CN209037840U - A kind of unmanned plane wing safeguard structure - Google Patents
A kind of unmanned plane wing safeguard structure Download PDFInfo
- Publication number
- CN209037840U CN209037840U CN201821854328.XU CN201821854328U CN209037840U CN 209037840 U CN209037840 U CN 209037840U CN 201821854328 U CN201821854328 U CN 201821854328U CN 209037840 U CN209037840 U CN 209037840U
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- CN
- China
- Prior art keywords
- baffle
- support
- support ring
- buckle
- 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.)
- Expired - Fee Related
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- 230000001681 protective effect Effects 0.000 claims abstract description 13
- 229920003023 plastic Polymers 0.000 claims description 5
- 239000004033 plastic Substances 0.000 claims description 5
- 230000000694 effects Effects 0.000 claims description 2
- 230000001174 ascending effect Effects 0.000 abstract description 3
- 238000010586 diagram Methods 0.000 description 3
- 238000009434 installation Methods 0.000 description 3
- 238000000034 method Methods 0.000 description 3
- RZVHIXYEVGDQDX-UHFFFAOYSA-N 9,10-anthraquinone Chemical compound C1=CC=C2C(=O)C3=CC=CC=C3C(=O)C2=C1 RZVHIXYEVGDQDX-UHFFFAOYSA-N 0.000 description 1
- 230000001771 impaired effect Effects 0.000 description 1
- 230000000630 rising effect Effects 0.000 description 1
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Abstract
The utility model discloses a kind of unmanned plane wing safeguard structures, including drone body, support foot rest, support arm and electric propeller, buckle is connected on the outside of the support arm, the buckle two sides are respectively connected with integrally formed support rod, support ring is equipped with above the electric propeller, the support ring and support rod, which are integrally formed, to be arranged, and is connected with protective device on the outside of the support ring, the protective device includes cutting ferrule, first baffle and second baffle.Protection is supported using support ring above electric propeller, the ascending air that electric propeller can be made to generate is not blocked, guarantee that drone body being capable of stabilized flight, the first baffle in the protective device of support ring side can protect the side of electric propeller simultaneously, the setting of fixed pin and spring is to make first baffle have good elastic property by the elastic force of spring, is hardly damaged when colliding.
Description
Technical field
The utility model relates to air vehicle technique field, specially a kind of unmanned plane wing safeguard structure.
Background technique
For unmanned plane when flight, screw blade touches that will cause screw blade after other objects impaired, when serious
Unmanned plane is resulted even in fall damage.It is such as protected and is tied with wing application No. is a kind of unmanned plane of CN201720949236.9
Structure, including drone body are each provided with 1 cavity on four angles of the drone body；The cavity inside is each
Equipped with 1 wing；1 motor is respectively connected with below the wing；The lower end of the motor is fixedly connected with connecting rod；Institute
The connecting rod stated is fixed in drone body.
The upwind portion that mesh enclosure in above-mentioned safeguard structure be easy to cause screw blade to generate is blocked, so that rising
Air-flow is unstable, the flight control of unmanned plane is influenced, while there is also inconvenience for the replacement of above-mentioned protection mechanism integral demounting, so mentioning
Solved for a kind of unmanned plane wing safeguard structure the above-mentioned problem very it is necessary to.
Utility model content
The purpose of this utility model is to provide a kind of unmanned plane wing safeguard structures, to solve in above-mentioned background technique
The problem of proposition.
To achieve the above object, the utility model provides the following technical solutions: a kind of unmanned plane wing safeguard structure, packet
Drone body, support foot rest, support arm and electric propeller are included, buckle, the buckle two are connected on the outside of the support arm
Side is respectively connected with integrally formed support rod, is equipped with support ring, the support ring and support rod one above the electric propeller
Body formed setting, the support ring outside are connected with protective device, and the protective device includes cutting ferrule, first baffle and second
Baffle, the first baffle and second baffle, which are integrally formed, is connected to cutting ferrule bottom end two sides, the first baffle and second gear
Fixed pin is installed between plate, is socketed with spring on the outside of the fixed pin between the first baffle and second baffle.
Protection is supported using support ring above this setting electric propeller, electric propeller can be made to generate
Ascending air is not blocked, guarantee drone body can stabilized flight, while first in the protective device of support ring side
Baffle can protect the side of electric propeller, and the setting of fixed pin and spring is to make first by the elastic force of spring
Baffle has good elastic property, is hardly damaged when colliding.
Preferably, it is provided with mounting hole on the first baffle and second baffle, the fixed pin activity is through installation
Inside hole.
This setting mounting hole is convenient for the installation of fixed pin.
Preferably, it is fixed by screw between the buckle and support arm and between cutting ferrule and support ring.
Cutting ferrule in this setting safeguard structure is all made of screw with drone body with buckle and fixes, so that safeguard structure
Entirety is easily installed and dismantles, and in safeguard structure damage, is conveniently replaceable.
Preferably, the buckle, support ring, cutting ferrule, first baffle and second baffle are elasticity of plastics component.
This setting buckle, support ring, cutting ferrule, first baffle and second baffle are that there will be good for elasticity of plastics component
Good elasticity, has better protection to electric propeller.
Preferably, the quantity of the buckle, support rod and fixed pin is two groups.
Detailed description of the invention
Fig. 1 is the utility model overlooking structure diagram；
Fig. 2 is the utility model protective device structure schematic diagram；
Fig. 3 is the utility model buckle structure schematic diagram.
In figure: 1, drone body；2, support foot rest；3, mounting hole；4, support arm；5, electric propeller；6, it buckles；7,
Support rod；8, support ring；9, protective device；10, cutting ferrule；11, first baffle；12, second baffle；13, fixed pin；14, spring.
Specific embodiment
The following will be combined with the drawings in the embodiments of the present invention, carries out the technical scheme in the embodiment of the utility model
Clearly and completely describe, it is clear that the described embodiments are only a part of the embodiments of the utility model, rather than whole
Embodiment.Based on the embodiments of the present invention, those of ordinary skill in the art are without making creative work
Every other embodiment obtained, fall within the protection scope of the utility model.
Fig. 1-3 is please referred to, the utility model provides a kind of technical solution: a kind of unmanned plane wing safeguard structure, including
Drone body 1, support foot rest 2, support arm 4 and electric propeller 5 are connected with buckle 6, the card on the outside of the support arm 4
Detain 6 two sides and be respectively connected with integrally formed support rod 7, be equipped with support ring 8 above the electric propeller 5, the support ring 8 with
Support rod 7 is integrally formed setting, is connected with protective device 9 on the outside of the support ring 8, the protective device 9 include cutting ferrule 10,
First baffle 11 and second baffle 12, the first baffle 11 and second baffle 12, which are integrally formed, is connected to 10 bottom end two of cutting ferrule
Side, is equipped with fixed pin 13 between the first baffle 11 and second baffle 12, the first baffle 11 and second baffle 12 it
Between fixed pin 13 on the outside of be socketed with spring 14.
Mounting hole 3 is provided on the first baffle 11 and second baffle 12, the fixed pin 13 is movable through installation
Inside hole 3.It is fixed by screw between the buckle 6 and support arm 4 and between cutting ferrule 10 and support ring 8.The buckle
6, support ring 8, cutting ferrule 10, first baffle 11 and second baffle 12 are elasticity of plastics component.It is described to buckle 6, support rod 7 and consolidate
The quantity of rationed marketing 13 is two groups.
Working principle: the utility model structure novel is supported protection using support ring 8 above electric propeller 5, can
So that electric propeller 5 generate ascending air be not blocked, guarantee drone body 1 can stabilized flight, support simultaneously
First baffle 11 in the protective device 9 of 8 side of ring can protect the side of electric propeller 5, fixed pin 13 and bullet
The setting of spring 14 is to make first baffle 11 have good elastic property by the elastic force of spring 14, first gear when colliding
Plate 11 is hardly damaged；Cutting ferrule 10 in safeguard structure is all made of screw with drone body 1 with buckle 6 and fixes, so that protection knot
Structure is integrally easily installed and dismantles, and in safeguard structure damage, is conveniently replaceable；Buckle 6, support ring 8, cutting ferrule 10, first baffle
11 and second baffle 12 be that elasticity of plastics component then can make safeguard structure integrally and have good elasticity, to electric propeller
5 have better protection.
While there has been shown and described that the embodiments of the present invention, for the ordinary skill in the art,
It is understood that these embodiments can be carried out with a variety of variations in the case where not departing from the principles of the present invention and spirit, repaired
Change, replacement and variant, the scope of the utility model is defined by the appended claims and the equivalents thereof.
Claims (5)
1. a kind of unmanned plane wing safeguard structure, including drone body (1), support foot rest (2), support arm (4) and electronic
Propeller (5), it is characterised in that: be connected with buckle (6) on the outside of the support arm (4), described buckle (6) two sides are respectively connected with one
Body formed support rod (7), electric propeller (5) top are equipped with support ring (8), the support ring (8) and support rod (7)
It is integrally formed setting, is connected with protective device (9) on the outside of the support ring (8), the protective device (9) includes cutting ferrule
(10), first baffle (11) and second baffle (12), the first baffle (11) and second baffle (12) are integrally formed connection
It is equipped with fixed pin (13) between cutting ferrule (10) bottom end two sides, the first baffle (11) and second baffle (12), described
Spring (14) are socketed on the outside of fixed pin (13) between one baffle (11) and second baffle (12).
2. a kind of unmanned plane wing safeguard structure according to claim 1, it is characterised in that: the first baffle (11)
With mounting hole (3) are provided on second baffle (12), the fixed pin (13) activity is internal through mounting hole (3).
3. a kind of unmanned plane wing safeguard structure according to claim 1, it is characterised in that: the buckle (6) and branch
It is fixed by screw between brace (4) and between cutting ferrule (10) and support ring (8).
4. a kind of unmanned plane wing safeguard structure according to claim 1, it is characterised in that: the buckle (6), support
Ring (8), cutting ferrule (10), first baffle (11) and second baffle (12) are elasticity of plastics component.
5. a kind of unmanned plane wing safeguard structure according to claim 1, it is characterised in that: the buckle (6), support
The quantity of bar (7) and fixed pin (13) is two groups.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201821854328.XU CN209037840U (en) | 2018-11-12 | 2018-11-12 | A kind of unmanned plane wing safeguard structure |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201821854328.XU CN209037840U (en) | 2018-11-12 | 2018-11-12 | A kind of unmanned plane wing safeguard structure |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN209037840U true CN209037840U (en) | 2019-06-28 |
Family
ID=67041367
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201821854328.XU Expired - Fee Related CN209037840U (en) | 2018-11-12 | 2018-11-12 | A kind of unmanned plane wing safeguard structure |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN209037840U (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN110667834A (en) * | 2019-11-18 | 2020-01-10 | 湖南捷飞科技有限公司 | Wing protective structure for unmanned aerial vehicle |
| CN112212881A (en) * | 2020-12-14 | 2021-01-12 | 成都飞航智云科技有限公司 | Flight navigator based on big dipper is used |
-
2018
- 2018-11-12 CN CN201821854328.XU patent/CN209037840U/en not_active Expired - Fee Related
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN110667834A (en) * | 2019-11-18 | 2020-01-10 | 湖南捷飞科技有限公司 | Wing protective structure for unmanned aerial vehicle |
| CN112212881A (en) * | 2020-12-14 | 2021-01-12 | 成都飞航智云科技有限公司 | Flight navigator based on big dipper is used |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| CP02 | Change in the address of a patent holder | ||
| CP02 | Change in the address of a patent holder |
Address after: No.5 workshop, No.398, Wenhui Road, Wuyi Town, Chuzhou City, Anhui Province Patentee after: Anhui dream wing UAV Technology Co., Ltd. Address before: No.5 workshop, No.398, Wenhui Road, Wuyi Town, Chuzhou City, Anhui Province Patentee before: Anhui dream wing UAV Technology Co., Ltd. |
|
| 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: 20190628 Termination date: 20201112 |