SYSTEM AND METHOD FOR REPAIRING COMPOSITE AIRCRAFT STRUCTURES
    3.
    发明公开
    SYSTEM AND METHOD FOR REPAIRING COMPOSITE AIRCRAFT STRUCTURES 有权
    系统VERFAHREN ZUR REPARATUR VON FLUGZEUGSTRUKTUREN AUS VERBUNDWERKSTOFF

    公开(公告)号:EP2943405A1

    公开(公告)日:2015-11-18

    申请号:EP13774542.8

    申请日:2013-09-19

    摘要: The present disclosure describes one or more systems, methods, routines and/or techniques for thermal management. One or more systems, methods, routines and/or techniques may provide advice or guidance (e.g., to a repair technician) regarding how to perform a hot bond repair, for example, on an aircraft component that has been damaged. The thermal management advisor may provide advice or guidance regarding how to prepare a repair field prior to running a thermal survey. For example, thermal management advisor may recommend a particular heat blanket, a configuration of the heat blanket, placement of various temperature sensors and other preparation guidance. The thermal management advisor may provide advice or guidance regarding how to alter or manage the repair setup during a thermal survey and during the actual curing process. For example, thermal management advisor may recommend particular temperature sensors or areas of the repair field that should be insulated.

    摘要翻译: 本公开描述了用于热管理的一个或多个系统,方法,例程和/或技术。 一个或多个系统,方法,例程和/或技术可以提供关于如何执行热粘合修复(例如在已经损坏的飞行器部件上)的建议或指导(例如,到维修技术人员)。 热管理顾问可以在运行热测量之前就如何准备维修领域提供建议或指导。 例如,热管理顾问可以推荐特定的热毯,热毯的配置,各种温度传感器的放置和其他准备指导。 热管理顾问可以提供关于如何在热测量期间和在实际固化过程期间更改或管理修理设置的建议或指导。 例如,热管理顾问可以推荐特定的温度传感器或应该被绝缘的修复区域。