公开(公告)号：US09115649B2

公开(公告)日：2015-08-25

申请号：US13176473

申请日：2011-07-05

Applicant: Edward J. Gallagher ,  Becky E. Rose ,  Lisa I. Brilliant

Inventor： Edward J. Gallagher ,  Becky E. Rose ,  Lisa I. Brilliant

IPC: F02C7/36 ,  F01D15/12 ,  F01D25/34 ,  F02C7/05 ,  F02K3/06

CPC classification number: F02C7/36 ,  F01D5/141 ,  F01D15/12 ,  F01D21/045 ,  F01D25/34 ,  F02C7/05 ,  F02K3/06 ,  Y02T50/673

Abstract: A gas turbine engine includes a spool, a turbine coupled to drive the spool, a propulsor coupled to be rotated about an axis by the turbine through the spool, and a gear assembly coupled between the propulsor and the spool such that rotation of the turbine drives the propulsor at a different speed than the spool. The propulsor includes a hub and a row of propulsor blades that extend from the hub. Each of the propulsor blades has a span between a root at the hub and a tip, and a chord between a leading edge and a trailing edge. The chord forms a stagger angle α with the axis, and the stagger angle α is less than 15° at a position along the propulsor blade that is within an inboard 20% of the span.

Abstract translation: 燃气涡轮发动机包括阀芯，联接以驱动阀芯的涡轮机，被连接以通过阀芯绕涡轮机绕轴旋转的推进器，以及联接在推进器和阀芯之间的齿轮组件，使得涡轮机驱动 推进器的速度不同于阀芯。 推进器包括从轮毂延伸的轮毂和一排推杆叶片。 每个推进器叶片具有在轮毂的根部与顶端之间的跨度，以及前缘和后缘之间的弦。 弦与轴线形成交错角α，并且在沿着推进刀片的位置处的交错角α小于15°，该推进角度在跨度的20％内。

公开(公告)号：US20150101344A1

公开(公告)日：2015-04-16

申请号：US14053969

申请日：2013-10-15

Applicant: BHA Altair, LLC

Inventor： Etienne Rene Jarrier ,  Martin Gregory Hatfield ,  Paul Michael Kienitz

IPC: F02C7/05 ,  F02M35/08 ,  F02M35/024

CPC classification number: F02C7/05 ,  B01D46/0087 ,  B01D46/0095 ,  B01D2273/14 ,  F02M35/024 ,  F02M35/082

Abstract: A system including an air intake subsystem having a housing is provided. A coalescer having a frame is disposed inside the housing. The system includes a mounting bracket, and a release mechanism coupled to the frame and the mounting bracket. The release mechanism is adapted to selectively release the frame.

Abstract translation: 提供一种包括具有壳体的进气子系统的系统。 具有框架的聚结器设置在壳体内。 该系统包括安装支架和联接到框架和安装支架的释放机构。 释放机构适于选择性地释放框架。

公开(公告)号：US08833083B2

公开(公告)日：2014-09-16

申请号：US12587340

申请日：2009-10-06

Applicant: Ben M. Enis ,  Paul Lieberman

Inventor： Ben M. Enis ,  Paul Lieberman

IPC: F02C1/00

CPC classification number: F02C7/143 ,  F02C7/05 ,  F05D2260/601 ,  Y02E20/14 ,  Y10T137/794

Abstract: An apparatus for increasing the efficiency of a fuel driven turbine generator, including a system comprising a turbo compressor and turbo expander that produces super chilled air mixed with ambient air to produce relatively cool dry inlet air that can be introduced under pressure into the generator. A separation compartment with a passageway extending normal to the travel direction of the chilled air is used to remove ice particles and particulates from the cool inlet air to avoid damage to the turbine blades. Additional apparatuses such as heat exchangers and steam driven turbine generators and chillers, as well as thermal energy storage systems, are contemplated.

Abstract translation: 一种用于提高燃料驱动涡轮发电机的效率的装置，包括包括涡轮压缩机和涡轮膨胀机的系统，该系统产生与环境空气混合的超冷却空气，以产生可在压力下引入发电机的相对较冷的干入口空气。 使用具有垂直于冷冻空气行进方向延伸的通道的分离室，以从冷入口空气中除去冰粒和颗粒，以避免损坏涡轮叶片。 考虑了诸如热交换器和蒸汽驱动的涡轮发电机和冷却器的附加装置以及热能储存系统。

公开(公告)号：US20130255359A1

公开(公告)日：2013-10-03

申请号：US13433371

申请日：2012-03-29

Applicant: Peter John Duncan Smith ,  Stephen David Hiner ,  Stephen Francis Banks

Inventor： Peter John Duncan Smith ,  Stephen David Hiner ,  Stephen Francis Banks

IPC: G01N15/08

CPC classification number: F02C7/05 ,  F05D2260/83

Abstract: A portable filter testing assembly for testing filter elements is provided. The portable filter testing assembly includes a first modular component including filter elements disposed within an interior and a fluid flow inlet. The testing assembly further includes a second modular component in fluid communication with the first modular component and includes fluid flow drawing means for drawing fluid flow through the filter elements of the first modular component such that the fluid flow is filtered by the filter elements. Each of the first modular component and second modular component includes an external structure of a modular International Organization for Standardization (ISO) shipping container. A kit of plural modular components for testing filter elements is provided. A method of using ISO modular components for testing filter elements is also provided.

Abstract translation: 提供了一种用于测试过滤元件的便携式过滤器测试组件。 便携式过滤器测试组件包括第一模块化组件，包括设置在内部的过滤元件和流体流入口。 测试组件还包括与第一模块化部件流体连通的第二模块化部件，并且包括流体流动拉伸装置，用于抽取流过第一模块化部件的过滤元件的流体流动，使得流体流被过滤元件过滤。 第一模块化部件和第二模块部件中的每一个包括模块化国际标准化组织（ISO）运输集装箱的外部结构。 提供了一套用于测试过滤元件的多个模块化部件。 还提供了使用ISO模块化组件测试过滤元件的方法。

公开(公告)号：US20130087045A1

公开(公告)日：2013-04-11

申请号：US13253273

申请日：2011-10-05

Applicant: Michael Adelbert Sullivan ,  Huong Van Vu ,  Bhalchandra Arun Desai ,  Eric M. Lafontaine ,  Mark Andrew Cournoyer

Inventor： Michael Adelbert Sullivan ,  Huong Van Vu ,  Bhalchandra Arun Desai ,  Eric M. Lafontaine ,  Mark Andrew Cournoyer

IPC: B01D46/42

CPC classification number: F02C7/05 ,  F02C7/143 ,  F05D2250/70 ,  F05D2250/71 ,  F05D2300/522 ,  F28F13/14

Abstract: A system for conditioning air flow to a gas turbine includes a filter housing and a conditioning media inside the filter housing to adjust the temperature of the air flowing through the filter housing. At least one of a depth or a density of the conditioning media varies across the filter housing. A method for conditioning air flow to a gas turbine includes flowing air through a filter housing connected to the gas turbine and flowing the air across a conditioning media in the filter housing. The method further includes conditioning the air flow to reduce the temperature difference of the air exiting the filter housing across a dimension of the filter housing.

Abstract translation: 用于调节到燃气轮机的空气流的系统包括过滤器壳体和过滤器壳体内部的调节介质，以调节流过过滤器壳体的空气的温度。 调节介质的深度或密度中的至少一个在过滤器壳体上变化。 用于调节到燃气轮机的空气流的方法包括使空气流过连接到燃气轮机的过滤器壳体并使空气流过过滤器壳体中的调节介质。 该方法还包括调节空气流量以减小过滤器壳体的空气在过滤器壳体的尺寸上的温度差。

公开(公告)号：US08402737B2

公开(公告)日：2013-03-26

申请号：US13028510

申请日：2011-02-16

Applicant: Sam D. Draper ,  Douglas S. Byrd ,  Carl G. Schott ,  Rahul J. Chillar ,  Amit S. Toprani

Inventor： Sam D. Draper ,  Douglas S. Byrd ,  Carl G. Schott ,  Rahul J. Chillar ,  Amit S. Toprani

IPC: F02G5/02 ,  F02M35/024 ,  F02M25/07 ,  F02M35/00 ,  B01D50/00 ,  B01D19/00

CPC classification number: F02C1/005 ,  F02C3/34 ,  F02C7/05 ,  F05D2270/08

Abstract: An embodiment of the present invention takes the form of a system that may recirculate a portion of the exhaust of at least one turbomachine where it may be mixed with the inlet air and re-enter the turbomachine without affecting reliability and availability of the unit. An embodiment of the present invention provides an inlet system for an exhaust gas recirculation system. This inlet system may take a variety of forms and may optimize the direction that the portion of the recirculated exhaust stream flows within the inlet system.

公开(公告)号：US08397483B2

公开(公告)日：2013-03-19

申请号：US13028490

申请日：2011-02-16

Applicant: Sam D. Draper ,  Douglas S. Byrd ,  Carl G. Schott ,  Rahul J. Chillar ,  Amit S. Toprani

Inventor： Sam D. Draper ,  Douglas S. Byrd ,  Carl G. Schott ,  Rahul J. Chillar ,  Amit S. Toprani

IPC: F02G5/02 ,  F02C7/052 ,  F02C7/055 ,  F02M35/024 ,  F02M25/07

CPC classification number: F02C1/005 ,  F02C3/34 ,  F02C7/05 ,  F05D2270/08

Abstract: An embodiment of the present invention takes the form of a system that may recirculate a portion of the exhaust of at least one turbomachine where it may be mixed with the inlet air and re-enter the turbomachine without affecting reliability and availability of the unit. An embodiment of the present invention provides an inlet system for an exhaust gas recirculation system. This inlet system may take a variety of forms and may optimize the direction that the portion of the recirculated exhaust stream flows within the inlet system.

Abstract translation: 本发明的一个实施例采用的系统的形式可以使至少一个涡轮机的排气的一部分再循环，在那里它可以与入口空气混合并重新进入涡轮机，而不会影响单元的可靠性和可用性。 本发明的实施例提供了一种用于废气再循环系统的入口系统。 该入口系统可以采取各种形式并且可优化再循环排气流的部分在入口系统内流动的方向。

公开(公告)号：US08349043B2

公开(公告)日：2013-01-08

申请号：US13025219

申请日：2011-02-11

Applicant: Etienne Rene Jarrier

Inventor： Etienne Rene Jarrier

IPC: B01D50/00

CPC classification number: F02C7/052 ,  F01D25/32 ,  F02C7/05

Abstract: The present application provides a turbine inlet air system. The turbine inlet air system may include a small droplet coalescer, a moisture eliminator positioned about the small droplet coalescer, and a filter downstream of the small droplet coalescer and the moisture eliminator.

Abstract translation: 本申请提供了一种涡轮机入口空气系统。 涡轮机入口空气系统可以包括小液滴聚结器，围绕小液滴聚结器定位的除湿器，以及小液滴聚结器和除湿器下游的过滤器。

公开(公告)号：US20120204568A1

公开(公告)日：2012-08-16

申请号：US13025219

申请日：2011-02-11

Applicant: Etienne Rene Jarrier

Inventor： Etienne Rene Jarrier

IPC: F02C7/04 ,  F01D25/32

CPC classification number: F02C7/052 ,  F01D25/32 ,  F02C7/05

Abstract: The present application provides a turbine inlet air system. The turbine inlet air system may include a small droplet coalescer, a moisture eliminator positioned about the small droplet coalescer, and a filter downstream of the small droplet coalescer and the moisture eliminator.

Abstract translation: 本申请提供了一种涡轮机入口空气系统。 涡轮机入口空气系统可以包括小液滴聚结器，围绕小液滴聚结器定位的除湿器，以及小液滴聚结器和除湿器下游的过滤器。

公开(公告)号：US08182587B2

公开(公告)日：2012-05-22

申请号：US12200087

申请日：2008-08-28

Applicant: Stephen David Hiner ,  Rahul Jaikaran Chillar ,  Bradly Aaron Kippel ,  Lisa Kamdar Ammann ,  Jack Thomas Clements ,  Marcus Carr Walters ,  Sebastien Cloarec ,  Marc Malivernay ,  Liberto Gandia

Inventor： Stephen David Hiner ,  Rahul Jaikaran Chillar ,  Bradly Aaron Kippel ,  Lisa Kamdar Ammann ,  Jack Thomas Clements ,  Marcus Carr Walters ,  Sebastien Cloarec ,  Marc Malivernay ,  Liberto Gandia

IPC: B01D46/00

CPC classification number: F01D25/32 ,  B01D45/08 ,  B01D46/0024 ,  B01D46/0031 ,  B01D46/0068 ,  B01D46/4236 ,  B01D46/4263 ,  B01D50/002 ,  B01D2277/20 ,  B01D2279/60 ,  F02C7/05 ,  F02C7/055 ,  F05D2260/96

Abstract: A system for use with an inlet of a gas turbine through which an airflow toward the gas turbine proceeds is provided and includes a first self-cleaning stage to remove dust, snow and ice from the airflow, a second water tight stage, disposed downstream from the first stage, to prevent aerosol droplets and aqueous solutions of deliquesced particulates, which include at least portions of the dust not removed by the first stage and which are re-released into the airflow from the first stage, from proceeding along the airflow and to remove solid particulates not removed by the first stage from the airflow, and a third water removal stage, disposed downstream from the second stage, to remove from the airflow aerosol droplets leaking from the second stage.

Abstract translation: 一种与燃气轮机的入口一起使用的系统，通过该进气口进入朝向燃气轮机的气流，并且包括第一自清洁台，用于从空气流中除去灰尘，雪和冰，第二防水台，设置在下游 第一阶段，以防止气溶胶微滴和潮解微粒的水溶液，其包括至少部分灰尘未被第一阶段除去并被再次释放到第一阶段的气流中，沿着气流进行到达 从气流中去除第一阶段未被除去的固体微粒，以及设置在第二阶段下游的第三除水阶段，以从第二阶段泄漏的气流中除去气溶胶微滴。