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Delamination Induced by Laser Drilling on a Base Cobalt Superalloy

机译:激光钻孔在钴基高温合金上引起的分层

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Temperatures in the high pressure chamber of aircraftengines are continuously increasing to improve theengine efficiency and constitutive materials need to bethermally protected. The first protection is a ceramicthermal barrier coating (TBC) cast on all the hot gasexposedstructure. The second protection is providedby a cool air layer realized by the use of a thousand ofdrills on the parts where a cool air is flowing through.The laser drilling process is used to realize these holesat acute angles on this coated mutlimaterial. Thepresent work aims at characterizing interfacialcracking induced by laser drilling on coated cobaltbase super alloy. This work attached to quantify thecrack by several microscopic observations with regardsto the most significant process parameters related asthe angle beam. The difference between thelaser/ceramic and the laser/substrate interaction is alsostudied with real time observation by using a fastmovie camera.
机译:飞机高压舱内的温度 引擎不断增加以改善 发动机效率和本构材料需要 受热保护。第一个保护是陶瓷 在所有暴露于热气中的热障涂层(TBC) 结构体。提供第二种保护 通过使用一千个冷气层来实现 在流过冷空气的零件上钻孔。 激光钻孔工艺用于实现这些孔 以这种锐角涂覆在这种多层材料上。这 目前的工作旨在表征界面 涂层钴激光钻孔引起的裂纹 基础超级合金。这项工作所附以量化 通过一些微观观察发现裂纹 与以下最重要的工艺参数有关 角钢。两者之间的区别 激光/陶瓷和激光/基材的相互作用也是 通过使用快速观察进行实时观察 电影摄影机。

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