Dynamic system estimation device and method

Patent metadata

Field	Value
Publication number	US-9863268-B2
Application number	US-201615222084-A
Country	US
Kind code	B2
Filing date	Jul 28, 2016
Priority date	Apr 28, 2014
Publication date	Jan 9, 2018
Grant date	Jan 9, 2018

Abstract

A dynamic system estimation device and method, whereby estimation for more performance parameters than there are sensors can be performed, the estimation taking temporal changes into account. The dynamic system estimation device includes: a prescribed number of sensors that detect prescribed observation values from a gas turbine engine; and a Kalman filter that uses a dynamic model of the gas turbine engine and estimates the state of the gas turbine engine, on the basis of the observation values detected by the sensors. The gas turbine engine includes an element having changes in temporal performance recorded by performance parameters. The Kalman filter enables more than the prescribed number of performance parameters to be estimated, as a result of introducing a first-order lag element in place of the element.

First claim

What is claimed is:

1. A dynamic system estimation device that estimates a state and performance parameters of a dynamic system, comprising:
a predetermined number of sensors which detect predetermined observed values from the dynamic system; and
a Kalman filter that estimates the state of the dynamic system by using a dynamic model of the dynamic system based on the observed values detected by the sensors,
wherein the dynamic system includes elements in which temporal changes of performance are described by the performance parameters, and the Kalman filter also enables estimation of performance parameters, of which number is larger than the predetermined number, by introducing first-order lag elements in place of the elements.

2. The estimation device according to claim 1 , wherein each of the performance parameters is given as a ratio of an output value of the first-order lag element to an input value of the first-order lag element.

3. The estimation device according to claim 1 , wherein the dynamic system is a gas turbine engine, and the observed values detected by the sensors include a number of revolutions, a temperature and a pressure in the gas turbine engine.

4. The estimation device according to claim 2 , wherein the dynamic system is a gas turbine engine, and the observed values detected by the sensors include number of revolutions, temperature and pressure in the gas turbine engine.

5. A dynamic system estimation method for estimating a state and performance parameters of a dynamic system, comprising:
a step of detecting predetermined observed values from the dynamic system by a predetermined number of sensors; and
a step of estimating the state of the dynamic system by a Kalman filter based on the observed values detected by the sensors, the Kalman filter using a dynamic model of the dynamic system,
wherein the dynamic system includes elements in which temporal changes of performance are described by the performance parameters, and the Kalman filter also enables estimation of performance parameters, of which number is larger than the predetermined number, by introducing first-order lag elements in place of the elements.

Assignees

• Ihi Corp

Inventors

• Furukawa Hiroyuki
• Kakiuchi Daiki
• Kimura Mai

Classifications

• G05B13/04

  involving the use of models or simulators · CPC title

• F01D21/003 Primary

  Arrangements for testing or measuring (for measuring vibrations G01H) · CPC title

• F02C9/00

  Controlling gas-turbine plants; Controlling fuel supply in air- breathing jet-propulsion plants (controlling air intakes F02C7/057; controlling turbines F01D; controlling compressors F04D27/00; controlling in general G05) · CPC title

• F02C7/00

  Features, components parts, details or accessories, not provided for in, or of interest apart form groups F02C1/00 - F02C6/00; Air intakes for jet-propulsion plants (controlling F02C9/00) · CPC title

• G05B23/02

  Electric testing or monitoring · CPC title