Specific weight: A challenge for a fuel-cell-powered electric helicopter

被引：0
|
作者：
Guinea, D.M. [1 ,4 ]
Roura, M. [2 ,5 ]
Garciáa-Alegre, M.C. [3 ,6 ]
Ribeiro, A. [3 ,6 ]
Guinea, D. [3 ,6 ]
机构：
[1] Ceramics and Glass Institute, 28049 Madrid, Spain
[2] Politechnical University, 28040 Madrid, Spain
[3] Industrial Automation Institute, Arganda, 28500 Madrid, Spain
[4] Glass Department, Spanish Council for Scientific Research, Calle Kelsen, 5, Spain
[5] Instituto Universitario de Microgravedad Ignacio da Riva, Universidad Politeácnica de Madrid, Technical School of Aeronautical Engineers, Plaza del Cardenal Cisneros 3, Spain
[6] Systems Department, Spanish Council for Scientific Research, Carretera de Campo Real, kilometre 0.2, Spain
来源：
Journal of Aircraft | 1600年 / 44卷 / 06期
关键词：
The specific weight; or weight/power ratio; is a very important factor for a fuel-cell-powered helicopters. The objective of determining the specific weight is to analyze whether or not fuel cells are appropriate for the power electric helicopters. The helicopter specific-weight is obtained by the measurement of the variables including helicopter current; voltage; and lifting force. Current and voltage are required for the derivation of the electrical power consumption; and the lifting force is required to know the maximum weight of the required fuel cell. Analysis of the three recorded input variables such as voltage; current; and lifting force is performed by a computer algorithm under different conditions including payload and safety. The analysis demonstrates that the lower fuel-cell specific weights are safer as they have the higher probability of lifting the helicopter as well as heavy payloads successfully;
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摘要：
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页码：2073 / 2076
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