Aircraft intelligence power supply system

• Main Author: ZHANG YONGJUN
• Format: Patent
• Language: Chinese; English
• Published: 13.04.2018
• Subjects: AEROPLANES; AIRCRAFT; AVIATION; CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TOTRANSPORTATION; COSMONAUTICS; ELECTRIC EQUIPMENT OR PROPULSION OF ELECTRICALLY-PROPELLEDVEHICLES; ELECTRODYNAMIC BRAKE SYSTEMS FOR VEHICLES, IN GENERAL; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; HELICOPTERS; MAGNETIC SUSPENSION OR LEVITATION FOR VEHICLES; 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; VEHICLES IN GENERAL

The utility model relates to an aircraft intelligence power supply system, it includes that one end gives flexibility or rigidity feed cable that the heavy burden aircraft charges, is used for to liftlifting unmanned aerial vehicle and being used for lifting the flexibility or the afterbody of the rigidity feed cable other end unmanned aerial vehicle that charges of flexibility or rigidity feed cable, the afterbody charges unmanned aerial vehicle and is connected the other end of flexibility or rigidity feed cable and ground power supply electric wire netting electricity. Hung transfer universal joint, transfer universal joint lower extreme and be connected with the floating bearing on lifting unmanned aerial vehicle, the floating bearing lower extreme is connected with the circle of hanging that is used for lifting flexibility or rigidity feed cable. Hang the afterbody universal joint on the afterbody charges unmanned aerial vehicle, afterbody universal joint lower extreme is connected with the afterbody nod