초록

A method and apparatus for conducting dynamic characterization of a gas turbine engine which involves generating exciting pressure pulses and measuring responses in the engine, and, in one aspect, then analyzing the measured response for engine dynamic characteristics.

대표청구항 ▼

The invention claimed is: 1. A method for conducting dynamic characterization of a gas turbine engine, comprising: (a) generating a plurality of exciting pressure pulses in series in an air flow passing through a main gas path of the gas turbine engine, the exciting pressure pulses having varying f

The invention claimed is: 1. A method for conducting dynamic characterization of a gas turbine engine, comprising: (a) generating a plurality of exciting pressure pulses in series in an air flow passing through a main gas path of the gas turbine engine, the exciting pressure pulses having varying frequencies; (b) measuring a response in at least one location of the gas turbine engine, excited by the exciting pressure pulses with varying frequencies; and (c) analyzing the measured response for engine dynamic characteristics, wherein the measured response is a structural vibratory response of an engine mechanical structure. 2. The method as defined in claim 1 wherein steps (a) and (b) are conducted when the engine is operating. 3. The method as defined in claim 1 wherein step (a) is practised by intermittently injecting said air flow into the main gas path of the gas turbine engine at the varying frequencies. 4. The method as defined in claim 1 wherein step (a) is practised by intermittently bleeding said air flow from the gas turbine engine at the varying frequencies. 5. The method as defined in claim 4 wherein the intermittently bled air flow is generated by a compressor of the gas turbine engine. 6. The method as defined in claim 1 wherein the exciting pressure pulses in series are variable in magnitude. 7. The method as defined in claim 1 wherein step (a) is conducted by generating the exciting pressure pulses in series in said air flow passing through a passage, the passage being in fluid communication with the main gas path of the gas turbine engine to thereby allow the exciting pressure pulses to propagate into the main gas path. 8. The method as defined in claim 7 wherein the generating of the exciting pressure pulses in the air flow is achieved by alternately opening and blocking the passage. 9. The method as defined in claims 8 comprising changing time intervals between the alternate opening and blocking of the passage to thereby achieve the varying frequencies of the exciting pressure pulses. 10. An apparatus for gas turbine engine dynamic characterization comprising: a passage adapted to be connected to the gas turbine engine in fluid communication with a main as path of the gas turbine engine; a mechanism including a body having a plurality of openings, the body being rotatable in the airflow to alternately open and block the passage for generating a series of exciting pressure pulses in the airflow; and a motor adapted to rotate the body in a varying rotational speed to change frequencies of the generated exciting pressure pulses. 11. The apparatus as defined in claim 10 further comprising means for adjusting a magnitude of the exciting pressure pulses. 12. An apparatus for generating a plurality of pressure pulses in an air flow for testing dynamic characteristics of a gas turbine engine, the apparatus comprising: an air flow passage adapted to be connected to the gas turbine engine to allow an air flow to be injected into or bled from a main gas path of the gas turbine engine; and a pressure pulsing device including a rotating body for generating the plurality of pressure pulses in the air flow with varying frequencies, the rotating body intermittently interrupting the air flow provided through the air flow passage. 13. The apparatus as defined in claim 12 wherein the pressure pulsing device comprises a valve for adjusting a maximum flow rate of the air flow passing through the flow pipe, thereby adjusting a magnitude of the generated pressure pulses in the air flow. 14. The apparatus as defined in claim 12 wherein the rotating body comprises a plurality of openings and is rotated by a speed-adjustable motor.