CN205891210U - Unmanned aerial vehicle horn folding mechanism and plant protection unmanned aerial vehicle - Google Patents
Unmanned aerial vehicle horn folding mechanism and plant protection unmanned aerial vehicle Download PDFInfo
- Publication number
- CN205891210U CN205891210U CN201620619436.3U CN201620619436U CN205891210U CN 205891210 U CN205891210 U CN 205891210U CN 201620619436 U CN201620619436 U CN 201620619436U CN 205891210 U CN205891210 U CN 205891210U
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- Prior art keywords
- unmanned plane
- folded piece
- installing hole
- alignment pin
- horn
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- 239000002002 slurry Substances 0.000 description 3
- 230000004048 modification Effects 0.000 description 2
- 238000012986 modification Methods 0.000 description 2
- 230000009286 beneficial effect Effects 0.000 description 1
- 239000008280 blood Substances 0.000 description 1
- 210000004369 blood Anatomy 0.000 description 1
- 230000007547 defect Effects 0.000 description 1
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Abstract
The utility model provides an unmanned aerial vehicle horn folding mechanism and plant protection unmanned aerial vehicle, including first folded piece and second folded piece, wherein, first folded piece is provided with first pivot mounting hole and first locating pin mounting hole, the second folded piece be provided with with first pivot mounting hole assorted second pivot mounting hole, with first locating pin mounting hole assorted second locating pin mounting hole, first pivot mounting hole with be provided with the pivot in the second pivot mounting hole, first locating pin mounting hole with be provided with the locating pin in the second locating pin mounting hole. The utility model provides having risen unmanned aerial vehicle, specifically being the portability of many rotor crafts, first folded piece and second folded piece quick assembly disassembly can be realized to the spring position fixing round pin, have saved the time.
Description
Technical field
This utility model is related to unmanned plane, in particular it relates to a kind of unmanned plane horn fold mechanism and plant protection unmanned plane.
Background technology
General multi-rotor aerocraft cannot be folded due to horn, leads to take up room greatly.In addition, with the machine being folded down
The aircraft of arm has the risk damaging oar in transportation again.Therefore, laterally folded horn have save space more portable,
The advantages of transportation is without having to worry about damaging oar.
Through the retrieval to prior art, find Application No. 201410241181.7, entitled many rotor wing unmanned aerial vehicles
Patent discloses a kind of many rotor wing unmanned aerial vehicles, including fuselage fairshaped in strip, described fuselage be provided with multiple with respect to institute
State the slurry arm that the symmetrical plane in fuselage is symmetric, the outer end of each slurry arm is provided with paddle components, described blade group
Part includes the motor being arranged on described slurry arm and the blade being connected on the output shaft of described motor, the often rotation of a piece of blade
Axis is respectively positioned on the same face of cylinder.But horn cannot fold in this patent, take up room larger it has not been convenient to receive.
Utility model content
For defect of the prior art, the purpose of this utility model is to provide a kind of unmanned plane horn fold mechanism and plant
Protect unmanned plane.
The unmanned plane horn fold mechanism being provided according to this utility model is it is characterised in that include the first folded piece and the
Eighty percent discount overlapping piece；
Wherein, described first folded piece is provided with first rotating shaft installing hole and the first alignment pin installing hole；
Described second folded piece is provided with the second rotating shaft installing hole matching with described first rotating shaft installing hole, and described
The second alignment pin installing hole that first alignment pin installing hole matches；
Described first rotating shaft installing hole and described second rotating shaft are installed in the hole and are provided with rotating shaft；Described first alignment pin is installed
Hole and described second alignment pin are installed in the hole and are provided with alignment pin.
Preferably, described alignment pin adopts spring holder；
When by described spring holder pin press-in second alignment pin install in the hole when, will described first folded piece with
The spacing connection of described second folded piece.
Preferably, described rotating shaft adopts socket cap screw.
Preferably, described spring holder includes pin, spring and lock screw；
Wherein, described spring is arranged on described second alignment pin and installs in the hole；Described spring one end is arranged on described second
The bottom hole of alignment pin installing hole, the other end connects one end of described pin；
The thread groove connecting described second alignment pin installing hole is provided with described second folded piece；Described lock screw sets
Put in described thread groove, and described pin is withstood in one end of described lock screw.
Preferably, described pin is provided with the locating slot being matched with one end of described lock screw；
The bottom land of described locating slot is withstood in one end of described lock screw.
Preferably, described thread groove is in waist-hole type.
The plant protection unmanned plane that this utility model provides, including described unmanned plane horn fold mechanism, also includes unmanned plane
Body and horn；
Wherein, described first folded piece is arranged on described unmanned plane body；Described horn connects described second folded piece.
Preferably, one end of described horn is set in described second folded piece.
Preferably, described horn passes through described unmanned plane horn fold mechanism along described unmanned plane body horizontal folding.
Compared with prior art, this utility model has a following beneficial effect:
1st, this utility model improves unmanned plane, the specially portability of multi-rotor aerocraft, and spring holder can be real
Existing first folded piece and the second folded piece fast assembling-disassembling, save the time；
2nd, in this utility model, horn passes through unmanned plane horn fold mechanism along unmanned plane body horizontal folding, that is, realize horizontal
To folding, so that the oar of unmanned plane can be dismounted without frequent in transportation, meanwhile, laterally folded mode more saves sky
Between, the space of formed objects can accommodate more unmanned planes；
3rd, this utility model structure is simple, reliable and stable it is easy to safeguard.
Brief description
By reading detailed description non-limiting example made with reference to the following drawings, of the present utility model other special
Levy, objects and advantages will become more apparent upon:
Fig. 1 is the structural representation in a direction of the present utility model；
Fig. 2 is the structural representation in another direction of the present utility model.
In figure:
1 is the first folded piece；
2 is the second folded piece；
3 is the first alignment pin installing hole；
4 is first rotating shaft installing hole；
5 is thread groove；
6 is horn.
Specific embodiment
With reference to specific embodiment, this utility model is described in detail.Following examples will be helpful to this area
Technical staff further understands this utility model, but does not limit this utility model in any form.It should be pointed out that to ability
For the those of ordinary skill in domain, without departing from the concept of the premise utility, some deformation can also be made and improve.
These broadly fall into protection domain of the present utility model.
In the present embodiment, the unmanned plane horn fold mechanism that this utility model provides, including the first folded piece and second
Folded piece；
Wherein, described first folded piece is provided with first rotating shaft installing hole and the first alignment pin installing hole；
Described second folded piece is provided with the second rotating shaft installing hole matching with described first rotating shaft installing hole, and described
The second alignment pin installing hole that first alignment pin installing hole matches；
Described first rotating shaft installing hole and described second rotating shaft are installed in the hole and are provided with rotating shaft；Described first alignment pin is installed
Hole and described second alignment pin are installed in the hole and are provided with alignment pin.
Described alignment pin adopts spring holder；
When in the hole installed by pin press-in the second alignment pin by described spring holder, by described first folded piece and institute
State the spacing connection of the second folded piece.
Described rotating shaft adopts socket cap screw.
Described spring holder includes pin, spring and lock screw；
Wherein, described spring is arranged on described second alignment pin and installs in the hole；Described spring one end is arranged on described second
The bottom hole of alignment pin installing hole, the other end connects one end of described pin；
The thread groove connecting described second alignment pin installing hole is provided with described second folded piece；Described lock screw sets
Put in described thread groove, and described pin is withstood in one end of described lock screw.
One end of described second installing hole arranges the first limiting stand terrace, and the other end is provided with the second limiting stand terrace；
One end of described spring is arranged on described first limiting stand terrace；One end of described pin is provided with and the second limit
The locating part that position step surface matches.
The locating slot being matched with one end of described lock screw is provided with described pin；One end of described lock screw
Withstand the bottom land of described locating slot.
Described thread groove is in waist-hole type.
The unmanned plane that this utility model provides, it is characterised in that including described unmanned plane horn fold mechanism, also includes
Unmanned plane body and horn；Wherein, described first folded piece is arranged on described unmanned plane body；Described horn connects described the
Eighty percent discount overlapping piece.
One end of described horn is set in described second folded piece.Described horn passes through described unmanned plane horn folding machine
Structure is along described unmanned plane body horizontal folding.
In the present embodiment, this utility model improves unmanned plane, the specially portability of multi-rotor aerocraft, and spring is fixed
Position pin is capable of the first folded piece and the second folded piece fast assembling-disassembling, saves the time；In this utility model, horn passes through no
Man-machine horn fold mechanism along unmanned plane body horizontal folding, that is, is realized laterally folded, so that the oar of unmanned plane can be being transported
Without frequent dismounting in journey, meanwhile, laterally folded mode more save space, can accommodate more in the space of formed objects
Unmanned plane；This utility model structure is simple, reliable and stable it is easy to safeguard.
Above specific embodiment of the utility model is described.It is to be appreciated that this utility model not office
It is limited to above-mentioned particular implementation, those skilled in the art can make various modifications or modification within the scope of the claims,
This has no effect on flesh and blood of the present utility model.
Claims (9)
1. a kind of unmanned plane horn fold mechanism is it is characterised in that include the first folded piece and the second folded piece；
Wherein, described first folded piece is provided with first rotating shaft installing hole and the first alignment pin installing hole；
Described second folded piece is provided with the second rotating shaft installing hole matching with described first rotating shaft installing hole, with described first
The second alignment pin installing hole that alignment pin installing hole matches；
Described first rotating shaft installing hole and described second rotating shaft are installed in the hole and are provided with rotating shaft；Described first alignment pin installing hole and
Described second alignment pin is installed in the hole and is provided with alignment pin.
2. unmanned plane horn fold mechanism according to claim 1 is it is characterised in that described alignment pin adopts spring to position
Pin；
When in the hole installed by pin press-in the second alignment pin by described spring holder, by described first folded piece and described the
The spacing connection of eighty percent discount overlapping piece.
3. unmanned plane horn fold mechanism according to claim 1 is it is characterised in that described rotating shaft adopts six in socket cap
Angle screw.
4. unmanned plane horn fold mechanism according to claim 2 is it is characterised in that described spring holder includes pin
Post, spring and lock screw；
Wherein, described spring is arranged on described second alignment pin and installs in the hole；Described spring one end is arranged on described second positioning
The bottom hole of pin installing hole, the other end connects one end of described pin；
The thread groove connecting described second alignment pin installing hole is provided with described second folded piece；Described lock screw is arranged on
In described thread groove, and described pin is withstood in one end of described lock screw.
5. unmanned plane horn fold mechanism according to claim 4 it is characterised in that be provided with described pin with described
The locating slot that one end of lock screw matches；
The bottom land of described locating slot is withstood in one end of described lock screw.
6. unmanned plane horn fold mechanism according to claim 4 is it is characterised in that described thread groove is in waist-hole type.
7. a kind of plant protection unmanned plane is it is characterised in that include the unmanned plane horn folding machine described in any one of claim 1 to 6
Structure, also includes unmanned plane body and horn；
Wherein, described first folded piece is arranged on described unmanned plane body；Described horn connects described second folded piece.
8. plant protection unmanned plane according to claim 7 is it is characterised in that one end of described horn is set in described second folding
In overlapping piece.
9. plant protection unmanned plane according to claim 7 is it is characterised in that described horn passes through described unmanned plane horn folding
Mechanism is along described unmanned plane body horizontal folding.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201620619436.3U CN205891210U (en) | 2016-06-21 | 2016-06-21 | Unmanned aerial vehicle horn folding mechanism and plant protection unmanned aerial vehicle |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201620619436.3U CN205891210U (en) | 2016-06-21 | 2016-06-21 | Unmanned aerial vehicle horn folding mechanism and plant protection unmanned aerial vehicle |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN205891210U true CN205891210U (en) | 2017-01-18 |
Family
ID=57770257
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201620619436.3U Active CN205891210U (en) | 2016-06-21 | 2016-06-21 | Unmanned aerial vehicle horn folding mechanism and plant protection unmanned aerial vehicle |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN205891210U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106904267A (en) * | 2017-04-18 | 2017-06-30 | 昆山优尼电能运动科技有限公司 | Unmanned plane horn mechanism and unmanned plane |
-
2016
- 2016-06-21 CN CN201620619436.3U patent/CN205891210U/en active Active
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106904267A (en) * | 2017-04-18 | 2017-06-30 | 昆山优尼电能运动科技有限公司 | Unmanned plane horn mechanism and unmanned plane |
| CN106904267B (en) * | 2017-04-18 | 2023-08-11 | 昆山合朗航空科技有限公司 | Unmanned aerial vehicle horn mechanism and unmanned aerial vehicle |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| TR01 | Transfer of patent right | ||
| TR01 | Transfer of patent right |
Effective date of registration: 20240116 Address after: No. 158 Tangming Road, Shihudang Town, Songjiang District, Shanghai, April 2016 Patentee after: Shanghai Eagle Peak Industrial Co.,Ltd. Address before: 200135, Room 2203, 1200 Pudong Avenue, Pudong New Area, Shanghai Patentee before: AVIC SHANGHAI XINSHENG AVIATION TECHNOLOGY Co.,Ltd. |
|
| TR01 | Transfer of patent right | ||
| TR01 | Transfer of patent right |
Effective date of registration: 20240427 Address after: No.398, Xinlu Road, Xinbang Town, Songjiang District, Shanghai, 201600 Patentee after: Tushibao (Shanghai) Digital Technology Co.,Ltd. Country or region after: China Address before: No. 158 Tangming Road, Shihudang Town, Songjiang District, Shanghai, April 2016 Patentee before: Shanghai Eagle Peak Industrial Co.,Ltd. Country or region before: China |