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Numerical study on the impact response of aircraft fuselage structures subjected to large-size tire fragment
Science Progress ( IF 2.6 ) Pub Date : 2019-09-27 , DOI: 10.1177/0036850419877744
Senqing Jia 1 , Fusheng Wang 1 , Lingjun Yu 2 , Zheng Wei 1 , Bin Xu 1
Affiliation  

With the starts of large-scale civil aircraft project, the development of new fuselage structure is an effective means to improve fuselage life, economy, safety, comfort, and reliability of large passenger aircraft. Aircraft tire is a very important component which requires high safety and reliability. The safe taking off and landing of aircraft must be accomplished by the unique functions of aviation tire.1 The relevant data show that accident rate caused by aircraft tire bursting is the highest in all influential factors of aviation accidents, for example, the Douglas DC-10 and Boeing B747 both have experienced serious accidents due to tire bursting. The famous supersonic Concorde aircraft also has experienced accident crash caused by tire bursting. In 2004, the CRJ200 overran the runway due to the brake failure caused by tire bursting.2

中文翻译:

大尺寸轮胎碎片冲击下飞机机身结构响应数值研究

随着大型民机项目的启动,新型机身结构的研制是提高大型客机机身寿命、经济性、安全性、舒适性、可靠性的有效手段。飞机轮胎是一个非常重要的部件,对安全性和可靠性要求很高。飞机的安全起降必须依靠航空轮胎的独特功能来完成。1相关数据显示,在所有航空事故影响因素中,飞机爆胎引起的事故发生率最高,例如道格拉斯 DC-10 和波音 B747 都曾发生过因爆胎而发生的严重事故。著名的超音速协和式飞机也曾发生过因轮胎爆裂而导致的坠毁事故。2004年,CRJ200因轮胎爆裂导致刹车失灵冲出跑道。2
更新日期:2020-04-10
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