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11. 发明申请

US20150233580A1 GAS TURBINE COMBUSTION ACOUSTIC DAMPING SYSTEM 有权
标题翻译：气体涡轮机燃烧阻尼系统
公开(公告)号：US20150233580A1
公开(公告)日：2015-08-20
申请号：US14566963
申请日：2014-12-11
申请人： Andrew J. Olsen , Ivar Austrem , M. Serkan Yildirim , Zheji Liu
发明人： Andrew J. Olsen , Ivar Austrem , M. Serkan Yildirim , Zheji Liu
IPC分类号： F23R3/26 , F02C3/04
CPC分类号： F02C7/24 , F01D5/02 , F02C3/04 , F02C3/145 , F02C7/18 , F04D29/321 , F05D2220/32 , F05D2240/35 , F05D2240/60 , F05D2260/201 , F05D2260/96 , F05D2260/963 , F05D2270/14 , F23R3/002 , F23R3/06 , F23R3/14 , F23R3/286 , F23R3/54 , F23R3/60 , F23R2900/00014 , F23R2900/03041 , F23R2900/03042 , F23R2900/03044
摘要： A gas turbine may include a rotatable shaft, a compressor disposed about the rotatable shaft and configured to output compressed air, and a combustor disposed about the rotatable shaft. The combustor may be configured to receive the compressed air and output high temperature compressed gas. The gas turbine may further include a power turbine disposed about the rotatable shaft and configured to receive the high temperature compressed gas, and a first liner defining a plurality of holes and disposed around the combustor. The power turbine may be configured to expand the high temperature compressed gas and rotate the rotatable shaft. The first liner may have a first end and a longitudinally opposite second end. The first end may be coupled to an inner surface of the casing at or adjacent an upstream end of the combustor and the second end may be substantially free from any connection with the casing.
摘要翻译：燃气轮机可以包括可旋转的轴，围绕可旋转轴布置并被构造成输出压缩空气的压缩机和围绕可旋转轴设置的燃烧器。燃烧器可以构造成接收压缩空气并输出高温压缩气体。燃气轮机还可以包括设置在可旋转轴周围并被配置为容纳高温压缩气体的动力涡轮机，以及限定多个孔并设置在燃烧器周围的第一衬套。动力涡轮机可构造成膨胀高温压缩气体并旋转可旋转轴。第一衬垫可以具有第一端和纵向相对的第二端。第一端可以在燃烧器的上游端处或邻近燃烧器的上游端处联接到壳体的内表面，并且第二端可以基本上没有与壳体的任何连接。

12. 发明授权

US08453253B2 Controller device 有权
标题翻译：控制器设备
公开(公告)号：US08453253B2
公开(公告)日：2013-05-28
申请号：US12709822
申请日：2010-02-22
申请人： Matthew B. Strong , Paul J. Hepworth , Mark L. Gray , Andrew J. Olsen , Tim Pruss
发明人： Matthew B. Strong , Paul J. Hepworth , Mark L. Gray , Andrew J. Olsen , Tim Pruss
IPC分类号： G06F7/04 , G06F21/00 , G06F21/62
CPC分类号： G06F21/00 , B26D5/00 , B26D5/005 , B26F1/38 , G05B19/042 , G05B2219/23049 , G05B2219/23417 , G05B2219/25107 , G05B2219/36513 , G06F21/6218 , G06Q30/0185 , G06Q30/0251
摘要： A method of operating a controller device of an electronic cutting machine. The method includes writing a controller device identifier to memory of the cartridge, writing a cartridge identifier to memory of the controller device, and permitting communication between the controller device and the cartridge.
摘要翻译：一种操作电子切割机的控制装置的方法。该方法包括将控制器设备标识符写入盒的存储器，将盒标识符写入控制器设备的存储器，以及允许控制器设备和盒之间的通信。

13. 发明申请

US20100107876A1 SYSTEM AND METHOD FOR REMOVING WATER AND SILOXANES FROM GAS 失效
标题翻译：从气体中去除水和硅氧烷的系统和方法
公开(公告)号：US20100107876A1
公开(公告)日：2010-05-06
申请号：US12648900
申请日：2009-12-29
申请人： Andrew J. Olsen , Shaun D. Sullivan
发明人： Andrew J. Olsen , Shaun D. Sullivan
IPC分类号： B01D5/00 , B01D9/04
CPC分类号： B01D53/002 , B01D5/0045 , B01D5/0048 , B01D53/265 , B01D2257/70 , F05B2250/82
摘要： A method of removing siloxanes from a gas that contains siloxanes and water, the method comprising: (a) expanding the gas to cool the gas and freeze at least some of the water in the gas; and (b) removing the siloxanes and frozen water from the expanded and cooled gas. The method may also include compressing the gas prior to expanding it. The step of expanding the gas may include expanding it through a turbine. The method may also include using an energy input mechanism to drive one or both of the compressor or turbine. The ice and siloxanes may be removed from the gas with a cyclonic separator.
摘要翻译：一种从含有硅氧烷和水的气体中除去硅氧烷的方法，该方法包括：（a）使气体膨胀以冷却气体并冷冻气体中的至少一些水; 和（b）从膨胀和冷却的气体中除去硅氧烷和冷冻水。该方法还可以包括在膨胀之前压缩气体。膨胀气体的步骤可以包括通过涡轮膨胀。该方法还可以包括使用能量输入机构来驱动压缩机或涡轮机中的一个或两个。冰和硅氧烷可以用气旋分离器从气体中除去。

14. 发明授权

US5630700A Floating vane turbine nozzle 失效
标题翻译：浮动叶片涡轮喷嘴
公开(公告)号：US5630700A
公开(公告)日：1997-05-20
申请号：US638094
申请日：1996-04-26
申请人： Andrew J. Olsen , William L. Blair
发明人： Andrew J. Olsen , William L. Blair
IPC分类号： F01D5/18 , F01D9/04 , F01D25/26
CPC分类号： F01D5/189 , F01D9/042 , Y02T50/672 , Y02T50/673 , Y02T50/676
摘要： A turbine nozzle includes outer and inner bands having respective mounting holes therein. A plurality of vanes extends through respective pairs of outer and inner holes in the bands. The vane outer and inner ends are resiliently supported to the bands to allow differential thermal movement therebetween so that the individual vanes float relative to the outer and inner bands to prevent thermal stress failure thereof.
摘要翻译：涡轮喷嘴包括其中具有各自的安装孔的外带和内带。多个叶片延伸穿过带中的相应的一对外孔和内孔。叶片外端和内端弹性地支撑在带上，以允许它们之间差异的热运动，使得各个叶片相对于外带和内带漂浮以防止其热应力衰竭。

15. 发明申请

US20100217427A1 Controller Device 有权
标题翻译：控制器设备
公开(公告)号：US20100217427A1
公开(公告)日：2010-08-26
申请号：US12709822
申请日：2010-02-22
申请人： Mark L. Gray , Andrew J. Olsen , Paul J. Hepworth , Tim Pruss , Matthew B. Strong
发明人： Mark L. Gray , Andrew J. Olsen , Paul J. Hepworth , Tim Pruss , Matthew B. Strong
IPC分类号： G06F19/00 , G06F12/00 , G06F12/14 , G06Q10/00 , G06Q30/00 , G06Q50/00
CPC分类号： G06F21/00 , B26D5/00 , B26D5/005 , B26F1/38 , G05B19/042 , G05B2219/23049 , G05B2219/23417 , G05B2219/25107 , G05B2219/36513 , G06F21/6218 , G06Q30/0185 , G06Q30/0251
摘要： A method of operating a controller device of an electronic cutting machine. The method includes writing a controller device identifier to memory of the cartridge, writing a cartridge identifier to memory of the controller device, and permitting communication between the controller device and the cartridge.
摘要翻译：一种操作电子切割机的控制装置的方法。该方法包括将控制器设备标识符写入盒的存储器，将盒标识符写入控制器设备的存储器，以及允许控制器设备和盒之间的通信。

16. 发明授权

US06814537B2 Interchangeable power turbine cartridge assembly 失效
标题翻译：可互换动力涡轮机组件
公开(公告)号：US06814537B2
公开(公告)日：2004-11-09
申请号：US10253219
申请日：2002-09-24
申请人： Andrew J. Olsen
发明人： Andrew J. Olsen
IPC分类号： F01D2508
CPC分类号： F01D1/08 , F01D25/164 , F01D25/166 , F01D25/186 , F02C7/06 , F05D2220/40 , F16C21/00 , F16C33/1045 , F16C2360/00
摘要： The invention recites a power turbine assembly including a turbine rotor and a plurality of turbine blades mounted to said rotor and adapted to rotate said rotor in response to a flow of hot gas over said blades. A support structure having a journal bearing and at least one other bearing supports said rotor for rotation, said journal bearing having a proximal end and a distal end with respect to said turbine blades. A supply of lubricant communicates with said journal bearing to provide lubricant between said rotor and an inner surface of said journal bearing, said lubricant damping rotational frequencies of said rotor and creating a temperature gradient from greater than about 1000° F. at said blades to less than about 350° F. at said distal end.
摘要翻译：本发明叙述了一种动力涡轮组件，其包括涡轮转子和安装在所述转子上的多个涡轮叶片，并适于响应于所述叶片上的热气流而旋转所述转子。具有轴颈轴承和至少一个其它轴承的支撑结构支撑所述转子用于旋转，所述轴颈轴承具有相对于所述涡轮叶片的近端和远端。所述润滑剂供应装置与所述轴颈轴承连通，以在所述转子和所述轴颈轴承的内表面之间提供润滑剂，所述润滑剂阻止所述转子的旋转频率，并产生在所述叶片处大于约1000°F的温度梯度小于在所述远端约350°F。

17. 发明授权

US06735952B2 Single pump lubrication and starter system 有权
标题翻译：单泵润滑和起动系统
公开(公告)号：US06735952B2
公开(公告)日：2004-05-18
申请号：US10238526
申请日：2002-09-10
申请人： Andrew J. Olsen
发明人： Andrew J. Olsen
IPC分类号： F02C706
CPC分类号： F01D25/16 , F01D25/18 , F01D25/186 , F01D25/20 , F02C7/27 , F02C7/277
摘要： The invention recites a microturbine system comprising a housing and a turbine including a rotary element having a shaft supported by the housing and rotatable about a rotary axis. A starter wheel is coupled to the shaft and rotatable in response to a stream of high-pressure fluid flowing from a high-pressure flow path. A pump is operable to provide a supply of lubricating fluid. The engine further includes a starter valve receiving the supply of lubricating fluid and being selectively operable to provide one of the stream of high-pressure fluid to the high-pressure flow path and a stream of low-pressure fluid to a low-pressure flow path.
摘要翻译：本发明阐述了一种微型涡轮机系统，其包括壳体和涡轮机，该涡轮机包括旋转元件，该旋转元件具有由壳体支撑并可围绕旋转轴线旋转的轴。启动轮联接到轴上并响应于从高压流动路径流动的高压流体流而可旋转。泵可操作以提供润滑流体的供应。发动机还包括接收润滑流体供应的起动阀，并且可选择性地操作以将高压流体流中的一个提供给高压流动路径，并将低压流体流提供到低压流动路径。

18. 发明授权

US06598400B2 Gas turbine with articulated heat recovery heat exchanger 失效
标题翻译：带铰接热回收热交换器的燃气轮机
公开(公告)号：US06598400B2
公开(公告)日：2003-07-29
申请号：US09968297
申请日：2001-10-01
申请人： James S. Nash , James B. Kesseli , Andrew J. Olsen
发明人： James S. Nash , James B. Kesseli , Andrew J. Olsen
IPC分类号： F02C710
CPC分类号： F02C6/18 , F02C7/08 , F05D2220/76 , F28D21/001 , F28F2280/10 , Y02E20/14 , Y10S165/138
摘要： A cogenerating recuperated microturbine includes a recuperator, an air compressor and a combustor. The combustor burns a fuel along with the compressed air received from the recuperator to create products of combustion. A turbine generator operates in response to expansion of the products of combustion to generate electricity. The products of combustion then flow through the recuperator to preheat the compressed air. The products of combustion then flow out of the recuperator as an exhaust flow. A heat exchanger is movable into and out of the exhaust flow to selectively heat a fluid in the heat exchanger. The heat exchanger is actuated by a piston-cylinder type actuator that operates under the influence of compressed air selectively bled from the air compressor. The actuator may be a single-acting cylinder used in conjunction with a biasing spring, or may be a double-acting cylinder.
摘要翻译：热交换式回热微型涡轮机包括换热器，空气压缩机和燃烧器。燃烧器将燃烧器与从换热器接收的压缩空气一起燃烧以产生燃烧产物。涡轮发电机响应于燃烧产物的膨胀而发电。然后，燃烧产物流过换热器以预热压缩空气。然后，燃烧产物作为废气流从换热器中流出。热交换器可移动进出排气流以选择性地加热热交换器中的流体。热交换器由在空气压缩机选择性地排出的压缩空气的影响下运行的活塞 - 气缸式致动器致动。致动器可以是与偏置弹簧一起使用的单作用缸，或者可以是双作用缸。

19. 发明授权

US06484490B1 Gas turbine system and method 有权
标题翻译：燃气轮机系统及方法
公开(公告)号：US06484490B1
公开(公告)日：2002-11-26
申请号：US09679555
申请日：2000-10-06
申请人： Andrew J. Olsen , John H. Thomson , Jason K. Hargrove
发明人： Andrew J. Olsen , John H. Thomson , Jason K. Hargrove
IPC分类号： F02C322
CPC分类号： F02C7/22
摘要： A gas booster system in which a variable frequency drive is used to control, by means of a variable speed motor, the compression rate of a pump in a gas turbine combustion engine. The rate of the variable speed motor, and thus the rate of compression, is controlled by monitoring turbine temperature. The gas turbine system responds to the turbine temperature to regulate the rate of compression of the fuel.
摘要翻译：一种燃气增压系统，其中使用变频驱动器通过变速电动机来控制燃气轮机内燃机中的泵的压缩比。通过监测涡轮机温度来控制变速电动机的速率以及压缩速率。燃气轮机系统响应于涡轮机温度以调节燃料的压缩速率。

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