Rotor health monitoring combining spin tests and data-driven anomaly detection methods

Health monitoring is highly dependent on sensor systems that are capable of performing in various engine environmental conditions and able to transmit a signal upon a predetermined crack length, while acting in a neutral form upon the overall performance of the engine system. Efforts are under way at NASA Glenn Research Center through support of the Intelligent Vehicle Health Management Project (IVHM) to develop and implement such sensor technology for a wide variety of applications. These efforts are focused on developing high temperature, wireless, low cost, and durable products. In an effort to address technical issues concerning health monitoring, this article considers data collected from an experimental study using high frequency capacitive sensor technology to capture blade tip clearance and tip timing measurements in a rotating turbine engine-like-disk to detect the disk faults and assess its structural integrity. The experimental results composed at a range of rotational speeds from tests conducted at the NASA Glenn Research Center’s Rotordynamics Laboratory are evaluated and integrated into multiple data-driven anomaly detection techniques to identify faults and anomalies in the disk. In summary, this study presents a select evaluation of online health monitoring of a rotating disk using high caliber capacitive sensors and demonstrates the capability of the in-house spin system.

[1]  M. Zielinski,et al.  Noncontact vibration measurements on compressor rotor blades , 2000 .

[2]  Khlefa Alarbe Esaklul,et al.  Handbook of case histories in failure analysis , 1992 .

[3]  Robert P. W. Duin,et al.  Support vector domain description , 1999, Pattern Recognit. Lett..

[4]  David L. Iverson Inductive System Health Monitoring , 2004, IC-AI.

[5]  Ali Abdul-Aziz,et al.  Combined experimental and analytical study using cruciform specimen for testing advanced aeropropulsion materials under in-plane biaxial loading , 2006, SPIE Smart Structures and Materials + Nondestructive Evaluation and Health Monitoring.

[6]  P. Tappert,et al.  Health monitoring and prognostics of blades and disks with blade tip sensors , 2000, 2000 IEEE Aerospace Conference. Proceedings (Cat. No.00TH8484).

[7]  Wayne C. Haase,et al.  Detection, discrimination, and real-time tracking of cracks in rotating disks , 2002, SPIE Smart Structures and Materials + Nondestructive Evaluation and Health Monitoring.

[8]  M. Drumm,et al.  High performance rotor monitoring , 2000, 19th DASC. 19th Digital Avionics Systems Conference. Proceedings (Cat. No.00CH37126).

[9]  Jörg Wauer,et al.  On the Dynamics of Cracked Rotors: A Literature Survey , 1990 .

[10]  P. Young,et al.  On the material characterization of a composite using micro CT image based finite element modeling , 2006, SPIE Smart Structures and Materials + Nondestructive Evaluation and Health Monitoring.

[11]  A. S. Sekhar,et al.  Condition monitoring of cracked rotors through transient response , 1998 .

[12]  Mark R. Woike,et al.  NDE using sensor based approach to propulsion health monitoring of a turbine engine disk , 2009, Smart Structures and Materials + Nondestructive Evaluation and Health Monitoring.

[13]  Mark R. Woike,et al.  Health Monitoring of a Rotating Disk Using a Combined Analytical-Experimental Approach , 2009 .

[14]  Stephen D. Bay,et al.  Mining distance-based outliers in near linear time with randomization and a simple pruning rule , 2003, KDD '03.

[15]  Ali Abdul-Aziz,et al.  Finite element design study of a bladed flat rotating disk to simulate cracking in a typical turbine disk: Part II , 2006, SPIE Smart Structures and Materials + Nondestructive Evaluation and Health Monitoring.

[16]  Bernhard Schölkopf,et al.  Estimating the Support of a High-Dimensional Distribution , 2001, Neural Computation.