Invention Grant
US08668434B2 Robust flow parameter model for component-level dynamic turbine system control
有权
用于组件级动态涡轮机系统控制的鲁棒流量参数模型
- Patent Title: Robust flow parameter model for component-level dynamic turbine system control
- Patent Title (中): 用于组件级动态涡轮机系统控制的鲁棒流量参数模型
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Application No.: US12552711Application Date: 2009-09-02
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Publication No.: US08668434B2Publication Date: 2014-03-11
- Inventor: Boris Karpman , Thomas J. Roadinger , Richard P. Meisner
- Applicant: Boris Karpman , Richard P. Meisner , Sheryl H. Roadinger
- Applicant Address: US CT Hartford
- Assignee: United Technologies Corporation
- Current Assignee: United Technologies Corporation
- Current Assignee Address: US CT Hartford
- Agency: Kinney & Lange, P.A.
- Main IPC: F01B25/00
- IPC: F01B25/00

Abstract:
A system comprises an apparatus, an actuator and a processor. The apparatus defines a flow path through an aperture, the aperture defines a pressure drop along the flow path, and the actuator regulates fluid flow across the pressure drop. The processor comprises a flow module, a comparator, an estimator and a control law. The flow module maps a flow curve relating a flow parameter to a pressure ratio, and defines a solution point located on the flow curve and a focus point located off the flow curve. The comparator generates an error as a function of a slope defined between the focus and solution points. The estimator moves the solution point along the flow curve, such that the error is minimized. The control law directs the actuator to position the control element, such that the flow parameter describes the fluid flow and the pressure ratio describes the pressure drop.
Public/Granted literature
- US20110052370A1 ROBUST FLOW PARAMETER MODEL FOR COMPONENT-LEVEL DYNAMIC TURBINE SYSTEM CONTROL Public/Granted day:2011-03-03
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