Crashworthy subfloor structure with shock absorbers using fixed-to-hinged transforming joints and inward-folding composite tube filled with foam

Author:

Zhu Lingang1,Du Xin2,Yu Pu23,Yu Zhefeng2,Zhou Xiang2

Affiliation:

1. Shanghai Aircraft Design & Research Institute, Shanghai, China

2. School of Aeronautics and Astronautics, Aerospace Structure Research Center, Shanghai Jiao Tong University, Shanghai, China

3. Shanghai Aircraft Manufacturing Co., Ltd., Shanghai, China

Publisher

Informa UK Limited

Reference37 articles.

1. Advances in crash dynamics for aircraft safety

2. Research status and future development of crashworthiness of civil aircraft fuselage structures: An overview

3. Waimer M. Development of a kinematics model for the assessment of global crash scenarios of a composite transport aircraft fuselage. University of Stuttgart, Stuttgart, Baden-Württemberg, Germany; 2013.

4. Waimer M Dieter K Hachenberg D et al. The kinematics model – a numerical method for the development of a crashworthy composite fuselage design of transport aircraft in. 6th Triennial International Aircraft Fire and Cabin Safety Research Conference Atlantic City New Jersey USA; 2010.

5. Impact test and numerical simulation of typical sub-cargo fuselage section of civil aircraft

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