CN206068145U - A kind of foldable type unmanned plane - Google Patents
A kind of foldable type unmanned plane Download PDFInfo
- Publication number
- CN206068145U CN206068145U CN201621034382.0U CN201621034382U CN206068145U CN 206068145 U CN206068145 U CN 206068145U CN 201621034382 U CN201621034382 U CN 201621034382U CN 206068145 U CN206068145 U CN 206068145U
- Authority
- CN
- China
- Prior art keywords
- section
- foldable
- fuselage
- horn
- unmanned plane
- 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.)
- Active
Links
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U30/00—Means for producing lift; Empennages; Arrangements thereof
- B64U30/20—Rotors; Rotor supports
- B64U30/29—Constructional aspects of rotors or rotor supports; Arrangements thereof
- B64U30/293—Foldable or collapsible rotors or rotor supports
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C27/00—Rotorcraft; Rotors peculiar thereto
- B64C27/32—Rotors
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U10/00—Type of UAV
- B64U10/10—Rotorcrafts
- B64U10/13—Flying platforms
- B64U10/14—Flying platforms with four distinct rotor axes, e.g. quadcopters
Abstract
The utility model discloses a kind of foldable type unmanned plane, including fuselage and horn, horn includes non-collapsible section, fold mechanism and foldable section, and non-collapsible section is fixedly connected with fuselage, and foldable section is flexibly connected with non-collapsible section by fold mechanism.Under flap state, foldable section of multiple horns two-by-two with respect to folded inward.Foldable section of top mutually abuts two-by-two, and contacts with fuselage；Or, foldable section parallel two-by-two to stack；Or, foldable section intersect it is overlapping.This utility model can make the unmanned plane volume after flap little as much as possible, be easy to carry and convey, and reduce collision rate；Horn is folded in around fuselage simultaneously, and protective action, the infringement in reduction transportation to fuselage effectively can be played to fuselage.
Description
Technical field
This utility model is related to unmanned air vehicle technique field, more particularly to a kind of horn folding unmanned plane.
Background technology
The horn of traditional unmanned plane is fixedly connected with fuselage, has that volume is larger, transports the problem of inconvenience.For
Above-mentioned situation, has actively developed development horn and folding " flap " unmanned plane of fuselage both at home and abroad.Design common at present
The design of droop flap and the design of horizontal turnover type flap nothing more than.It is inadequate that these designs are all done in space utilization
It is good.For example, droop flap design is to roll over the front end of horizontal horn vertically downward, vertical section horn is meaningless occupy it is very big by one
Block space；Horizontal turnover type flap design is then that the front end level of horizontal horn is rolled over to side, but is had between two sections of horns
Larger angle, causes very big one piece of area is occupied on horizontal space；And multiple horns each occupy a block space, to space
Utilization rate wretched insufficiency.
Utility model content
The purpose of this utility model is volume foldable type unmanned plane as little as possible when providing a kind of folding.
To reach above-mentioned purpose, embodiment of the present utility model is adopted the following technical scheme that：
A kind of foldable type unmanned plane, including fuselage and the multiple horns on fuselage, the horn include non-collapsible
Section, fold mechanism and foldable section, the non-collapsible section of horn is fixedly connected with fuselage, and foldable section of horn passes through folding machine
Structure is flexibly connected with non-collapsible section, and described foldable section can be turned back to coaxial expansion by axle of fold mechanism relative to non-collapsible section
State or non-coaxial flap state, under flap state, foldable section of multiple horns two-by-two with respect to folded inward.
According to one side of the present utility model, the non-collapsible section of the horn and foldable section under flap state, place
In same level or on different level.
According to one side of the present utility model, under flap state, foldable section of multiple horns of top two is biphase
Mutually abut, and contact with the fuselage.
According to one side of the present utility model, under flap state, foldable section of multiple horns parallel two-by-two to stack
Together.
According to one side of the present utility model, under flap state, foldable section of multiple horns intersect it is overlapping
Together.
The advantage that this utility model is implemented：
Horn is divided into two sections of before and after by this utility model, and one section of horn of front end can be folded, and this section of horn is when folding
Two-by-two with respect to folded inward, or as far as possible near fuselage, or parallel stack, or it is overlapping to intersect, so that
Whole unmanned plane volume after flap is very little, is easy to carry and conveys, and reduces collision rate；Horn is folded in fuselage week simultaneously
Enclose, protective action, the infringement in reduction transportation to fuselage effectively can be played to fuselage.
Description of the drawings
For the technical scheme being illustrated more clearly that in this utility model embodiment, below will be to making needed for embodiment
Accompanying drawing is briefly described, it should be apparent that, drawings in the following description are only some embodiments of the present utility model,
For those of ordinary skill in the art, on the premise of not paying creative work, can be with according to these accompanying drawings acquisitions
Other accompanying drawings.
Fig. 1 is the structural representation of this utility model deployed condition.
Fig. 2 is the structural representation of the first embodiment flap state of this utility model.
Fig. 3 is the structural representation of second embodiment flap state of this utility model.
Fig. 4 is the structural representation of the third embodiment flap state of this utility model.
Specific embodiment
Below in conjunction with the accompanying drawing in this utility model embodiment, the technical scheme in this utility model embodiment is carried out
Clearly and completely describe, it is clear that described embodiment is only this utility model a part of embodiment, rather than whole
Embodiment.Based on the embodiment in this utility model, those of ordinary skill in the art are not under the premise of creative work is made
The every other embodiment for being obtained, belongs to the scope of this utility model protection.
Embodiment one, level folding is to formula flap unmanned plane
As depicted in figs. 1 and 2, the structure of the present embodiment is as follows：Including fuselage 1 and multiple horns, each horn includes non-
Folded section 2, fold mechanism 3 and foldable section 4, the non-collapsible section 2 of each horn are fixedly connected with fuselage 1, each horn
It is flexibly connected with corresponding non-collapsible section 2 by fold mechanism 3 respectively for foldable section 4, foldable section 4 with fold mechanism 3 as axle
Can turn back to coaxial deployed condition or non-coaxial flap state relative to non-collapsible section 2.As shown in Fig. 2 in flap shape
State, the non-collapsible section 2 of each horn and foldable section 4 are in same level, and the top of foldable section 4 of each horn
Mutually abut two-by-two, and contact with fuselage 1.In fig. 2 in order to be shown more clearly by flap state, nobody is concealed hereby
The rotor part of machine.
Embodiment two, side run-in index flap unmanned plane
As shown in figures 1 and 3, the structure of the present embodiment is as follows：Including fuselage 1 and multiple horns, each horn includes non-
2 sections, fold mechanism 3 and foldable section 4 are folded, the non-collapsible section 2 of each horn is fixedly connected with fuselage 1, each horn
It is flexibly connected with corresponding non-collapsible section 2 by fold mechanism 3 respectively for foldable section 4, foldable section 4 with fold mechanism 3 as axle
Coaxial deployed condition or non-coaxial flap state can be gone to relative to non-collapsible section folding 2.As shown in figure 3, in flap shape
State, the non-collapsible section 2 of each horn and foldable section 4 are on different level, and foldable section 4 of each horn is put down two-by-two
Row is stacked together.In figure 3 in order to be shown more clearly by flap state, the rotor part of unmanned plane is concealed hereby.
Embodiment three, side intersect overlapping type flap unmanned plane
As shown in Figure 1 and Figure 4, the structure of the present embodiment is as follows：Including fuselage 1 and multiple horns, each horn includes non-
2 sections, fold mechanism 3 and foldable section 4 are folded, the non-collapsible section 2 of each horn is fixedly connected with fuselage 1, each horn
It is flexibly connected with corresponding non-collapsible section 2 by fold mechanism 3 respectively for foldable section 4, foldable section 4 with fold mechanism 3 as axle
Coaxial deployed condition or non-coaxial flap state can be gone to relative to non-collapsible section folding 2.As shown in figure 4, in flap shape
State, the non-collapsible section 2 of each horn and foldable section 4 are on different level, and 4 liang of foldable section of each horn is biphase
Mutually intersect and overlap together.In the diagram in order to be shown more clearly by flap state, the undercarriage part of unmanned plane is concealed hereby
With rotor part.
The above, specific embodiment only of the present utility model, but protection domain of the present utility model do not limit to
In this, any those skilled in the art disclosed in this utility model in technical scope, the change that can be readily occurred in
Change or replace, should all cover within protection domain of the present utility model.Therefore, protection domain of the present utility model should be with described
Scope of the claims is defined.
Claims (5)
1. a kind of foldable type unmanned plane, it is characterised in that：Multiple horns including fuselage and on fuselage, the horn bag
Non-collapsible section, fold mechanism and foldable section are included, the non-collapsible section of horn is fixedly connected with fuselage, foldable section of horn leads to
Cross fold mechanism to be flexibly connected with non-collapsible section, described foldable section can relative to non-collapsible section with fold mechanism as axle turn back to
Coaxial deployed condition or non-coaxial flap state, under flap state, foldable section of multiple horns is rolled over two-by-two relatively inwards
It is folded.
2. foldable type unmanned plane according to claim 1, it is characterised in that：The non-collapsible section of the horn and foldable section
Under flap state, in same level or on different level.
3. foldable type unmanned plane according to claim 1 and 2, it is characterised in that：Under flap state, multiple horns can
The top of folded section mutually abuts two-by-two, and contacts with the fuselage.
4. foldable type unmanned plane according to claim 1 and 2, it is characterised in that：Under flap state, multiple horns can
Folded section is parallel two-by-two to be stacked together.
5. foldable type unmanned plane according to claim 1 and 2, it is characterised in that：Under flap state, multiple horns can
Folded section intersects and overlaps together.
Priority Applications (3)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201621034382.0U CN206068145U (en) | 2016-08-31 | 2016-08-31 | A kind of foldable type unmanned plane |
| PCT/CN2016/107103 WO2018040312A1 (en) | 2016-08-31 | 2016-11-24 | Unmanned aerial vehicle of folding wing-type |
| KR1020187008592A KR102126142B1 (en) | 2016-08-31 | 2016-11-24 | Folding wing drone |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201621034382.0U CN206068145U (en) | 2016-08-31 | 2016-08-31 | A kind of foldable type unmanned plane |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN206068145U true CN206068145U (en) | 2017-04-05 |
Family
ID=58436906
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201621034382.0U Active CN206068145U (en) | 2016-08-31 | 2016-08-31 | A kind of foldable type unmanned plane |
Country Status (3)
| Country | Link |
|---|---|
| KR (1) | KR102126142B1 (en) |
| CN (1) | CN206068145U (en) |
| WO (1) | WO2018040312A1 (en) |
Cited By (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108545190A (en) * | 2018-06-15 | 2018-09-18 | 芜湖万户航空航天科技有限公司 | Miniature drone |
| CN108609169A (en) * | 2018-06-15 | 2018-10-02 | 芜湖万户航空航天科技有限公司 | The unmanned plane of folding can be stablized |
| CN108773480A (en) * | 2018-06-15 | 2018-11-09 | 芜湖万户航空航天科技有限公司 | Unmanned plane |
| CN108791854A (en) * | 2018-06-15 | 2018-11-13 | 芜湖万户航空航天科技有限公司 | Fold unmanned plane |
| CN108860586A (en) * | 2018-06-15 | 2018-11-23 | 芜湖万户航空航天科技有限公司 | Novel unmanned plane |
| CN108910012A (en) * | 2018-07-26 | 2018-11-30 | 瀚伦贝尔通用航空器有限公司 | A kind of big boom device of folding aircraft |
| CN112874771A (en) * | 2021-03-15 | 2021-06-01 | 中国民航大学 | Deformation can vert four rotor unmanned aerial vehicle |
Families Citing this family (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| KR102355526B1 (en) | 2020-07-24 | 2022-02-07 | 주식회사 샘코 | Unmanned Aerial Vehicle having folding type wings |
Family Cites Families (10)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN101391651A (en) * | 2008-11-17 | 2009-03-25 | 西安智澜科技发展有限公司 | Foldable Y shaped three axis two-layer six rotorcraft |
| CA2904575C (en) * | 2013-03-14 | 2022-02-01 | Aeryon Labs Inc. | Folding propellers system |
| CN203528812U (en) * | 2013-09-06 | 2014-04-09 | 天津云友科技有限公司 | Foldable four-rotor aircraft |
| KR101594313B1 (en) * | 2013-12-26 | 2016-02-16 | 한국항공대학교 산학협력단 | Multicopter system for crop-dusting |
| CN106061838A (en) * | 2014-01-20 | 2016-10-26 | 罗博杜伯公司 | Multicopters with variable flight characteristics |
| CN204056294U (en) * | 2014-09-12 | 2014-12-31 | 西北工业大学明德学院 | A kind of collapsible four axle multi-rotor aerocrafts |
| CN104260878A (en) * | 2014-10-16 | 2015-01-07 | 北京理工大学 | Four-rotor aircraft rack with capacity of automatic folding and spreading |
| CN205311891U (en) * | 2015-12-09 | 2016-06-15 | 上海游族智能科技有限公司 | Two anti wind suddenly that vert increase steady bendable flap aircraft |
| CN105416569A (en) * | 2015-12-09 | 2016-03-23 | 上海游族智能科技有限公司 | Double-tilting gusty-wind-resistant stability augmentation bendable wing aircraft |
| CN105416568A (en) * | 2015-12-09 | 2016-03-23 | 上海游族智能科技有限公司 | Self-adaptive gusty-wind-resistant bent wing |
-
2016
- 2016-08-31 CN CN201621034382.0U patent/CN206068145U/en active Active
- 2016-11-24 WO PCT/CN2016/107103 patent/WO2018040312A1/en active Application Filing
- 2016-11-24 KR KR1020187008592A patent/KR102126142B1/en active IP Right Grant
Cited By (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108545190A (en) * | 2018-06-15 | 2018-09-18 | 芜湖万户航空航天科技有限公司 | Miniature drone |
| CN108609169A (en) * | 2018-06-15 | 2018-10-02 | 芜湖万户航空航天科技有限公司 | The unmanned plane of folding can be stablized |
| CN108773480A (en) * | 2018-06-15 | 2018-11-09 | 芜湖万户航空航天科技有限公司 | Unmanned plane |
| CN108791854A (en) * | 2018-06-15 | 2018-11-13 | 芜湖万户航空航天科技有限公司 | Fold unmanned plane |
| CN108860586A (en) * | 2018-06-15 | 2018-11-23 | 芜湖万户航空航天科技有限公司 | Novel unmanned plane |
| CN108910012A (en) * | 2018-07-26 | 2018-11-30 | 瀚伦贝尔通用航空器有限公司 | A kind of big boom device of folding aircraft |
| CN112874771A (en) * | 2021-03-15 | 2021-06-01 | 中国民航大学 | Deformation can vert four rotor unmanned aerial vehicle |
Also Published As
| Publication number | Publication date |
|---|---|
| KR102126142B1 (en) | 2020-06-24 |
| WO2018040312A1 (en) | 2018-03-08 |
| KR20180042405A (en) | 2018-04-25 |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CN206068145U (en) | A kind of foldable type unmanned plane | |
| CN206187532U (en) | Double -walled packing carton of folding inside lining in area | |
| CN203410717U (en) | Single-piece folding package box with inner lining | |
| CN107214999A (en) | A kind of novel package cartridge manufacturing method | |
| CN203228440U (en) | Paper sycee folder | |
| CN202891047U (en) | Folding computer desk | |
| CN206381617U (en) | A kind of tipping bucket type railway carriage folded toy structure | |
| CN205240129U (en) | Integration package box structure | |
| CN203473593U (en) | Paper box with practical structure | |
| CN206827217U (en) | A kind of telescopic clothing packaging bag | |
| CN204096204U (en) | A kind of electrical equipment packing box | |
| CN207565995U (en) | A kind of packing box of rapid shaping | |
| CN203699014U (en) | Packaging box for craft porcelain dish | |
| CN207157728U (en) | A kind of trapezoidal Multifunctional box | |
| CN205972161U (en) | Plug -in type cigarette packing barrel | |
| CN207253009U (en) | A kind of portable travel bag | |
| CN206424041U (en) | The motor section of dust catcher and the attachment structure of main frame | |
| CN207329065U (en) | A kind of packing box of columnar product | |
| CN207186191U (en) | A kind of house type still bank | |
| CN107343696A (en) | A kind of portable travel bag | |
| CN207157737U (en) | A kind of pyramid box | |
| CN203345309U (en) | Foldable gift box | |
| CN215246891U (en) | Cabinet transport package structure | |
| CN207346240U (en) | A kind of handled packing box | |
| CN218704611U (en) | Foldable hamburger box |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| GR01 | Patent grant |