Characterization of wrinkles and periodic variations in material using infrared thermography
AssigneeThe Boeing Company
InventorsJeffrey G. Thompson, Gary E. Georgeson, Hong Hue Tat, Tyler M. Holmes
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AssigneeThe Boeing Company
InventorsJeffrey G. Thompson, Gary E. Georgeson, Hong Hue Tat, Tyler M. Holmes
Estimating the term…
Methods for identifying and quantifying wrinkles in a composite structure by processing infrared image data. The intensity and first and second time derivatives thereof at a particular time can be displayed as thermography line profiles on a graph in which the horizontal axis represents the pixel number across the field of view of an infrared camera. The spatial derivatives of the foregoing thermography line profiles can also be calculated and displayed as a graph. The maximum amplitude (i.e., height) of an out-of-plane wrinkle can be determined using a correlation/calibration curve that is constructed by correlating infrared image data with optical measurement data. In addition, the wavelength and maximum amplitude of an in-plane wrinkle can be measured directly from the thermography line profiles.
A method for non-destructive inspection of composite structures, comprising:
A method for measuring an out-of-plane wrinkle in a structure made of a composite material, the method comprising:
A method for measuring an in-plane wrinkle in a composite structure, comprising:
A method for calibrating an infrared imaging system, comprising:
An infrared imaging system comprising a computer configured to convert infrared image data to a wrinkle maximum amplitude measurement value based on a calibration curve that correlates infrared image data indicative of an out-of-plane wrinkle to optical cross-section measurement data indicative of an out-of-plane wrinkle.
Dependencies are inferred from the claim text.