Use of Electron Fractography to Dianose Stress-Corrosion Cracking of an AISI 4340 Nose Landing Gear Cylinder

J. A. Scott
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Abstract

A nose landing gear cylinder made from AISI 4340 Ni-Cr-Mo alloy steel was found cracked and leaking, causing partial depressurization. Investigation revealed the crack to be a stress-corrosion type, judging by the 6500x electron fractograph. It had started in a region of concentrated, large non-metallic inclusions near the chromium-plated ID of the cylinder. Also, there were breaks in the chromium plate and pits in the underlying base metal. The cylinder had been in service for 18,017 h, and 5948 h had passed since the first and only overhaul. Substandard plating of the ID at this time ultimately resulted in pitting of the metal. The combination of surface pitting and stress concentration at the nearby inclusions resulted in stress-corrosion cracking.
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用电子断口分析AISI 4340前起落架气缸应力腐蚀开裂
前起落架气缸由AISI 4340 Ni-Cr-Mo合金钢制造,发现裂纹和泄漏,造成部分减压。通过6500x电子断口分析,发现裂纹为应力腐蚀型。它开始于一个集中的区域,大的非金属夹杂物附近镀铬的内径圆筒。此外,铬板上有断裂,下面的贱金属上有凹坑。该汽缸已服役18017小时,自第一次也是唯一一次大修以来已经过了5948小时。此时内径的不合格电镀最终导致了金属的点蚀。表面点蚀和夹杂附近的应力集中共同作用导致应力腐蚀开裂。
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