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AIR1609A
(R) Aircraft Humidification
(R) Aircraft Humidification
0001-01-01
有效
【范围】 This SAE Aerospace Information Report (AIR) covers the design parameters for various methods of humidification applicable to aircraft, the physiological aspects of low humidities, the possible benefits of controlling cabin humidity, the penalties associated with humidification, and the problems which must be solved for practical aircraft humidification systems. The design information is applicable to commercial and military aircraft. The physiological aspects cover all aircraft environmental control applications. 1.1 Purpose: The purpose of this AIR is to provide guidelines for the design of aircraft humidification systems. Physiological effects of humidity levels on crew and passengers are reviewed. Various techniques used for cabin humidification are discussed and evaluated. Various technical issues are addressed, and effects associated with humidification systems are described.strRefField
【与前一版的变化】

替代标准

引用文件/被引文件

The Control of Excess Humidity in Avionics Cooling
Control of Water Carryover from the Environmental Control System and Condensation on the Structure
Aerospace Applied Thermodynamics Manual

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包含图表

formula 1
Moisture Loss from t
formula 2
formula 3
Water Requirements f
Total Dissolved Soli

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