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Combined Amplitude and Frequency Measurements for Non-Contacting Turbomachinery Blade VibrationA method and apparatus for measuring the vibration of rotating blades, such as turbines, compressors, fans, or pumps, including sensing the return signal from projected energy and/or field changes from a plurality of sensors mounted on the machine housing. One or more of the sensors has a narrow field of measurement and the data is processed to provide the referenced time of arrival of each blade, and therefore the blade tip deflection due to vibration. One or more of the sensors has a wide field of measurement, providing a time history of the approaching and receding blades, and the data is processed to provide frequency content and relative magnitudes of the active mode(s) of blade vibration. By combining the overall tip deflection magnitude with the relative magnitudes of the active modes, the total vibratory stress state of the blade can be determined.
Document ID
20150003169
Acquisition Source
Headquarters
Document Type
Other - Patent
Authors
Platt, Michael J.
Jagodnik, John J.
Date Acquired
March 18, 2015
Publication Date
December 10, 2013
Subject Category
Aircraft Propulsion And Power
Instrumentation And Photography
Numerical Analysis
Structural Mechanics
Report/Patent Number
Patent Application Number: US-Patent-Appl-SN-12/795,124
Patent Number: US-Patent-8,606,541
Funding Number(s)
CONTRACT_GRANT: NNX09CA34C
CONTRACT_GRANT: N68335-08-C-0215
CONTRACT_GRANT: NNX08CC54P
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Patent
US-Patent-8,606,541
Patent Application
US-Patent-Appl-SN-12/795,124
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