CN205707370U - Portable and collapsible unmanned plane - Google Patents
Portable and collapsible unmanned plane Download PDFInfo
- Publication number
- CN205707370U CN205707370U CN201620490252.1U CN201620490252U CN205707370U CN 205707370 U CN205707370 U CN 205707370U CN 201620490252 U CN201620490252 U CN 201620490252U CN 205707370 U CN205707370 U CN 205707370U
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- China
- Prior art keywords
- fuselage
- undercarriage
- rotor support
- buckle
- unmanned plane
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Abstract
A kind of portable and collapsible unmanned plane, including fuselage, it is hinged on the rotor support of described fuselage upper end and is hinged on the undercarriage of described fuselage lower end, described rotor support is provided with rotor and electromotor, the upper end of described fuselage is provided with the first elastic shelf, the two ends of described first elastic shelf connect described fuselage and described rotor support respectively, described rotor support is provided with the first button and the first buckle, described fuselage is provided with described first buckle to the first adaptive draw-in groove, the lower end of described fuselage is provided with the second elastic shelf, the two ends of described second elastic shelf connect described fuselage and described undercarriage respectively, described undercarriage is provided with the second button and the second buckle, described fuselage is provided with second draw-in groove suitable with described second buckle, described fuselage is provided with the described rotor support of collecting and the accepting groove of described undercarriage.This utility model fixes rotor support and undercarriage by elastic shelf, facilitates and launches in the accepting groove from fuselage of rotor support and undercarriage and reclaim.
Description
Technical field
This utility model relates to unmanned plane field, particularly relates to a kind of portable and collapsible unmanned plane.
Background technology
At present, more and more obvious in the development of aviation field, the particularly effect in military field along with unmanned plane.Modern
War needs soldier to carry out shallow bid army even individual combat under rugged environment.And unmanned plane is as obtaining enemy's information
High efficiency weapon, role is more and more important.
Conventional unmanned plane wing and undercarriage cannot fold, and it is the most inconvenient to carry, and more existing collapsible unmanned
Machine realizes wing and the folding of undercarriage and expansion generally by dismounting set screw, operates very inconvenient, and
And set screw is easily lost, unmanned plane is caused to use.
Utility model content
In view of above-mentioned condition, it is necessary to provide a kind of convenient portable and collapsible unmanned plane folded and launch.
A kind of portable and collapsible unmanned plane, the rotor support including fuselage, being hinged on described fuselage upper end and hinged
At the undercarriage of described fuselage lower end, described rotor support is provided with rotor and electromotor, and the upper end of described fuselage is provided with first
Elastic shelf, the two ends of described first elastic shelf connect described fuselage and described rotor support respectively, and described rotor support is provided with
First button and the first buckle, described fuselage is provided with first draw-in groove suitable with described first buckle, described first button
For controlling the engaging of described first buckle and described first draw-in groove and getting loose, the lower end of described fuselage is provided with the second elastic shelf,
The two ends of described second elastic shelf connect described fuselage and described undercarriage respectively, and described undercarriage is provided with the second button and
Two buckles, described fuselage is provided with second draw-in groove suitable with described second buckle, and described second button is used for controlling described
The engaging of the second buckle and described second draw-in groove with get loose, described fuselage is provided with the described rotor support of collecting and described undercarriage
Accepting groove.
Above-mentioned portable and collapsible unmanned plane, by using elastic shelf to fix rotor support and undercarriage, uses this portable
During the collapsible unmanned plane of formula, press the first button and the second button, make the first bayonet socket and the second buckle unclamp, by elastic shelf
Elastic force makes rotor support and undercarriage launch from accepting groove；When need not use, rotor support and undercarriage are taken in machine
In accepting groove with it.Its simple in construction, it is not necessary to fold and launch rotor support by the way of the complexity such as dismounting screw and rise
Fall frame.
Further, described rotor support and described undercarriage position on described fuselage are staggered like state.
Further, four fins of described rotor are connected by rotary connection structure, by described rotary connection structure,
The rotatable coincidence of described fin.
Further, described fuselage is oval.
Further, one is formed with described fuselage after described rotor support and described undercarriage income accepting groove complete ellipse
Spheroid.
Accompanying drawing explanation
Fig. 1 is the structural representation of the portable and collapsible unmanned plane that this utility model embodiment proposes.
Main element symbol description
Following detailed description of the invention will further illustrate this utility model in conjunction with above-mentioned accompanying drawing.
Detailed description of the invention
For the ease of understanding this utility model, below with reference to relevant drawings, this utility model is more fully retouched
State.Accompanying drawing gives this utility model embodiment.But, this utility model can realize in many different forms, and
It is not limited to embodiment described herein.On the contrary, providing the purpose of this embodiment is to make disclosure of the present utility model
More thorough comprehensive.
It should be noted that when element is referred to as " being fixedly arranged on " another element, and it can be directly on another element
Or element placed in the middle can also be there is.When an element is considered as " connection " another element, and it can be to be directly connected to
To another element or may be simultaneously present centering elements.Term as used herein " vertical ", " level ", " left ",
" right " and similar statement are for illustrative purposes only.
Unless otherwise defined, all of technology used herein and scientific terminology are led with belonging to technology of the present utility model
The implication that the technical staff in territory is generally understood that is identical.At term used in the description of the present utility model it is simply herein
The purpose of specific embodiment is described, it is not intended that in limiting this utility model.Term as used herein " and/or " include
Arbitrary and all of combination of one or more relevant Listed Items.
Referring to Fig. 1, a kind of portable and collapsible unmanned plane that this utility model embodiment provides, including fuselage 1, hinged
Rotor support 2 in described fuselage 1 upper end and be hinged on the undercarriage 3 of described fuselage 1 lower end, described fuselage 1 is oval.
Described rotor support 2 is staggered like state with the described undercarriage 3 position on described fuselage 1.Described rotor support 2 is provided with rotation
The wing 4 and electromotor 5, described electromotor 5 is connected with rotor 4, and provides lift upwards for this portable and collapsible unmanned plane.Institute
Four fins stating rotor 4 are connected by rotary connection structure, and by described rotary connection structure, described fin is rotatable heavy
Close.
The upper end of described fuselage 1 is provided with the first elastic shelf 6, and the two ends of described first elastic shelf 6 connect described fuselage 1 respectively
And described rotor support 2, described rotor support 2 is provided with the first button 61 and the first buckle 62, and described fuselage 1 is provided with and institute
Stating first buckle 62, first draw-in groove 63 to adaptation, described first button 61 is used for controlling institute's first buckle 62 and described first card
The engaging of groove 63 with get loose.Described fuselage 1 is provided with the accepting groove 8a housing described rotor support 2, and described rotor support 2 houses
In described accepting groove 8a.Pressing the first button 61 on rotor support 2, described first buckle 62 is pine from the first draw-in groove 63
De-, the first elastic shelf 6 provides elastic force that rotor support 2 is supported expansion.
The lower end of described fuselage 1 is provided with the second elastic shelf 7, and the two ends of described second elastic shelf 7 connect described fuselage 1 respectively
Rising and falling 3 described in and, described undercarriage 3 is provided with the second button 71 and the second buckle 72, and described fuselage 1 is provided with and described second card
Detaining 72 the second suitable draw-in groove (not shown), described second button 71 is used for controlling institute's the second buckle 72 and described second draw-in groove
Engaging with get loose.Described fuselage 1 is provided with the accepting groove 8b housing described undercarriage 3, described in the support 3 that rises and falls be contained in described
In accepting groove 8b.When pressing the second button 71 on undercarriage 3, described second buckle 72 gets loose from the second draw-in groove, the second bullet
Property frame 7 provides elastic force that undercarriage 3 is supported expansion.
When using this portable and collapsible unmanned plane, press the first button 61 and the second button 71, make the first bayonet socket 62 He
Second buckle 72 unclamps, and by elastic shelf 6, rotor support 2 and undercarriage 3 from accepting groove 8a, are supported in 8b by 7 elastic force provided
Launch；When need not use, rotor support 2 and undercarriage 3 are housed the accepting groove 8a to fuselage 1, in 8b.Described rotor props up
Accepting groove 8a taken in by frame 2 and described undercarriage 3, forms a complete spheroid after 8b with fuselage 1.
Embodiment described above only have expressed embodiment of the present utility model, and it describes more concrete and detailed, but also
Therefore the restriction to this utility model the scope of the claims can not be interpreted as.It should be pointed out that, for the ordinary skill of this area
For personnel, without departing from the concept of the premise utility, it is also possible to make some deformation and improvement, these broadly fall into this
The protection domain of utility model.Therefore, the protection domain of this utility model patent should be as the criterion with claims.
Claims (5)
1. a portable and collapsible unmanned plane, it is characterised in that include fuselage, be hinged on the rotor support of described fuselage upper end
And it being hinged on the undercarriage of described fuselage lower end, described rotor support is provided with rotor and electromotor, the upper end of described fuselage
Being provided with the first elastic shelf, the two ends of described first elastic shelf connect described fuselage and described rotor support respectively, and described rotor props up
Frame is provided with the first button and the first buckle, and described fuselage is provided with first draw-in groove suitable with described first buckle, described
First button is for controlling the engaging of described first buckle and described first draw-in groove and getting loose, and the lower end of described fuselage is provided with second
Elastic shelf, the two ends of described second elastic shelf connect described fuselage and described undercarriage respectively, and described undercarriage is provided with second
Button and the second buckle, described fuselage is provided with second draw-in groove suitable with described second buckle, and described second button is used for
Controlling the engaging of described second buckle and described second draw-in groove and get loose, described fuselage is provided with the described rotor support of collecting and institute
State the accepting groove of undercarriage.
2. portable and collapsible unmanned plane as claimed in claim 1, it is characterised in that described rotor support and described undercarriage
Position on described fuselage is staggered like state.
3. portable and collapsible unmanned plane as claimed in claim 1, it is characterised in that four fins of described rotor are by rotation
Turn attachment structure to be connected, by described rotary connection structure, the rotatable coincidence of described fin.
4. portable and collapsible unmanned plane as claimed in claim 1, it is characterised in that described fuselage is oval.
5. portable and collapsible unmanned plane as claimed in claim 4, it is characterised in that described rotor support and described undercarriage
A complete spheroid is formed with described fuselage after income accepting groove.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201620490252.1U CN205707370U (en) | 2016-05-25 | 2016-05-25 | Portable and collapsible unmanned plane |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201620490252.1U CN205707370U (en) | 2016-05-25 | 2016-05-25 | Portable and collapsible unmanned plane |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN205707370U true CN205707370U (en) | 2016-11-23 |
Family
ID=57299645
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201620490252.1U Expired - Fee Related CN205707370U (en) | 2016-05-25 | 2016-05-25 | Portable and collapsible unmanned plane |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN205707370U (en) |
Cited By (9)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106585954A (en) * | 2016-12-31 | 2017-04-26 | 歌尔科技有限公司 | Unmanned aerial vehicle |
| CN106741876A (en) * | 2016-12-28 | 2017-05-31 | 深圳市道通智能航空技术有限公司 | A kind of unmanned plane |
| CN106976563A (en) * | 2017-04-27 | 2017-07-25 | 峨眉山市博派乐无人机科技有限公司 | Pesticide spraying unmanned plane |
| CN108238243A (en) * | 2016-12-27 | 2018-07-03 | 中国科学院遥感与数字地球研究所 | 5kg load-carryings length six rotor wing unmanned aerial vehicles of continuation of the journey |
| CN108313259A (en) * | 2018-02-13 | 2018-07-24 | 深圳臻迪信息技术有限公司 | A kind of unmanned plane |
| CN108583845A (en) * | 2018-01-29 | 2018-09-28 | 安徽理工大学 | A kind of foldable anti-unmanned plane to fall over into water |
| WO2020122433A1 (en) * | 2018-12-11 | 2020-06-18 | 전남도립대학교산학협력단 | Drone provided with foldable rotary wing |
| CN111994261A (en) * | 2020-08-25 | 2020-11-27 | 五邑大学 | Unmanned plane |
| CN114313245A (en) * | 2022-01-05 | 2022-04-12 | 广东电网有限责任公司 | Electric power patrols line unmanned aerial vehicle that obstacles removing |
-
2016
- 2016-05-25 CN CN201620490252.1U patent/CN205707370U/en not_active Expired - Fee Related
Cited By (13)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108238243A (en) * | 2016-12-27 | 2018-07-03 | 中国科学院遥感与数字地球研究所 | 5kg load-carryings length six rotor wing unmanned aerial vehicles of continuation of the journey |
| US11091249B2 (en) | 2016-12-28 | 2021-08-17 | Autel Robotics Co., Ltd. | Unmanned aerial vehicle |
| CN106741876A (en) * | 2016-12-28 | 2017-05-31 | 深圳市道通智能航空技术有限公司 | A kind of unmanned plane |
| WO2018120890A1 (en) * | 2016-12-28 | 2018-07-05 | 深圳市道通智能航空技术有限公司 | Unmanned aerial vehicle |
| CN106741876B (en) * | 2016-12-28 | 2022-07-29 | 深圳市道通智能航空技术股份有限公司 | Unmanned aerial vehicle |
| CN106585954A (en) * | 2016-12-31 | 2017-04-26 | 歌尔科技有限公司 | Unmanned aerial vehicle |
| CN106585954B (en) * | 2016-12-31 | 2023-07-21 | 歌尔科技有限公司 | Unmanned aerial vehicle |
| CN106976563A (en) * | 2017-04-27 | 2017-07-25 | 峨眉山市博派乐无人机科技有限公司 | Pesticide spraying unmanned plane |
| CN108583845A (en) * | 2018-01-29 | 2018-09-28 | 安徽理工大学 | A kind of foldable anti-unmanned plane to fall over into water |
| CN108313259A (en) * | 2018-02-13 | 2018-07-24 | 深圳臻迪信息技术有限公司 | A kind of unmanned plane |
| WO2020122433A1 (en) * | 2018-12-11 | 2020-06-18 | 전남도립대학교산학협력단 | Drone provided with foldable rotary wing |
| CN111994261A (en) * | 2020-08-25 | 2020-11-27 | 五邑大学 | Unmanned plane |
| CN114313245A (en) * | 2022-01-05 | 2022-04-12 | 广东电网有限责任公司 | Electric power patrols line unmanned aerial vehicle that obstacles removing |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| CF01 | Termination of patent right due to non-payment of annual fee | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20161123 Termination date: 20170525 |