Vibration monitoring system for gas turbine engines

• US 7,013,210 B2
• Filed: 03/16/2004
• Issued: 03/14/2006
• Est. Priority Date: 11/16/2001
• Status: Expired due to Term

• Current Assignee: Triumph Engine Control Systems LLC (Triumph Group, Inc.)
• Original Assignee: Goodrich Pump & Engine Control Systems, Inc. (Raytheon Technologies Corporation d/b/a RTX)
• Inventors: McBrien, Gary M., Gottwald, James
• Primary Examiner(s): NGUYEN, TAN QUANG
• Application Number:
  US10/801,301
• Publication Number:
  US 20040176902A1
• Time in Patent Office: 728 Days
• Field of Search: 701/100, 701/29, 701/35, 340/438, 340/439, 340/441, 702/56, 702/34, 702/182, 702/183, 702/185, 702/189, 736/60, 735/79, 736/59
• US Class Current: 701/100
• CPC Class Codes: G01H 1/006 of the rotor of turbo machines

Abstract

Disclosed is a system and method for monitoring the vibration levels of gas turbine engines. The vibration monitoring system acquires vibration data from an engine, and processes the data with advanced algorithms to determine engine component health, both in a diagnostic and prognostic fashion. The method includes the steps of measuring an operating parameter and a corresponding set of vibration amplitudes for a plurality of rotating component during a period of operation and normalizing the set of measured vibration amplitudes based on established amplitude limits. The set of normalized amplitude data points are stored in parameter-based data blocks, which extend over a predetermined range of the operating parameter. For each data block, a time period remaining to reach the established amplitude limits is estimated based on changes in the normalized amplitude data points stored in the data blocks. An alarm setting is then established based on the estimated time period remaining to reach the established amplitude limits for each data block.

Claims

1. A method for monitoring bearing vibration levels associated with a rotating component and establishing an alarm setting therefor, the method comprising the steps of:

a) measuring an operating parameter and a corresponding set of vibration amplitudes for a rotating component during a period of operation, the rotating component including a plurality of bearings and at least one sensor for measuring vibration amplitudes;

b) selecting a bearing to be monitored from the plurality of bearings of the rotating component;

c) selecting the vibration sensor to be used for monitoring the vibration amplitudes of the selected bearing;

d) demodulate the set of measured vibration amplitudes monitored by the sensor;

e) convert the demodulated set of measured vibration amplitudes into spectral data;

f) compare the spectral data to predetermined tonal frequencies for the bearing so as to define a set of normalized amplitude data points; and

g) trend the normalized amplitude data points over the period of operation so as to establish a time period remaining to reach an established amplitude limit.