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1. 发明授权

US6102071A Elastomeric element valve 有权
标题翻译：弹性元件阀
公开(公告)号：US6102071A
公开(公告)日：2000-08-15
申请号：US287663
申请日：1999-04-07
申请人： Herbert H. Walton , Douglas C. Pfantz , Gary L. Scott , William J. Bonzer , James L. Griffin, Jr. , Bernard Cornu , Donald K. Day , Paul R. Adams
发明人： Herbert H. Walton , Douglas C. Pfantz , Gary L. Scott , William J. Bonzer , James L. Griffin, Jr. , Bernard Cornu , Donald K. Day , Paul R. Adams
IPC分类号： G05D16/06 , F16K15/00
CPC分类号： G05D16/0641 , G05D16/02 , G05D16/0633 , Y10T137/7929 , Y10T137/8275
摘要： A fluid control valve having a valve body, a cage, and a flexible elastomeric diaphragm with a formed convolution to fully open the cage opening. An elastomeric diaphragm regulator with a flow diverter in the fluid flow path to reduce fluid flow separation and thereby reduce the required flow recovery area before pressure throttling. A raised knife edge seat located on the cage top in a position of stagnant fluid flow to reduce the build-up of contaminants on the seat. An elastomeric diaphragm regulator with a valve actuator coupled to a guided valve stem attached to the regulator diaphragm.
摘要翻译：一种流体控制阀，其具有阀体，保持架和柔性弹性体膜片，其具有形成的卷积以完全打开保持架开口。一种在流体流动路径中具有流动分流器的弹性体膜片调节器，以减少流体流动分离，从而在压力调节之前减少所需的流动恢复面积。位于笼顶上的升高的刀刃座位处于停滞的流体流动的位置，以减少座椅上污染物的积聚。一个弹性膜片调节器，带有一个阀门执行器，阀门执行器连接到连接到调节器膜片上的导向阀杆。

2. 发明授权

US08844265B2 Turbine section of high bypass turbofan 有权
标题翻译：高旁路涡轮风扇涡轮段
公开(公告)号：US08844265B2
公开(公告)日：2014-09-30
申请号：US13475252
申请日：2012-05-18
申请人： Paul R. Adams , Shankar S. Magge , Joseph B. Staubach , Wesley K. Lord , Frederick M. Schwarz , Gabriel L. Suciu
发明人： Paul R. Adams , Shankar S. Magge , Joseph B. Staubach , Wesley K. Lord , Frederick M. Schwarz , Gabriel L. Suciu
IPC分类号： F02K3/02 , F02C7/36 , F02K3/06 , F02C3/113 , F02K3/075
CPC分类号： F02C9/18 , F01D1/02 , F01D5/02 , F01D9/041 , F01D25/24 , F02C3/04 , F02C3/107 , F02C3/113 , F02C7/20 , F02C7/36 , F02K3/025 , F02K3/06 , F02K3/075 , F02K7/06 , F05D2220/32 , F05D2260/40311 , F05D2260/606 , Y02T50/671
摘要： A turbofan engine has an engine case and a gaspath through the engine case. A fan has a circumferential array of fan blades. The engine further has a compressor, a combustor, a gas generating turbine, and a low pressure turbine section. A speed reduction mechanism couples the low pressure turbine section to the fan. A bypass area ratio is greater than about 6.0. The low pressure turbine section airfoil count to bypass area ratio is below about 170.
摘要翻译：涡轮风扇发动机具有发动机壳体和通过发动机壳体的气路。风扇具有圆周阵列的风扇叶片。发动机还具有压缩机，燃烧器，气体发生涡轮机和低压涡轮部分。减速机构将低压涡轮部分连接到风扇。旁路面积比大于约6.0。低压涡轮机翼型计数到旁路面积比低于约170。

3. 发明授权

US6035878A Diagnostic device and method for pressure regulator 失效
标题翻译：压力调节器的诊断装置和方法
公开(公告)号：US6035878A
公开(公告)日：2000-03-14
申请号：US935176
申请日：1997-09-22
申请人： Paul R. Adams , Karl J. Gabel , Daniel G. Roper
发明人： Paul R. Adams , Karl J. Gabel , Daniel G. Roper
IPC分类号： G01L9/00 , F16K31/128 , F16K31/365 , F16K37/00 , G05D16/20 , G05D16/02
CPC分类号： G05D16/2093 , Y10T137/0318 , Y10T137/0379 , Y10T137/7761 , Y10T137/7768 , Y10T137/8326
摘要： A diagnostic device and method for an intelligent pressure regulator which maintains a fluid in a process at a predetermined pressure. The regulator includes an electronic controller which enhances regulator performance and provides self-diagnostics and communications capabilities. The electronic controller includes a pressure sensor which provides a signal indicating the pressure of the fluid being controlled, an adjusting pressure for adjusting the position of a throttling element; and a PID controller which receives the signal indicating the pressure of the fluid being controlled and applies the adjusting pressure to the actuator in response to the signal.
摘要翻译：一种智能压力调节器的诊断装置和方法，其将过程中的流体保持在预定压力。调节器包括一个电子控制器，可增强稳压器性能，并提供自诊断和通信功能。电子控制器包括：压力传感器，其提供指示被控制的流体的压力的信号;调节压力，用于调节节流元件的位置; 以及PID控制器，其接收指示被控制的流体的压力的信号，并响应于该信号将调节压力施加到致动器。

4. 发明授权

US09010085B2 Turbine section of high bypass turbofan 有权
标题翻译：高旁路涡轮风扇涡轮段
公开(公告)号：US09010085B2
公开(公告)日：2015-04-21
申请号：US13599175
申请日：2012-08-30
申请人： Paul R. Adams , Shankar S. Magge , Joseph B. Staubach , Wesley K. Lord , Frederick M. Schwarz , Gabriel L. Suciu
发明人： Paul R. Adams , Shankar S. Magge , Joseph B. Staubach , Wesley K. Lord , Frederick M. Schwarz , Gabriel L. Suciu
IPC分类号： F02K3/02 , F02C7/36 , F02K3/06 , F02C3/113 , F02K3/075
CPC分类号： F02C9/18 , F01D1/02 , F01D5/02 , F01D9/041 , F01D25/24 , F02C3/04 , F02C3/107 , F02C3/113 , F02C7/20 , F02C7/36 , F02K3/025 , F02K3/06 , F02K3/075 , F02K7/06 , F05D2220/32 , F05D2260/40311 , F05D2260/606 , Y02T50/671
摘要： A turbofan engine has an engine case and a gaspath through the engine case. A fan has a circumferential array of fan blades. The engine further has a compressor, a combustor, a gas generating turbine, and a low pressure turbine section. A speed reduction mechanism couples the low pressure turbine section to the fan. A bypass area ratio is greater than about 6.0. The low pressure turbine section airfoil count to bypass area ratio ratio is below about 170.
摘要翻译：涡轮风扇发动机具有发动机壳体和通过发动机壳体的气路。风扇具有圆周阵列的风扇叶片。发动机还具有压缩机，燃烧器，气体发生涡轮机和低压涡轮部分。减速机构将低压涡轮部分连接到风扇。旁路面积比大于约6.0。低压涡轮机翼型计数到旁路面积比率低于约170。

5. 发明授权

US06895351B2 Regulator flow measurement apparatus 有权
标题翻译：调节器流量测量仪
公开(公告)号：US06895351B2
公开(公告)日：2005-05-17
申请号：US10373209
申请日：2003-02-24
申请人： Bruce F. Grumstrup , Paul R. Adams
发明人： Bruce F. Grumstrup , Paul R. Adams
IPC分类号： G01F1/24 , G01F1/26 , G01F1/36 , G01F1/38 , G01F1/40 , G01F1/42 , G05D16/06 , G05D16/20 , G01L27/00 , G01F1/00 , G16K31/36
CPC分类号： G01F1/383 , G01F1/24 , G01F1/26 , G01F1/363 , G01F1/40 , G01F1/42 , G01F25/0007 , G05D16/2093 , Y10T137/7761
摘要： A method and an apparatus for determining fluid flow through a pressure regulator is disclosed. The pressure regulator is disposed in a fluid flow passage and has a throttling element moveable in the flow passage. A stem is attached to the throttling element. The apparatus includes a first pressure sensor for measuring pressure upstream of the throttling element, a second pressure sensor for measuring pressure downstream of the throttling element, and a travel sensor for detecting the position of the throttling element. A processor is provided which includes a stored algorithm for determining flow rate based on the measured pressure and travel values and for calibrating the pressure regulator using a temporary flow meter disposed downstream of the throttling element. A system and method is also provided for calibrating a temperature transmitter associated with the pressure regulator.
摘要翻译：公开了一种用于确定通过压力调节器的流体流动的方法和装置。压力调节器设置在流体流动通道中并且具有可在流动通道中移动的节流元件。阀杆连接到节流元件。该装置包括用于测量节流元件上游压力的第一压力传感器，用于测量节流元件下游压力的第二压力传感器，以及用于检测节流元件位置的行进传感器。提供了一种处理器，其包括用于基于测量的压力和行进值来确定流量的存储算法，并且使用设置在节流元件下游的临时流量计来校准压力调节器。还提供了用于校准与压力调节器相关联的温度变送器的系统和方法。

6. 发明授权

US6056008A Intelligent pressure regulator 失效
标题翻译：智能压力调节器
公开(公告)号：US6056008A
公开(公告)日：2000-05-02
申请号：US934943
申请日：1997-09-22
申请人： Paul R. Adams , Karl J. Gabel , Daniel G. Roper
发明人： Paul R. Adams , Karl J. Gabel , Daniel G. Roper
IPC分类号： G05D16/20 , F16K31/40
CPC分类号： G05D16/2093
摘要： An intelligent pressure regulator for maintaining a fluid in a process at a predetermined pressure includes an electronic controller which enhances regulator performance and provides self-diagnostics and communications capabilities. The electronic controller includes a pressure sensor which provides a signal indicating the pressure of the fluid being controlled, an adjusting pressure for adjusting the position of a throttling element; and a PID controller which receives the signal indicating the pressure of the fluid being controlled and applies the adjusting pressure to the actuator in response to the signal.
摘要翻译：用于将处理中的流体维持在预定压力的智能压力调节器包括增强调节器性能并提供自诊断和通信能力的电子控制器。电子控制器包括：压力传感器，其提供指示被控制的流体的压力的信号;调节压力，用于调节节流元件的位置; 以及PID控制器，其接收指示被控制的流体的压力的信号，并响应于该信号将调节压力施加到致动器。

7. 发明授权

US06903659B2 Low power regulator system and method 有权
标题翻译：低功率调节系统及方法
公开(公告)号：US06903659B2
公开(公告)日：2005-06-07
申请号：US10679558
申请日：2003-10-06
申请人： Richard J. Vanderah , Paul R. Adams , David E. Woolums , Jon B. Milliken
发明人： Richard J. Vanderah , Paul R. Adams , David E. Woolums , Jon B. Milliken
IPC分类号： G05D16/06 , G01F1/36 , G01F1/40 , G01F1/42 , G05B19/042 , G05D16/20 , G08B17/10
CPC分类号： G05B19/042 , G01F1/363 , G01F1/40 , G01F1/42 , G05B2219/24138 , G05B2219/25036 , G05B2219/25289 , G05D16/2053 , G05D16/2093
摘要： Methods are disclosed for collecting sensor data in a pressure regulator system including a controller and a plurality of sensors. The controller and each of the individual sensors are activated as required to collect sensor data during a sampling period thereby reducing the amount of power consumed by the pressure regulator system. Further power conservation measures are implemented by using a battery sensor to monitor the capacity of the pressure regulator battery and placing the pressure regulator in reduced power consumption operating modes as the capacity of the battery is reduced.
摘要翻译：公开了用于在包括控制器和多个传感器的压力调节器系统中收集传感器数据的方法。根据需要，控制器和每个单独的传感器被激活以在采样周期期间收集传感器数据，从而减少压力调节器系统消耗的功率量。通过使用电池传感器来监测压力调节器电池的容量并且将压力调节器放置在降低的功耗操作模式中以进一步节能措施，因为电池的容量减小。

8. 发明授权

US06499940B2 Compressor casing for a gas turbine engine 有权
标题翻译：用于燃气涡轮发动机的压缩机壳体
公开(公告)号：US06499940B2
公开(公告)日：2002-12-31
申请号：US09812001
申请日：2001-03-19
申请人： Paul R. Adams
发明人： Paul R. Adams
IPC分类号： F01D2100
CPC分类号： F01D11/08 , F04D29/164 , F04D29/526 , F04D29/685 , Y10S415/914
摘要： The cylindrical compressor casing of a gas turbine engine has a plurality of radially inwardly and axially rearwardly opening anti-surge grooves disposed on a radially inner surface thereof whereby foreign objects ingested into the engine and entering the grooves are free to move axially rearwardly of the engine.
摘要翻译：燃气涡轮发动机的圆筒形压缩机壳体具有设置在其径向内表面上的多个径向向内和轴向向后打开的防喘振槽，由此吸入发动机并进入槽的异物自由地沿着发动机的轴向向后移动。

9. 发明申请

US20140102076A1 Turbine Section of High Bypass Turbofan 审中-公开
标题翻译：高旁路涡轮风机部分
公开(公告)号：US20140102076A1
公开(公告)日：2014-04-17
申请号：US13599175
申请日：2012-08-30
申请人： Paul R. Adams , Shankar S. Magge , Joseph B. Staubach , Wesley K. Lord , Frederick M. Schwarz , Gabriel L. Suciu
发明人： Paul R. Adams , Shankar S. Magge , Joseph B. Staubach , Wesley K. Lord , Frederick M. Schwarz , Gabriel L. Suciu
IPC分类号： F02C3/113 , F02K3/075 , F02K3/02
CPC分类号： F02C9/18 , F01D1/02 , F01D5/02 , F01D9/041 , F01D25/24 , F02C3/04 , F02C3/107 , F02C3/113 , F02C7/20 , F02C7/36 , F02K3/025 , F02K3/06 , F02K3/075 , F02K7/06 , F05D2220/32 , F05D2260/40311 , F05D2260/606 , Y02T50/671
摘要： A turbofan engine has an engine case and a gaspath through the engine case. A fan has a circumferential array of fan blades. The engine further has a compressor, a combustor, a gas generating turbine, and a low pressure turbine section. A speed reduction mechanism couples the low pressure turbine section to the fan. A bypass area ratio is greater than about 6.0. The low pressure turbine section airfoil count to bypass area ratio ratio is below about 170.
摘要翻译：涡轮风扇发动机具有发动机壳体和通过发动机壳体的气路。风扇具有圆周阵列的风扇叶片。发动机还具有压缩机，燃烧器，气体发生涡轮机和低压涡轮部分。减速机构将低压涡轮部分连接到风扇。旁路面积比大于约6.0。低压涡轮机翼型计数到旁路面积比率低于约170。

10. 发明申请

US20120291449A1 Turbine Section of High Bypass Turbofan 有权
标题翻译：高旁路涡轮风机部分
公开(公告)号：US20120291449A1
公开(公告)日：2012-11-22
申请号：US13475252
申请日：2012-05-18
申请人： Paul R. Adams , Shankar S. Magge , Joseph B. Staubach , Wesley K. Lord , Frederick M. Schwarz , Gabriel L. Suciu
发明人： Paul R. Adams , Shankar S. Magge , Joseph B. Staubach , Wesley K. Lord , Frederick M. Schwarz , Gabriel L. Suciu
IPC分类号： F02C3/04
CPC分类号： F02C9/18 , F01D1/02 , F01D5/02 , F01D9/041 , F01D25/24 , F02C3/04 , F02C3/107 , F02C3/113 , F02C7/20 , F02C7/36 , F02K3/025 , F02K3/06 , F02K3/075 , F02K7/06 , F05D2220/32 , F05D2260/40311 , F05D2260/606 , Y02T50/671
摘要： A turbofan engine has an engine case and a gaspath through the engine case. A fan has a circumferential array of fan blades. The engine further has a compressor, a combustor, a gas generating turbine, and a low pressure turbine section. A speed reduction mechanism couples the low pressure turbine section to the fan. A bypass area ratio is greater than about 6.0. The low pressure turbine section airfoil count to bypass area ratio is below about 170.
摘要翻译：涡轮风扇发动机具有发动机壳体和通过发动机壳体的气路。风扇具有圆周阵列的风扇叶片。发动机还具有压缩机，燃烧器，气体发生涡轮机和低压涡轮部分。减速机构将低压涡轮部分连接到风扇。旁路面积比大于约6.0。低压涡轮机翼型计数到旁路面积比低于约170。

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