Conceptual Design of an Energy System for High Altitude Airships Considering Thermal Effect
Autor: | Xiande Fang, Daoming Xing, Qiumin Dai, Yingjie Zhao |
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Rok vydání: | 2021 |
Předmět: |
Technology
Control and Optimization 020209 energy thermal-electric model Energy Engineering and Power Technology chemistry.chemical_element 02 engineering and technology high altitude airships energy system Altitude Conceptual design Thermal 0202 electrical engineering electronic engineering information engineering Electrical and Electronic Engineering Aerospace engineering Regenerative fuel cell Engineering (miscellaneous) Helium solar array Renewable Energy Sustainability and the Environment Payload business.industry Photovoltaic system 021001 nanoscience & nanotechnology Power (physics) chemistry Physics::Space Physics Environmental science Astrophysics::Earth and Planetary Astrophysics 0210 nano-technology business Energy (miscellaneous) |
Zdroj: | Energies, Vol 14, Iss 4204, p 4204 (2021) Energies; Volume 14; Issue 14; Pages: 4204 |
ISSN: | 1996-1073 |
DOI: | 10.3390/en14144204 |
Popis: | High altitude airships possess tremendous potential for long-endurance spot hovering platforms for both commercial and strategic applications. The energy system, which is mainly made up of solar array and regenerative fuel cell, is the key component of a high altitude airship. The thermal effect is a major factor that affects the performance of the energy system of long endurance stratospheric vehicles. In this paper, a conceptual design method focusing on the thermal and power characteristics of an energy system for stratospheric airships is proposed. The effect of thermal behavior of solar array on the energy system is analyzed. An optimized case is obtained on the consideration of power supply, thermal behaviors of helium and solar array. Results show that the maximum temperature difference of the solar array may be reduced by about 20 K and the mass of payload can be improved by up to 5%. |
Databáze: | OpenAIRE |
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