Development of strain-life based fatigue design methodology for landing gear components

开发起落架部件基于应变寿命的疲劳设计方法

• 批准号: 469182-2014
• 负责人: Fawaz, Zouheir
• 金额: $ 0.91万
• 依托单位: Ryerson University
• 依托单位国家: 加拿大
• 项目类别: Engage Plus Grants Program
• 财政年份: 2014
• 资助国家: 加拿大
• 起止时间: 2014-01-01 至 2015-12-31
• 项目状态: 已结题
• 来源: https://www.nserc-crsng.gc.ca/ase-oro/Details-Detailles_eng.asp?id=563325
• 关键词: Development; strain; life; based; fatigue

This is the continuation of a research effort supported initially by an Engage grant in partnership with SPP Canada Aircraft (SPPCA). The multiple phase project described in the initial proposal has progressed extremely well and the research already completed have uncovered potential research areas into fatigue phenomena that may be investigated further as the testing progresses. The Engage Plus will support both the continuation of the first two phases of the project, as described in the original Engage grant proposal, as well as additional variable amplitude tests that will be completed to verify the applicability of the developed fatigue methodology, leading to the development of new software based on a more enhanced version of strain-life fatigue (third phase). The first month of the Engage Plus project will be dedicated to the completion of

这是与SPP加拿大飞机（SPPCA）合作，最初由订单赠款支持的研究工作的延续。初始提案中描述的多个阶段项目进展非常好，并且已经完成的研究已经发现了潜在的研究领域，这些研究领域可能会随着测试的进行进一步研究。正如原始参与赠款提案中所述，GAND PLUS将支持该项目的前两个阶段的延续，以及将完成的其他可变幅度测试，以验证开发的疲劳方法的适用性，从而根据应变寿命疲劳（第三阶段）基于更增强的新软件开发新软件。参与Plus项目的第一个月将致力于完成