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System and process for detecting and monitoring surface defectsA system and process for detecting and monitoring defects in large surfaces such as the field joints of the container segments of a space shuttle booster motor. Beams of semi-collimated light from three non-parallel fiber optic light panels are directed at a region of the surface at non-normal angles of expected incidence. A video camera gathers some portion of the light that is reflected at an angle other than the angle of expected reflectance, and generates signals which are analyzed to discern defects in the surface. The analysis may be performed by visual inspection of an image on a video monitor, or by inspection of filtered or otherwise processed images. In one alternative embodiment, successive predetermined regions of the surface are aligned with the light source before illumination, thereby permitting efficient detection of defects in a large surface. Such alignment is performed by using a line scan gauge to sense the light which passes through an aperture in the surface. In another embodiment a digital map of the surface is created, thereby permitting the maintenance of records detailing changes in the location or size of defects as the container segment is refurbished and re-used. The defect detection apparatus may also be advantageously mounted on a fixture which engages the edge of a container segment.
Document ID
20080004383
Acquisition Source
Marshall Space Flight Center
Document Type
Other - Patent
Authors
Mueller, Mark K.
Date Acquired
August 24, 2013
Publication Date
October 25, 1994
Subject Category
Spacecraft Design, Testing And Performance
Report/Patent Number
Patent Application Number: US-PATENT-APPL-SN-963572
Patent Number: US-PATENT-5,359,416
Funding Number(s)
CONTRACT_GRANT: NAS8-3049
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Patent
US-PATENT-5,359,416
Patent Application
US-PATENT-APPL-SN-963572
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