[특허]Method and system for balancing bleed flows from gas turbine engines

Honeywell International Inc.

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특허 상세정보

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Method and system for balancing bleed flows from gas turbine engines

특허상세정보
국가/구분	United States(US) Patent 등록
국제특허분류(IPC7판)	F02C-009/00
미국특허분류(USC)	060/795; 060/782
출원번호	UP-0054421 (2005-02-09)
등록번호	US-7536865 (2009-07-01)
발명자 / 주소	Mikhail, Sami H.
출원인 / 주소	Honeywell International Inc.
대리인 / 주소	Oral Caglar, Esq.
인용정보	피인용 횟수 : 9 인용 특허 : 12

초록
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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.

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I claim: 1. A method of balancing bleed air flows in a plurality of bleed air flow paths associated with a plurality of gas turbine engines comprising: providing a pressure regulating valve in each of the plurality of bleed air flow paths; measuring a flow rate in each of the bleed air flow paths; determining a common flow setpoint for each bleed air flow path of the plurality based on the measured flow rate in each of the bleed air flow paths; measuring a pressure in each of the bleed air flow paths; providing a reference pressure; and controlling a position of the pressure regulating valve in each bleed air flow path based on a flow difference between the measured flow rate in said each bleed air flow path and said common flow setpoint and a pressure difference between the measured pressure in said each bleed air flow path and the reference pressure. 2. The method of claim 1 wherein determining said common flow setpoint comprises the step of determining an average of a predicted flow rate in each of the plurality of bleed air flow paths. 3. The method of claim 1 wherein determining said common flow setpoint comprises measuring a temperature in each of the bleed air flow paths and determining said common flow setpoint for each of the bleed air flow paths based on the measured temperature in said each of the bleed air flow paths. 4. The method of claim 1 wherein controlling a position of the pressure regulating valve comprises for each of the plurality of flow paths: providing a controller for the pressure regulating valve; providing the flow difference for the each bleed air flow path as a first input to the controller; providing the pressure difference for the each bleed air flow path as a second input to the controller; and providing a control signal output from the controller to the pressure regulating valve based on the first and second inputs. 5. The method of claim 4 wherein providing a control signal output comprises adding the pressure difference and the flow difference to a control bias. 6. The method of claim 1 wherein controlling a position of the pressure regulating valve comprises: determining a flow difference gain; determining a pressure difference gain; multiplying the pressure difference by the pressure difference gain; and multiplying the flow difference by the flow difference gain. 7. The method of claim 6 including varying the flow difference gain and the pressure difference gain based on measured operating conditions of the plurality of engines. 8. The method of claim 6 wherein the flow difference gain comprises a proportional gain and an integral gain and the pressure difference gain comprises a proportional gain and an integral gain, and including varying the proportional gains and integral gains based on measured operating conditions of the engines. 9. The method of claim 6 including setting the flow difference gain to a first flow difference gain value and the pressure difference gain to a first pressure difference gain value and further including reducing the first flow difference gain value when the pressure difference falls below a predetermined value. 10. The method of claim 8 including reducing the integral gain of the flow difference gain to 0 when the pressure difference falls below a predetermined value. 11. The method of claim 8 including reducing the proportional and integral gains of the flow difference gain and reducing the integral gain of the pressure difference gain to 0 when the pressure difference falls below a predetermined value. 12. The method of claim 1 wherein controlling a position of the pressure regulating valve in each channel further comprises independently controlling a position of the pressure regulating valve in each channel. 13. A bleed air balancing system comprising: a plurality of bleed air flow paths each carrying bleed air from one of a plurality of gas turbine engines and including a flow rate sensor; a circuit outputting at least one common flow rate setpoint based on flow rates measured by each of the flow rate sensors; wherein each of the plurality of bleed air flow paths includes: a pressure regulating valve; a pressure sensor; and a controller for controlling the position of the pressure regulating valve, said controller including an output connected to said pressure regulating valve, a pressure control loop generating a pressure correction signal, and a flow control loop generating a flow correction signal; wherein said controller outputs a control signal on said output based on said pressure correction signal and said flow correction signal. 14. The system of claim 13 wherein said at least one common flow rate setpoint comprises an average of a predicted flow rate in each of the plurality of bleed air flow paths. 15. The system of claim 13 wherein said pressure control loop has a variable pressure gain and said flow control loop has a variable flow gain. 16. The system of claim 15 wherein said variable pressure gain comprises a variable integral gain and a variable proportional gain and said variable flow gain has a variable integral gain and a variable proportional gain. 17. The system of claim 15 wherein said variable pressure gain has a first value under a first set of operating conditions and a second value under a second set of operating conditions. 18. The system of claim 16 wherein said variable pressure integral gain takes on a first value and said variable pressure proportional gain takes on a second value under a first set of operating conditions and wherein said variable pressure integral gain takes on a third value and said variable pressure proportional gain takes on a fourth value under a second set of operating conditions. 19. The system of claim 13 including: a temperature sensor in each of said plurality of bleed air flow paths; and a circuit connected to each of said temperature sensors for adjusting said at least one common flow rate setpoint based on measured temperatures in said bleed air flow paths. 20. A method of balancing bleed air flows in a plurality of bleed air flow paths associated with a plurality of gas turbine engines comprising the steps of: providing a pressure regulating valve in each of the plurality of bleed air flow paths; measuring a flow rate in each of the bleed air flow paths; measuring a temperature in each of the bleed air flow paths; determining a common flow setpoint for each of the bleed air flow paths of the plurality based on the measured temperature and measured flow rate in each of the bleed air flow paths; providing a reference pressure; for each of the bleed air flow paths: measuring a pressure in said each bleed air flow path; determining a pressure difference between the reference pressure and the measured pressure in the flow path; determining a flow difference between said common flow set point for said bleed air flow path and the measured flow rate; weighting the pressure difference by a first amount; weighting the flow difference by a second amount; and controlling a position of the pressure regulating valve based on said weighted pressure difference and said weighted flow difference.

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이 특허를 인용한 특허 피인용횟수: 9

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Method and system for balancing bleed flows from gas turbine engines

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Method and system for balancing bleed flows from gas turbine engines

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