基于某低空飞艇压力高度及载荷能力的研究

由于大气压力、温度随着海拔高度的变化而变化.在飞艇升降过程中,艇囊中的浮升气体(氦气)随着外界大气压力、温度的变化产生压缩或膨胀,使飞艇净静升力发生变化,从而影响了飞艇的载荷能力和能够达到的海拔高度.为了在标准大气(International Standard Atmosphere)和非标准大气(Off-Standard Atmosphere)条件下,研究了飞艇压力高度随充氦体积变化规律和载荷能力随高度变化的规律,给出了充氦体积占飞艇总气囊体积比例、压力高度、净静升力和有效载荷之间的变化关系,并结合某低空试验飞艇进行了仿真计算和分析,为飞艇的总体设计和实际使用提供了理论基础.

Research on Pressure Height and Load Capability of Low-Altitude Airship

Atmospheric pressure and temperature vary with the altitude,so during the airship's ups and downs the helium in its gasbag compresses and inflates with the atmospheric pressure and temperature,then make the net static lift change,thus influencing the airship's load capability and its height.Under the conditions of both International Standard Atmosphere and Off-Standard Atmosphere,this paper researched on the rules that the pressure height varies with the filling helium volume and rules that the load capabil...