Method and system for determining ply-by-ply damage in a composite structure
AssigneeThe Boeing Company
InventorsKenneth J. Hunziker, Jenna K. Pang
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AssigneeThe Boeing Company
InventorsKenneth J. Hunziker, Jenna K. Pang
Estimating the term…
A computer-implemented method that facilitates determining ply-by-ply damage in a composite structure comprises receiving, by a computing system, a geometric model that specifies geometric aspects of a composite structure. The geometric model facilitates the performance of finite element analysis (FEA). FEA logic of the computing system applies each of a plurality of material failure models (MFMs) to the geometric model to predict different types of damage to the composite structure due to an applied force or stress. Each MFM relates a force or stress applied to a material to a particular type of damage to the material. The machine learning logic predicts, based on each of the predicted different types of damage, an aggregate prediction of damage to the composite structure.
A computer-implemented method for determining ply-by-ply damage in a three-dimensional (3D) composite structure, method comprising:
A computing system that for determining ply-by-ply damage in a three-dimensional (3D) composite structure, the computing system comprising:
A non-transitory computer-readable medium that stores instruction code that facilitates determining ply-by-ply damage in a three-dimensional (3D) composite structure, wherein execution of the instruction code by one or more processors of a computing system causes the computing system to perform operations comprising:
Dependencies are inferred from the claim text.