Least-squares health parameter identification techniques, such as the Kalman filter, have been extensively used to solve diagnosis problems. Indeed, such methods give a good estimate provided that the discrepancies between the model prediction and the measurements are zero-mean, white, Gaussian random variables. In a turbine engine diagnosis, however, this assumption does not always hold due to the presence of biases in the model. This is especially true for a transient operation. As a result, the estimated parameters tend to diverge from their actual values, which strongly degrades the diagnosis. The purpose of this contribution is to present a Kalman filter diagnosis tool where the model biases are treated as an additional random measurement error. The new methodology is tested on simulated transient data representative of a current turbofan engine configuration. While relatively simple to implement, the newly developed diagnosis tool exhibits a much better accuracy than the original Kalman filter in the presence of model biases.

1.
Volponi
,
A. J.
, 2003,
Foundation of Gas Path Analysis (Part I and II)
,
Gas Turbine Condition Monitoring and Fault Diagnosis
, Lecture Series No. 2003-01, von Karman Institute for Fluid Dynamics, Brussels, Belgium.
2.
Kalman
,
R. E.
, and
Bucy
,
R. S.
, 1961, “
New Results in Linear Filtering and Prediction Theory
,”
ASME J. Basic Eng.
0021-9223,
83
, pp.
95
107
.
3.
Dewallef
,
P.
, 2005, “
Application of the Kalman Filter to Health Monitoring of Gas Turbine Engines: A Sequential Approach to Robust Diagnosis
,” Ph.D. thesis, University of Liège.
4.
Urban
,
L. A.
, 1972, “
Gas Path Analysis Applied to Turbine Engine Condition Monitoring
,” Eighth Joint Propulsion Specialist Conference, Paper No. 72-1082.
5.
Duponchel
,
J.-P.
,
Loisy
,
J.
, and
Carillo
,
R.
, 1992, “
Steady and Transient Performance Calculation Method for Prediction, Analysis and Identification
,” Paper No. AGARD LS-183.
6.
Grönstedt
,
T.
, 2005, “
Least Squares Based Transient Nonlinear Gas Path Analysis
,” ASME Paper No. GT2005-68717.
7.
Ogaji
,
S.
,
Li
,
Y.
,
Sampath
,
S.
, and
Singh
,
R.
, 2003, “
Gas Path Fault Diagnosis of a Turbofan Engine from Transient Data Using Artificial Neural Networks
,” ASME Paper No. GT2003-38423.
8.
Simon
,
D.
, and
Simon
,
D. L.
, 2003, “
Aircraft Turbofan Engine Health Estimation Using Constrained Kalman Filtering
,” ASME Paper No. GT2003-38584.
9.
Dewallef
,
P.
, and
Léonard
,
O.
, 2003, “
On-Line Performance Monitoring and Engine Diagnostic Using Robust Kalman Filtering Techniques
,” ASME Paper No. GT2003-38379.
10.
Borguet
,
S.
,
Dewallef
,
P.
, and
Léonard
,
O.
, 2005, “
On-Line Transient Engine Diagnostics in a Kalman Filtering Framework
,” ASME Paper No. GT2005-68013.
11.
Volponi
,
A. J.
, 2005, “
Use of Hybrid Engine Modeling for On-Board Module Performance Tracking
,” ASME Paper No. GT2005-68169.
12.
RTO, 2002, “
Performance Prediction and Simulation of Gas Turbine Engine Operation
,” Research and Technology Organisation, Technical Report No. 44.
13.
Nielsen
,
A. E.
,
Moll
,
C. W.
, and
Staudacher
,
S.
, 2005, “
Modeling and Validation of the Thermal Effects on Gas Turbine Transients
,”
ASME J. Eng. Gas Turbines Power
0742-4795,
127
, pp.
564
572
.
14.
Wan
,
E.
, and
van der Merwe
,
R.
, 2001, “
The Unscented Kalman Filter
,”
Kalman Filtering and Neural Networks
,
Wiley Series on Adaptive and Learning Systems for Signal Processing, Communications and Control
,
Wiley
,
New York
.
15.
Nelson
,
A. T.
, 2000, “
Nonlinear Estimation and Modeling of Noisy Time Series by Dual Kalman Filtering Methods
,” Ph.D. thesis, Oregon Graduate Institute of Technology.
16.
Bishop
,
C. M.
, 1995,
Neural Networks for Pattern Recognition
,
Clarendon
,
Oxford
.
17.
Roth
,
B. A.
,
Doel
,
D. L.
, and
Cissell
,
J. J.
, 2005, “
Probabilistic Matching of Turbofan Engine Performance Models to Test Data
,” ASME Paper No. GT2005-68201.
18.
Cerri
,
G.
,
Borghetti
,
S.
, and
Salvini
,
C.
, 2005, “
Inverse Methodologies for Actual Status Recognition of Gas Turbine Components
,” ASME Paper No. PWR2005-50033.
19.
Stamatis
,
A.
,
Mathioudakis
,
K.
,
Ruiz
,
J.
, and
Curnock
,
B.
, 2001, “
Real-Time Engine Model Implementation for Adaptive Control and Performance Monitoring of Large Civil Turbofans
,” ASME Paper No. 2001-GT-0362.
20.
Curnock
,
B.
, 2000, “
Obidicote Project -WP4: Steady-State Test Cases
,” Rolls-Royce plc, Technical Report No. DNS62433.
21.
Walsh
,
P. P.
, and
Fletcher
,
P.
, 1998,
Gas Turbine Performance
,
Blackwell Science
,
London
.
22.
Volponi
,
A. J.
, 1999, “
Gas Turbine Parameter Corrections
,”
ASME J. Eng. Gas Turbines Power
0742-4795,
121
, pp.
613
621
.
23.
Kurzke
,
J.
, 2003, “
Model Based Gas Turbine Parameter Corrections
,” ASME Paper No. GT2003-38234.
You do not currently have access to this content.