Can be in case electronic single rotor unmanned aerial vehicle of crash

• Main Authors: QI BING, YU JUN
• Format: Patent
• Language: Chinese; English
• Published: 12.04.2017
• Subjects: AEROPLANES; AIRCRAFT; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT; AVIATION; CIRCUIT ARRANGEMENTS OR SYSTEMS FOR SUPPLYING OR DISTRIBUTINGELECTRIC POWER; CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TOTRANSPORTATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER; COSMONAUTICS; ELECTRICITY; 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; GENERATION; HELICOPTERS; PARACHUTES; PERFORMING OPERATIONS; SYSTEMS FOR STORING ELECTRIC ENERGY; 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 can be in case electronic single rotor unmanned aerial vehicle of crash, including organism, signal receiver, turncap, sound pressure sensor, acceleration sensor, signal transmission ware, remote switch and directional control button, plastic window is installed in the organism left side, and installs signal receiver on the left of the plastic window below, the flabellum is installed to signal receiver right side top, and installs the turncap on the left of the flabellum below, solar cell panel is installed in turncap below left side, and installs sound pressure sensor below the solar cell panel right side, sound pressure sensor installs the parachute at below left side, and parachute below right side installs acceleration sensor, the support frame is installed to acceleration sensor left side top, and the shaft is installed to support frame left side below. The utility model discloses an install solar cell panel in organism right side top to can follow the duration who improves