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51. 发明授权

US08834134B2 Flow sensing dual pump switching system and method 有权
标题翻译：流量传感双泵切换系统及方法
公开(公告)号：US08834134B2
公开(公告)日：2014-09-16
申请号：US12972905
申请日：2010-12-20
申请人： Carthel C. Baker , Dmitriy Baryshnikov
发明人： Carthel C. Baker , Dmitriy Baryshnikov
IPC分类号： F04B49/00 , G05D7/00 , F02C7/236 , F04B23/04
CPC分类号： F02C7/236 , F02C7/232 , F02C9/263 , F04B23/04 , F05D2260/606 , F05D2270/3015
摘要： A flow sensing dual pump switching system and method are provided that control the supply of fuel from a dual pump fuel system to a fuel metering unit. The system senses bypass pressure from the fuel metering unit to control the differential pressurization of the second pump. As the bypass is reduced, the pressure of the second pump is increased so that it may be added to that of the first pump to supply the increased fuel consumption needs of an engine. As the fuel consumption needs decrease, the flow from the second pump added to the first pump is reduced and the differential pressure of the second pump is similarly reduced. If the bypass pressure remains high, the switching system disconnects the output of the second pump from that of the first in favor of bypassing the flow to its input to reduce its differential pressure and conserve energy.
摘要翻译：提供一种流量检测双泵切换系统和方法，其控制从双泵燃料系统向燃料计量单元的燃料供应。该系统感测来自燃料计量单元的旁路压力以控制第二泵的差压。当旁路减少时，第二泵的压力增加，使得其可以被添加到第一泵的压力以提供发动机的增加的燃料消耗需求。随着燃料消耗量的降低，加入到第一泵的第二泵的流量减少，并且第二泵的差压也同样降低。如果旁路压力保持较高，则开关系统将第二泵的输出与第一泵的输出断开，有利于将流量旁路到其输入端，以减小其压差并节约能源。

52. 发明申请

US20140123621A1 ACTUATED BYPASS HOOD FOR GAS TURBINE AIR INLET SYSTEM AND METHODS 审中-公开
标题翻译：用于气体涡轮空气入口系统和方法的致动旁路
公开(公告)号：US20140123621A1
公开(公告)日：2014-05-08
申请号：US13776095
申请日：2013-02-25
申请人： Donaldson Company, Inc.
发明人： Robin Driessens , Erwin Jean Marie Verbelen , Jimmy Vanderlinden , Jon Haag
IPC分类号： F02C7/055 , B23P11/00
CPC分类号： F02C7/055 , B01D46/10 , B01D46/12 , B01D2273/10 , B01D2273/14 , B01D2279/60 , B23P11/00 , F02C7/052 , F05D2270/3015 , Y10T29/49323
摘要： An inlet hood for use with a gas turbine or compressor air inlet system includes a frame and at least one pre-filter pivotably held by the frame in an operating position. The pre-filter is pivotable to a bypass position angled relative to the operating position. Methods of assembly and use are provided.
摘要翻译：与燃气轮机或压缩机空气入口系统一起使用的入口罩包括框架和至少一个在工作位置由框架可枢转地保持的预过滤器。预过滤器可枢转到相对于操作位置成角度的旁路位置。提供组装和使用方法。

53. 发明授权

US08667803B2 Turbine starter valve 有权
标题翻译：涡轮起动阀
公开(公告)号：US08667803B2
公开(公告)日：2014-03-11
申请号：US12888147
申请日：2010-09-22
申请人： Leo Veilleux, Jr.
发明人： Leo Veilleux, Jr.
IPC分类号： F02C7/275
CPC分类号： F02C7/277 , F05D2220/3217 , F05D2270/3015 , F05D2270/62
摘要： A turbine starter including a valve to modulate an amount of air permitted to flow to a turbine section, a sensor to detect a characteristic of the air at locations defined between the valve and the turbine section and downstream from the turbine section and an electrically powered motor coupled to the valve and the sensor to control the valve to modulate the amount of the air permitted to flow to the turbine section in accordance with the detected characteristic.
摘要翻译：一种涡轮起动器，包括用于调节允许流向涡轮机部分的空气量的阀;传感器，用于检测在阀和涡轮部分之间以及涡轮部分下游的限定位置处的空气的特性;以及电动马达耦合到阀和传感器以根据检测到的特性来控制阀来调节允许流向涡轮机部分的空气的量。

54. 发明授权

US08517040B2 Valve control of pump inlet pressure with bootstrap reservoir 有权
标题翻译：泵入口压力与自举油箱的阀门控制
公开(公告)号：US08517040B2
公开(公告)日：2013-08-27
申请号：US13208501
申请日：2011-08-12
申请人： Kurt J. Doughty
发明人： Kurt J. Doughty
IPC分类号： F15B1/26
CPC分类号： F24D19/1036 , F04D13/16 , F04D15/0022 , F04D15/0281 , F05D2270/3011 , F05D2270/3015 , F15B1/265 , F15B21/047 , F15B2211/50563 , F15B2211/513 , F15B2211/5158 , F15B2211/526 , F15B2211/57 , F15B2211/6306 , F15B2211/6309 , F15B2211/8609 , Y10T137/0379 , Y10T137/0396 , Y10T137/8158 , Y10T137/85954 , Y10T137/86002
摘要： A closed-loop system includes a pump driving a fluid through a series of conduits. A control system is included that minimizes pressure fluctuations in a bootstrap reservoir to maintain a desired minimum pressure at the pump inlet. Moreover, the control system reduces a maximum system pressure by reducing the magnitude of pressure fluctuations encountered by the bootstrap reservoir.
摘要翻译：闭环系统包括通过一系列导管驱动流体的泵。包括一个控制系统，其使自举储存器中的压力波动最小化以在泵入口处保持期望的最小压力。此外，控制系统通过减小自举储存器遇到的压力波动的大小来降低最大系统压力。

55. 发明申请

US20130149112A1 GAS TURBINE ENGINE WITH FAN VARIABLE AREA NOZZLE 审中-公开
标题翻译：燃气涡轮发动机与风扇变化区域喷嘴
公开(公告)号：US20130149112A1
公开(公告)日：2013-06-13
申请号：US13340798
申请日：2011-12-30
申请人： Gregory A. Kohlenberg , Sean P. Zamora , Frederick M. Schwarz
发明人： Gregory A. Kohlenberg , Sean P. Zamora , Frederick M. Schwarz
IPC分类号： F01D17/00 , F01D15/12
CPC分类号： B64D33/04 , F02K1/30 , F02K1/72 , F05D2270/3015
摘要： A nacelle assembly for a high-bypass gas turbine engine includes a fan variable area nozzle movable relative to a fan nacelle to vary a fan nozzle exit area and adjust a pressure ratio of the fan bypass airflow during engine operation.
摘要翻译：用于高旁通燃气涡轮发动机的机舱组件包括可相对于风扇机舱移动的风扇可变区域喷嘴，以改变风扇喷嘴出口区域并调节发动机运行期间风扇旁路气流的压力比。

56. 发明授权

US08408864B2 Device for regulating the flow rate of air feeding a turbine ventilation cavity of a turbomachine turbine section 有权
标题翻译：用于调节供应涡轮机涡轮机部分的涡轮机通风空气的空气的流量的装置
公开(公告)号：US08408864B2
公开(公告)日：2013-04-02
申请号：US12615798
申请日：2009-11-10
申请人： Ion Fintescu , Laurent Gille , Jean-Pierre Andre Joseph Mourlan , Matthieu Savarit
发明人： Ion Fintescu , Laurent Gille , Jean-Pierre Andre Joseph Mourlan , Matthieu Savarit
IPC分类号： F01B25/02
CPC分类号： F01D17/145 , F01D9/065 , F02C6/08 , F05D2260/205 , F05D2270/3015 , F16K15/038 , Y02T50/676 , Y10T137/7839 , Y10T137/7848
摘要： A device for regulating the flow rate of air feeding a turbine ventilation cavity of a turbomachine turbine section is disclosed. The device includes at least one tubular duct opening into a take-off cavity and leading into a turbine ventilation cavity, the pressure inside the take-off cavity being higher than the pressure inside the turbine ventilation cavity; an air flow rate regulation valve disposed in the tubular duct, the valve being suitable for moving under the effect of the pressure difference between the take-off cavity and the turbine ventilation cavity; and a mechanical return device for holding the valve in a maximum closure position for the duct so long as the pressure difference between the take-off cavity and the turbine ventilation cavity remains below a predetermined threshold pressure.
摘要翻译：公开了一种用于调节供应涡轮机涡轮部分的涡轮机通风腔的空气流量的装置。该装置包括至少一个管状管道，该管状管道通向起飞腔并引入涡轮机通风腔，该起飞腔内的压力高于涡轮机通风腔内的压力; 设置在管状管道中的空气流量调节阀，该阀适于在起飞腔和涡轮机通风腔之间的压力差的作用下移动; 以及用于将阀保持在用于管道的最大关闭位置中的机械返回装置，只要起飞腔和涡轮机通风腔之间的压力差保持在预定阈值压力以下即可。

57. 发明申请

US20130019952A1 METHOD FOR MONITORING A PRESSURE RELIEF VALVE OF A FUEL INJECTION CIRCUIT FOR A TURBOMACHINE 有权
标题翻译：用于监测涡轮机油燃料注入电路的压力释放阀的方法
公开(公告)号：US20130019952A1
公开(公告)日：2013-01-24
申请号：US13552066
申请日：2012-07-18
申请人： Brice ANDRE , Nicolas POTEL
发明人： Brice ANDRE , Nicolas POTEL
IPC分类号： F17D3/00
CPC分类号： F02C7/236 , F02C9/26 , F05D2270/3015 , Y10T137/0318
摘要： A detection method of a breakdown of a pressure relief valve of a fuel injection circuit for a turbomachine, the injection circuit including a low pressure stage and a high pressure stage, the low pressure stage having an inlet and an outlet, the high pressure stage having an inlet and an outlet, the low pressure stage being connected to the high pressure stage, the pressure relief valve being connected in parallel with respect to the high pressure stage, the injection circuit further including a recirculation loop including an inlet connected to the outlet of the high pressure stage and an outlet connected to the outlet of the low pressure stage, the method including measuring a differential pressure in the injection circuit.
摘要翻译：一种用于涡轮机的燃料喷射回路的泄压阀的故障的检测方法，所述喷射回路包括低压级和高压级，所述低压级具有入口和出口，所述高压级具有入口和出口，所述低压级连接到所述高压级，所述减压阀相对于高压级并联连接，所述注入回路还包括再循环回路，所述再循环回路包括连接到所述高压级的出口的入口所述高压级和连接到所述低压级的出口的出口，所述方法包括测量所述注入回路中的压差。

58. 发明申请

US20120308399A1 TURBINE NOZZLE SLASHFACE COOLING HOLES 有权
标题翻译：涡轮喷嘴冷却孔
公开(公告)号：US20120308399A1
公开(公告)日：2012-12-06
申请号：US13151564
申请日：2011-06-02
申请人： Evan Andrew SEWALL , James William VEHR , Frederic Woodrow ROBERTS, JR.
发明人： Evan Andrew SEWALL , James William VEHR , Frederic Woodrow ROBERTS, JR.
IPC分类号： F01D25/12
CPC分类号： F01D5/187 , F01D9/065 , F01D11/006 , F05D2240/81 , F05D2270/3015
摘要： A turbine vane or blade segment includes at least one airfoil extending radially outwardly from a radially inner band. The radially inner band is formed with substantially axially-extending side edges, and the at least one airfoil is formed with a leading edge, a trailing edge, a pressure side, a suction side, and an internal cooling plenum. The pressure side faces one of the substantially axially-extending side edges and the leading edge is located proximate to that one edge. A plurality of cooling passages are formed in the radially inner band in fluid communication with the internal plenum and exiting the inner band via a plurality of exit holes in the one of the substantially axially-extending side edges. The plurality of exit holes are confined to a region along the one of the substantially axially-extending side edges where static pressure PS along the one of the substantially axially-extending side edges lies in a pressure range, ΔPD, substantially between the stage inlet total pressures PT that is substantially about 1.5 times the dynamic pressure range ΔPD, below the stage inlet total pressure.
摘要翻译：涡轮机叶片或叶片段包括从径向内部带径向向外延伸的至少一个翼型件。径向内带形成有基本上轴向延伸的侧边缘，并且至少一个翼型件形成有前缘，后缘，压力侧，吸力侧和内部冷却增压室。压力侧面向大致轴向延伸的侧边缘之一，并且前缘位于该一个边缘附近。多个冷却通道形成在径向内部带中，与内部气室流体连通并且经由大致轴向延伸的侧边缘中的一个中的多个出口孔离开内部带。多个出口孔被限制在沿着基本上轴向延伸的侧边缘中的一个的区域中，其中沿着基本上轴向延伸的侧边缘中的一个的静态压力PS位于压力范围（Dgr; PD）之间，入口总压力PT，基本上约为动态压力范围Dgr; PD的1.5倍，低于载物台入口总压力。

59. 发明申请

US20120247115A1 Gas compressor operating method and gas turbine equipped with gas compressor 有权
标题翻译：燃气压缩机运行方式和配备燃气压缩机的燃气轮机
公开(公告)号：US20120247115A1
公开(公告)日：2012-10-04
申请号：US13268763
申请日：2011-10-07
申请人： Jun Sasahara , Masamitsu Okuzono
发明人： Jun Sasahara , Masamitsu Okuzono
IPC分类号： F02C9/16 , F01D17/00
CPC分类号： F04D27/001 , F02C6/18 , F02C9/20 , F04D27/0246 , F05D2270/3015
摘要： In a method for operating a gas compressor which compresses gas whose supply conditions change and which is equipped with an intake-flow regulating mechanism, a limit pressure ratio that defines the operational upper limit of the pressure ratio relative to the intake flow rate of the gas compressor or the degree of opening of the intake-flow regulating mechanism to prevent surging in the gas compressor is corrected by multiplying a reference limit pressure ratio calculated from the design conditions of the gas compressor by a first correction factor calculated depending on a detected operating-state value of the gas compressor.
摘要翻译：在压缩供给条件变化的气体并具有进气流量调节机构的气体压缩机的方法中，限定相对于气体的进气流量的压力比的运行上限的极限压力比通过将从气体压缩机的设计条件计算的基准限制压力比乘以根据检测到的操作状态计算的第一校正因子来校正压缩机或进气流量调节机构的开度，以防止气体压缩机中的喘振，气体压缩机的状态值。

60. 发明申请

US20120156061A1 Flow Sensing Dual Pump Switching System and Method 有权
标题翻译：流量传感双泵切换系统及方法
公开(公告)号：US20120156061A1
公开(公告)日：2012-06-21
申请号：US12972905
申请日：2010-12-20
申请人： Carthel C. Baker , Dmitriy Baryshnikov
发明人： Carthel C. Baker , Dmitriy Baryshnikov
IPC分类号： F04B49/035 , F02C7/236 , F04B23/04
CPC分类号： F02C7/236 , F02C7/232 , F02C9/263 , F04B23/04 , F05D2260/606 , F05D2270/3015
摘要： A flow sensing dual pump switching system and method are provided that control the supply of fuel from a dual pump fuel system to a fuel metering unit. The system senses bypass pressure from the fuel metering unit to control the differential pressurization of the second pump. As the bypass is reduced, the pressure of the second pump is increased so that it may be added to that of the first pump to supply the increased fuel consumption needs of an engine. As the fuel consumption needs decrease, the flow from the second pump added to the first pump is reduced and the differential pressure of the second pump is similarly reduced. If the bypass pressure remains high, the switching system disconnects the output of the second pump from that of the first in favor of bypassing the flow to its input to reduce its differential pressure and conserve energy.
摘要翻译：提供一种流量检测双泵切换系统和方法，其控制从双泵燃料系统向燃料计量单元的燃料供应。该系统感测来自燃料计量单元的旁路压力以控制第二泵的差压。当旁路减少时，第二泵的压力增加，使得其可以被添加到第一泵的压力以提供发动机的增加的燃料消耗需求。随着燃料消耗量的降低，加入到第一泵的第二泵的流量减少，并且第二泵的差压也同样降低。如果旁路压力保持较高，则开关系统将第二泵的输出与第一泵的输出断开，有利于将流量旁路到其输入端，以减小其压差并节约能源。

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