Patent 10285219 was granted and assigned to Aurora Flight Sciences on May, 2019 by the United States Patent and Trademark Office.
A composite structure cured by the process of: electrically coupling a first lead to a first portion of said composite structure; electrically coupling a second lead to a second portion of said composite structure; and using an electric power source to pass electric current through said composite structure from said first portion to said second portion, wherein passing said electric current through said composite structure causes the temperature of at least a portion of said composite structure increase to a predetermined temperature.