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公开(公告)号：US20210107644A1
公开(公告)日：2021-04-15
申请号：US16986661
申请日：2020-08-06
发明人： Longxue QIU , Xingwen WU
摘要： The present invention discloses an unmanned aerial vehicle including a main body, a plurality of arms, a propulsion assembly and a battery assembly, where each arm is coupled to the main body and the propulsion assembly is disposed on the each arm. The battery assembly is accommodated in a battery compartment of the main body. The battery assembly includes a shell, a battery body substantially disposed in the shell, a clamp button, and a restorable elastic piece. An end of the clamp button is mounted or connects to the shell, and the other end of the clamp button is detachably coupled to the main body. An end of the restorable elastic piece is disposed on the shell or connect to the shell, and the other end of the restorable elastic piece contacts the clamp button.
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公开(公告)号：US20180069218A1
公开(公告)日：2018-03-08
申请号：US15812860
申请日：2017-11-14
发明人： Longxue QIU , Xingwen WU
CPC分类号： H01M2/1083 , B64C39/024 , B64C2201/042 , B64C2201/06 , H01M2220/20
摘要： The present invention discloses an unmanned aerial vehicle and a battery thereof. The battery includes a battery body and a shell disposed on one end of the battery body. The shell has a clamp button disposed on the side opposite the unmanned aerial vehicle. One end of the clamp button is fixed on the shell and the other is used for detachably connecting with the unmanned aerial vehicle. The clamp button makes the battery detachably connect with the main body of the unmanned aerial vehicle be possible and it is very convenient for changing the battery.
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公开(公告)号：US20170338455A1
公开(公告)日：2017-11-23
申请号：US15671371
申请日：2017-08-08
发明人： Longxue QIU , Xingwen WU
CPC分类号： H01M2/1083 , B64C39/024 , B64C2201/042 , B64C2201/06 , H01M2220/20
摘要： The present invention discloses an unmanned aerial vehicle and a battery thereof. The battery includes a battery body and a shell disposed on one end of the battery body. The shell has a clamp button disposed on the side opposite the unmanned aerial vehicle. One end of the clamp button is fixed on the shell and the other is used for detachably connecting with the unmanned aerial vehicle. The clamp button makes the battery detachably connect with the main body of the unmanned aerial vehicle be possible and it is very convenient for changing the battery.
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公开(公告)号：US20220234718A1
公开(公告)日：2022-07-28
申请号：US17659683
申请日：2022-04-19
发明人： Longxue QIU
摘要： The embodiment is an unmanned aerial vehicle, including a body and wings. A first connection portion is disposed on one of the body and the wing. A second connection portion is disposed on the other of the body and the wing. The first connection portion and the second connection portion are detachably connected. The first connection portion is engaged with the second connection portion. The body and the wing are locked by rotating or sliding the second connection portion. The body can be conveniently assembled with or disassembled from the wing and the connection part meets the reliability of strength and rigidity and does not affect the flight performance.
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公开(公告)号：US20180292042A1
公开(公告)日：2018-10-11
申请号：US16004931
申请日：2018-06-11
发明人： Longxue QIU , Jiakun WANG , Zengfei WANG
CPC分类号： F16M11/041 , B64C39/024 , B64C2201/127 , B64D47/08 , F16M11/06 , F16M13/02 , F16M2200/025
摘要： A clamping apparatus includes a carrier portion formed on a regularly shaped panel, where a track slot is formed in a length direction in the carrier portion; a movable unit, mounted at an end of the carrier portion and capable of being separated from the carrier portion along a length direction of the track slot; and a clamping unit, mounted on a movable unit and configured to prevent, in at least four directions, a clamped object from being separated from the carrier portion. The problem that a size range of clamped objects applicable to the clamping apparatus is limited. The clamping unit is configured to prevent, in the at least four directions, the clamped object from being separated from the carrier portion, effectively preventing the clamped object from being separated from the carrier portion and allowing the clamped object to be protected even in a complex environment.
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公开(公告)号：US20170256763A1
公开(公告)日：2017-09-07
申请号：US15598914
申请日：2017-05-18
发明人： Longxue QIU , Xingwen WU
CPC分类号： H01M2/1083 , B64C39/024 , B64C2201/042 , B64C2201/06 , H01M2220/20
摘要： The present invention discloses an unmanned aerial vehicle and a battery thereof. The battery includes a battery body and a shell disposed on one end of the battery body. The shell has a clamp button disposed on the side opposite the unmanned aerial vehicle. One end of the clamp button is fixed on the shell and the other is used for detachably connecting with the unmanned aerial vehicle. The clamp button makes the battery detachably connect with the main body of the unmanned aerial vehicle be possible and it is very convenient for changing the battery.
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公开(公告)号：US20200001997A1
公开(公告)日：2020-01-02
申请号：US16565911
申请日：2019-09-10
发明人： Longxue QIU , Xingwen WU
摘要： The present invention discloses an unmanned aerial vehicle including a main body, a plurality of arms, a propulsion assembly and a battery assembly, where each arm is coupled to the main body and the propulsion assembly is disposed on the each arm. The battery assembly is accommodated in a battery compartment of the main body. The battery assembly includes a shell, a battery body substantially disposed in the shell, a clamp button, and a restorable elastic piece. An end of the clamp button is mounted or connects to the shell, and the other end of the clamp button is detachably coupled to the main body. An end of the restorable elastic piece is disposed on the shell or connect to the shell, and the other end of the restorable elastic piece contacts the clamp button.
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公开(公告)号：US20190100301A1
公开(公告)日：2019-04-04
申请号：US16193271
申请日：2018-11-16
发明人： Liangjun HU , Longxue QIU
摘要： The present invention provides a power assembly, including: a motor, a fixing base and a propeller. The fixing base is sleeved over a motor rotation shaft and is fastened to a base body of the motor, and the fixing base is provided with a first clamping portion. The propeller includes a base portion and a blade extending from the base portion, and the base portion is provided with a second clamping portion clamped to the first clamping portion. The propeller is detachably connected to the motor by engaging the first clamping portion with the second clamping portion, so that the propeller can be effectively prevented from loosening from the motor during the vibration or acceleration, and is easy to disassemble/assemble and carry.
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公开(公告)号：US20190071180A1
公开(公告)日：2019-03-07
申请号：US16180520
申请日：2018-11-05
发明人： Longxue QIU , Xingwen WU
CPC分类号： B64C39/024 , B64C25/08 , B64C27/50 , B64C2201/027 , B64C2201/042 , B64C2201/145 , B64D27/24 , H01M2/1083 , H01M2220/20
摘要： The present invention discloses an unmanned aerial vehicle including a main body, a plurality of arms, a propulsion assembly and a battery assembly, where each arm is coupled to the main body and the propulsion assembly is disposed on the each arm. The battery assembly is accommodated in a battery compartment of the main body. The battery assembly includes a shell, a battery body substantially disposed in the shell, a clamp button, and a restorable elastic piece. An end of the clamp button is mounted or connects to the shell, and the other end of the clamp button is detachably coupled to the main body. An end of the restorable elastic piece is disposed on the shell or connect to the shell, and the other end of the restorable elastic piece contacts the clamp button.
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10.发明申请公开(公告)号：US20180237158A1
公开(公告)日：2018-08-23
申请号：US15958530
申请日：2018-04-20
发明人： Zhiying LIANG , Longxue QIU
CPC分类号： B64D47/08 , B64C39/02 , B64C39/024 , B64C2201/02 , B64C2201/127 , F16M11/041 , F16M13/02 , G03B15/006 , G03B17/561
摘要： The present application provides a gimbal quick assembly/disassembly apparatus and an unmanned aerial vehicle having the same. The gimbal quick assembly/disassembly apparatus includes a fuselage seat component, a gimbal seat component and a locking component. The fuselage seat component is fixedly mounted on a bearing member, the gimbal seat component is fixedly mounted on a gimbal and the gimbal seat component includes a gimbal seat. The locking component is mounted on the fuselage seat component or on the gimbal seat component and the gimbal seat component and the fuselage seat component are detachably mounted together by using the locking component. The gimbal is detachably mounted on the unmanned aerial vehicle, resolving problems of complex assembled/disassembled operations and low efficiency that are caused when the gimbal is fixedly mounted on the unmanned aerial vehicle and realizing quick assembly/disassembly of the gimbal to/from the unmanned aerial vehicle.
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