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3-D Surface Depression Profiling Using High Frequency Focused Air-Coupled Ultrasonic PulsesSurface topography is an important variable in the performance of many industrial components and is normally measured with diamond-tip profilometry over a small area or using optical scattering methods for larger area measurement. This article shows quantitative surface topography profiles as obtained using only high-frequency focused air-coupled ultrasonic pulses. The profiles were obtained using a profiling system developed by NASA Glenn Research Center and Sonix, Inc (via a formal cooperative agreement). (The air transducers are available as off-the-shelf items from several companies.) The method is simple and reproducible because it relies mainly on knowledge and constancy of the sound velocity through the air. The air transducer is scanned across the surface and sends pulses to the sample surface where they are reflected back from the surface along the same path as the incident wave. Time-of-flight images of the sample surface are acquired and converted to depth/surface profile images using the simple relation (d = V*t/2) between distance (d), time-of-flight (t), and the velocity of sound in air (V). The system has the ability to resolve surface depression variations as small as 25 microns, is useable over a 1.4 mm vertical depth range, and can profile large areas only limited by the scan limits of the particular ultrasonic system. (Best-case depth resolution is 0.25 microns which may be achievable with improved isolation from vibration and air currents.) The method using an optimized configuration is reasonably rapid and has all quantitative analysis facilities on-line including 2-D and 3-D visualization capability, extreme value filtering (for faulty data), and leveling capability. Air-coupled surface profilometry is applicable to plate-like and curved samples. In this article, results are shown for several proof-of-concept samples, plastic samples burned in microgravity on the STS-54 space shuttle mission, and a partially-coated cylindrical ceramic composite sample. Impressive results were obtained for all samples when compared with diamond-tip profiles and measurements from micrometers. The method is completely nondestructive, noninvasive, non-contact and does not require light-reflective surfaces.
Document ID
19990047656
Acquisition Source
Glenn Research Center
Document Type
Technical Memorandum (TM)
Authors
Roth, Don J. (NASA Glenn Research Center Cleveland, OH United States)
Kautz, Harold E. (NASA Glenn Research Center Cleveland, OH United States)
Abel, Phillip B. (NASA Glenn Research Center Cleveland, OH United States)
Whalen, Mike F. (Sonix, Inc. Springfield, VA United States)
Hendricks, J. Lynne (Sonix, Inc. Springfield, VA United States)
Bodis, James R. (Cleveland State Univ. Cleveland, OH United States)
Date Acquired
September 6, 2013
Publication Date
May 1, 1999
Subject Category
Quality Assurance And Reliability
Report/Patent Number
NASA/TM-1999-209053
E-11589
NAS 1.15:209053
Funding Number(s)
PROJECT: RTOP 523-22-13
CONTRACT_GRANT: NCC3-304
CONTRACT_GRANT: NCC3-489
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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