首页> 外国专利> METHOD OF FORMING MODELS FORECAST formation of condensation trails (COP) civilian aircraft (GA) with a particular type of gas turbine engines and condensation of cirrus clouds (KPO) using quantitative education indicators COP and KPO FOR ENVIRONMENTAL OPTIMIZATION plane flight GA on specific routes in different regions of the Earth and FEATURES reduce the impact of engine emissions on the greenhouse effect

METHOD OF FORMING MODELS FORECAST formation of condensation trails (COP) civilian aircraft (GA) with a particular type of gas turbine engines and condensation of cirrus clouds (KPO) using quantitative education indicators COP and KPO FOR ENVIRONMENTAL OPTIMIZATION plane flight GA on specific routes in different regions of the Earth and FEATURES reduce the impact of engine emissions on the greenhouse effect

机译:形成模型的方法使用定量教育指标COP和KPO预测特定类型的燃气轮机发动机的凝结痕迹(COP)民用飞机(GA)的形成和卷云(KPO)的凝结,以预测特定航线上的环境优化飞机飞行地球的不同区域和特征减少了发动机排放对温室效应的影响

摘要

FIELD: aircraft engineering.;SUBSTANCE: in cruising flight of aircraft with definite gas turbine engine the following parameters are measured: altitude, pressure, ambient air temperature and relative humidity, flight speed, full temperature of low-pressure turbine exhaust gases, rpm of one of engine rotors and fuel consumption. CT availability or absence is registered. For every preset altitude, calculated is total quantitative statistic of steam oversaturation at relative humidity of atmospheric air of 60% and equality of outside air and standard temperature. CT formation boundary height is calculated at different deviation of ambient air temperature from standard value and different magnitudes of relative humidity. Model for forecasting of CT and CFC formation and availability in preset lanes is constructed. Indications of heat effect change caused by CFC in preset lane sector at definite altitude are defined with allowance for density of air traffic.;EFFECT: higher accuracy of evaluation of ecological optimization of daily flights and peculiarities of atmospheric conditions at airliner cruising altitudes.;11 dwg
机译:领域:飞机工程;实质:在使用定型燃气涡轮发动机的飞机巡航飞行中,测量以下参数:高度,压力,环境空气温度和相对湿度,飞行速度,低压涡轮废气的全温度,之一是发动机转子和油耗。已记录CT的可用性或缺失。对于每个预设高度,在大气相对湿度为60%且外部空气与标准温度相等的情况下,将计算出蒸汽过饱和的总定量统计量。 CT地层边界高度是在环境空气温度与标准值的不同偏差和相对湿度的不同幅度下计算的。构建了用于预测预设车道中CT和CFC形成及可用性的模型。定义了在一定高度下预设车道区域中由CFC引起的热效应变化的指示,并考虑了空中交通密度。;效果:日常飞行生态优化和客机巡航高度的大气条件的特殊性评估的准确性更高; 11 dwg

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