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首页> 外文期刊>Fatigue Fracture Mechanics >Experiences and Modeling of Hydrogen Cracking in a Thick-Walled Pressure Vessel
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Experiences and Modeling of Hydrogen Cracking in a Thick-Walled Pressure Vessel

机译:厚壁压力容器中氢裂解的经验和建模

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Hydrogen cracking associated with armament structures has become more prevalent in recent times. In this work, a thick-walled, autofrettaged pressure vessel was manufactured from ASTM A723 Grade 2 steel and heat-treated to yield strength of 1170 MPa. An outside diameter keyway was then machined. The keyway was exposed to concentrated sulfuric acid, leading to apparent cracking within 20 hours of exposure. Investigation of the affected keyway in the pressure vessel indicated that localized hardened areas were present. The base material possessed hardness values of Rc 37-39, while areas near the keyway possessed a local hard zone up to Rc 44. These zones extended to a depth of approximately 4 mm. The different hardness layers suggest that the environmental cracking incubated and propagated in two separate stages. It is speculated that cracking in the hard layer incubated quickly and propagated to approximately the 4 mm depth, then arrested itself once it encountered the more ductile base material. Previously published crack growth (da/dt) test data, and new data verify that this process of incubation and propagation could have occurred in a matter of seconds. The cracking then resumed in the softer base material after approximately 300 hours of incubation time. Additional da/dt testing of this condition has been performed over a range of yield strengths and verifies that incubation times and crack propagation rates are similar to those observed in this pressure vessel.
机译:近年来,与武器结构相关的氢裂变得越来越普遍。在这项工作中,使用ASTM A723 2级钢制造了厚壁的自动密封压力容器,并对其进行了热处理,以产生1170 MPa的强度。然后加工外径键槽。键槽暴露于浓硫酸中,导致暴露后20小时内出现明显的裂纹。对压力容器中受影响的键槽的调查表明,存在局部的硬化区域。基体材料的硬度值为Rc 37-39,而键槽附近的区域则具有局部硬质区域,最高为Rc44。这些区域延伸到大约4毫米的深度。不同的硬度层表明环境裂纹是在两个单独的阶段中温育和传播的。据推测,在硬质层中的裂纹很快被孵化并传播到大约4mm的深度,一旦遇到更易延展的基础材料,其自身就被阻止了。先前发布的裂纹扩展(da / dt)测试数据和新数据验证了这种温育和传播过程可能在几秒钟内发生。在大约300小时的孵育时间后,裂纹会在较软的基材中恢复。此条件的附加da / dt测试已在一定的屈服强度范围内进行,并验证了保温时间和裂纹扩展速率与在此压力容器中观察到的相似。

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