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The physical simulations on meteorological conditions and standards, the surface simulation equipments and mothdologies involved in fight icing are reviewed. To meet the features of climate and types of aircraft in China, the principles to set the appropriate meteorological conditions for anti-icing system design, and experimental plans made for the typical freighter, helicopter and fighter are put forward. Combined with the domestic design and experiment of Icing Wind Tunnel(IWT), critical techniques are presented, e.g., its inner temperature, wind speed and the reproducing of the cloud and fog. During the experiments, a closed-loop controlled refrigerating system is employed to keep a low temperature condition, and a wind turbine system is used to generate airflow with high speed, and a fog spray system is applied to produce the artificial cloud, and the liquid water content and the cloud particle diameter can be controlled by adjusting the water pressure, the air pressure and the quantities of the operative nozzle. Further, the apparatuses and methods are discussed and compared for the correct observation on Liquid Water Content (LWC), Median Volume Diameter (MVD) and uniformity of the cloud and fog., authors=ZHENG Li1 , PENG Youxin1 , BU Xueqin2 , FENG Kang1 , authorsList=ZHENG Li;PENG Youxin;BU Xueqin;FENG Kang, authorCompany=1. Aviation Industry Corporation of China, Wuhan Aviation Instrument Corporation, Wuhan 430074, China;2. 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科技导报
| 研究论文 2013, 31(25): 26-31
飞机防冰系统设计中气象条件模拟及参数测量方法
全屏
郑莉1 , 彭又新1 , 卜雪琴2 , 冯康1
作者信息
1. 中国航空工业集团公司武汉航空仪表有限责任公司, 武汉 430074;2. 北京航空航天大学航空科学与工程学院, 北京 100191
Parameter Measurement Method and Physical Meteorology Simulation for Designing Anti-icing System of Aircraft
Affiliations
出版时间: 2013-09-08
doi: 10.3981/j.issn.1000-7857.2013.25.003
文章导航
飞机结冰的气象条件是防冰系统设计的重要依据。在综述国内外飞机结冰的气象条件及标准、气象参数地面模拟设备及模拟方法的基础上,针对中国气候特点及不同飞机类型,分析了防冰系统设计中气象条件的选取原则,给出了某型运输机、直升机、战斗机的典型试验条件。结合国内现有冰风洞的设计及试验经验,阐述了冰风洞气象条件的模拟方法:以闭环控制的制冷系统实现低温环境,以风扇动力系统模拟产生高速气流,以喷雾系统产生人工云,并通过调节喷雾水压、喷雾气压以及喷嘴开启个数实现对液态水含量和云雾粒子直径的控制;探讨了液态水含量、云雾粒子直径以及云雾均匀性等气象参数的测量方法。
飞机结冰
/
防冰系统
/
气象条件模拟
/
参数测量
The design of anti-icing system is in term of the meteorological conditions causing aircraft icing during flight. The physical simulations on meteorological conditions and standards, the surface simulation equipments and mothdologies involved in fight icing are reviewed. To meet the features of climate and types of aircraft in China, the principles to set the appropriate meteorological conditions for anti-icing system design, and experimental plans made for the typical freighter, helicopter and fighter are put forward. Combined with the domestic design and experiment of Icing Wind Tunnel(IWT), critical techniques are presented, e.g., its inner temperature, wind speed and the reproducing of the cloud and fog. During the experiments, a closed-loop controlled refrigerating system is employed to keep a low temperature condition, and a wind turbine system is used to generate airflow with high speed, and a fog spray system is applied to produce the artificial cloud, and the liquid water content and the cloud particle diameter can be controlled by adjusting the water pressure, the air pressure and the quantities of the operative nozzle. Further, the apparatuses and methods are discussed and compared for the correct observation on Liquid Water Content (LWC), Median Volume Diameter (MVD) and uniformity of the cloud and fog.
aircraft icing
/
anti-icing system
/
simulation of meteorological conditions
/
parameter measurement
郑莉;彭又新;卜雪琴;冯康.
飞机防冰系统设计中气象条件模拟及参数测量方法.
科技导报,
2013
, 31
(25)
: 26
-31
.
DOI: 10.3981/j.issn.1000-7857.2013.25.003
ZHENG Li;PENG Youxin;BU Xueqin;FENG Kang.
Parameter Measurement Method and Physical Meteorology Simulation for Designing Anti-icing System of Aircraft[J].
Science & Technology Review ,
2013
, 31
(25)
: 26
-31
.
DOI: 10.3981/j.issn.1000-7857.2013.25.003
2013年第31卷第25期
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文章信息
doi: 10.3981/j.issn.1000-7857.2013.25.003
接收时间:2013-02-25
首发时间:2013-09-08
出版时间:2013-09-08
收稿日期:2013-02-25
修回日期:2013-06-25
https://castjournals.cast.org.cn/joweb/kjdb/CN/10.3981/j.issn.1000-7857.2013.25.003
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2种不同金属材料的力学参数
科 Family 属数 Number of genus 种数 Number of species 占总种数比例 Percentage of total species (%) 属 Genus 种数 Number of species 占总种数比例 Percentage of total species (%) 鹅膏菌科Amanitaceae 2 11 5.26 鹅膏菌属 Amanita 10 4.78 小菇科 Mycenaceae 2 12 5.74 丝盖伞属 Inocybe 5 2.39 多孔菌科 Polyporaceae 8 14 6.70 蜡蘑属 Laccaria 5 2.39 红菇科 Russulaceae 3 23 11.00 小皮伞属 Marasmius 6 2.87 小菇属 Mycena 11 5.26 光柄菇属 Pluteus 5 2.39 红菇属 Russula 17 8.13 栓菌属 Trametes 5 2.39
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