Dual-rotor unmanned aerial vehicle

The embodiment of the invention discloses a dual-rotor unmanned aerial vehicle, which comprises a vehicle body, coaxial dual rotors, fixed wings, two tilting ducted fans and a hybrid power system, wherein the coaxial dual rotors are arranged at the top of the vehicle body, the two tilting ducted fan...

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Hauptverfasser:	ZHANG YUZHOU, BU JIANGUO, FENG GUANGSHUO, LI HAOYU, YAN HUIHUI, LAN XUDONG, WANG CAIZHENG, LI HAO, ZHOU MING, LI CHUNHUI
Format:	Patent
Sprache:	chi ; eng
Schlagworte:	AEROPLANES AIRCRAFT ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT AVIATION COSMONAUTICS EQUIPMENT FOR FITTING IN OR TO AIRCRAFT FLYING SUITS HELICOPTERS PARACHUTES PERFORMING OPERATIONS TRANSPORTING
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creator	ZHANG YUZHOU BU JIANGUO FENG GUANGSHUO LI HAOYU YAN HUIHUI LAN XUDONG WANG CAIZHENG LI HAO ZHOU MING LI CHUNHUI
description	The embodiment of the invention discloses a dual-rotor unmanned aerial vehicle, which comprises a vehicle body, coaxial dual rotors, fixed wings, two tilting ducted fans and a hybrid power system, wherein the coaxial dual rotors are arranged at the top of the vehicle body, the two tilting ducted fans are symmetrically arranged on the two sides of the vehicle body through the fixed wings, and the hybrid power system is arranged in the vehicle body. The hybrid power system is connected with the coaxial dual rotors and the tilting ducted fan so as to drive the coaxial dual rotors and the tilting ducted fan, and the tilting ducted fan can rotate around the vehicle body under driving of the hybrid power system. The coaxial dual rotors and the ducted fan can be adjusted according to actual conditions, so that vertical take-off and landing and horizontal flight of the unmanned aerial vehicle are completed, flight resistance of the unmanned aerial vehicle is reduced, the voyage of the unmanned aerial vehicle is impro
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The hybrid power system is connected with the coaxial dual rotors and the tilting ducted fan so as to drive the coaxial dual rotors and the tilting ducted fan, and the tilting ducted fan can rotate around the vehicle body under driving of the hybrid power system. 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The hybrid power system is connected with the coaxial dual rotors and the tilting ducted fan so as to drive the coaxial dual rotors and the tilting ducted fan, and the tilting ducted fan can rotate around the vehicle body under driving of the hybrid power system. The coaxial dual rotors and the ducted fan can be adjusted according to actual conditions, so that vertical take-off and landing and horizontal flight of the unmanned aerial vehicle are completed, flight resistance of the unmanned aerial vehicle is reduced, the voyage of the unmanned aerial vehicle is impro</description><subject>AEROPLANES</subject><subject>AIRCRAFT</subject><subject>ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT</subject><subject>AVIATION</subject><subject>COSMONAUTICS</subject><subject>EQUIPMENT FOR FITTING IN OR TO AIRCRAFT</subject><subject>FLYING SUITS</subject><subject>HELICOPTERS</subject><subject>PARACHUTES</subject><subject>PERFORMING OPERATIONS</subject><subject>TRANSPORTING</subject><fulltext>true</fulltext><rsrctype>patent</rsrctype><creationdate>2021</creationdate><recordtype>patent</recordtype><sourceid>EVB</sourceid><recordid>eNrjZFByKU3M0S3KL8kvUijNy03My0tNUUhMLcpMzFEoS83ITM5J5WFgTUvMKU7lhdLcDIpuriHOHrqpBfnxqcUFicmpeakl8c5-hoZGFoYGFoaGjsbEqAEAqW0l5A</recordid><startdate>20210518</startdate><enddate>20210518</enddate><creator>ZHANG YUZHOU</creator><creator>BU JIANGUO</creator><creator>FENG GUANGSHUO</creator><creator>LI HAOYU</creator><creator>YAN HUIHUI</creator><creator>LAN XUDONG</creator><creator>WANG CAIZHENG</creator><creator>LI HAO</creator><creator>ZHOU MING</creator><creator>LI CHUNHUI</creator><scope>EVB</scope></search><sort><creationdate>20210518</creationdate><title>Dual-rotor unmanned aerial vehicle</title><author>ZHANG YUZHOU ; BU JIANGUO ; FENG GUANGSHUO ; LI HAOYU ; YAN HUIHUI ; LAN XUDONG ; WANG CAIZHENG ; LI HAO ; ZHOU MING ; LI CHUNHUI</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-epo_espacenet_CN112810811A3</frbrgroupid><rsrctype>patents</rsrctype><prefilter>patents</prefilter><language>chi ; eng</language><creationdate>2021</creationdate><topic>AEROPLANES</topic><topic>AIRCRAFT</topic><topic>ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT</topic><topic>AVIATION</topic><topic>COSMONAUTICS</topic><topic>EQUIPMENT FOR FITTING IN OR TO AIRCRAFT</topic><topic>FLYING SUITS</topic><topic>HELICOPTERS</topic><topic>PARACHUTES</topic><topic>PERFORMING OPERATIONS</topic><topic>TRANSPORTING</topic><toplevel>online_resources</toplevel><creatorcontrib>ZHANG YUZHOU</creatorcontrib><creatorcontrib>BU JIANGUO</creatorcontrib><creatorcontrib>FENG GUANGSHUO</creatorcontrib><creatorcontrib>LI HAOYU</creatorcontrib><creatorcontrib>YAN HUIHUI</creatorcontrib><creatorcontrib>LAN XUDONG</creatorcontrib><creatorcontrib>WANG CAIZHENG</creatorcontrib><creatorcontrib>LI HAO</creatorcontrib><creatorcontrib>ZHOU MING</creatorcontrib><creatorcontrib>LI CHUNHUI</creatorcontrib><collection>esp@cenet</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>ZHANG YUZHOU</au><au>BU JIANGUO</au><au>FENG GUANGSHUO</au><au>LI HAOYU</au><au>YAN HUIHUI</au><au>LAN XUDONG</au><au>WANG CAIZHENG</au><au>LI HAO</au><au>ZHOU MING</au><au>LI CHUNHUI</au><format>patent</format><genre>patent</genre><ristype>GEN</ristype><title>Dual-rotor unmanned aerial vehicle</title><date>2021-05-18</date><risdate>2021</risdate><abstract>The embodiment of the invention discloses a dual-rotor unmanned aerial vehicle, which comprises a vehicle body, coaxial dual rotors, fixed wings, two tilting ducted fans and a hybrid power system, wherein the coaxial dual rotors are arranged at the top of the vehicle body, the two tilting ducted fans are symmetrically arranged on the two sides of the vehicle body through the fixed wings, and the hybrid power system is arranged in the vehicle body. The hybrid power system is connected with the coaxial dual rotors and the tilting ducted fan so as to drive the coaxial dual rotors and the tilting ducted fan, and the tilting ducted fan can rotate around the vehicle body under driving of the hybrid power system. The coaxial dual rotors and the ducted fan can be adjusted according to actual conditions, so that vertical take-off and landing and horizontal flight of the unmanned aerial vehicle are completed, flight resistance of the unmanned aerial vehicle is reduced, the voyage of the unmanned aerial vehicle is impro</abstract><oa>free_for_read</oa></addata></record>
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subjects	AEROPLANES AIRCRAFT ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT AVIATION COSMONAUTICS EQUIPMENT FOR FITTING IN OR TO AIRCRAFT FLYING SUITS HELICOPTERS PARACHUTES PERFORMING OPERATIONS TRANSPORTING
title	Dual-rotor unmanned aerial vehicle
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