A Simulation Analysis Method for Emergency Evacuation of Blended Wing-Body (BWB) Passenger Aircraft

Abstract

This invention relates to a simulation analysis method for emergency evacuation of blended wing-body (BWB) passenger aircraft, comprising: constructing a sudden accident scenario and risk evolution model for the passenger aircraft; determining the emergency evacuation simulation experimental conditions; and building a simulation environment. A three-dimensional model of the BWB passenger aircraft is established and imported into Anylogic simulation software to construct a realistic emergency evacuation module for BWB aircraft personnel, and a personnel emergency evacuation behavior model is established using the simulation software. Based on the simulation environment, the realistic emergency evacuation module, and the personnel emergency evacuation behavior model, a simulation of emergency evacuation of BWB aircraft personnel is conducted to obtain the risk factors and weaknesses existing in the emergency evacuation process. This invention provides a convenient, fast, low-investment, and highly feasible method for verifying and analyzing the relevant layout design of future new BWB passenger aircraft, providing data support for the design of this type of aircraft.

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