发明名称 Compressor start bleed system for a turbine system and method of controlling a compressor start bleed system
摘要 A compressor start bleed system for a turbine system includes a compressor section. Also included is a turbine section disposed downstream of the compressor section. Further included is at least one duct fluidly coupled to the compressor section, wherein the at least one duct is configured to route a start bleed extraction from the compressor section to a location downstream of the turbine section. Yet further included is at least one control device of the at least one duct configured to actively modulate the start bleed extraction during a part speed operation of the turbine system.
申请公布号 US9611752(B2) 申请公布日期 2017.04.04
申请号 US201313836225 申请日期 2013.03.15
申请人 General Electric Company 发明人 Tillery Steven William;Snider David August
分类号 F02C6/08;F01D19/00;F02C7/26 主分类号 F02C6/08
代理机构 代理人 Darling John P.
主权项 1. A method of controlling a compressor start bleed extraction during start-up operation of a turbine system having a compressor section, a turbine section and a combustor section, comprising: monitoring at least one operating parameter of the turbine system; comparing the at least one operating parameter to a control schedule; routing a start bleed extraction through at least one duct from the compressor section to a location downstream of the turbine section; and: modulating the start bleed extraction through the at least one duct with at least one control device at least partially in response to the control schedule, wherein comparing the at least one operating parameter comprises comparing a compressor speed to a compressor operating limit line.
地址 Niskayuna NY US