first member when the first and second members are joined together. Pressurized fluid which flows from a passage in the first member into the second passage in the second member acts on the cylindrical body to further urge the end into engagement with the first member to prevent fluid leakage along the engagement plane there between.
摘要翻译：一种用于防止加压流体沿着沿着第一和第二构件之间的接合平面的流动路径泄漏的密封件。密封件具有圆柱形主体，其具有位于端部上的第一弹性体环和位于圆柱形主体的外周表面上的第二弹性体环。圆柱体位于第二构件的通道中。当第一和第二构件连接在一起时，弹簧促使第一弹性体环与第一构件上的面接合。从第一构件中的通道流入第二构件中的第二通道的加压流体作用在圆柱体上，以进一步推动端部与第一构件接合，以防止沿其间的接合平面流体泄漏。

4. 发明授权

US07565793B2 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：US07565793B2
公开(公告)日：2009-07-28
申请号：US11362004
申请日：2006-02-27
申请人： Jeffrey Dugan Shelby , Paul W. Futa, Jr. , George S. Wieger
发明人： Jeffrey Dugan Shelby , Paul W. Futa, Jr. , George S. Wieger
IPC分类号： F02C7/22
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. 发明授权

US07841841B2 Flow prioritizing valve system 有权
标题翻译：流量优先阀系统
公开(公告)号：US07841841B2
公开(公告)日：2010-11-30
申请号：US11844199
申请日：2007-08-23
申请人： Eric M. Arnett , Paul W. Futa, Jr.
发明人： Eric M. Arnett , Paul W. Futa, Jr.
IPC分类号： F04B49/00
CPC分类号： G05D16/166 , F02C7/22 , F15B13/0402 , F15B2211/40515 , F15B2211/40523 , F15B2211/413 , F15B2211/428 , Y10T137/2605 , Y10T137/7838
摘要： A flow prioritizing system includes a regulating valve and a flow prioritizing valve. The regulating valve receives a first portion of the fluid supplied from a fuel supply pump, and is responsive to a control pressure to selectively allow or prohibit flow to secondary loads. The flow prioritizing control valve is responsive to fluid pressure representative of delivery pump discharge pressure to control the control pressure to which the regulating valve is responsive.
摘要翻译：流量优先系统包括调节阀和流量优先阀。调节阀接收从燃料供应泵供应的流体的第一部分，并且响应于控制压力以选择性地允许或禁止流向次级负载。流量优先控制阀响应于表示输送泵排出压力的流体压力，以控制调节阀响应的控制压力。

6. 发明授权

US06385962B2 Fuel divider and ecology system for a gas turbine engine 有权
公开(公告)号：US06385962B2
公开(公告)日：2002-05-14
申请号：US09875336
申请日：2001-06-06
申请人： Paul W. Futa, Jr. , Steven F. Fisher , Kevin R. Sharp
发明人： Paul W. Futa, Jr. , Steven F. Fisher , Kevin R. Sharp
IPC分类号： F02C7232
CPC分类号： F02C7/232 , F02C7/228 , F05D2260/602 , Y02T50/671 , Y10T137/86509
摘要： A fuel control system for supplying metered quantities of fuel from a fuel supply (11), through a fuel pump (13), a metering valve (15) and a pressurizing valve (17) to a plurality of engine fuel manifolds (31a, 31b, 33) includes an ecology valve (43) for withdrawing fuel from the engine fuel manifolds (31a, 31b, 33) during cessation of engine operation and for returning fuel to the engine fuel manifolds (31a, 31b, 33) to be burned during normal engine operation. The ecology valve (43) includes a valve housing (44) having a plurality of ecology ports (50, 52, 54) adapted to be coupled to corresponding ones of the engine fuel manifolds (31a, 31b, 33) and a control port (46) adapted to be connected to a corresponding control port (45) of the fuel pressurizing valve (17). A movable piston (63) is supported within the valve housing (44) for reciprocable motion and divides the interior of the valve housing (44) into a variable volume control chamber (71) coupled to the control port (46) and a variable volume fuel reservoir (55) which is selectively coupled to and uncoupled from the ecology ports (50, 52, 54) by the piston (63). Fuel is withdrawn from the manifolds (31a, 31b, 33) seriatim. A fuel flow dividing arrangement is located intermediate the pressurizing valve (17) and the engine fuel manifolds (31a, 31b, 33) for distributing appropriately fuel flow among the manifolds and includes a concatenated pair of two-way splitter valves (39, 41) comprising a first splitter valve (39) distributing the fuel flow between an atomizer nozzle manifold (31b) and the remaining manifolds (31a, 33), and a second splitter valve (41) distributing down stream fuel flow from the first splitter valve (39) between upper and lower manifolds (31, 33).

7. 发明授权

US6092546A Fuel flow divider and pressurizing valve for gas turbine 失效
标题翻译：燃气轮机燃油分流器和加压阀
公开(公告)号：US6092546A
公开(公告)日：2000-07-25
申请号：US989606
申请日：1997-12-12
申请人： Ivan P. Lebrun , Paul W. Futa, Jr.
发明人： Ivan P. Lebrun , Paul W. Futa, Jr.
IPC分类号： F02C7/228 , F02C9/26 , F02C7/232
CPC分类号： F02C9/263 , F02C7/228 , Y02T50/671
摘要： A combination pressurizing valve (27) and fuel flow divider for a gas turbine is operable in three different fuel distribution modes utilizing three windows which are successively opened to control the flow distribution to the engine atomizing or start-up nozzles (23) and engine air blast or running nozzles (25) respectively by way of two fixed orifices (51, 55) in a way that satisfies the start-up flow distribution favoring the atomizing nozzles (23) as well as the need for balanced flow distribution between the different types of engine nozzles after a successful start. The first window position corresponds to an engine ignition mode and includes a range of intermediate valve spool (33, 133) positions where one outlet port (57) is open and the other outlet port (67) receives a restricted flow of fuel. The second window position includes a range of valve spool (33, 133) positions where the one outlet port (57) is open and the other outlet port (67) is open to receive a flow of fuel greater than the restricted flow. The third window position corresponds to a full power engine condition and includes a range of valve spool (33, 133) positions including the another extreme position where the one outlet port (57) is open and the other outlet port (67) is open to receive a still further increased flow of fuel.
摘要翻译：用于燃气轮机的组合加压阀（27）和燃料分流器可在三种不同的燃料分配模式中操作，利用三个窗口，这三个窗口连续打开以控制向发动机雾化或启动喷嘴（23）和发动机空气分别通过两个固定孔口（51,55）以满足启动流分布的方式喷射或运行喷嘴（25），有利于雾化喷嘴（23），以及需要不同类型之间的平衡流量分配发动机喷嘴成功启动后。第一窗口位置对应于发动机点火模式，并且包括一个中间阀阀芯（33,133）的位置，其中一个出口（57）打开，另一个出口（67）接收受限制的燃料流。第二窗口位置包括一个阀芯（33,133）的位置，其中一个出口端口（57）打开，另一个出口端口（67）打开以接收大于限制流量的燃料流。第三窗口位置对应于全功率发动机状态，并且包括一个阀芯（33,133）的范围，该位置包括一个出口（57）打开的另一个极限位置，另一个出口（67）打开还会进一步增加燃油流量。

8. 发明授权

US08529221B2 Method and system for fuel control in a gas turbine engine 有权
标题翻译：燃气涡轮发动机燃油控制方法和系统
公开(公告)号：US08529221B2
公开(公告)日：2013-09-10
申请号：US10863298
申请日：2004-06-08
申请人： Paul W. Futa, Jr. , Brent J. Gassman , Harold I. Miller , Timothy F. Wiegand
发明人： Paul W. Futa, Jr. , Brent J. Gassman , Harold I. Miller , Timothy F. Wiegand
IPC分类号： F02C9/00 , F02G3/00 , F04B49/00
CPC分类号： F02C9/30 , F02C9/36 , F05D2270/301 , F05D2270/3015
摘要： A fuel control system (100) for supplying metered fuel flow to a gas turbine engine is disclosed that includes a variable delivery fuel pump (116) for outputting a fuel flow that includes a burn fuel flow for the gas turbine engine and a surplus fuel flow recirculated back to an inlet (124) of the variable delivery fuel pump (116) and a pump control (148, 158, 122) for controlling the output of the variable delivery fuel pump to maintain the surplus fuel flow at a substantially constant rate. A method of controlling a fuel system (100) is also disclosed.
摘要翻译：公开了一种用于向燃气涡轮发动机供应计量燃料流的燃料控制系统（100），其包括用于输出燃料流的可变输送燃料泵（116），所述燃料流包括用于燃气涡轮发动机的燃料燃料流和剩余燃料流再循环回到可变输送燃料泵（116）的入口（124）和用于控制可变输送燃料泵的输出以将过剩燃料流维持在基本上恒定的速率的泵控制（148,158,122）。还公开了一种控制燃料系统（100）的方法。

9. 发明授权

US07484522B2 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：US07484522B2
公开(公告)日：2009-02-03
申请号：US11040745
申请日：2005-01-21
申请人： Chris D. Eick , Paul W. Futa, Jr. , Mitchell J. Laidlaw , Anthony C. Libera , Donald M. Purcell
发明人： Chris D. Eick , Paul W. Futa, Jr. , Mitchell J. Laidlaw , Anthony C. Libera , Donald M. Purcell
IPC分类号： 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。

10. 发明授权

US07093420B2 Flow divider and ecology valve 失效
标题翻译：流量分配器和生态阀
公开(公告)号：US07093420B2
公开(公告)日：2006-08-22
申请号：US10832674
申请日：2004-04-27
申请人： Paul W. Futa, Jr. , Dennis G. Demers
发明人： Paul W. Futa, Jr. , Dennis G. Demers
IPC分类号： F02C7/228
CPC分类号： F02C7/228 , F02C7/232 , F02C9/26
摘要： A fuel flow dividing ecology valve conveys fuel from a fuel source to at least a secondary gas turbine engine intake manifold during engine operation and withdraws fuel therefrom upon cessation of engine operation. The valve includes a flow dividing valve portion having an inlet coupled to the fuel source and an outlet coupled to the secondary manifold. The valve also includes an ecology valve portion controlled by the fuel pressure differential between the fuel source and the flow restricting inlet. The ecology valve portion includes a housing with a movable piston disposed therein. The piston defines, in conjunction with the housing, a variable volume chamber for withdrawing fuel from the engine intake manifolds. When the engine is de-energized, the piston moves from a first position toward a second position thereby purging the manifolds of fuel.
摘要翻译：燃料分流生态阀在发动机运行期间将燃料从燃料源传递到至少二次燃气涡轮发动机进气歧管，并且在停止发动机操作时从其中提取燃料。阀包括分流阀部分，其具有联接到燃料源的入口和连接到次级歧管的出口。阀还包括由燃料源和流量限制入口之间的燃料压力差控制的生态阀部分。生态阀部分包括其中设置有可移动活塞的壳体。活塞与壳体一起限定了用于从发动机进气歧管中抽出燃料的可变容积室。当发动机断电时，活塞从第一位置向第二位置移动，从而清除燃料歧管。

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