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1. 发明授权

US06449953B1 Methods for reducing gas turbine engine emissions 有权
标题翻译：减少燃气轮机发动机排放的方法
公开(公告)号：US06449953B1
公开(公告)日：2002-09-17
申请号：US09560459
申请日：2000-04-28
申请人： Richard B. Hook, Jr. , M. Waseem Adhami , Narendra D. Joshi
发明人： Richard B. Hook, Jr. , M. Waseem Adhami , Narendra D. Joshi
IPC分类号： F02C330
CPC分类号： F02C3/30 , F05D2220/32
摘要： A gas turbine engine includes a compressor rotor assembly including a first rotor, a combustor configured to operate with a fuel/air mixture equivalence ratio less than one, and a water injection assembly. The water injection assembly includes a water delivery system including a first plurality of spray nozzles to supply water upstream from the first rotor. The water being supplied to the first rotor is atomized with the first plurality of spray nozzles prior to being supplied to the engine to lower the emissions generated by the combustor.
摘要翻译：燃气涡轮发动机包括压缩机转子组件，该压缩机转子组件包括第一转子，构造成以小于1的燃料/空气混合物当量比操作的燃烧器和水喷射组件。注水组件包括水输送系统，其包括第一多个喷嘴，以从第一转子上游供水。供给到第一转子的水在被供给到发动机之前用第一多个喷嘴雾化，以降低由燃烧器产生的排放。

2. 发明授权

US06536206B2 Apparatus for decreasing combustor emissions 有权
标题翻译：减少燃烧器排放的装置
公开(公告)号：US06536206B2
公开(公告)日：2003-03-25
申请号：US10176875
申请日：2002-06-21
申请人： Richard B. Hook, Jr. , M. Waseem Adhami , Narendra D. Joshi
发明人： Richard B. Hook, Jr. , M. Waseem Adhami , Narendra D. Joshi
IPC分类号： F02C330
CPC分类号： F02C3/30 , F05D2220/32
摘要： A gas turbine engine includes a compressor rotor assembly including a first rotor, a combustor configured to operate with a fuel/air mixture equivalence ratio less than one, and a water injection assembly. The water injection assembly includes a water delivery system including a first plurality of spray nozzles to supply water upstream from the first rotor. The water being supplied to the first rotor is atomized with the first plurality of spray nozzles prior to being supplied to the engine to lower the emissions generated by the combustor.
摘要翻译：燃气涡轮发动机包括压缩机转子组件，该压缩机转子组件包括第一转子，构造成以小于1的燃料/空气混合物当量比操作的燃烧器和水喷射组件。注水组件包括水输送系统，其包括第一多个喷嘴，以从第一转子上游供水。供给到第一转子的水在被供给到发动机之前用第一多个喷嘴雾化，以降低由燃烧器产生的排放。

3. 发明授权

US4730979A Sensor guide tube assembly for turbine with clearance restoration adjustment 失效
标题翻译：用于涡轮机的传感器导管组件，具有间隙恢复调节
公开(公告)号：US4730979A
公开(公告)日：1988-03-15
申请号：US811976
申请日：1985-12-23
申请人： Richard B. Hook, Jr.
发明人： Richard B. Hook, Jr.
IPC分类号： F01D11/00 , F01D21/00 , G01K1/14 , G01K7/02 , F01D25/00
CPC分类号： G01K1/14 , F01D11/001 , F01D21/003 , F05D2230/644
摘要： A sensor guide tube for bridging a plenum between a turbine housing and a nozzle assembly includes an offset portion whose offset is substantially equal to half the distance which the nozzle assembly is displaced upstream for clearance restoration. After clearance restoration, the guide tube is rotated 180 degrees to align its lower end with an opening in the nozzle assembly without requiring a sharp bend in the axis of the sensor guide tube.
摘要翻译：用于桥接涡轮壳体和喷嘴组件之间的气室的传感器引导管包括偏移部分，其偏移基本上等于喷嘴组件向上游移动以使间隙恢复的距离的一半。在间隙恢复之后，引导管旋转180度以将其下端与喷嘴组件中的开口对齐，而不需要传感器导管的轴线的尖锐弯曲。

4. 发明授权

US4948264A Apparatus for indirectly determining the temperature of a fluid 失效
标题翻译：用于间接测定流体温度的装置
公开(公告)号：US4948264A
公开(公告)日：1990-08-14
申请号：US882564
申请日：1986-07-07
申请人： Richard B. Hook, Jr.
发明人： Richard B. Hook, Jr.
IPC分类号： G01K13/02
CPC分类号： G01K13/02
摘要： A technique for indirectly determining the temperature of a fluid includes directing at least a portion of the fluid around the outside of a thermally conductive body so as to produce a substantially uniform temperature therein. The fluid temperature is then determined by measuring the resulting temperature within the body. In one embodiment, the fluid is directed around the body by enclosing the body in a shell which has an inlet opening, an outlet opening, and at least one passageway connecting the inlet opening to the outlet opening. In an embodiment which is particularly useful for gas turbine applications, the body is located inside of the outer casing of the turbine and is connected to a guide tube which extends through the outer casing in such a manner that the means employed for measuring the temperature within the body is insertable into and removable from the body through the guide tube. For gas turbines having two or more turbine wheel stages, the inlet opening may be connected in flow communication with a wheelspace of a relatively forward one of the stages, and the outlet opening may be connected to a wheelspace of a stage located downstream of the forward stage, so that the pressure differential created between the stages during turbine operation causes at least a portion of the gas located in the forward wheelspace to pass into the inlet opening, through the connecting passageway, and out of the outlet opening.
摘要翻译：用于间接地确定流体温度的技术包括将流体的至少一部分引导到导热体外部，以便在其中产生基本均匀的温度。然后通过测量体内产生的温度来确定流体温度。在一个实施例中，流体通过将主体包围在具有入口开口，出口开口和连接入口与出口开口的至少一个通道的壳体中而引导身体周围。在对燃气轮机应用特别有用的实施例中，主体位于涡轮机的外壳内部，并且连接到引导管，该导管延伸穿过外壳，使得用于测量内部温度的装置身体可以通过导管插入身体并从身体移除。对于具有两个或多个涡轮机叶轮级的燃气轮机，入口开口可以与相对前进的一个级的轮的空间流动连通地连接，并且出口开口可以连接到位于向前的下游的台的车轮空间使得在涡轮机操作期间在级之间产生的压力差使得位于前轮空间中的气体的至少一部分通过连接通道进入入口开口并且离开出口。

5. 发明授权

US4666368A Swirl nozzle for a cooling system in gas turbine engines 失效
标题翻译：用于燃气轮机发动机冷却系统的涡流喷嘴
公开(公告)号：US4666368A
公开(公告)日：1987-05-19
申请号：US857869
申请日：1986-05-01
申请人： Richard B. Hook, Jr. , Richard D. Montanye
发明人： Richard B. Hook, Jr. , Richard D. Montanye
IPC分类号： F02C7/18 , F01D5/08 , F01D9/02 , F01D5/18
CPC分类号： F01D5/082
摘要： Cooling air from turbine nozzle vanes of a hot gas turbine engine is collected from the vanes by an air connector. A conduit connects to the connector and terminates adjacent a turbine wheel so that air flows through the vanes and through the conduit to be emitted from the end thereof in a jet stream directed against the turbine wheel. A vaned swirl nozzle is inserted in the conduit and adjacent a turbine wheel to impart a turning impetus to the air flow stream being emitted from the nipple. The emitted air stream is then directed tangentially against or adjacent the turbine wheel in the direction of rotation thereof.
摘要翻译：来自热燃气涡轮发动机的涡轮喷嘴叶片的冷却空气通过空气连接器从叶片收集。导管连接到连接器并且邻近涡轮机叶轮终止，使得空气流过叶片并且通过导管从其端部以指向涡轮机叶轮的喷射流中发射。一个叶状漩涡喷嘴被插入管道中并且与涡轮机轮相邻，以向从乳头发射的空气流动流提供转动动力。然后将排出的空气流沿着旋转方向与涡轮机叶轮切向或相邻地引导。

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