CN208616185U - A kind of unmanned plane - Google Patents
A kind of unmanned plane Download PDFInfo
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- CN208616185U CN208616185U CN201821116255.4U CN201821116255U CN208616185U CN 208616185 U CN208616185 U CN 208616185U CN 201821116255 U CN201821116255 U CN 201821116255U CN 208616185 U CN208616185 U CN 208616185U
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- horn
- accommodating groove
- unmanned plane
- fuselage
- blade
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Abstract
The utility model discloses a kind of unmanned planes, including fuselage and the horn that the fuselage two sides are arranged in, the fuselage two sides are provided with accommodating groove, and the accommodating groove is extended along fuselage side front-rear direction, and the horn folding storage is in the accommodating groove.The utility model is collapsed so that horn folds into accommodating groove by the way that accommodating groove is arranged on the two sides of fuselage, substantially reduces the size after collapsing in unmanned plane width direction, so that the size after unmanned plane collapses is reduced, it is easy to carry；Meanwhile there is certain protective effect, and good integrity to horn in horn gathering to accommodating groove, increase aesthetic effect.
Description
Technical field
The utility model relates to unmanned aerial vehicle design technical fields, and in particular to a kind of small and exquisite, compact unmanned plane.
Background technique
Unmanned plane is widely used because to have the advantages that maneuverability, rapid reaction, unmanned flight, operation require low for it
In fields such as agricultural, exploration, photography, border patrols.
It is provided with folding horn on existing unmanned aerial vehicle body, folds the side that horn is directly folded in fuselage, this set
Although mode can reduce the volume after unmanned plane collapses to a certain extent, the unmanned plane volume that remains unchanged after collapsing is larger,
It is not readily portable.
Utility model content
In order to solve the problems, such as that the volume after existing unmanned plane collapses is big, not readily portable, the utility model provides one
Small and exquisite, the compact unmanned plane of kind, including fuselage and the horn that the fuselage two sides are arranged in, the fuselage two sides are provided with receipts
Receive slot, and the accommodating groove is extended along fuselage side front-rear direction, the horn folding storage is in the accommodating groove
It is interior.
Preferably, the fuselage two sides are respectively provided with two horns, respectively preceding horn and rear horn；The preceding horn and
Horn is pivotally attached to the front and back end of the accommodating groove respectively afterwards, and the preceding horn and the rear horn rotation are accommodated in the receipts
It receives in slot.
Preferably, the link position of the preceding horn, the rear horn and the accommodating groove is not located in same level.
Preferably, the rear horn is located at institute after the preceding horn, the rear horn rotation are accommodated in the accommodating groove
The top of horn before stating.
Preferably, the front and back end of the accommodating groove is respectively arranged with preceding attachment base, rear attachment base；One end of the preceding horn
It is pivotally attached on the preceding attachment base, the first propeller mounting base is provided on the other end；One end rotation of horn after described
It is connected on the rear attachment base, the second propeller mounting base is provided on the other end；
After the preceding horn, rear horn are received into the accommodating groove, the first propeller mounting base be stuck in it is described after
Between attachment base and the rear end face of the accommodating groove；The second propeller mounting base is against on the front end face of the accommodating groove.
Preferably, the preceding attachment base, it is described after attachment base be all made of reverse U-shaped seat, the preceding horn, it is described after
One end of horn is mounted in U-typed seat by shaft.
Preferably, being provided with propeller, the spiral in the first propeller mounting base, the second propeller mounting base
Paddle includes motor, blade seat and blade, and the motor is mounted on the first propeller mounting base/second propeller mounting base
On, the blade seat is mounted on the motor, and the blade is mounted on the blade seat.
Preferably, the blade is rotatably installed on the blade seat, the blade rotation is accommodated in the accommodating groove.
The utility model due to using the technology described above, is allowed to compared with prior art, have the following advantages that and accumulate
Pole effect:
Unmanned plane provided by the utility model is received by the way that accommodating groove is arranged on the two sides of fuselage so that horn folds
Hold together into accommodating groove, substantially reduce the size after collapsing in unmanned plane width direction, thus after reducing unmanned plane gathering
Size, it is easy to carry；Meanwhile there is certain protective effect, and good integrity to horn in horn gathering to accommodating groove, increase
Big aesthetic effect.
Detailed description of the invention
In conjunction with attached drawing, by hereafter state detailed description, can be more clearly understood that the above-mentioned and other spy of the utility model
It seeks peace advantage, in which:
Fig. 1 is unmanned plane horn unfolded state schematic diagram provided by the utility model；
Fig. 2 is unmanned plane horn rounding state schematic diagram provided by the utility model.
Symbol description:
1- fuselage, 101- accommodating groove fold horn after 2-, and horn, attachment base after 4-, the second propeller of 5- peace are folded before 3-
Fill seat, attachment base before 6-, 7- the first propeller mounting base, 8- blade, 9- blade seat.
Specific embodiment
Referring to the attached drawing for showing the utility model embodiment, the utility model is described in more detail.However, this reality
It can be realized in many different forms with novel, and should not be construed as being limited by the embodiment herein proposed.On the contrary, proposing
These embodiments be in order to reach sufficiently and complete disclosure, and make those skilled in the art understands completely this it is practical newly
The range of type.In these attached drawings, for clarity, the size and relative size in layer and region may be exaggerated.
Referring to Fig.1-2, the utility model provides a kind of small and exquisite, compact unmanned plane, including fuselage 1 and setting in fuselage
The horn of 1 two sides, 1 two sides of fuselage are provided with accommodating groove 101, and accommodating groove 101 is set along the extension of 1 side front-rear direction of fuselage
It sets, horn folding storage is in accommodating groove 101.
Unmanned plane provided by the utility model, by the way that accommodating groove 101 is arranged on the two sides of fuselage, so that horn folds
It collapses in accommodating groove 101, substantially reduces the size after collapsing in unmanned plane width direction, to reduce unmanned plane gathering
Size afterwards, it is easy to carry；Meanwhile there is certain protective effect to horn in horn gathering to accommodating groove 101, and whole
Property is good, increases aesthetic effect.
In the present embodiment, accommodating groove 101 uses structure shown in FIG. 1, certainly the accommodating groove 101 in other area's embodiments
Shape can also be adjusted as the case may be, herein with no restrictions, as long as guarantee to a certain extent accommodate horn effect
?.
In the present embodiment, 1 two sides of fuselage are respectively provided with two horns, respectively preceding horn 3 and rear horn 2；Preceding horn 3 is with after
Horn 2 is pivotally attached to the front and back end of accommodating groove 101 respectively, and preceding horn 3 and rear horn 2 are turned to be extended along 1 side of fuselage
Arrangement, to be accommodated in accommodating groove 101.
Wherein, the link position of preceding horn 3, rear horn 2 and accommodating groove 101 is not located at same level, i.e., preceding horn 3,
After the rotation of horn 2 is accommodated in accommodating groove 101 afterwards, preceding horn 3, about 2 rear horn are arranged, in the present embodiment 2 cloth of rear horn
It sets in the top of preceding horn 3, is also designed to the top that preceding horn 3 is arranged in rear horn 2 in other embodiments certainly, herein
With no restrictions.The present embodiment is by the restriction on the position to preceding horn 3, rear horn 2, so that preceding horn 3, rear horn 2
It is set side by side up and down after gathering, so that the size of unmanned plane width direction after gathering is further shortened, it is further to reduce
The size of unmanned plane.
In the present embodiment, the front and back end of accommodating groove 101 is respectively arranged with preceding attachment base 6, rear attachment base 4；Preceding horn 3
Before one end is pivotally attached on attachment base 6, one end of rear horn 2 is pivotally attached on rear attachment base 4.
Further, preceding attachment base 6, rear attachment base 4 are all made of reverse U-shaped seat, one end of preceding horn 3, rear horn 2
It is mounted in U-typed seat by shaft；Certainly, in other embodiments, the specific structure shape of preceding attachment base 6, rear attachment base 4
Rotation connection mode between formula and preceding horn 3, rear horn 2 and preceding attachment base 6, rear attachment base 4, can be according to specific feelings
Condition is adjusted, herein with no restrictions, as long as guaranteeing that preceding horn 3, rear horn 2 can rotate in the horizontal plane.
In the present embodiment, the first propeller mounting base 7, the other end of rear horn 2 are provided on the other end of preceding horn 3
On be provided with the second propeller mounting base 5, the first propeller mounting base 7 upwardly extends setting, the second spiral perpendicular to preceding horn 3
Paddle mounting base 5 upwardly extends setting perpendicular to rear horn 2.
As shown in Figure 2, after preceding horn 3, rear horn 2 are received into accommodating groove 101, the first propeller mounting base 5 is stuck in
Afterwards between attachment base 4 and the rear end face of accommodating groove 101, the second propeller mounting base 5 is against on the front end face of accommodating groove 101；On
State preceding horn 3, the tucked way of rear horn 2 makes the storage of unmanned plane more compact, be conducive to further reduce collapse after
The size of unmanned plane, and preceding horn 3, rear horn 2 is avoided arbitrarily to be unfolded after collapsing.
In this embodiment, the first propeller mounting base 7, be provided with propeller, propeller in the second propeller mounting base 5
Motor, blade seat 9 and blade 8 are generally included, motor is mounted on 7/ second propeller mounting base 5 of the first propeller mounting base
On, blade seat 9 is mounted on motor, and blade 8 is rotatably installed on blade seat 9；When needing to pack up unmanned plane, turn first
Blade 8 on dynamic blade seat 9 is collapsed into it to be arranged along horn 2 after preceding horn 3/, be rotated further by preceding horn 3, rear horn 2 will be whole
A horn is collapsed into accommodating groove 101.
Blade design is that can be rotated blade by the present embodiment, so that blade can also rotate during unmanned plane collapses
It collapses in accommodating groove 101, is conducive to the size for further reducing the unmanned plane after collapsing, it is easy to carry.
Those skilled in the art should be understood that the utility model can be realized with many other concrete forms without de-
Spirit or scope from itself.Although the case study on implementation of the utility model has been described, it should be understood that the utility model should not limit
Be made as these embodiments, those skilled in the art can as defined by the following claims the spirit of the utility model and
Within the scope of make change and modification.
Claims (8)
1. a kind of unmanned plane, which is characterized in that including fuselage and the horn that the fuselage two sides are arranged in, the fuselage two sides
It is provided with accommodating groove, and the accommodating groove is extended along fuselage side front-rear direction, the horn folding storage is in institute
It states in accommodating groove.
2. unmanned plane according to claim 1, which is characterized in that the fuselage two sides are respectively provided with two horns, respectively
For preceding horn and rear horn；The preceding horn and rear horn are pivotally attached to the front and back end of the accommodating groove, the preceding machine respectively
Arm and the rear horn rotation are accommodated in the accommodating groove.
3. unmanned plane according to claim 2, which is characterized in that the preceding horn, the rear horn and the accommodating groove
Link position be not located in same level.
4. unmanned plane according to claim 3, which is characterized in that the preceding horn, the rear horn rotation are accommodated in institute
After stating in accommodating groove, the rear horn is located at the top of the preceding horn.
5. according to unmanned plane described in Claims 2 or 3 or 4, which is characterized in that the front and back end of the accommodating groove is respectively arranged with
Preceding attachment base, rear attachment base；One end of the preceding horn is pivotally attached on the preceding attachment base, and first is provided on the other end
Propeller mounting base；One end of horn is pivotally attached on the rear attachment base after described, and the second spiral is provided on the other end
Paddle mounting base；
After the preceding horn, rear horn are received into the accommodating groove, the first propeller mounting base is stuck in the rear connection
Between seat and the rear end face of the accommodating groove；The second propeller mounting base is against on the front end face of the accommodating groove.
6. unmanned plane according to claim 5, which is characterized in that the preceding attachment base, the rear attachment base are all made of down
The U-typed seat set, the preceding horn, it is described after one end of horn be mounted in U-typed seat by shaft.
7. unmanned plane according to claim 5, which is characterized in that the first propeller mounting base, the second propeller peace
It is provided with propeller on dress seat, the propeller includes motor, blade seat and blade, and the motor is mounted on described first
In propeller mounting base/second propeller mounting base, the blade seat is mounted on the motor, and the blade is mounted on described
On blade seat.
8. unmanned plane according to claim 7, which is characterized in that the blade is rotatably installed on the blade seat, institute
Blade rotation is stated to be accommodated in the accommodating groove.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201821116255.4U CN208616185U (en) | 2018-07-13 | 2018-07-13 | A kind of unmanned plane |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201821116255.4U CN208616185U (en) | 2018-07-13 | 2018-07-13 | A kind of unmanned plane |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN208616185U true CN208616185U (en) | 2019-03-19 |
Family
ID=65705562
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201821116255.4U Active CN208616185U (en) | 2018-07-13 | 2018-07-13 | A kind of unmanned plane |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN208616185U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN110341896A (en) * | 2019-07-25 | 2019-10-18 | 广东华中科技大学工业技术研究院 | A kind of empty amphibious unmanned boat of water and its application method |
-
2018
- 2018-07-13 CN CN201821116255.4U patent/CN208616185U/en active Active
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN110341896A (en) * | 2019-07-25 | 2019-10-18 | 广东华中科技大学工业技术研究院 | A kind of empty amphibious unmanned boat of water and its application method |
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