Phenomena of Foamed Concrete under Rolling of Aircraft Wheels

2014 International Conference on Science & Engineering in Mathematics, Chemistry and Physics

数学;化学;物理学

Jiang, Chun-Shui^1 ; Yao, Hong-Yu^1 ; Xiao, Xian-Bo^1 ; Kong, Xiang-Jun^1 ; Shi, Ya-Jie^1

China Academy of Civil Aviation Science and Technology, Xibahe Beili #24, Chaoyang District, Beijing, 100028, China^1

关键词: Aircraft wheels;    Boeing 737;    Design concept;    Engineered materials;    Foamed concrete;    Pure rolling;    Tire pressure;    Vertical load;   

Others  :  https://iopscience.iop.org/article/10.1088/1742-6596/495/1/012035/pdf
DOI  :  10.1088/1742-6596/495/1/012035

来源: IOP

【 摘 要 】

Engineered Material Arresting System (EMAS) is an effective technique to reduce hazards associated with aircraft overrunning runway. In order to ascertain phenomena of the foamed concrete used for EMAS under rolling of aircraft wheel, a specially designed experimental setup was built which employed Boeing 737 aircraft wheels bearing actual vertical loads to roll through the foamed concrete. A number of experiments were conducted upon this setup. It is discovered that the wheel rolls the concrete in a pure rolling manner and crushes the concrete downwards, instead of crushing it forward, as long as the concrete is not higher than the wheel axle. The concrete is compressed into powder in-situ by the wheel and then is brought to bottom of the wheel. The powder under the wheel is loose and thus is not able to sustain wheel braking. It is also found that after being rolled by the wheel the concrete exhibits either of two states, i.e. either 'crushed through' whole thickness of the concrete or 'crushed halfway', depending on combination of strength of the concrete, thickness of the concrete, vertical load the wheel carries, tire dimension and tire pressure. A new EMAS design concept is developed that if an EMAS design results in the 'crushed through' state for the main gears while the 'crushed halfway' state for the nose gear, the arresting bed would be optimal to accommodate the large difference in strength between the nose gear and the main gear of an aircraft.