The invention belongs to a structural
impact dynamics experimental technology, and particularly relates to an experiment apparatus and an experiment method for the
dynamic energy absorption characteristic of an arresting
system. EMAS is a safety facility for blocking the safety
hazard caused by the running of the large aircraft out of the
runway and is spread at the end of the airport
runway, andthe predictable blocking resistance can be produced for the aircraft through the aircraft wheel rolling material, such that the aircraft can reduce the speed and stay in the safe area under the premise of the safety so as to ensure the structure of the aircraft and the safety of the occupants. The invention provides an experiment test method for performing
dynamic energy absorption characteristicsof EMAS, and designs a special experiment table frame for researching the influence of the type of an
aircraft landing gear wheel, the vertical loading state of the wheel, the wheel rotation speed and other parameters on the arresting load of EMAS. According to the present invention, the support can be provided for the research and development of the emergency arresting
system at the ends of
civil aviation and military airport runways, the real aircraft
verification experiment of the rushing of the real aircraft into the EMAS material can be partially replaced, and the apparatus and the method have advantages of economy, high efficiency, strong
operability, wider application prospect and the like.