Analyzing vibration of rotating blades

• US 6,584,849 B2
• Filed: 03/28/2002
• Issued: 07/01/2003
• Est. Priority Date: 04/17/2001
• Status: Expired due to Term

• Current Assignee: Rolls-Royce PLC (Rolls-Royce Holdings Plc)
• Original Assignee: Rolls-Royce PLC (Rolls-Royce Holdings Plc)
• Inventors: Parrish, Colin J, Loftus, Peter
• Primary Examiner(s): Kwok, Helen
• Assistant Examiner(s): Miller, Rose M.
• Application Number:
  US10/107,154
• Publication Number:
  US 20020162394A1
• Time in Patent Office: 460 Days
• Field of Search: 736/59, 736/60, 736/61, 737/63, 737/68, 737/74, 737/75, 735/93
• US Class Current: 73/659
• CPC Class Codes: F01D 21/003 Arrangements for testing or measuring for measuring vibrations G01H
• CPC Class Codes: G01H 1/006 of the rotor of turbo machines

Abstract

A method of characterizing the vibration of a plurality of rotating blades (12), such as turbine blades in a gas turbine engine, includes the steps of providing a single strain gauge (16A) on a single one (12A) of the blades and providing either one or two tip timing probes (22A, 22B) on a casing surrounding the blades. The data from the strain gauge (16A) allows the vibration of the single blade (12A) to be fully characterized while the data from the tip timing probes (22A, 22B) allows the amplitudes or velocities of vibration of all the blades to be determined. The relationship between the data from the tip timing probes for the single blade (12A) and the stress data from the strain gauge may be established. This relationship may then be assumed to apply to all the blades, thus allowing the stresses induced in all the blades by the vibrations to be determined.

Claims

1. A method of characterising the vibration of a plurality of rotating blades mounted on a rotor, the method including the steps of:

providing a strain gauge on one of the blades;

analysing data from the strain gauge to provide information about the frequencies of vibration and the vibrationally induced stresses in that blade;

providing at least one stationary timing probe for detecting the times at which respective blades pass the probe;

analysing data from the or each timing probe to obtain information about the amplitudes and/or velocities of vibration of each of the plurality of blades;

determining the relationship between vibrationally induced stress as measured by the strain gauge and vibrational amplitude or velocity as measured by the timing probe(s) for the blade on which the strain gauge is mounted, for a particular frequency of vibration; and

assuming that the above relationship is applicable to each of the plurality of blades, calculating the vibrationally induced stress for each blade from its amplitude or velocity of vibration as measured by the timing probe(s) and the said relationship.

2. A method according to claim 1, wherein the said relationship is a ratio of vibrationally induced stress as measured by the strain gauge to vibrational amplitude or velocity as measured by the timing probe(s).

3. A method according to claim 1, the method further including the step of providing a reference indicia on the rotor and a reference probe for providing a signal when the reference indicia passes the probe, thereby providing a signal once for every rotation of the rotor.

4. A method according to claim 3, wherein the timing probe(s) and the reference probe are mounted on a casing surrounding the blades.

5. A method according to claim 3, wherein the method includes the step of determining, for each of the plurality of blades, its spatial relationship with the reference indicia on the rotor and calculating an expected arrival time at which each blade tip would pass a respective timing probe were it undergoing no vibration.

6. A method according to claim 1, wherein the strain gauge data is analysed by Fourier analysis.

7. A method according to claim 6, wherein analysis for a particular frequency includes determining the amplitude of vibration of the blade and, from that information, the stresses induced in the blade by that mode of vibration.

8. A method according to claim 1, the method including the step of measuring the amplitude of asynchronous vibration by:

measuring the displacement of the blade from its expected position for each of a plurality of rotations of the blade;

determining the maximum displacement of the blade from its expected position; and

assuming that this maximum displacement is the vibrational amplitude.

9. A method according to claim 1, wherein the timing probe data is analysed using Fourier analysis on a plurality of timing probe measurements, the excited mode or modes of vibration being indicated by peaks in the spectrum.

10. A method according to claim 1, the method including the step of measuring synchronous vibration by:

determining an approximate resonance frequency for a blade;

rotating the blade at a plurality of frequencies in a range from below to above the approximate resonance frequency, and at each frequency measuring the displacement of the blade from its expected position, using a timing probe;

analysing the plurality of measured displacements at the respective plurality of frequencies to provide maximum and minimum displacement values; and

comparing the maximum and minimum displacement values to provide an indication of the amplitude of the vibration of the blade.

11. A method according to claim 1, wherein the method includes the use of two spaced timing probes, spaced between 5°

and 20°

apart.

12. Apparatus for characterising the vibration of rotating blades, the apparatus including:

a plurality of blades mounted for rotation on a rotor and extending radially outwardly therefrom;

a casing at least partially surrounding the blades;

a strain gauge mounted on one of the blades;

at least one timing probe mounted on the casing for indicating the passage of each of the individual blades;

means for analysing data from the strain gauge to provide information about the frequencies of vibration of the blade and the vibrationally induced stresses in that blade;

means for analysing data from the at least one timing probe to obtain information about the amplitudes and/or velocities of vibration of each of the plurality of blades; and

means for determining in the relationship between vibrationally induced stress as measured by the strain gauge and vibrational amplitude or velocity as measured by the at least one timing probe for the blade on which the strain gauge is mounted for a particular frequency of vibration;

and assuming that the above relationship is applicable to each of the plurality of blades, calculating the vibrationally induced stress for each blade from its amplitude or velocity of vibration as measured by the at least one timing probe and said relationship.

13. Apparatus according to claim 12, the apparatus further including a reference probe mounted on the casing and a reference indicia on the rotor, and means for providing signal when the reference indicia passes the reference probe.