发明名称 Method and system for balancing bleed flows from gas turbine engines
摘要 A bleed air balancing system includes a plurality of bleed air flow paths ( 12 ) each carrying bleed air from one of a plurality of gas turbine engines ( 10 ), each bleed air flow path ( 12 ) including a flow rate sensor ( 19 ), and a circuit ( 52, 200 ) outputting at least one flow rate setpoint based on flow rates measured by each of the flow rate sensors ( 19 ), wherein each of the plurality of bleed air flow paths ( 12 ) includes: a pressure regulating valve ( 16 ), a pressure sensor ( 18 ), and a controller ( 20 ) for controlling the position of the pressure regulating valve ( 16 ), the controller ( 20 ) including an output ( 26 ) connected to the pressure regulating valve ( 16 ), a pressure control loop ( 60 ) generating a pressure correction signal, and a flow control loop ( 62 ) generating a flow correction signal, wherein the controller ( 20 ) outputs a control signal ( 28 ) on the output ( 26 ) based on the pressure correction signal and the flow correction signal. A method of operating the system is also disclosed.
申请公布号 US2006174628(A1) 申请公布日期 2006.08.10
申请号 US20050054421 申请日期 2005.02.09
申请人 HONEYWELL INTERNATIONAL INC. 发明人 MIKHAIL SAMI H.
分类号 F02C6/08 主分类号 F02C6/08
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