CN206358358U - A kind of many rotary wing aircraft foldable structures being readily transported - Google Patents
A kind of many rotary wing aircraft foldable structures being readily transported Download PDFInfo
- Publication number
- CN206358358U CN206358358U CN201720008704.2U CN201720008704U CN206358358U CN 206358358 U CN206358358 U CN 206358358U CN 201720008704 U CN201720008704 U CN 201720008704U CN 206358358 U CN206358358 U CN 206358358U
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- CN
- China
- Prior art keywords
- horn
- wing
- groove
- strip groove
- readily transported
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- 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
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Abstract
The utility model discloses a kind of many rotary wing aircraft foldable structures being readily transported, including body, several horns, the strip groove with the quantity such as horn is provided with the top of body, the central axis of the strip groove and the central axis of horn are located at same straight line, the horn is matched with strip groove, it is additionally provided with the side wall of body at the top of end plate, the end plate and strip groove bottom level, one end and the horn of end plate are hinged；Wing is additionally provided with the end of horn, the wing includes two fins, groove is additionally provided with the top of horn, the width of the groove is matched with fin, and twice of depth more than or equal to foil thickness of groove.The utility model is solved during transport, the problem of horn, the wing of unmanned plane are easily damaged.
Description
Technical field
The utility model is related to a kind of unmanned plane, and in particular to a kind of many rotary wing aircraft foldable structures being readily transported.
Background technology
Multi-rotor unmanned aerial vehicle, to realize flight, is widely used in by the multiple propellers of multiple motor controls and takes photo by plane, monitors, searching
Rescue, the every field such as resource exploration, agricultural, with small volume, lightweight, expense is low, operation is flexible and safe the features such as.
Multi-rotor unmanned aerial vehicle possesses more horn, when collecting unmanned plane, it is necessary to twist off screw, and horn is disassembled could more preferably
Transport, repeatedly dismantle and install both wasted time.
To solve to dismantle and install the problem of both wasting time repeatedly, the wing of unmanned plane is rolled in the prior art
It is folded, but in unmanned plane collection transportation, this kind of folding mode easily causes horn, wing abrasion, influences performance.
Utility model content
The purpose of this utility model is to provide a kind of many rotary wing aircraft foldable structures being readily transported, solves transporting
During, the problem of horn, the wing of unmanned plane are easily damaged.
The utility model is achieved through the following technical solutions：
A kind of many rotary wing aircraft foldable structures being readily transported, including body, several horns, set at the top of body
The strip groove with the quantity such as horn is equipped with, the central axis of the strip groove and the central axis of horn are located at always
Line, the horn is matched with strip groove, is additionally provided with the side wall of body at the top of end plate, the end plate and strip groove bottom
Level, one end and the horn of end plate are hinged；Wing is additionally provided with the end of horn, the wing includes two fins, in machine
Groove is additionally provided with the top of arm, the width of the groove is matched with fin, and the depth of groove is more than or equal to foil thickness
Twice.
Further, the folding mode of unmanned plane of the prior art is varied, and oriented organism sidewall is folded, and also has picture
What body surrounding was folded, but the horn or wing in the prior art without doubling poststack carry out further protection, cause
Horn, wing cause damage in transportation.The utility model it is innovative devise a kind of foldable structure, by horn to machine
The top fold of body, sets the strip groove that is matched with horn at the top of body, and horn is with the end plate of body end to be hinged
Form connection, end plate is a linking arm integrated with body, and the horn after folding has just been placed in strip groove so that
Avoid horn abrasion.Groove is also provided with the top of horn, after two fins of wing are pulled down, is put into groove, it is recessed
The width of groove is matched with fin, makes fin be not easy to drop, and is put into after then horn is folded again in strip groove so that machine
The wing, horn are obtained for protection.
It is preferred that, the bottom of the groove is provided with rotary wings seat, and the top of the rotary wings seat is provided with wing, described
Wing includes two fins, and two fins are bolted.Further, this mode described in the utility model is without by the wing
Piece is removed, more convenient.The rotary wings seat for driving wing rotation is arranged on to the bottom of groove, wing is located at the top of rotary wings seat
Portion, two fins are bolted, when needing to collect fin, and the elasticity of adjustment bolt rotates fin, will
Postrotational fin coincides together, and is then placed in groove, to protect fin.
Height adjustment mechanism is additionally provided between the rotary wings seat and wing.Further, height adjustment mechanism is used for
The height that wing rises is adjusted, makes wing more flexible, while being also to avoid groove from limiting the further improvement that wing rotation is done.
It is preferred that, the height adjustment mechanism is telescopic rod.The length of telescopic rod is preferably between 0.5cm to 2cm.
The utility model compared with prior art, has the following advantages and advantages：
1st, a kind of many rotary wing aircraft foldable structures being readily transported of the utility model, are provided with and machine at the top of body
The strip groove of the quantity such as arm, the central axis of the strip groove and the central axis of horn are located at same straight line, the machine
Arm is matched with strip groove, and above structure is solved during transport, the problem of the horn easy damaged of unmanned plane；
2nd, a kind of many rotary wing aircraft foldable structures being readily transported of the utility model, end is additionally provided with the side wall of body
With strip groove bottom level at the top of plate, the end plate, one end and the horn of end plate are hinged；Also set up in the end of horn organic
The wing, the wing includes two fins, groove is additionally provided with the top of horn, the width of the groove is matched with fin, and recessed
The depth of groove is more than or equal to twice of foil thickness, with upper type so that wing, horn are obtained for protection；
3rd, a kind of many rotary wing aircraft foldable structures being readily transported of the utility model, the bottom of the groove is provided with rotation
Rotor seat, the top of the rotary wings seat is provided with wing, and the wing includes two fins, and two fins are connected by bolt
Connect, wing is not only protected with upper type, and without fin is removed, it is more convenient.
Brief description of the drawings
Accompanying drawing described herein is used for providing further understanding the utility model embodiment, constitutes the one of the application
Part, does not constitute the restriction to the utility model embodiment.In the accompanying drawings：
Fig. 1 is the utility model structural representation.
Mark and corresponding parts title in accompanying drawing：
1- bodies, 2- horns, 3- strip grooves, 4- end plates, 5- wings, 6- grooves, 7- fins, 8- bolts, 9- rotary wings
Seat.
Embodiment
For the purpose of this utility model, technical scheme and advantage is more clearly understood, with reference to embodiment and accompanying drawing,
The utility model is described in further detail, and exemplary embodiment of the present utility model and its explanation are only used for explaining this
Utility model, is not intended as limiting of the present utility model.
Embodiment 1
As shown in figure 1, a kind of many rotary wing aircraft foldable structures being readily transported of the utility model, including body 1,4
Horn 2, the strip groove 3 with the quantity such as horn 2, the central axis and machine of the strip groove 3 are provided with the top of body 1
The central axis of arm 2 is located at same straight line, and the horn 2 is matched with strip groove 3, and end plate is additionally provided with the side wall of body 1
4, the top of the end plate 4 and the bottom level of strip groove 3, one end and the horn 2 of end plate 4 are hinged；Also set up in the end of horn 2
There is wing 5, the wing 5 includes two fins 7, groove 6, the width and fin of the groove 6 are additionally provided with the top of horn 2
7 matchings, and the depth of groove 6 is 2.5 times of the thickness of fin 7.With upper type so that wing, horn are obtained for protection.
Embodiment 2
As shown in figure 1, a kind of many rotary wing aircraft foldable structures being readily transported of the utility model, in the base of embodiment 1
On plinth, the bottom of the groove 6 is provided with rotary wings seat 9, and the top of the rotary wings seat is provided with wing 5, and the wing 5 is wrapped
Two fins 7 are included, two fins 7 are connected by bolt 8.Height regulation machine is additionally provided between the rotary wings seat 9 and wing 5
Structure；The height adjustment mechanism is telescopic rod.Wing is not only protected with upper type, and without fin is removed, it is more convenient.
Above-described embodiment, is entered to the purpose of this utility model, technical scheme and beneficial effect
One step is described in detail, be should be understood that and be the foregoing is only embodiment of the present utility model, is not used to limit
Fixed protection domain of the present utility model, all any modifications within spirit of the present utility model and principle, made, is equally replaced
Change, improve, should be included within protection domain of the present utility model.
Claims (4)
1. a kind of many rotary wing aircraft foldable structures being readily transported, including body (1), several horns (2), its feature exist
In being provided with the strip groove (3) with the quantity such as horn (2), the central shaft of the strip groove (3) at the top of body (1)
The central axis of line and horn (2) is located at same straight line, and the horn (2) matches with strip groove (3), the side in body (1)
Wall is additionally provided with the top of end plate (4), the end plate (4) and strip groove (3) bottom level, one end and the horn (2) of end plate (4)
It is hinged；Wing (5) is additionally provided with the end of horn (2), the wing (5) includes two fins (7), at the top of horn (2)
Groove (6) is additionally provided with, the width of the groove (6) is matched with fin (7), and the depth of groove (6) is more than or equal to fin
(7) twice of thickness.
2. a kind of many rotary wing aircraft foldable structures being readily transported according to claim 1, it is characterised in that described recessed
The bottom of groove (6) is provided with rotary wings seat (9), and the top of the rotary wings seat is provided with wing (5), and the wing (5) includes
Two fins (7), two fins (7) are connected by bolt (8).
3. a kind of many rotary wing aircraft foldable structures being readily transported according to claim 2, it is characterised in that the rotation
Height adjustment mechanism is additionally provided between rotor seat (9) and wing (5).
4. a kind of many rotary wing aircraft foldable structures being readily transported according to claim 3, it is characterised in that the height
Degree governor motion is telescopic rod.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201720008704.2U CN206358358U (en) | 2017-01-04 | 2017-01-04 | A kind of many rotary wing aircraft foldable structures being readily transported |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201720008704.2U CN206358358U (en) | 2017-01-04 | 2017-01-04 | A kind of many rotary wing aircraft foldable structures being readily transported |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN206358358U true CN206358358U (en) | 2017-07-28 |
Family
ID=59379318
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201720008704.2U Expired - Fee Related CN206358358U (en) | 2017-01-04 | 2017-01-04 | A kind of many rotary wing aircraft foldable structures being readily transported |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN206358358U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106672226A (en) * | 2017-01-04 | 2017-05-17 | 四川克瑞斯航空科技有限公司 | Multi-rotor vehicle body structure capable of effectively reducing transport space |
-
2017
- 2017-01-04 CN CN201720008704.2U patent/CN206358358U/en not_active Expired - Fee Related
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106672226A (en) * | 2017-01-04 | 2017-05-17 | 四川克瑞斯航空科技有限公司 | Multi-rotor vehicle body structure capable of effectively reducing transport space |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| 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: 20170728 Termination date: 20210104 |