CN205633056U - Foldable unmanned aerial vehicle horn latching device - Google Patents
Foldable unmanned aerial vehicle horn latching device Download PDFInfo
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- CN205633056U CN205633056U CN201620450006.3U CN201620450006U CN205633056U CN 205633056 U CN205633056 U CN 205633056U CN 201620450006 U CN201620450006 U CN 201620450006U CN 205633056 U CN205633056 U CN 205633056U
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- horn
- draw
- buckle
- groove
- fuselage
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Abstract
The utility model provides a foldable unmanned aerial vehicle horn latching device for locking after foldable unmanned aerial vehicle horn is opened, the horn articulates on the fuselage, and latching device includes buckle and draw -in groove, and the buckle articulates the one side that is close to the horn at the unmanned aerial vehicle fuselage, and buckle and draw -in groove cooperation set up. When the horn was opened, the rotation buckle made fuselage and horn lock relatively in making its card income draw -in groove, need fold when depositing as unmanned aerial vehicle, open latching device, make buckle and draw -in groove break away from, rotate the horn and make its be close to fuselage relatively, the volume can be reduced is convenient for accomodate, carry. This latching device simple structure, convenient operation.
Description
Technical field
This utility model belongs to unmanned air vehicle technique field, is specifically related to a kind of collapsible unmanned plane horn kayser dress
Put.
Background technology
The most volume of unmanned plane is relatively big in the market, and the horn especially stretched out occupies the biggest space, for
The depositing of unmanned plane, transport and cause the biggest trouble.Consumer level unmanned plane is badly in need of making as a kind of portable equipment
It makes its miniaturization and portability in the case of keeping its original function.Application No. 201510439156.4
Patent, entitled one collapsible unmanned plane horn locking device, this application uses driving lever and snap fit to horn
Lock and unlock, but its structure is complex.Utility model patent 201520772186.2, entitled
Unmanned plane horn fold mechanism and unmanned plane, it is the next that this application uses scalable horn and bayonet socket to fix on horn
Put, but this can make horn become unstable along its telescopic direction.
Summary of the invention
The purpose of this utility model is to provide a kind of collapsible unmanned plane horn buckling and locking device, solves prior art
The technical problem that middle unmanned plane horn buckling and locking device structure is complicated, locking is unstable.
In order to solve above-mentioned technical problem, this utility model adopts the following technical scheme that
A kind of collapsible unmanned plane horn buckling and locking device, the locking after collapsible unmanned plane horn is opened, institute
Stating horn to be hinged on fuselage, buckling and locking device includes buckle and draw-in groove, and buckle is hinged on unmanned aerial vehicle body near machine
The side of arm, buckle and draw-in groove are equipped with.When horn is opened, rotate buckle and make it snap in draw-in groove,
Make that fuselage is relative with horn to be locked；When unmanned plane needs stored collapsed, open buckling and locking device, make buckle and card
Groove departs from, and rotates horn and makes its relatively close fuselage, reduces volume, it is simple to receive, carry.This buckling and locking device
Simple in construction, easy to operate.
Improving further, described draw-in groove includes two parts, for first part and Part II, wherein the first position
On fuselage, Part II is positioned on horn；When described horn is opened, the sidewall that two parts of draw-in groove are corresponding is total to
Face, rotates buckle and makes it snap in draw-in groove, make that fuselage is relative with horn to be locked.
Improving further, the Part I of described draw-in groove is divided into two sections by horn, for first paragraph and second segment, its
Middle first paragraph is near the hinged place of buckle, and second segment is away from the hinged place of buckle.Horn is arranged on fuselage side
Middle part, then the Part I of draw-in groove is divided into two sections by horn, so when opening horn, rotates buckle and makes it snap in
Time in draw-in groove, then the draw-in groove Part II being positioned on horn is surrounded by fuselage upper and lower part and buckle and locks,
Improve locking effect.
Improving further, one end away from hinged place of described buckle is provided with barb, the second segment of draw-in groove sets
It is equipped with barb draw-in groove；When described horn is opened, rotating buckle and make it snap in draw-in groove, barb snaps in barb draw-in groove
In, prevent unmanned plane buckle in flight course from undesirably falling off draw-in groove.
Improving further, the middle part of the inner side of described buckle is provided with support member, when described horn is opened, rotates
Buckle makes it snap in draw-in groove, and support member offsets with the bottom surface of draw-in groove Part II, it is ensured that horn with fuselage is
One entirety, prevents unmanned plane from affecting because producing relative rocking between horn with fuselage in flight course normally
Flight.
Improving further, described support member is two, by increasing the quantity of support member, it is ensured that horn and fuselage
Steadiness.
Improving further, the back side of described buckle is cambered surface, when described horn is opened, rotates buckle and makes it snap in
In draw-in groove, the back side of buckle is connected smoothly with the surface of fuselage, horn.
Compared with prior art, this utility model has the advantages that
1, by arranging this buckling and locking device, when horn is opened, rotate buckle and make it snap in draw-in groove, make machine
Body is relative with horn to be locked；When unmanned plane needs stored collapsed, open buckling and locking device, make buckle take off with draw-in groove
From, rotate horn and make its relatively close fuselage, reduce volume, it is simple to receive, carry.This buckling and locking device structure
Simply, easy to operate.
2, by arranging barb and barb draw-in groove, when horn is opened, rotate buckle and make it snap in draw-in groove,
Barb snaps in barb draw-in groove, prevents unmanned plane buckle in flight course from undesirably falling off draw-in groove.
3, by being provided with support member at the middle part of the inner side of buckle, when horn is opened, rotate buckle and make it block
Entering in draw-in groove, support member offsets with the bottom surface of draw-in groove Part II, it is ensured that horn and fuselage are an entirety,
Prevent unmanned plane from affecting normal flight because producing relative rocking between horn with fuselage in flight course, locking
Effect stability.
Accompanying drawing explanation
Fig. 1 is the structural representation of the novel described cloud unmanned plane of this reality.
Fig. 2 is the structural representation of the novel described collapsible unmanned plane horn buckling and locking device of this reality.
Fig. 3 is the structural representation of the novel described buckle of this reality.
Detailed description of the invention
In order to be more fully understood that this utility model, explain of the present utility model interior further below in conjunction with embodiment
Hold, but content of the present utility model is not limited solely to the following examples.
As Figure 1-3, a kind of collapsible unmanned plane horn buckling and locking device, for collapsible unmanned plane horn 2
Locking after opening, described horn 2 is hinged on the fuselage 1, and buckling and locking device includes buckle 3 and draw-in groove 4, card
Button 3 is hinged on the unmanned aerial vehicle body 1 side near horn 2, buckle 3 and draw-in groove 4 and is equipped with.Work as machine
When arm 2 is opened, rotate buckle 3 and make it snap in draw-in groove 4, make that fuselage 1 is relative with horn 2 to be locked；Work as nothing
Man-machine when needing stored collapsed, open buckling and locking device, make buckle 3 depart from draw-in groove 4, rotate horn 2 and make it
Relatively close fuselage 1, reduces volume, it is simple to receives, carry.This buckling and locking device simple in construction, easy to operate.
In this application, when snapping in draw-in groove 4 with buckle 3, buckle 3 is inner side near the side of fuselage, away from machine
The side of body 1 is outside.
In the present embodiment, described draw-in groove 4 includes two parts, for first part and Part II, and wherein first
Portion is positioned on fuselage 1, and Part II is positioned on horn 2；When described horn 2 is opened, two parts of draw-in groove 4
Corresponding sidewall is coplanar, rotates buckle 3 and makes it snap in draw-in groove 4, makes that fuselage 1 is relative with horn 2 to be locked.
In the present embodiment, the Part I of described draw-in groove 4 is divided into two sections by horn 2, for first paragraph and second
Section, wherein first paragraph is near the hinged place of buckle 3, and second segment is away from the hinged place of buckle 3.Horn 2 is arranged
At the middle part of fuselage 1 side, the Part I of draw-in groove 4 is divided into two sections by horn 2, so when opening horn 2,
When rotation buckle 3 makes it snap in draw-in groove 4, then the draw-in groove Part II being positioned on horn 2 is upper and lower by fuselage
Portion and buckle 3 are surrounded and are locked, and improve locking effect.
In the present embodiment, one end away from hinged place of described buckle 3 is provided with barb 31, the of draw-in groove 4
Barb draw-in groove it is provided with on two-stage nitration；When described horn 2 is opened, rotate buckle 3 and make it snap in draw-in groove 4, fall
Hook 31 snaps in barb draw-in groove, prevents unmanned plane buckle 3 in flight course from undesirably falling off draw-in groove 4.
In the present embodiment, the middle part of the inner side of described buckle 3 is provided with support member 32, and described horn 2 is opened
Time, rotating buckle 3 and make it snap in draw-in groove 4, support member 32 offsets with the bottom surface of draw-in groove 4 Part II,
Ensure that horn 2 and fuselage 1 are an entirety, prevent unmanned plane in flight course because of horn 2 and fuselage 1
Between produce and relatively rock and affect normal flight.
In the present embodiment, described support member 32 is two, by increasing the quantity of support member 32, it is ensured that machine
Arm 2 and the steadiness of fuselage 1.In other embodiments, support member 32 can be one or three or more
Individual.
In the present embodiment, the back side of described buckle 3 is cambered surface, when described horn 2 is opened, rotates buckle 3
Making it snap in draw-in groove 4, the back side of buckle 3 is connected smoothly with the surface of fuselage 1, horn 2.
This utility model does not does illustrate be prior art or can be realized by prior art, and
And be embodied as case described in this utility model and be only preferable case study on implementation of the present utility model, not use
Limit practical range of the present utility model.The most all according to the content of this utility model claim made etc.
Effect change and modification, all should be used as technology category of the present utility model.
Claims (7)
1. a collapsible unmanned plane horn buckling and locking device, the locking after collapsible unmanned plane horn is opened,
Described horn is hinged on fuselage, it is characterised in that include buckle and draw-in groove, and buckle is hinged on unmanned aerial vehicle body
Near the side of horn, buckle and draw-in groove are equipped with.
Collapsible unmanned plane horn buckling and locking device the most according to claim 1, it is characterised in that described
Draw-in groove includes two parts, and for first part and Part II, wherein first is positioned on fuselage, Part II position
On horn；When described horn is opened, the sidewall that two parts of draw-in groove are corresponding is coplanar, rotates buckle and makes it snap in
In draw-in groove, make that fuselage is relative with horn to be locked.
Collapsible unmanned plane horn buckling and locking device the most according to claim 2, it is characterised in that described
The Part I of draw-in groove is divided into two sections by horn, and for first paragraph and second segment, wherein first paragraph is near the hinge of buckle
Meeting place, second segment is away from the hinged place of buckle.
Collapsible unmanned plane horn buckling and locking device the most according to claim 3, it is characterised in that described
One end away from hinged place of buckle is provided with barb, and the second segment of draw-in groove is provided with barb draw-in groove；Described machine
When arm is opened, rotating buckle and make it snap in draw-in groove, barb snaps in barb draw-in groove.
5., according to the collapsible unmanned plane horn buckling and locking device according to any one of claim 2-4, its feature exists
In, the middle part of the inner side of described buckle is provided with support member, when described horn is opened, rotates buckle and makes it snap in
In draw-in groove, support member offsets with the bottom surface of draw-in groove Part II.
Collapsible unmanned plane horn buckling and locking device the most according to claim 5, it is characterised in that described
Support member is two.
7. according in claim 1-4 described collapsible unmanned plane horn buckling and locking device, it is characterised in that
The back side of described buckle is cambered surface, when described horn is opened, rotates buckle and makes it snap in draw-in groove, the back of the body of buckle
Face is connected smoothly with the surface of fuselage, horn.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201620450006.3U CN205633056U (en) | 2016-05-17 | 2016-05-17 | Foldable unmanned aerial vehicle horn latching device |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201620450006.3U CN205633056U (en) | 2016-05-17 | 2016-05-17 | Foldable unmanned aerial vehicle horn latching device |
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| Publication Number | Publication Date |
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| CN205633056U true CN205633056U (en) | 2016-10-12 |
Family
ID=57057343
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
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| CN201620450006.3U Active CN205633056U (en) | 2016-05-17 | 2016-05-17 | Foldable unmanned aerial vehicle horn latching device |
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Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN107000834A (en) * | 2016-12-07 | 2017-08-01 | 深圳市大疆创新科技有限公司 | Many rotor unmanned aircrafts |
| CN107697265A (en) * | 2017-09-11 | 2018-02-16 | 珠海天晴航空航天科技有限公司 | A kind of fuselage wing attachment structure and locking device |
| WO2018157833A1 (en) * | 2017-03-02 | 2018-09-07 | 亿航智能设备（广州）有限公司 | Novel unmanned aerial vehicle |
| CN111301663A (en) * | 2020-03-16 | 2020-06-19 | 王会涛 | Arm folding and rotating device for multi-gyroplane |
-
2016
- 2016-05-17 CN CN201620450006.3U patent/CN205633056U/en active Active
Cited By (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN107000834A (en) * | 2016-12-07 | 2017-08-01 | 深圳市大疆创新科技有限公司 | Many rotor unmanned aircrafts |
| WO2018103026A1 (en) * | 2016-12-07 | 2018-06-14 | 深圳市大疆创新科技有限公司 | Multi-rotor unmanned aerial vehicle |
| CN107000834B (en) * | 2016-12-07 | 2019-05-24 | 深圳市大疆创新科技有限公司 | More rotor unmanned aircrafts |
| WO2018157833A1 (en) * | 2017-03-02 | 2018-09-07 | 亿航智能设备（广州）有限公司 | Novel unmanned aerial vehicle |
| CN107697265A (en) * | 2017-09-11 | 2018-02-16 | 珠海天晴航空航天科技有限公司 | A kind of fuselage wing attachment structure and locking device |
| CN111301663A (en) * | 2020-03-16 | 2020-06-19 | 王会涛 | Arm folding and rotating device for multi-gyroplane |
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