CN211281462U - Unmanned aerial vehicle with wing protection architecture - Google Patents
Unmanned aerial vehicle with wing protection architecture Download PDFInfo
- Publication number
- CN211281462U CN211281462U CN201922150312.1U CN201922150312U CN211281462U CN 211281462 U CN211281462 U CN 211281462U CN 201922150312 U CN201922150312 U CN 201922150312U CN 211281462 U CN211281462 U CN 211281462U
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- aerial vehicle
- unmanned aerial
- wing
- shield structure
- motor
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Abstract
The utility model discloses an unmanned aerial vehicle with wing protection structure, including the unmanned aerial vehicle body, install battery, wing and motor on the unmanned aerial vehicle body, battery and motor electricity are connected, and the wing is installed on the output shaft of motor, still include guard shield structure, driving motor, drive gear and driven gear, guard shield structure, driving motor, drive gear and driven gear all install on the unmanned aerial vehicle body, driving motor and the battery electricity is connected, and the guard shield structure wholly becomes cylindrical structure, the wing is located guard shield structure; the protective cover structure is provided with a notch, the side wall of the protective cover structure is provided with a cavity, a movable baffle is arranged in the cavity, and the structure of the movable baffle is matched with the notch; the outer wall of the movable baffle is provided with a toothed belt, an output shaft of the driving motor is in transmission connection with the driving gear, the driven gear is meshed with the driving gear, and the toothed belt on the movable baffle is meshed with the driven gear. The utility model discloses an unmanned aerial vehicle's wing has set up the guard shield structure.
Description
Technical Field
The utility model relates to an unmanned aerial vehicle with wing protection architecture belongs to four rotor unmanned aerial vehicle technical field.
Background
An unmanned aircraft, abbreviated as "drone", and abbreviated in english as "UAV", is an unmanned aircraft that is operated by a radio remote control device and a self-contained program control device, or is operated autonomously, either completely or intermittently, by an onboard computer. At present, use rotor unmanned aerial vehicle in the market to be main, mainly because its stability is stronger with the controllability, but unmanned aerial vehicle's rotor is high-speed rotatory at flight in-process, in case with external object bump wing will damage because of the collision.
SUMMERY OF THE UTILITY MODEL
An object of the utility model is to provide an unmanned aerial vehicle with wing protection architecture has set up the guard shield structure for unmanned aerial vehicle's wing, can prevent that unmanned aerial vehicle from colliding at high-speed rotatory wing and external object in the flight process.
In order to solve the technical problem, the utility model discloses a following technical scheme:
an unmanned aerial vehicle with a wing protection structure comprises an unmanned aerial vehicle body, wherein a storage battery, a wing and a motor are mounted on the unmanned aerial vehicle body, the storage battery is electrically connected with the motor, the wing is mounted on an output shaft of the motor, the unmanned aerial vehicle further comprises a shield structure, a driving motor, a driving gear and a driven gear, the shield structure, the driving motor, the driving gear and the driven gear are mounted on the unmanned aerial vehicle body, the driving motor is electrically connected with the storage battery, the shield structure is integrally cylindrical, and the wing is located in the shield structure; the protective cover structure is provided with a notch, the side wall of the protective cover structure is provided with a cavity, a movable baffle is arranged in the cavity, and the structure of the movable baffle is matched with the notch; the outer wall of the movable baffle is provided with a toothed belt, an output shaft of the driving motor is in transmission connection with the driving gear, the driven gear is meshed with the driving gear, and the toothed belt on the movable baffle is meshed with the driven gear.
In the aforesaid unmanned aerial vehicle with wing protection structure, the guard shield has the slide rail structurally, the last spout that has of adjustable fender, the spout sets up on the slide rail.
In the unmanned aerial vehicle with wing protection structure, the movable baffle plate is provided with an upper circular ring and a lower circular ring, and the toothed belt is arranged on the upper circular ring or the lower circular ring.
In the above-mentioned unmanned aerial vehicle with wing protection structure, the number of the wings and the driven gears is equal, and is four.
Compared with the prior art, the utility model discloses an unmanned aerial vehicle's wing has set up the guard shield structure, can prevent that unmanned aerial vehicle from colliding at high-speed rotatory wing and external object in the flight process.
Drawings
Fig. 1 is a schematic structural view of an operating state of the present invention;
fig. 2 is a schematic structural view of another operation state of the present invention;
FIG. 3 is a schematic structural view of a driving principle of the flapper;
fig. 4 is a schematic structural view of the flapper.
Reference numerals: the unmanned aerial vehicle comprises a driving motor 1, wings 2, a shield structure 3, driven gears 4, a driving gear 5, an unmanned aerial vehicle body 6, a notch 7, a movable baffle 8, a sliding rail 9, an upper ring 10 and a lower ring 11.
The present invention will be further described with reference to the accompanying drawings and the detailed description.
Detailed Description
Example 2: an unmanned aerial vehicle with a wing protection structure comprises an unmanned aerial vehicle body 6, wherein a storage battery, a wing 2 and a motor are mounted on the unmanned aerial vehicle body 6, the storage battery is electrically connected with the motor, the wing 2 is mounted on an output shaft of the motor, the unmanned aerial vehicle further comprises a shield structure 3, a driving motor 1, a driving gear 5 and a driven gear 4, the shield structure 3, the driving motor 1, the driving gear 5 and the driven gear 4 are all mounted on the unmanned aerial vehicle body 6, the driving motor 1 is electrically connected with the storage battery, the shield structure 3 is integrally of a cylindrical structure, and the wing 2 is located in the shield structure 3; the protective cover structure 3 is provided with a notch 7, the side wall of the protective cover structure 3 is provided with a cavity, a movable baffle 8 is arranged in the cavity, and the structure of the movable baffle 8 is matched with the notch 7; the outer wall of the movable baffle plate 8 is provided with a toothed belt, the output shaft of the driving motor 1 is in transmission connection with the driving gear 5, the driven gear 4 is meshed with the driving gear 5, and the toothed belt on the movable baffle plate 8 is meshed with the driven gear 4.
The guard shield structure 3 is provided with a slide rail 9, the movable baffle 8 is provided with a slide groove, and the slide groove is arranged on the slide rail 9. The movable baffle 8 is provided with an upper circular ring 10 and a lower circular ring 11, and the toothed belt is arranged on the upper circular ring 10 or the lower circular ring 11. The number of the wings 2 and the driven gears 4 is equal, and the number of the wings is four.
The utility model discloses a theory of operation of embodiment: under the non-flight state, adjustable fender 8 is located the cavity, and when taking off, driving motor 1 drive gear 5 rotates, and drive gear 5 drives driven gear 4 and rotates, and driven gear 4 drives adjustable fender 8 through the insection area and rotates, makes adjustable fender 8 be located guard shield structure 3's notch 7 to adjustable fender 8 shelters from notch 7, resumes to initial condition again after the aircraft lands, and driving motor 1's rotation and stopping can be controlled through the remote control. Notch 7 on the guard shield structure 3 is located the one side of keeping away from unmanned aerial vehicle body 6 on the guard shield structure 3, can still be clear when standby state can see wing 2, and science and technology sense is sufficient. The movable baffle 5 shields the notch 7 in the flying state, so that the effect of protecting the wings 2 can be achieved, and the influence of airflow on the wings can be reduced, so that the unmanned aerial vehicle flies more stably.
Claims (4)
1. The utility model provides an unmanned aerial vehicle with wing protection architecture, including unmanned aerial vehicle body (6), install the battery on unmanned aerial vehicle body (6), wing (2), and the motor, battery and motor electricity are connected, wing (2) are installed on the output shaft of motor, a serial communication port, still include guard shield structure (3), driving motor (1), drive gear (5) and driven gear (4), guard shield structure (3), driving motor (1), drive gear (5) and driven gear (4) are all installed on unmanned aerial vehicle body (6), driving motor (1) and the battery electricity is connected, guard shield structure (3) wholly becomes cylindric structure, wing (2) are located guard shield structure (3); a notch (7) is arranged on the shield structure (3), a cavity is arranged on the side wall of the shield structure (3), a movable baffle (8) is arranged in the cavity, and the structure of the movable baffle (8) is matched with the notch (7); the outer wall of the movable baffle (8) is provided with a toothed belt, an output shaft of the driving motor (1) is in transmission connection with the driving gear (5), the driven gear (4) is meshed with the driving gear (5), and the toothed belt on the movable baffle (8) is meshed with the driven gear (4).
2. An unmanned aerial vehicle with wing protection structure according to claim 1, characterized in that, there is slide rail (9) on the guard structure (3), has the spout on the adjustable fender (8), and the spout sets up on slide rail (9).
3. An unmanned aerial vehicle with wing protection structure according to claim 2, characterized in that the adjustable fender (8) is provided with an upper ring (10) and a lower ring (11), and the toothed belt is provided on the upper ring (10) or the lower ring (11).
4. A drone with a wing protection structure according to claim 3, characterised in that the wings (2) and the driven gears (4) are equal in number, four each.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201922150312.1U CN211281462U (en) | 2019-12-04 | 2019-12-04 | Unmanned aerial vehicle with wing protection architecture |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201922150312.1U CN211281462U (en) | 2019-12-04 | 2019-12-04 | Unmanned aerial vehicle with wing protection architecture |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN211281462U true CN211281462U (en) | 2020-08-18 |
Family
ID=72038089
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201922150312.1U Active CN211281462U (en) | 2019-12-04 | 2019-12-04 | Unmanned aerial vehicle with wing protection architecture |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN211281462U (en) |
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2019
- 2019-12-04 CN CN201922150312.1U patent/CN211281462U/en active Active
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| PP01 | Preservation of patent right |
Effective date of registration: 20220314 Granted publication date: 20200818 |