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1. 发明授权

US06763324B1 Integrated engineering analysis process with solution feedback 有权
标题翻译：集成工程分析流程与解决方案反馈
公开(公告)号：US06763324B1
公开(公告)日：2004-07-13
申请号：US09534677
申请日：2000-03-24
申请人： Robert N. Pittman , Scott J. Dennison , Kenneth E. Seitzer , John D. Bibler , Stephen P. Schrantz , John C. Blanton , Mir M. Ali , Robert J. Maffeo , James C. Dudley , David M. Johnson
发明人： Robert N. Pittman , Scott J. Dennison , Kenneth E. Seitzer , John D. Bibler , Stephen P. Schrantz , John C. Blanton , Mir M. Ali , Robert J. Maffeo , James C. Dudley , David M. Johnson
IPC分类号： G06F1710
CPC分类号： G05B17/02 , F05B2230/00 , F05B2260/20 , F05B2270/303 , G05B19/0426 , G05B2219/23292 , G05B2219/23293 , Y02T50/675
摘要： An integrated engineering analysis system that determines at least one final output value in response to at least one initial input value. A first subprocesses provides at least one output value in response to the initial input value. A plurality of subprocesses provide a plurality of output values in response to the output values of the first subprocess. The plurality of output values and the output value of the first subprocess are inputted into at least one of the plurality of subprocesses. A command code executes each of the plurality of subprocesses in response to the output values and determines which one of the plurality of subprocesses to run and a final subprocess provides a final output. The final output is the result of a plurality of calculations executed by the plurality of subprocesses and the command code compares the final output with the initial input.
摘要翻译：综合工程分析系统，其响应于至少一个初始输入值确定至少一个最终输出值。第一子处理器响应于初始输入值提供至少一个输出值。多个子处理器响应于第一子过程的输出值提供多个输出值。将多个输出值和第一子过程的输出值输入到多个子处理中的至少一个。命令代码响应于输出值执行多个子处理中的每一个，并且确定要运行的多个子处理中的哪个子进程和最后的子进程提供最终的输出。最终输出是由多个子处理执行的多个计算的结果，并且命令代码将最终输出与初始输入进行比较。

2. 发明授权

US5351478A Compressor casing assembly 失效
标题翻译：压缩机套管总成
公开(公告)号：US5351478A
公开(公告)日：1994-10-04
申请号：US891494
申请日：1992-05-29
申请人： Roger C. Walker , Richard J. Fallon , Harold P. Rieck, Jr. , John D. Bibler
发明人： Roger C. Walker , Richard J. Fallon , Harold P. Rieck, Jr. , John D. Bibler
IPC分类号： F02C7/00 , F01D25/26 , F02C7/18 , F02C9/18 , F04D29/58 , F02C6/18
CPC分类号： F01D25/26 , F04D29/522 , F04D29/584 , F05D2240/126 , F05D2260/201 , F05D2260/941 , Y02T50/676
摘要： An apparatus and method for minimizing compressor casing distortion due to bleed air extraction wherein the compressor casing includes an annular outer casing having at least one outlet duct, an annular inner casing disposed co-axially with the outer casing and spaced radially inwardly therefrom to define a plenum, two radial discs extending inwardly from the outer casing defining a plenum, a plurality of small area bleed openings located in the inner casing for imparting a radial velocity to the bleed air greater than the circumferential velocity entering the plenum, an air tube located over each bleed opening, and a baffle plate located on top of the air tubes and communicating with the radial discs for supporting the casings, whereby the bleed air impinges on the outer casing and controls distortion by sufficiently reducing the circumferential temperature gradient forming at the outer casing.
摘要翻译：一种用于使压缩机壳体由于排气提取引起的变形最小化的装置和方法，其中所述压缩机壳体包括具有至少一个出口管道的环形外壳，与所述外壳同轴并与所述外壳径向向内间隔开的环形外壳，气室，从限定集气室的外壳向内延伸的两个径向盘，位于内壳中的多个小区域排放口，用于使放气速度大于进入气室的圆周速度，空气管位于每个排气口和位于空气管顶部的挡板，并与用于支撑壳体的径向盘连通，由此泄放空气冲击外壳并通过充分降低在外壳处形成的周向温度梯度来控制变形。

3. 发明授权

US06339923B1 Fuel air mixer for a radial dome in a gas turbine engine combustor 失效
标题翻译：用于燃气涡轮发动机燃烧器中的径向圆顶的燃料空气混合器
公开(公告)号：US06339923B1
公开(公告)日：2002-01-22
申请号：US09398559
申请日：1999-09-17
申请人： Ely E. Halila , Stuart C. Greenfield , Paul V. Heberling , John D. Bibler , John A. Kastl
发明人： Ely E. Halila , Stuart C. Greenfield , Paul V. Heberling , John D. Bibler , John A. Kastl
IPC分类号： F23R330
CPC分类号： F23R3/286 , F23R3/343 , F23R3/50
摘要： A fuel air mixer for a gas turbine engine combustor having a longitudinal axis therethrough, wherein the fuel air mixer is configured for use in a dome oriented substantially radial to the longitudinal axis. The fuel air mixer includes a fuel injection assembly having a first end, a second end, a fuel passage extending therethrough, and a flange portion having a plurality of spaced openings formed therein which extends from the first end. The fuel air mixer also includes a mixer assembly having a first end, a second end, a cavity formed in a central portion thereof, and a flange portion having a plurality of spaced openings formed therein which extends from the first end. The mixer assembly is configured to receive the fuel injection assembly in the cavity so that the fuel injection assembly and the mixer assembly are able to be connected to an outer casing of the combustor by means of the respective flange portions.
摘要翻译：一种用于燃气涡轮发动机燃烧器的燃料空气混合器，其具有穿过其的纵向轴线，其中所述燃料空气混合器构造成用于基本上径向于所述纵向轴线的圆顶。燃料空气混合器包括燃料喷射组件，其具有第一端，第二端，延伸穿过其中的燃料通道，以及在其中形成有从第一端延伸的多个间隔开口的凸缘部分。燃料空气混合器还包括具有第一端，第二端，形成在其中心部分中的空腔的混合器组件，以及形成在其中的从第一端延伸的多个间隔开口的凸缘部分。混合器组件构造成在空腔中接收燃料喷射组件，使得燃料喷射组件和混合器组件能够通过相应的凸缘部分连接到燃烧器的外壳。

4. 发明授权

US06871501B2 Method and apparatus to decrease gas turbine engine combustor emissions 有权
标题翻译：降低燃气轮机发动机燃烧器排放的方法和装置
公开(公告)号：US06871501B2
公开(公告)日：2005-03-29
申请号：US10308711
申请日：2002-12-03
申请人： John D. Bibler , Timothy J. Held , Mark A. Mueller
发明人： John D. Bibler , Timothy J. Held , Mark A. Mueller
IPC分类号： F23R3/00 , F23R3/14 , F23R3/18 , F23R3/28 , F02C7/22 , F23R3/10
CPC分类号： F23R3/286 , F23R3/002 , F23R3/14 , F23R2900/03044 , Y02T50/675
摘要： A method enables a gas turbine engine including a combustor to be operated. The combustor includes a mixer assembly including an air swirler, a premixer, a dome plate, and a heat shield. The method comprises discharging fluids from the air swirler into the premixer, and directing cooling fluids through a cooling opening defined in at least one of the swirler and the dome plate towards an upstream side of the heat shield for impingement cooling of the heat shield.
摘要翻译：一种方法使得能够操作包括燃烧器的燃气涡轮发动机。燃烧室包括一个包括空气旋流器，预混合器，圆顶板和隔热罩的混合器组件。该方法包括将流体从空气旋流器排放到预混合器中，并且将冷却流体引导通过限定在旋流器和圆顶板中的至少一个的冷却开口朝向隔热罩的上游侧，以对隔热板进行冲击冷却。

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