公开(公告)号：US20180080376A1

公开(公告)日：2018-03-22

申请号：US15272050

申请日：2016-09-21

Applicant: General Electric Company

Inventor： Kenneth Robert Austin ,  Vineet Sethi ,  Raymond Kalok Fong ,  Jose Emmanuel Guillen ,  Robert Allen Baten ,  Donald Gordon Laing

IPC: F02C6/00 ,  H02K7/18 ,  F02C3/04

CPC classification number: F02C6/00 ,  F02B63/044 ,  F02C3/04 ,  F05D2220/76 ,  F16M3/00 ,  H02K7/1823

Abstract: A system includes a first mobile body configured to support a turbine engine and an air intake section coupled to the turbine engine. The system also includes a second mobile body configured to support a generator. The first and second mobile bodies are configured to guide a removable coupling between the turbine engine and the generator. The system also includes a third mobile body configured to support one or more partially assembled components associated with the turbine engine and the generator.

公开(公告)号：US09447982B2

公开(公告)日：2016-09-20

申请号：US14735963

申请日：2015-06-10

Applicant: General Electric Company

Inventor： Robert Allen Baten ,  David Joseph Drobniak ,  Harley Matthew Ross

IPC: F24F7/06 ,  F24F7/007 ,  F24F7/08 ,  F02C3/32 ,  F02C7/12

CPC classification number: F24F7/08 ,  F01D25/12 ,  F02C3/32 ,  F02C7/12 ,  F05D2260/601 ,  Y02E20/16

Abstract: A turbine ventilation system includes at least one fan configured to provide a first air flow into a gas turbine enclosure, a fan bypass configured to circumvent the at least one fan to provide a second air flow into the gas turbine enclosure, and an eductor configured to draw the first or second air flows through and out of the gas turbine enclosure.

公开(公告)号：US10106378B2

公开(公告)日：2018-10-23

申请号：US14931834

申请日：2015-11-03

Applicant: General Electric Company

Inventor： Artemio Josue Aguilar ,  Robert Allen Baten ,  Mario Oscar Ramirez

IPC: B66C17/00 ,  B66C17/06 ,  B66C17/04

Abstract: A system includes a load moving machine, including a frame and a movable assembly coupled to the frame. The movable assembly includes a lift portion, a rotational portion, a first translational portion, and a second translational portion.

公开(公告)号：US09950758B2

公开(公告)日：2018-04-24

申请号：US14489323

申请日：2014-09-17

Applicant: General Electric Company

Inventor： Raymond Ka Lok Fong ,  Robert Allen Baten

IPC: B60D1/36 ,  B62D63/08 ,  B62D53/04 ,  G01S17/08 ,  G01S17/93 ,  B60D1/62 ,  B60D1/64 ,  F01D15/10 ,  F02C7/36 ,  F01D21/00 ,  F01D25/28

CPC classification number: B62D63/08 ,  B60D1/36 ,  B60D1/62 ,  B60D1/64 ,  B62D53/04 ,  F01D15/10 ,  F01D21/003 ,  F01D25/285 ,  F02C7/36 ,  F05D2240/90 ,  F05D2260/403 ,  G01S17/08 ,  G01S17/936

Abstract: A system includes a docking guide comprising a first alignment guide configured to couple with a first mobile unit that supports a turbine engine and a second alignment guide configured to couple with a second mobile unit that supports a generator. The first and second alignment guides are configured to guide a coupling between the first and second mobile units to help align the turbine engine with the generator.

公开(公告)号：US20160075387A1

公开(公告)日：2016-03-17

申请号：US14489323

申请日：2014-09-17

Applicant: General Electric Company

Inventor： Raymond Ka Lok Fong ,  Robert Allen Baten

IPC: B62D63/08 ,  G01S17/08 ,  G01S17/93 ,  B62D53/04

CPC classification number: B62D63/08 ,  B60D1/36 ,  B60D1/62 ,  B60D1/64 ,  B62D53/04 ,  F01D15/10 ,  F01D21/003 ,  F01D25/285 ,  F02C7/36 ,  F05D2240/90 ,  F05D2260/403 ,  G01S17/08 ,  G01S17/936

Abstract: A system includes a docking guide comprising a first alignment guide configured to couple with a first mobile unit that supports a turbine engine and a second alignment guide configured to couple with a second mobile unit that supports a generator. The first and second alignment guides are configured to guide a coupling between the first and second mobile units to help align the turbine engine with the generator.

Abstract translation: 一种系统包括对接引导件，其包括配置成与支撑涡轮发动机的第一移动单元联接的第一对准引导件和配置成与支撑发电机的第二移动单元联接的第二对准引导件。 第一和第二对准引导件构造成引导第一和第二移动单元之间的联接，以帮助将涡轮发动机与发电机对准。

公开(公告)号：US20150082768A1

公开(公告)日：2015-03-26

申请号：US14453919

申请日：2014-08-07

Applicant: General Electric Company

Inventor： Fernando LOPEZ-PARRA ,  Pawel Jan Jablecki ,  Robert Allen Baten ,  Balakrishnan Ponnuraj ,  Pawel Barej

IPC: F02C7/18

CPC classification number: F02C7/18 ,  F01D25/14 ,  F05D2220/32 ,  F05D2260/2212 ,  F05D2260/232

Abstract: A diffuser assembly for a ventilation system is disclosed herein. The diffuser assembly may include a boundary defining an interior of the diffuser assembly. The diffuser assembly also may include at least one inlet to the interior of the diffuser assembly. The at least one inlet to the interior of the diffuser assembly may be in fluid communication with at least one ventilation fan. Moreover, the diffuser assembly may include an outlet from the interior of the diffuser assembly. The outlet from the interior of the diffuser assembly may be in fluid communication with an engine enclosure. In this manner, the outlet from the interior of the diffuser assembly may be configured to provide a flow of ventilation air from the at least one ventilation fan as a substantially uniform flow of ventilation air within the engine enclosure.

Abstract translation: 本文公开了一种用于通风系统的扩散器组件。 扩散器组件可以包括限定扩散器组件的内部的边界。 扩散器组件还可以包括至少一个到扩散器组件内部的入口。 扩散器组件内部的至少一个入口可以与至少一个通风扇流体连通。 此外，扩散器组件可以包括从扩散器组件的内部的出口。 来自扩散器组件的内部的出口可以与发动机外壳流体连通。 以这种方式，来自扩散器组件的内部的出口可以被配置为提供来自至少一个通风扇的通风空气流，作为发动机外壳内基本上均匀的通风空气流。

公开(公告)号：US20140219781A1

公开(公告)日：2014-08-07

申请号：US13761305

申请日：2013-02-07

Applicant: GENERAL ELECTRIC COMPANY

Inventor： Eric Tracy Watson ,  Robert Allen Baten ,  Doyle Jackson Marrs

IPC: F02M35/12

CPC classification number: F02M35/12 ,  F04D29/664 ,  F04D29/665 ,  F04D29/668

Abstract: An air inlet silencer for turbomachines is provided. In one embodiment, the air inlet silencer includes a body, and a plurality of concentric baffles coupled to and axially surrounding the body. In another embodiment, an air inlet system for a turbomachine includes the air inlet silencer, as discussed herein, positioned within a silencer housing. The air inlet system may also include a deflector positioned within the silencer housing adjacent the air inlet silencer. In a further embodiment, a turbomachine includes a turbine coupled to a compressor, and an air inlet system, as described herein, coupled to the compressor.

Abstract translation: 提供了用于涡轮机的进气消音器。 在一个实施例中，空气入口消音器包括主体和耦合到并且轴向包围主体的多个同心挡板。 在另一个实施例中，用于涡轮机的进气系统包括位于消声器壳体内的如本文所讨论的进气消音器。 空气入口系统还可以包括定位在邻近空气入口消声器的消音器壳体内的偏转器。 在进一步的实施例中，涡轮机包括联接到压缩机的涡轮机和联接到压缩机的如本文所述的空气入口系统。