Title:
SOLAR AIRPLANE STRUCTURE AND SOLAR CELL PLATE CONTROL METHOD
Document Type and Number:
WIPO Patent Application WO/2014/178503
Kind Code:
A1
Abstract:
A solar airplane with solar cell modules mounted in the wings includes: a first solar cell module arranged in the main wings or tail wings for receiving the solar energy directly from the sun; a second solar cell module arranged in the main wings or tail wings for receiving the directed energy transmitted from the earth; and a rotatable shaft for turning the first solar cell module and the second solar cell module facing opposite directions respectively. The first solar cell module in the upper part receives the solar energy from the sun, and the second solar cell module in the lower part the directed energy transmitted from the earth. The solar cell modules on both sides are turned so as to receive the energy as much as possible, and have improved durability because they are arranged inside the wings so as to be less affected by the environment during flying.
Inventors:
AHN HYO JUNG (KR)
Application Number:
PCT/KR2013/010343
Publication Date:
November 06, 2014
Filing Date:
November 14, 2013
Export Citation:
Assignee:
KOREA AEROSPACE RES INST (KR)
International Classes:
B64D41/00; B64C39/00; H01L31/042
Foreign References:
| KR101249645B1 | 2013-04-01 | |||
| US8356770B2 | 2013-01-22 | |||
| US20100102202A1 | 2010-04-29 | |||
| KR101114061B1 | 2012-02-21 |
Attorney, Agent or Firm:
SEAH INTERNATIONAL PATENT AND LAW FIRM (KR)
특허법인 세아 (KR)
특허법인 세아 (KR)
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