首页> 外文期刊>Thin-Walled Structures >Reverse ballistic experiment resembling the conditions in turbine blade off event for containment structures
【24h】

Reverse ballistic experiment resembling the conditions in turbine blade off event for containment structures

机译:反向弹道实验类似于安全壳结构的涡轮叶片脱落事件中的条件

获取原文
获取原文并翻译 | 示例
           

摘要

An experimental technique has been developed which allows loading of heated sheet material under impact conditions with simultaneous measurement of the impact force history. The combined characteristics of impact loading at elevated temperature makes the experiment ideal for validation of models used to simulate the containment structure surrounding aircraft engines. In this paper experimental results for Alloy 718 are presented, a nickel based super alloy commonly used in hot parts of the containment structure. The experimental results are then compared to simulations in order to validate previously calibrated material parameters. The basic principle of the validation experiment is based on reverse ballistics, in which a thin circular specimen with free boundaries impacts the end of an instrumented rod. Using induction heating the specimen is heated to temperatures up to 650 degrees C and a gun driven by compressed air accelerates the specimens to desired velocity. In the reported work velocities are kept low enough to avoid cracking and thus the study is limited to plastic conditions, even though the technique is applicable also for fracture studies. The free boundaries of the experiment makes numerical modelling and simulation straightforward, making it valuable as a validation tool. All numerical simulations are performed using the commercial finite element code LS-Dyna and plastic behaviour of the material was modelled with the Johnson-Cook material model. (C) 2016 Elsevier Ltd. All rights reserved.
机译:已经开发出一种实验技术,其允许在冲击条件下加载加热的片材,同时测量冲击力历史。高温下冲击载荷的综合特性使该实验成为验证用于模拟飞机发动机周围的安全壳结构的模型的理想选择。在本文中,提出了718合金的实验结果,这是一种常用于安全壳结构热部的镍基超级合金。然后将实验结果与模拟进行比较,以验证先前校准的材料参数。验证实验的基本原理是基于反向弹道技术,其中具有自由边界的薄圆形样本会影响仪器杆的末端。使用感应加热,将样品加热到高达650摄氏度的温度,由压缩空气驱动的喷枪将样品加速到所需的速度。在所报告的工作速度中,应保持足够低的速度以避免开裂,因此该研究仅限于塑性条件,即使该技术也可用于断裂研究。实验的自由边界使数值建模和仿真变得简单明了,使其作为验证工具非常有价值。所有数值模拟均使用商业有限元代码LS-Dyna进行,材料的塑性行为通过Johnson-Cook材料模型建模。 (C)2016 Elsevier Ltd.保留所有权利。

著录项

相似文献

  • 外文文献
  • 中文文献
  • 专利
获取原文

客服邮箱:kefu@zhangqiaokeyan.com

京公网安备:11010802029741号 ICP备案号:京ICP备15016152号-6 六维联合信息科技 (北京) 有限公司©版权所有
  • 客服微信

  • 服务号