直升机动力舱灭火剂浓度地面试验进气流量数值与试验研究

Numerical and experimental study on inflow rates for ground testing of fire extinguishing agent concentration in helicopter engine nacelles

  • 摘要: 民用直升机动力舱灭火剂浓度测试是重要的适航验证试验,该类试验验证长期依赖飞行试验,存在风险高、试飞费用高、改装幅度大、周期长等问题。本研究结合国内某直升机型号研制,在国内首次开展了地面模拟试验验证,对地面模拟试验的输入空气流量数值进行比对标定,依据飞行试验数据给定地面灭火剂浓度试验条件,最终通过地面模拟试验表明符合性。试验中,在精准模拟直升机空中流量与温度环境基础上,确定了空速管测量方式与流量计算方法,提供了地面模拟试验空气流量输入条件。地面模拟根据飞行数据确定飞行试验最大临界工况,并据此确认了灭火剂浓度分布情况地面模拟试验空气流量输入条件。

     

    Abstract: The fire extinguishing agent concentration test in civil helicopter engine nacelles is a critical airworthiness verification test. Such testing has long relied on flight tests, which face challenges including high risks, high flight test costs, substantial modifications, and prolonged cycles. Addressing the development of a domestic helicopter model, this study pioneered a ground simulation test in China. By comparing and calibrating the input airflow values for ground simulation against flight test data, the test conditions for agent concentration were established, ultimately demonstrating airworthiness compliance through ground-based testing. The ground simulation accurately replicated the in-flight airflow and temperature environment of the helicopter. It determined the pitot tube measurement method and airflow calculation approach, providing precise input conditions for the ground test. Based on flight test data, the simulation identified the maximum critical operating conditions encountered during flight tests, thereby defining the input airflow parameters for evaluating the fire extinguishing agent distribution in ground-based testing.

     

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