CN207225651U - A kind of unmanned plane wing safeguard structure - Google Patents
A kind of unmanned plane wing safeguard structure Download PDFInfo
- 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
- Authority
- CN
- China
- Prior art keywords
- unmanned plane
- wing
- cavity
- connecting rod
- safeguard structure
- Prior art date
- Legal status (The legal status 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 status listed.)
- Expired - Fee Related
Links
- 239000004677 Nylon Substances 0.000 claims description 3
- 229920001778 nylon Polymers 0.000 claims description 3
- 229910001220 stainless steel Inorganic materials 0.000 claims description 3
- 238000003466 welding Methods 0.000 claims description 3
- 230000005611 electricity Effects 0.000 claims 1
- 230000002633 protecting effect Effects 0.000 abstract description 4
- 238000010586 diagram Methods 0.000 description 3
- 230000009286 beneficial effect Effects 0.000 description 1
- 230000007812 deficiency Effects 0.000 description 1
- 238000000034 method Methods 0.000 description 1
- 239000007787 solid Substances 0.000 description 1
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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
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.
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 |
Family
ID=61856266
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201720949236.9U Expired - Fee Related CN207225651U (en) | 2017-08-01 | 2017-08-01 | A kind of unmanned plane wing safeguard structure |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN207225651U (en) |
Cited By (2)
| 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 |
-
2017
- 2017-08-01 CN CN201720949236.9U patent/CN207225651U/en not_active Expired - Fee Related
Cited By (3)
| 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 |
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. |
|
| CP03 | Change of name, title or address | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20180413 |