CN207225651U - A kind of unmanned plane wing safeguard structure - Google Patents

A kind of unmanned plane wing safeguard structure Download PDF

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Publication number
CN207225651U
CN207225651U CN201720949236.9U CN201720949236U CN207225651U CN 207225651 U CN207225651 U CN 207225651U CN 201720949236 U CN201720949236 U CN 201720949236U CN 207225651 U CN207225651 U CN 207225651U
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CN
China
Prior art keywords
unmanned plane
wing
cavity
connecting rod
safeguard structure
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Application number
CN201720949236.9U
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Chinese (zh)
Inventor
李晓岚
安明慧
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
SHENZHEN KUNONG UAV INDUSTRIAL DEVELOPMENT AND APPLICATION Co.,Ltd.
Xihua Jiuxiang UAV Industrial Park Operation Co.,Ltd.
Original Assignee
Henan Cool Agricultural Aviation Plant Protection Technology Co Ltd
Shenzhen Agricultural Uav Industrial Development And Application Co Ltd
Xihua Cool Agricultural Uav Industrial Park Operation Co Ltd
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Henan Cool Agricultural Aviation Plant Protection Technology Co Ltd, Shenzhen Agricultural Uav Industrial Development And Application Co Ltd, Xihua Cool Agricultural Uav Industrial Park Operation Co Ltd filed Critical Henan Cool Agricultural Aviation Plant Protection Technology Co Ltd
Priority to CN201720949236.9U priority Critical patent/CN207225651U/en
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Publication of CN207225651U publication Critical patent/CN207225651U/en
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Abstract

A kind of unmanned plane wing safeguard structure of the utility model, including unmanned plane body, it is characterised in that:1 cavity is each provided with four angles of the unmanned plane body;The cavity inside is respectively provided with 1 wing;1 motor is respectively connected with below the wing;The lower end of the motor is fixedly connected with connecting rod;The connecting rod is fixed on cavity upper surface described on unmanned plane body and is each provided with 1 cover body with lower face and is connected through a screw thread;The cover body is in net structure;Not only the safe handling of wing can have been protected, but also has solved safety problem caused by wing bumps against object, has had the advantages that coefficient simple in structure, easy to use, safe is high, protecting effect is good.

Description

A kind of unmanned plane wing safeguard structure
Technical field
The utility model belongs to unmanned air vehicle technique field, and in particular to a kind of unmanned plane wing safeguard structure.
Background technology
In recent years, unmanned plane is subject to more and more with its simple structure, convenient manipulation and higher security features People pursue.The wing of existing unmanned plane it is general it is exposed on the one hand presence can cause wing to come to a halt other objects outside, Cause easily to damage, influence to fly;On the other hand, come to a halt people there are possibility, cause safety problem.
The content of the invention
The purpose of the utility model is to overcome the deficiencies in the prior art, and offer one kind is simple in structure, safety coefficient is high, Protecting effect good unmanned plane wing safeguard structure.
The technical solution of the utility model is:A kind of unmanned plane wing safeguard structure, including unmanned plane body, its feature It is:1 cavity is each provided with four angles of the unmanned plane body;The cavity inside is respectively provided with 1 wing;Institute 1 motor is respectively connected with below the wing stated;The lower end of the motor is fixedly connected with connecting rod;The connecting rod is fixed On unmanned plane body;
The cavity upper surface is each provided with 1 cover body with lower face and is connected through a screw thread;The cover body is in Net structure.
The net structure forms for stainless steel wire welding distribution arrangement.
The net structure is formed for nylon rope is mutually interspersed.
Beneficial effect is caused by this programme:The utility model can not only protect the safe handling of wing, but also solve Wing bumps against safety problem caused by object, and it is excellent to have that simple in structure, coefficient easy to use, safe is high, protecting effect is good Point.
Brief description of the drawings
Fig. 1 is the structure diagram of the utility model.
Fig. 2 is the part-structure schematic diagram of the utility model.
Fig. 3 is the side structure schematic diagram of the utility model.
In figure:1st, unmanned plane body 2, cavity 3, wing 4, motor 5, connecting rod 6, cover body 7, netted Structure.
Embodiment:
The technical solution of the utility model is described further below in conjunction with the accompanying drawings.
As shown in Fig. 1-3:A kind of unmanned plane wing safeguard structure, including unmanned plane body 1, it is characterised in that:It is described Unmanned plane body 1 four angles on be each provided with 1 cavity 2;1 wing 3 is respectively provided with inside the cavity 2;Described Wing 3 is respectively connected with 1 motor 4 below;The lower end of the motor 4 is fixedly connected with connecting rod 5;The connecting rod 5 is solid It is scheduled on 1 on unmanned plane body;
2 upper surface of cavity is each provided with 1 cover body 6 with lower face and is connected through a screw thread;The cover body 6 be in net structure 7.
The net structure 7 forms for stainless steel wire welding distribution arrangement.
The net structure 7 is formed for nylon rope is mutually interspersed.
Unmanned plane can protect the safe handling of wing using such a wing protection structure, and solve wing and bump against object Caused by safety problem, have the advantages that coefficient simple in structure, easy to use, safe is high, protecting effect is good.

Claims (3)

1. a kind of unmanned plane wing safeguard structure, including unmanned plane body, it is characterised in that:The four of the unmanned plane body 1 cavity is each provided with a angle;The cavity inside is respectively provided with 1 wing;1 electricity is respectively connected with below the wing Machine;The lower end of the motor is fixedly connected with connecting rod;The connecting rod is fixed on unmanned plane body;
The cavity upper surface is each provided with 1 cover body with lower face and is connected through a screw thread;The cover body is in netted Structure.
A kind of 2. unmanned plane wing safeguard structure according to claim 1, it is characterised in that:The net structure is Stainless steel wire welding distribution arrangement forms.
A kind of 3. unmanned plane wing safeguard structure according to claim 1, it is characterised in that:The net structure is Nylon rope is mutually interspersed to be formed.
CN201720949236.9U 2017-08-01 2017-08-01 A kind of unmanned plane wing safeguard structure Active CN207225651U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201720949236.9U CN207225651U (en) 2017-08-01 2017-08-01 A kind of unmanned plane wing safeguard structure

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201720949236.9U CN207225651U (en) 2017-08-01 2017-08-01 A kind of unmanned plane wing safeguard structure

Publications (1)

Publication Number Publication Date
CN207225651U true CN207225651U (en) 2018-04-13

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Family Applications (1)

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CN201720949236.9U Active CN207225651U (en) 2017-08-01 2017-08-01 A kind of unmanned plane wing safeguard structure

Country Status (1)

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CN (1) CN207225651U (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN110077607A (en) * 2019-05-15 2019-08-02 深圳市智旋科技有限公司 A kind of unmanned plane proof equipment and means of defence
WO2021218168A1 (en) * 2020-04-27 2021-11-04 深圳市大疆创新科技有限公司 Rotor wing protection mechanism and aircraft

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN110077607A (en) * 2019-05-15 2019-08-02 深圳市智旋科技有限公司 A kind of unmanned plane proof equipment and means of defence
CN110077607B (en) * 2019-05-15 2020-09-04 南京溧水高新创业投资管理有限公司 Unmanned aerial vehicle collision protection device and protection method
WO2021218168A1 (en) * 2020-04-27 2021-11-04 深圳市大疆创新科技有限公司 Rotor wing protection mechanism and aircraft

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Legal Events

Date Code Title Description
GR01 Patent grant
GR01 Patent grant
CP03 Change of name, title or address
CP03 Change of name, title or address

Address after: Xihua East Road, Changping County of Zhoukou City, Henan province 466600

Co-patentee after: HENAN KUNONG AVIATION PLANT PROTECTION TECHNOLOGY Co.,Ltd.

Patentee after: Xihua Jiuxiang UAV Industrial Park Operation Co.,Ltd.

Co-patentee after: SHENZHEN KUNONG UAV INDUSTRIAL DEVELOPMENT AND APPLICATION Co.,Ltd.

Address before: 466600 east section of Changping Road, Xihua county, Zhoukou City, Zhoukou City, Henan Province

Co-patentee before: HENAN KUNONG AVIATION PLANT PROTECTION TECHNOLOGY Co.,Ltd.

Patentee before: XIHUA KUNONG UAV INDUSTRIAL PARK OPERATION Co.,Ltd.

Co-patentee before: SHENZHEN KUNONG UAV INDUSTRIAL DEVELOPMENT AND APPLICATION Co.,Ltd.