公开(公告)号：US10287993B2

公开(公告)日：2019-05-14

申请号：US15666607

申请日：2017-08-02

Applicant: Siemens Aktiengesellschaft

Inventor： Gavin Brickwood ,  Ghenadie Bulat

IPC: F02C9/28 ,  F23N5/24 ,  F23R3/34

Abstract: A method of operating a control unit for controlling at least two different input fuel flows to a combustion device, e.g. a gas turbine includes the step of determining on the basis of at least one operating parameter whether the combustion device is in a predefined operating stage. In response hereto, generating a control signal configured for setting a ratio of at least two different input fuel flows to a predetermined value (psc1, psc3) for a predetermined time (dt) in case the combustion device is in the predefined operating stage.

公开(公告)号：US20170328284A1

公开(公告)日：2017-11-16

申请号：US15666607

申请日：2017-08-02

Applicant: Siemens Aktiengesellschaft

Inventor： Gavin Brickwood ,  Ghenadie Bulat

IPC: F02C9/28 ,  F23R3/34 ,  F23N5/24

CPC classification number: F02C9/28 ,  F23N5/242 ,  F23N2041/20 ,  F23R3/34 ,  F23R3/343 ,  F23R2900/00013 ,  F23R2900/03281

Abstract: A method of operating a control unit for controlling at least two different input fuel flows to a combustion device, e.g. a gas turbine includes the step of determining on the basis of at least one operating parameter whether the combustion device is in a predefined operating stage. In response hereto, generating a control signal configured for setting a ratio of at least two different input fuel flows to a predetermined value (psc1, psc3) for a predetermined time (dt) in case the combustion device is in the predefined operating stage.

公开(公告)号：US20160298851A1

公开(公告)日：2016-10-13

申请号：US15034916

申请日：2014-10-27

Applicant: SIEMENS AKTIENGESELLSCHAFT

Inventor： Gavin Brickwood ,  Ghenadie Bulat

IPC: F23R3/34 ,  F02C9/34

CPC classification number: F23R3/343 ,  F02C9/34 ,  F05D2270/303 ,  F05D2270/306 ,  F05D2270/3061 ,  F05D2270/31 ,  F05D2270/44 ,  F23N2005/181 ,  F23N2021/10 ,  F23N2025/04 ,  F23N2025/08 ,  F23R2900/00013

Abstract: A combustor system for a gas turbine engine includes a combustion chamber into which a pilot fuel and a main fuel is injectable and flammable, wherein an exhaust gas generated by the burned pilot fuel and the burned main fuel is exhaustible out of the combustion chamber. A control unit is coupled to a fuel control unit for adjusting the pilot fuel ratio. The control unit is adapted for determining a predicted pollutant concentration of the exhaust gas on the basis of a temperature signal, a fuel signal, a mass flow signal and a fuel split ratio.

Abstract translation: 燃气涡轮发动机的燃烧器系统包括燃烧室，其中引燃燃料和主燃料是可注射和易燃的，其中由燃烧的先导燃料和燃烧的主燃料产生的废气可从燃烧室中排出。 控制单元联接到燃料控制单元以调节先导燃料比。 控制单元适于基于温度信号，燃料信号，质量流量信号和燃料分流比来确定排气的预测污染物浓度。