容损机身的整体寿命管理

Darryl Toni, A. Sarlashkar, Sikorsky
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引用次数: 0

摘要

机身结构容损技术的进步与结构健康监测(SHM)相结合,为利用这些技术的协同作用改变未来飞机机身寿命管理的范式创造了机会。在过去的十年或更长的时间里,西科斯基已经使用损伤和缺陷容忍认证要求验证了多种生产直升机机身。本文作者的经验对旋翼机结构完整性计划(MIL-STD-3063中规定的RSIP)设计未来军用旋翼机的近期联合服务和工业发展做出了贡献。此外,西科斯基还开发了一系列与SHM相关的技术,以减少过度检查和维护,从而提高运营可用性。综合起来,这些发展将允许新的机身设计满足美国陆军对无维护运行期(MFOP)的新要求,例如未来垂直升力(FVL)旋翼机的200飞行小时。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
Holistic Life Management of Damage Tolerant Airframes
Advancements in Damage Tolerant Airframe Structures in combination with Structural Health Monitoring (SHM) have created an opportunity to exploit the synergies in these technologies to change the paradigm for Airframe Life Management for future Aircraft. In the last decade or more, Sikorsky has validated multiple production helicopter Airframes using Damage and Flaw Tolerant certification requirements. The experience of the authors of this paper contributed to the recent joint services and industry development of the Rotorcraft Structural Integrity Program (RSIP as specified in MIL-STD-3063) for design of future military rotorcraft. In addition, Sikorsky has also developed a range of technologies relevant to SHM to reduce over-inspection and maintenance to drive increased operational availability. Combined, these developments will allow new Airframe designs to meet the US Army's new requirements for Maintenance Free Operational Periods (MFOP), for example 200 flight hours for the Future Vertical Lift (FVL) rotorcraft.
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