Detachable solar cell panel four shaft air vehicle

• Main Authors: LI XIAOLONG, YUAN QIANHUI, TAO ZEXU, CAI ZHIHUA, WANG LIBIN, WANG QING, YANG ZHIJIE, YAN HAILONG, YANG HUA
• Format: Patent
• Language: English
• Published: 28.10.2015
• Subjects: AEROPLANES; AIRCRAFT; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT; AVIATION; CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TOTRANSPORTATION; COSMONAUTICS; EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLYING SUITS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; HELICOPTERS; PARACHUTES; PERFORMING OPERATIONS; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS; TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINSTCLIMATE CHANGE; TRANSPORTING

The utility model discloses a detachable solar cell panel four shaft air vehicle, its structural feature is: solar cell panel attaches to kt backup pad surface, and carbon fiber pressure bears an upper end and bears solar cell panel and kt backup pad, and lower extreme and carbon fiber triangular pyramid horn are connected, and a motor is respectively installed to two ends about carbon fiber triangular pyramid horn, is connected with the screw on the motor, carbon fiber pressure bears a centre and studs with solar energy constant voltage power supply and buffer memory group, and the undercarriage is connected to solar energy constant voltage power supply and buffer memory group lower extreme. The utility model has the beneficial effects of: (1 )Carry out unmanned monitoring aloft, survey and the field of listening has extensive application on the spot, (2 )Adopt the GPS locater can fix a point to fix a position for communicate transportation fields such as express delivery, (3 )When having zero release solar drive, good flight performance, low cost, long boat, usage advantage such as wide.