在飞机工业中，复合材料在结构应用中的使用越来越多，这需要对复合材料维修有更深入的了解。这些知识只能通过确定概述维修过程的基本原理来提供。不同基体材料之间的相互作用，将允许在结构修复中更广泛地替代相容材料，已被确定为第一个基本步骤。因此，我们设计了一系列实验，通过直接加工或粘结预固化层压板来制造用相同连续碳纤维增强的异种基体。 DMA和DSC等热分析技术与传统的力学测试相结合，以确定材料的相容性。

THE INCREASED USE OF COMPOSITE MATERIALS FOR STRUCTURAL APPLICATIONS IN THE AIRCRAFT INDUSTRY REQUIRES A DEEPER UNDERSTANDING OF COMPOSITE REPAIR. THIS KNOWLEDGE CAN ONLY BE PROVIDED BY IDENTIFYING THE FUNDAMENTALS THAT OUTLINE THE REPAIR PROCESS. THE INTERACTION BETWEEN DISSIMILAR MATRIX MATERIALS, WHICH WOULD ALLOW WIDER SUBSTITUTION OF COMPATIBLE MATERIALS IN STRUCTURAL REPAIRS, HAS BEEN IDENTIFIED AS THE FIRST FUNDAMENTAL STEP. ACCORDINGLY, A SERIES OF EXPERIMENTS HAS BEEN DESIGNED WHERE DISSIMILAR MATRICES REINFORCED WITH THE SAME CONTINUOUS CARBON FIBERS WERE FABRICATED BY DIRECT PROCESSING OR BONDING OF PRECURED LAMINATES. THERMAL ANALYSIS TECHNIQUES SUCH AS DMA AND DSC WERE COUPLED WITH TRADITIONAL MECHANICAL TESTS TO DETERMINE MATERIAL COMPATIBILITY.