CN216332711U - Unmanned aerial vehicle for highway road condition exploration - Google Patents
Unmanned aerial vehicle for highway road condition exploration Download PDFInfo
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- CN216332711U CN216332711U CN202122816464.8U CN202122816464U CN216332711U CN 216332711 U CN216332711 U CN 216332711U CN 202122816464 U CN202122816464 U CN 202122816464U CN 216332711 U CN216332711 U CN 216332711U
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Abstract
The utility model belongs to the technical field of unmanned aerial vehicle damping equipment, in particular to an unmanned aerial vehicle for highway condition exploration, which comprises a shell and is characterized in that four groups of electric telescopic rods are fixedly connected to the shell at intervals along the circumferential direction, the extending ends of the four groups of electric telescopic rods are fixedly connected with a supporting seat, blades are vertically and rotatably connected to the supporting seat, two groups of first rectangular grooves are longitudinally arranged at intervals at the lower end of the shell, two groups of rotating plates are transversely and rotatably connected to the two groups of first rectangular grooves at intervals, the two groups of rotating plates are connected with a landing bracket through a damping device, in order to protect the landing bracket, a second rectangular groove arranged between the two groups of first rectangular grooves is arranged at the lower end of the shell, two groups of cameras are transversely and rotatably connected to the second rectangular groove at intervals, and first gears arranged in the second rectangular groove are fixedly connected to the two groups of rotating plates, and the two groups of camera rotating shafts are fixedly connected with second gears matched with the first gears.
Description
Technical Field
The utility model belongs to the technical field of unmanned aerial vehicle damping equipment, and particularly relates to an unmanned aerial vehicle for highway road condition exploration.
Background
The highway is put into use and has improved the speed of people's trip, highway's road conditions detection is also especially important, the road conditions that detects exploration highway is favorable to in time handling the relatively poor area of highway road conditions, it surveys to use unmanned aerial vehicle to survey at highway road conditions exploration in-process more, unmanned aerial vehicle is the unmanned aerial vehicle who utilizes radio remote control equipment and self-contained program control device to control, unmanned aerial vehicle is unmanned aerial vehicle's the general name in fact, can divide into from the technical angle definition: unmanned helicopters, unmanned fixed wing aircraft, unmanned multi-rotor aircraft, unmanned airships, and unmanned parawing aircraft;
present exploration unmanned aerial vehicle is when using, because of the camera lacks protector, most unmanned aerial vehicle flight in-process, and the support can not shrink, leads to easily hanging branch etc. leads to the air crash, damages whole fuselage.
SUMMERY OF THE UTILITY MODEL
Aiming at the defects in the prior art, the utility model aims to provide the unmanned aerial vehicle for highway road condition exploration, and solves the technical problems.
The scheme adopted by the utility model is as follows: an unmanned aerial vehicle for highway condition exploration comprises a shell and is characterized in that four groups of electric telescopic rods are fixedly connected to the shell at intervals along the circumferential direction, the extending ends of the four groups of electric telescopic rods are fixedly connected with supporting seats, blades are vertically and rotatably connected to the supporting seats, two groups of first rectangular grooves are longitudinally arranged at the lower end of the shell at intervals, two groups of rotating plates are transversely and rotatably connected to the two groups of first rectangular grooves at intervals, the two groups of rotating plates are connected with a ground support through a damping device, in order to protect the ground support, a second rectangular groove is arranged at the lower end of the shell and is positioned between the two groups of first rectangular grooves, two groups of cameras are transversely and rotatably connected to the second rectangular groove at intervals, first gears arranged in the second rectangular grooves are fixedly connected to the two groups of rotating plates, and second gears matched with the first gears are fixedly connected to the rotating shafts of the two groups of cameras, the two groups of rotating plate rotating shafts are driven by a power device, and the blades, the camera and the controller are electrically connected.
Preferably, the power device comprises a motor fixedly connected in the shell, and a rotating shaft of the motor is fixedly connected with a rotating shaft of the rotating plate.
Preferably, damping device include between falling to the ground support and the rotor plate interval fixed connection's two sets of shock absorber posts, fall to the ground between support and the rotor plate fixed connection cover establish the damping spring on the shock absorber post.
Preferably, the lower end of the floor stand is provided with damping rubber.
The utility model has the beneficial effects that:
the first gear and the second gear are matched, so that the landing support can be retracted in the flying process, the camera extends out, and photographing and routing inspection can be performed;
secondly, a shock absorption device arranged between the rotating plate and the landing bracket can play a good shock absorption effect when the flying landing is performed, so that the damage to the shell is reduced;
thirdly, simple structure, convenient operation, degree of automation is high, saves the labour, and the security performance is high.
Drawings
Fig. 1 is one of perspective views of the present invention.
Fig. 2 is a second perspective view of the present invention.
Reference numerals: 1. a housing; 2. an electric telescopic rod; 3. a supporting seat; 4. a blade; 5. a first rectangular groove; 6. a rotating plate; 7. a floor stand; 8. a second rectangular groove; 9. a camera; 10. a first gear; 11. a second gear; 12. a shock-absorbing post; 13. a shock absorbing spring.
Detailed Description
The foregoing and other technical and scientific aspects, features and utilities of the present invention will be apparent from the following detailed description of the embodiments, taken in conjunction with the accompanying drawings of fig. 1-2. The structural contents mentioned in the following embodiments are all referred to the attached drawings of the specification.
Exemplary embodiments of the present invention will be described below with reference to the accompanying drawings.
The embodiment I is an unmanned aerial vehicle for highway condition exploration, which comprises a shell 1 and is characterized in that four groups of electric telescopic rods 2 are fixedly connected to the shell 1 at intervals along the circumferential direction, the four groups of electric telescopic rods 2 are fixedly connected with supporting seats 3 in an extending mode, blades 4 are vertically and rotatably connected to the supporting seats 3, two groups of first rectangular grooves 5 are longitudinally arranged at the lower end of the shell 1 at intervals, two groups of rotating plates 6 are transversely and rotatably connected to the two groups of first rectangular grooves 5 at intervals, the two groups of rotating plates 6 are connected with a floor bracket 7 through a damping device, in order to protect the floor bracket 7, a second rectangular groove 8 positioned between the two groups of first rectangular grooves 5 is arranged at the lower end of the shell 1, two groups of cameras 9 are transversely and rotatably connected to the second rectangular groove 8 at intervals, first gears 10 arranged in the second rectangular grooves 8 are fixedly connected to the two groups of rotating plates 6, two sets of 9 axis of rotation of camera on fixedly connected with first gear 10 complex second gear 11, two sets of 6 axes of rotation of rotor plate by power device drive, blade 4 and camera 9 and controller between electric connection.
In the second embodiment, on the basis of the first embodiment, the power device comprises a motor fixedly connected in the housing 1, and a rotating shaft of the motor is fixedly connected with a rotating shaft of the rotating plate 6.
In the third embodiment, on the basis of the first embodiment, the damping device includes two groups of damping columns 12 fixedly connected between the floor stand 7 and the rotating plate 6 at intervals, and a damping spring 13 sleeved on the damping columns 12 is fixedly connected between the floor stand 7 and the rotating plate 6.
In the fourth embodiment, on the basis of the first embodiment, the lower end of the floor stand 7 is provided with a shock-absorbing rubber.
In the embodiment, when the electric telescopic rod is used, the blades 4 are started through the controller to drive the shell 1 to fly, when the shell 1 ascends, the four groups of floor brackets 7 can move by controlling the motor to be retracted into the first rectangular groove 5, meanwhile, the floor brackets 7 drive the first gear 10 to start moving, as the first gear 10 is meshed with the second gear 11, the camera 9 is ejected out of the second rectangular groove 8, the road condition is recorded in the flying process, when the electric telescopic rod descends, the camera 9 is retracted from the second rectangular groove 8, meanwhile, the four groups of floor brackets 7 are ejected out of the first rectangular groove 5, under the action of the shock absorption column 12 and the shock absorption spring 13, the self impact force is reduced, the whole shell 1 is well protected, the electric telescopic rod 2 is started, the electric telescopic rod can be retracted under the condition of not being used, the whole area is reduced, the electric telescopic rod is convenient and safe to carry, the whole area of the aircraft body is reduced, the collision probability is reduced, and the safety equipment of the whole aircraft is improved in the flying process.
The above description is only for the purpose of illustrating the present invention, and it should be understood that the present invention is not limited to the above embodiments, and various modifications conforming to the spirit of the present invention are within the scope of the present invention.
Claims (4)
1. An unmanned aerial vehicle for highway condition exploration comprises a shell (1) and is characterized in that the shell (1) is fixedly connected with four groups of electric telescopic rods (2) at intervals along the circumferential direction, the four groups of electric telescopic rods (2) are fixedly connected with a supporting seat (3) in an extending mode, blades (4) are vertically and rotatably connected onto the supporting seat (3), two groups of first rectangular grooves (5) are longitudinally arranged at the lower end of the shell (1) at intervals, two groups of rotating plates (6) are transversely and rotatably connected into the two groups of first rectangular grooves (5) at intervals, a ground support (7) is connected onto the two groups of rotating plates (6) through a damping device, in order to protect the ground support (7), a second rectangular groove (8) positioned between the two groups of first rectangular grooves (5) is arranged at the lower end of the shell (1), and two groups of cameras (9) are transversely and rotatably connected into the second rectangular groove (8) at intervals, two sets of rotor plate (6) on fixedly connected with arrange first gear (10) in second rectangular channel (8) in, two sets of camera (9) axis of rotation on fixedly connected with and first gear (10) complex second gear (11), two sets of rotor plate (6) axis of rotation by power device drive, blade (4) and camera (9) and controller between electric connection.
2. The unmanned aerial vehicle for highway condition exploration according to claim 1, wherein said power device comprises a motor fixedly connected in the housing (1), and a rotating shaft of said motor is fixedly connected with a rotating shaft of said rotating plate (6).
3. The unmanned aerial vehicle for highway condition exploration according to claim 1, wherein the damping device comprises two groups of damping columns (12) fixedly connected between the floor support (7) and the rotating plate (6) at intervals, and a damping spring (13) sleeved on the damping column (12) is fixedly connected between the floor support (7) and the rotating plate (6).
4. The unmanned aerial vehicle for highway condition exploration according to claim 1, wherein the lower end of said landing support (7) is provided with a shock-absorbing rubber.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202122816464.8U CN216332711U (en) | 2021-11-17 | 2021-11-17 | Unmanned aerial vehicle for highway road condition exploration |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202122816464.8U CN216332711U (en) | 2021-11-17 | 2021-11-17 | Unmanned aerial vehicle for highway road condition exploration |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN216332711U true CN216332711U (en) | 2022-04-19 |
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Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202122816464.8U Active CN216332711U (en) | 2021-11-17 | 2021-11-17 | Unmanned aerial vehicle for highway road condition exploration |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN216332711U (en) |
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2021
- 2021-11-17 CN CN202122816464.8U patent/CN216332711U/en active Active
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