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Ultrasonically Actuated Tools for Abrading Rock SurfacesAn ultrasonic rock-abrasion tool (URAT) was developed using the same principle of ultrasonic/sonic actuation as that of the tools described in two prior NASA Tech Briefs articles: Ultrasonic/ Sonic Drill/Corers With Integrated Sensors (NPO-20856), Vol. 25, No. 1 (January 2001), page 38 and Ultrasonic/ Sonic Mechanisms for Drilling and Coring (NPO-30291), Vol. 27, No. 9 (September 2003), page 65. Hence, like those tools, the URAT offers the same advantages of low power demand, mechanical simplicity, compactness, and ability to function with very small axial loading (very small contact force between tool and rock). Like a tool described in the second of the cited previous articles, a URAT includes (1) a drive mechanism that comprises a piezoelectric ultrasonic actuator, an amplification horn, and a mass that is free to move axially over a limited range and (2) an abrasion tool bit. A URAT tool bit is a disk that has been machined or otherwise formed to have a large number of teeth and an overall shape chosen to impart the desired shape (which could be flat or curved) to the rock surface to be abraded. In operation, the disk and thus the teeth are vibrated in contact with the rock surface. The concentrated stresses at the tips of the impinging teeth repeatedly induce microfractures and thereby abrade the rock. The motion of the tool induces an ultrasonic transport effect that displaces the cuttings from the abraded area. The figure shows a prototype URAT. A piezoelectric-stack/horn actuator is housed in a cylindrical container. The movement of the actuator and bit with respect to the housing is aided by use of mechanical sliders. A set of springs accommodates the motion of the actuator and bit into or out of the housing through an axial range between 5 and 7 mm. The springs impose an approximately constant force of contact between the tool bit and the rock to be abraded. A dust shield surrounds the bit, serving as a barrier to reduce the migration of rock debris to sensitive instrumentation or mechanisms in the vicinity. A bushing at the tool-bit end of the housing reduces the flow of dust into the actuator and retains the bit when no axial load is applied.
Document ID
20110012927
Acquisition Source
Jet Propulsion Laboratory
Document Type
Other - NASA Tech Brief
Authors
Dolgin, Benjamin
(California Inst. of Tech. Pasadena, CA, United States)
Sherrit, Stewart
(California Inst. of Tech. Pasadena, CA, United States)
Bar-Cohen, Yoseph
(California Inst. of Tech. Pasadena, CA, United States)
Rainen, Richard
(California Inst. of Tech. Pasadena, CA, United States)
Askin, Steve
(California Inst. of Tech. Pasadena, CA, United States)
Bickler, Donald
(California Inst. of Tech. Pasadena, CA, United States)
Lewis, Donald
(California Inst. of Tech. Pasadena, CA, United States)
Carson, John
(California Inst. of Tech. Pasadena, CA, United States)
Dawson, Stephen
(California Inst. of Tech. Pasadena, CA, United States)
Bao, Xiaoqi
(California Inst. of Tech. Pasadena, CA, United States)
Chang, Zensheu
(California Inst. of Tech. Pasadena, CA, United States)
Peterson, Thomas
(Cybersonics, Inc. Erie, PA, United States)
Date Acquired
August 25, 2013
Publication Date
July 1, 2006
Publication Information
Publication: NASA Tech Briefs, July 2006
Subject Category
Man/System Technology And Life Support
Report/Patent Number
NPO-30403
Report Number: NPO-30403
Distribution Limits
Public
Copyright
Public Use Permitted.
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