US 12,480,850 B2
Tension load fixture and method for evaluating fracture behavior of a composite material
Joseph D. Schaefer, Richmond Heights, MO (US); Brian P. Justusson, Saint Peters, MO (US); and Haozhong Gu, Ballwin, MO (US)
Assigned to The Boeing Company, Chicago, IL (US)
Filed by The Boeing Company, Chicago, IL (US)
Filed on Apr. 21, 2022, as Appl. No. 17/726,091.
Prior Publication US 2023/0341303 A1, Oct. 26, 2023
Int. Cl. G01N 3/08 (2006.01)
CPC G01N 3/08 (2013.01) [G01N 2203/0017 (2013.01); G01N 2203/04 (2013.01)] 20 Claims
OG exemplary drawing
 
1. A tension load fixture for applying tension or loading forces to a specimen, the tension load fixture comprising:
a pair of tension arms configured to releasably couple to opposite end regions of a specimen and to apply tension or loading forces to the specimen, wherein the specimen is configured to be positioned between the pair of tension arms and defines a notch between the opposite end regions of the specimen, wherein the notch extends from a side of the specimen to a middle region of the specimen;
an imaging device configured to capture one or more images of the middle region of the specimen, and that is configured to rotate about an axis to facilitate generation of a three-dimensional image of the middle region of the specimen as the specimen is subjected to tension or loading forces; and
a controller communicatively coupled to the imaging device and to a load generator, the controller configured to:
control, via the load generator, application of tension or loading forces to the specimen;
determine, based on the one or more images, dimensions of a plurality of cracks that develop beneath a surface of the specimen and determine specific layers associated with the plurality of cracks in response to the application of tension or loading forces to the specimen, wherein:
the plurality of cracks are different from the notch, and
the dimensions of a crack, of the plurality of cracks, comprise a length of the crack, a height of the crack, and a position of the crack;
track a damage mode, for each specific layer associated with the plurality of cracks, wherein, for each specific layer, the damage mode indicates a matrix crack or a fiber crack; and
output data for each specific layer associated with the plurality of cracks, wherein the data indicates the dimensions of the plurality of cracks and the corresponding damage mode.