COMPOSITE MATERIAL MOLDING JIG, COMPOSITE MATERIAL MOLDING METHOD, ULTRASONIC TEST SYSTEM, ULTRASONIC TEST METHOD AND AIRCRAFT STRUCTURAL OBJECT
According to one implementation, a composite material molding jig includes a rigid portion and a convex portion for forming a groove for inserting an optical fiber sensor. The rigid portion has a surface for laminating prepreg sheets. The convex portion is formed in a surface side of the rigid portion. Further, according to one implementation, a composite material molding method is a method for molding a composite material, on which the groove for inserting the optical fiber sensor has been formed, by heating and curing a laminated body of the prepreg sheets laminated on the above-mentioned composite material molding jig.
» Number: US2017276648A1 (A1)
» Publication Date: 28/09/2017
» Applicant: FUJI HEAVY IND LTD?[JP]
» Inventor: TAKAHASHI KOHEI?[JP]
This project has received funding from the European Union's Horizon 2020 research and innovation programme under grant agreement Nº 768737