Systems and methods for tracking and analyzing information associated with a life cycle of a composite part
AssigneeThe Boeing Company
InventorsAli Salour, Jolynnetta Aisha Neal
Life of this patent
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AssigneeThe Boeing Company
InventorsAli Salour, Jolynnetta Aisha Neal
Estimating the term…
A method for tracking information associated with a manufactured part is provided. The method is implemented by at least one computing device including at least one processor in communication with a memory. The method includes generating, by the at least one computing device, a panel identifier to be applied to a composite material panel. The method additionally includes storing, in the memory, at least one curing parameter associated with a curing process performed on the composite material panel in association with the panel identifier, generating, by the at least one computing device, at least one part identifier to be applied to at least one part machined from the composite material panel, and storing, in the memory, at least one part processing parameter in association with at least one process performed on the at least one part.
A method for tracking information associated with a manufactured part, the method is implemented by at least one computing device including at least one processor in communication with a memory, the method comprising:
(canceled)
A system for use in tracking information associated with a manufactured part, said system comprising at least one computing device in communication with a memory, said at least one computing device configured to:
An aircraft part formed from a panel of composite material, said aircraft part having at least one tag applied thereto, wherein the at least one tag includes a panel identifier and a part identifier, wherein the panel identifier and part identifier are stored in a repository in association with information pertaining to an origin of the composite material and manufacturing processes performed to generate said aircraft part, wherein the information pertaining to the origin further includes at least one of a peak temperature and a peak pressure applied to the composite material panel during a curing process.
Dependencies are inferred from the claim text.