公开(公告)号：WO2022119691A1

公开(公告)日：2022-06-09

申请号：PCT/US2021/058875

申请日：2021-11-11

Applicant: SOLAR TURBINES INCORPORATED

Inventor： SOLDI, Andrea ,  PYKA, Vincent E.

IPC: G06F9/4401 ,  G06F21/57

Abstract: A human-machine interface (HMI) (21), HMI system (2), turbomachinery package (1), and method of modifying a partition of an HMI (21) are disclosed. The HMI (21) comprises a first partition (211) storing a first operating system exclusively supporting a primary application; and a second partition (212) storing a second operating system exclusively supporting an imaging application. The HMI system (2) comprises the HMI (21); an external computing device (22); a serial cable (23); and, optionally, a network cable (24). The turbomachinery package (1) comprises a housing (11); a gas turbine (12); a plurality of sensors (14); a plurality of actuators (15); and an HMI (21). The imaging application may be an image deploy function, an image back-up function, and/or an image restore function, any of which can be executed without the use of removable media.

公开(公告)号：WO2021071645A1

公开(公告)日：2021-04-15

申请号：PCT/US2020/051199

申请日：2020-09-17

Applicant: SOLAR TURBINES INCORPORATED

Inventor： ROGERS, Richard A. ,  DOMINIQUE, Drew A. ,  EVANS, JR., Timothy R. ,  DUCKERS, Jonathan G. ,  BURKE, Stephen ,  ARCHER, Robert ,  HUMER, Stefan H. ,  LEE, Hanjie

IPC: F23R3/34 ,  F23R3/28 ,  F23R3/14

Abstract: A fuel injector (600) for a combustor of a gas turbine engine (100) is disclosed herein. The fuel injector (600) includes a fuel stem assembly (620) for receiving and distributing fuel and an injector head (630) receiving fuel from the fuel stem assembly (620). The injector head (630) includes an injector body (640), swirler vanes (660), a pilot assembly (700), passages (666, 667, 726, 745, 746), and fuel galleries (646, 647, 736). The pilot assembly (700) includes a pilot tube (746) and can include pilot struts (720). The swirler vanes (660) include passages (666) to transport the pilot fuel from the fuel stem assembly (620) to the pilot tube (746).

公开(公告)号：WO2020205141A1

公开(公告)日：2020-10-08

申请号：PCT/US2020/020971

申请日：2020-03-04

Applicant: SOLAR TURBINES INCORPORATED

Inventor： JOHNSTON, Ronald K.

IPC: B21C37/30 ,  B21D19/00 ,  B21D19/04 ,  B23B5/16 ,  B23B51/10 ,  B24B9/00

Abstract: A tube shaping tool (100) for a torque mechanism (50) to modify a tube end. The tube shaping tool includes an internal assembly (300). The internal tube assembly includes a stem (315) and an internal body (310). The stem can be received by the torque mechanism and transmit torque generated from the torque mechanism to the components of the tube shaping tool. The tube shaping tool roll-forms the outside diameter of the tube end using standard bearings (320) and a flange bearing (330) attached to the internal body. The flange bearing also includes a flange (325) that can provide facing of the tube end. The tube shaping tool can further comprise a cup (200).

公开(公告)号：WO2018136291A1

公开(公告)日：2018-07-26

申请号：PCT/US2018/013258

申请日：2018-01-11

Applicant: SOLAR TURBINES INCORPORATED

Inventor： SOLDI, Andrea

IPC: F02C9/16 ,  F02C7/052 ,  F02C6/12 ,  F01D21/00

Abstract: A method of monitoring a turbomachinery is disclosed herein. The method includes measuring the pressure drop across the intake filter (66). The method further includes determining clog rate parameters for a clog rate of a filter area of the intake filter (66) based on the measured pressure drop across the intake filter (66). The method yet further includes predicting the pressure drop across the intake filter (66) for the intake filter life cycle based on the determined clog rate parameters and providing a recommended time to service the intake filter (66) to an operator of the turbomachinery system (50) based on the predicted intake filter life cycle.

公开(公告)号：WO2018017211A1

公开(公告)日：2018-01-25

申请号：PCT/US2017/037618

申请日：2017-06-15

Applicant: SOLAR TURBINES INCORPORATED

Inventor： ADJAN, Bachar

IPC: F02C7/20 ,  F01D25/28

Abstract: A method and device for retrofitting a gas turbine engine for improved hot day performance are disclosed. The method can include removing a first selected stator bladerow from the plurality of compressor stages, the first selected stator bladerow having a first inlet swirl angle and including a first plurality of fixed stator vanes. Each stator vane of the first plurality of fixed stator vanes can have a first stator vane angle. The method can also include providing a first improved stator bladerow to replace the first selected stator bladerow. The first improved stator bladerow can have a second plurality of fixed stator vanes, each having a second stator vane angle smaller than the first stator vane angle. The method can also include replacing the first selected stator bladerow with the first improved stator bladerow to produce an increased pressure ratio and flow rate compared to the first selected stator bladerow.

Abstract translation: 公开了用于改进燃气涡轮发动机以改善热日性能的方法和装置。 所述方法可以包括从所述多个压缩机级中移除第一选定定子毛坯，所述第一选定定子毛坯具有第一入口旋流角且包括第一多个固定定子叶片。 第一组多个固定定子叶片中的每个定子叶片可以具有第一定子叶片角度。 该方法还可以包括提供第一改进的定子毛坯以替换第一选择的定子毛坯。 第一种改进的定子叶片可以具有多个第二固定定子叶片，每个固定定子叶片具有小于第一定子叶片角度的第二定子叶片角度。 该方法还可以包括用第一改进的定子波纹管代替第一选择的定子波纹管，以产生与第一选择的定子波纹管相比增加的压力比和流率。

公开(公告)号：WO2016167910A1

公开(公告)日：2016-10-20

申请号：PCT/US2016/022343

申请日：2016-03-14

Applicant: SOLAR TURBINES INCORPORATED

Inventor： WARREN, Martin Lewis ,  MOORE, Steven Wayne ,  JAFFURS, Jeffrey James ,  VAN DER STOK, Marcel

IPC: F04B41/00 ,  F04B39/00 ,  F04C29/00

CPC classification number: E04H5/00 ,  E04B2001/34876 ,  E04H2001/1283

Abstract: A method of deploying a modular gas compression plant (1000) is disclosed. In an embodiment, the method comprises constructing a building (100) of four substructures including a first lower housing (106), a first upper housing (107), a second lower housing (201), and a second upper housing (202). The method further includes assembling a turbomachinery equipment (108) into the first lower housing (106). The method further includes assembling an air inlet duct (104) and an exhaust duct (105) to the first upper housing (107). The method further includes disassembling the building (100) into the four substructures.

Abstract translation: 公开了一种部署模块化气体压缩设备（1000）的方法。 在一个实施例中，该方法包括构造四个子结构的建筑物（100），其包括第一下部壳体（106），第一上部壳体（107），第二下部壳体（201）和第二上部壳体（202）。 该方法还包括将涡轮机械设备（108）组装到第一下部壳体（106）中。 该方法还包括将进气管道（104）和排气管道（105）组装到第一上部壳体（107）。 该方法还包括将建筑物（100）拆卸成四个子结构。

公开(公告)号：WO2016044450A1

公开(公告)日：2016-03-24

申请号：PCT/US2015/050471

申请日：2015-09-16

Applicant: SOLAR TURBINES INCORPORATED

Inventor： STAFFORD, Scott L.

IPC: F01D5/08 ,  F02C7/18 ,  F01D9/04

CPC classification number: F01D9/041 ,  F01D25/12 ,  F01D25/243 ,  F05D2260/20

Abstract: A preswirler (470) for a gas turbine engine (100) diaphragm assembly (460) is disclosed herein. In embodiments, the preswirler (470) includes an outer ring (471) and an inner ring (474). The outer ring (471) includes an outer ring face (481), a first contact protrusion (484), and a second contact protrusion (485). The first and second contact protrusion (485)s are spaced apart and extend from an outer body portion (472) at the outer ring face (481). The inner ring (474) is located inward from the outer ring (471). The inner ring (474) includes an inner ring face (497) and a third contact protrusion (494). The third contact protrusion (494) extends in from an inner body portion (475) and at the inner ring face (497).

Abstract translation: 本文公开了一种用于燃气涡轮发动机（100）隔膜组件（460）的预旋流器（470）。 在实施例中，预旋流器（470）包括外环（471）和内环（474）。 外环（471）包括外环面（481），第一接触突起（484）和第二接触突起（485）。 第一和第二接触突起（485）被间隔开并且在外环面（481）处从外主体部分（472）延伸。 内环（474）位于外环（471）的内侧。 内环（474）包括内环面（497）和第三接触突起（494）。 第三接触突起（494）从内主体部分（475）和内环面（497）延伸。

公开(公告)号：WO2015175125A1

公开(公告)日：2015-11-19

申请号：PCT/US2015/025634

申请日：2015-04-14

Applicant: SOLAR TURBINES INCORPORATED

Inventor： ABRAHAM, Benjamin Richard ,  BRILL, Jeffrey C. ,  WELLER, Daniel Patrick

IPC: F02C7/00 ,  F01D25/00 ,  G01N23/02

CPC classification number: B23K31/125 ,  B23K11/02 ,  B23K15/0006 ,  B23K2201/001 ,  B23P15/008 ,  B23P2700/13 ,  F01D1/20 ,  F01D5/06 ,  F01D5/063 ,  F05D2260/80 ,  G01N23/02 ,  Y10T29/4932 ,  Y10T29/49323

Abstract: A weldment member for a gas turbine engine including a forward welding member and an aft welding member. The forward welding member has an annular shape with a forward welding face formed at one end. The forward welding face has a forward radiographic marking hole formed therein. The aft welding member has an annular shape with an aft welding face formed at one end. The aft welding face has an aft radiographic marking hole formed therein. The forward welding face is aligned with the aft welding face and the forward radiographic marking hole is angularly offset from the aft radiographic marking hole.

Abstract translation: 一种用于包括正向焊接构件和后部焊接构件的燃气涡轮发动机的焊件。 正向焊接部件具有在一端形成有正向焊接面的环状。 正向焊接面具有形成在其内的正面射线照相打标孔。 后焊接部件具有一端形成有后焊接面的环状。 后焊接面具有形成在其中的后射线照射标记孔。 正面焊接面与尾部焊接面对准，前方的射线照相标记孔与后方的射线照相标记孔成角度地偏移。

公开(公告)号：WO2015163999A1

公开(公告)日：2015-10-29

申请号：PCT/US2015/021251

申请日：2015-03-18

Applicant: SOLAR TURBINES INCORPORATED

Inventor： FREEMAN, Jess Lee ,  BRAILEAN, Gordon E. ,  FREEMAN, Benjamin Dee

IPC: F04D29/42 ,  F04D17/12

CPC classification number: F04D29/4206 ,  F04D17/125 ,  F04D29/624

Abstract: A universal housing (200) for a centrifugal gas compressor (100) is disclosed. The universal housing (200) includes a body (210), a suction port extending from the body (210), a discharge port extending from the body (210), and a first compartment (221) within the body (210). The first compartment (221) includes a suction inlet (211) in flow communication with the suction port and a discharge outlet (215) in flow communication with the discharge port. The first compartment (221) is configured to receive more than one staging length (129) for the staging. The staging inlet (146) is in flow communication with the suction inlet (211) and the staging outlet (147) is in flow communication with the discharge outlet (215).

Abstract translation: 公开了一种用于离心式气体压缩机（100）的通用壳体（200）。 通用壳体（200）包括主体（210），从主体（210）延伸的吸入口，从主体（210）延伸的排出口以及主体（210）内的第一隔室（221）。 第一隔室（221）包括与吸入口流体连通的吸入口（211）和与排出口流体连通的排出口（215）。 第一隔室（221）被配置为接收用于分段的多于一个的分段长度（129）。 分段入口（146）与抽吸入口（211）流动连通，分段出口（147）与排出口（215）流动连通。

公开(公告)号：WO2015153081A1

公开(公告)日：2015-10-08

申请号：PCT/US2015/019652

申请日：2015-03-10

Applicant: SOLAR TURBINES INCORPORATED

Inventor： JAHNZ, David B. ,  FONG, Jason Wing-Bin ,  ZHU, Lei

IPC: H02K9/08

CPC classification number: H02K1/20 ,  H02K3/00 ,  H02K3/44

Abstract: An electric motor (205) for a rotary machine (305) is disclosed. The electric motor (205) includes a first lamination section (221) and a second lamination section (222) radially spaced apart from a driver shaft (230) forming a first air gap (224) and a second air gap (225) respectively. The second lamination section (222) is axially spaced apart from the first lamination section (221) forming an air gap cooling outlet (226) there between. The electric motor (205) also includes motor windings (223) extending through the first lamination section (221) and the second lamination section (222), and across the air gap cooling outlet (226) in circumferential groups. A winding shield (260) is located around each of the circumferential groups of the motor windings (223).

Abstract translation: 公开了一种用于旋转机器（305）的电动机（205）。 电动机（205）包括分别与形成第一空气间隙（224）和第二气隙（225）的驱动轴（230）径向间隔开的第一层压部分（221）和第二层压部分（222）。 第二层压部分（222）与第一层压部分（221）轴向间隔开，在其间形成气隙冷却出口（226）。 电动机（205）还包括延伸穿过第一层压部分（221）和第二层压部分（222）的电动机绕组（223），并且在圆周组中穿过气隙冷却出口（226）。 绕组屏蔽（260）位于电动机绕组（223）的每个圆周组周围。