SYSTEM AND METHOD FOR REPAIRING COMPOSITE AIRCRAFT STRUCTURES

摘要

The present invention describes one or more systems, methods, procedures and / or techniques for thermal management. One or more systems, methods, processing sequences, and / or techniques may provide advice or guidance (e.g., to a repair technician) about how to perform a hot bond repair on, for example, a damaged aircraft component. The Thermal Management Advisor can provide advice or guidance on how to prepare the repair field before operating the thermal survey. For example, the thermal management advisor may recommend specific thermal blanks, thermal blanket configurations, placement of various temperature sensors, and other preparation guides. The thermal management advisor can provide advice or guidance as to how to manage or change the repair setup during the thermal survey and the actual curing process. For example, the thermal management advisor may recommend specific temperature sensors or areas of the repair field to be isolated.