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空中受油装置折断安全风险分析

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加油机与受油机在空中对接时,加油伞锥与受油装置可能发生碰撞,导致受油装置折断落入受油机发动机而严重影响飞行安全.通过有限元数值仿真计算方法探究了受油装置折断的边界条件,并建立了受油过程中折断物体在飞机尾流和自身重力作用下飘落的运动轨迹计算模型,并采用蒙特卡洛随机抽样的方法,分析折断物落入发动机的概率,评估受油装置的折断风险及其影响范围.可对加油机与受油机的空中对接安全性分析提供参考和借鉴.
Safety Risk Analysis of Air Oil Receiving Device Breakage
When the refueling aircraft and the receiving aircraft are docked in the air,the refueling parachute cone may collide with the receiving device,causing the receiving device to break and fall into the receiving aircraft engine,seriously affecting flight safety.This article explores the boundary conditions for the fracture of the oil receiving device through finite element numerical simulation cal-culation method,and establishes a calculation model for the motion trajectory of the fractured object falling under the influence of the aircraft wake and its own gravity during the oil receiving process.Monte Carlo random sampling method is used to analyze the probability of the fractured object fall-ing into the engine,evaluate the fracture risk and its impact range of the oil receiving device.This study can provide reference and inspiration for the safety analysis of aerial docking between refueling aircraft and receiving aircraft.

aerial refuelingoil receiving devicesafety risk analysisfinite element method

王凯、党双欢、李玉芳、刘康

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西安飞机工业集团股份有限公司,陕西西安 710086

空中加油 受油装置 安全风险分析 有限元

2024

飞机设计
沈阳飞机设计研究所

飞机设计

影响因子:0.138
ISSN:1673-4599
年,卷(期):2024.44(5)