CN220263092U - Electric vertical take-off and landing aircraft vision device - Google Patents
Electric vertical take-off and landing aircraft vision device Download PDFInfo
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- CN220263092U CN220263092U CN202321750907.0U CN202321750907U CN220263092U CN 220263092 U CN220263092 U CN 220263092U CN 202321750907 U CN202321750907 U CN 202321750907U CN 220263092 U CN220263092 U CN 220263092U
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- 238000003466 welding Methods 0.000 claims description 2
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- 230000009286 beneficial effect Effects 0.000 description 1
- 230000007547 defect Effects 0.000 description 1
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Abstract
The utility model discloses an electric vertical take-off and landing aircraft vision device which comprises a bottom plate, an L-shaped vertical plate, a fixed bin, a fixed disc, a mounting seat, a distance sensor and a panoramic camera, wherein one end of the top of the fixed bin is provided with a servo motor through a fixed seat, the power output end of the servo motor is connected with a gear, the top of the fixed bin is provided with a through groove, a sliding plate is arranged in the through groove, one end of the sliding plate is connected with a rack, the rack is meshed with the gear, the bottom of the sliding plate is welded with the fixed disc, the fixed disc is positioned in the fixed bin, the bottom of the fixed disc is provided with the mounting seat, and the panoramic camera is arranged at the position, close to the center, of the bottom of the mounting seat. This novel possesses can conveniently carry out the mechanism that goes up and down to visual structure, can conveniently pack up the protection when using, is fit for extensively using widely.
Description
Technical Field
The utility model relates to the technical field of unmanned aerial vehicle parts, in particular to an electric vertical take-off and landing aircraft vision device.
Background
Electric vertical takeoff and landing aircraft typically require the provision of a variety of vision devices to enable safe takeoff and landing and hover operations, with cameras and distance sensors typically integrated thereon.
The prior vision device has the following defects: 1. the mechanism capable of conveniently lifting the visual structure is not provided, and the folding protection can not be conveniently carried out when the visual structure is not used. To this end, we propose an electric vertical takeoff and landing aircraft vision device.
Disclosure of Invention
The utility model mainly aims to provide an electric vertical take-off and landing aircraft vision device which can effectively solve the problems in the background technology.
In order to achieve the above purpose, the technical scheme adopted by the utility model is as follows:
the utility model provides an electronic perpendicular take-off and landing aircraft vision device, includes bottom plate, L shape riser, fixed storehouse, fixed disc, mount pad, distance sensor and panoramic camera, fixed storehouse top one end is provided with servo motor through the fixing base, servo motor's power take off end is connected with the gear, fixed storehouse top is provided with the groove that link up, it is provided with the sliding plate to link up the inslot, sliding plate one end is connected with the rack, rack and gear engagement, sliding plate bottom welding has fixed disc, fixed disc is located fixed storehouse, fixed disc bottom is provided with the mount pad, the mount pad bottom is close to central department and is provided with panoramic camera, the mount pad bottom is close to panoramic camera one side department installs distance sensor through the mounting groove, the mount pad bottom periphery is provided with the ramp surface, install supplementary camera through the screw on the ramp surface.
Further, the bottom plate bottom is close to the central part and is provided with the guide rail through the connecting bolt, one end of the sliding plate is positioned in the guide rail, and the sliding plate can be well guided through the guide rail, so that the stability of the sliding plate during lifting can be improved.
Further, the top all is provided with vertical reservation groove near both ends department in the fixed storehouse, is close to vertical reservation groove both ends department all is provided with horizontal constant head tank and fixed slot, servo electric jar is installed through the screw to the top in the fixed slot, the montant has all been welded at fixed disc top both ends.
Further, the locating hole has been seted up in the montant one end penetration, servo electric jar's power take off end is connected with the locating lever, the locating lever tip runs through the locating hole and is located in the transverse positioning groove, through locating hole and transverse positioning groove cooperation, conveniently fix the montant in vertical reservation inslot position, and then conveniently fix the position of fixed disc in the direction of height.
Further, the top of the L-shaped vertical plate is provided with a mounting hole in a penetrating mode.
Compared with the prior art, the utility model has the following beneficial effects:
1. according to the electric vertical take-off and landing aircraft vision device, the servo motor conveniently drives the gear to rotate during working, so that the rack and the sliding plate move up and down along the direction of the guide rail, the heights of the auxiliary camera, the distance sensor and the panoramic camera can be adjusted according to the needs, and the vision device is provided with the mechanism capable of conveniently lifting the vision structure, so that the device is convenient to pack and protect when not used.
Drawings
Fig. 1 is a schematic diagram of the overall structure of an electric vertical takeoff and landing aircraft vision device according to the present utility model.
Fig. 2 is a schematic view showing the bottom view structure of an auxiliary camera, a distance sensor and a panoramic camera of the electric vertical take-off and landing aircraft vision device.
Fig. 3 is a schematic diagram of a detail structure of a visual device of an electric vertical takeoff and landing aircraft.
Fig. 4 is a schematic view of the structure of the guide rail, the sliding plate and the rack of the electric vertical take-off and landing aircraft vision device.
In the figure: 1. a bottom plate; 2. a guide rail; 3. a connecting bolt; 4. an L-shaped vertical plate; 5. a mounting hole; 6. a sliding plate; 7. a rack; 8. a servo motor; 9. a gear; 10. a fixed bin; 11. a fixed disc; 12. a mounting base; 13. a slope surface; 14. an auxiliary camera; 15. a distance sensor; 16. panoramic camera; 17. a fixing groove; 18. a servo electric cylinder; 19. a vertical reserve tank; 20. a transverse positioning groove; 21. a vertical rod; 22. and positioning holes.
Detailed Description
The utility model is further described in connection with the following detailed description, in order to make the technical means, the creation characteristics, the achievement of the purpose and the effect of the utility model easy to understand.
As shown in fig. 1-4, an electric vertical take-off and landing aircraft vision device comprises a bottom plate 1, an L-shaped vertical plate 4, a fixed bin 10, a fixed disc 11, a mounting seat 12, a distance sensor 15 and a panoramic camera 16, wherein one end of the top of the fixed bin 10 is provided with a servo motor 8 through a fixed seat, a power output end of the servo motor 8 is connected with a gear 9, the top of the fixed bin 10 is provided with a through groove, a sliding plate 6 is arranged in the through groove, one end of the sliding plate 6 is connected with a rack 7, the rack 7 is meshed with the gear 9, the bottom of the sliding plate 6 is welded with the fixed disc 11, the fixed disc 11 is positioned in the fixed bin 10, the bottom of the fixed disc 11 is provided with the mounting seat 12, the position close to the center of the bottom of the mounting seat 12 is provided with the panoramic camera 16, the position close to one side of the panoramic camera 16 is provided with the distance sensor 15 through the mounting groove, the periphery of the bottom of the mounting seat 12 is provided with a slope 13, and the slope surface 13 is provided with an auxiliary camera 14 through a screw.
Wherein, the bottom of the bottom plate 1 is near the center and is provided with a guide rail 2 through a connecting bolt 3, and one end of the sliding plate 6 is positioned in the guide rail 2.
In this embodiment, as shown in fig. 1 and 4, the guide rail 2 can perform a good guiding function on the sliding plate 6, so that the stability of the sliding plate 6 during lifting can be improved.
The top in the fixed bin 10 is close to both ends department and all is provided with vertical reservation groove 19, is close to vertical reservation groove 19 both ends department all is provided with horizontal constant head tank 20 and fixed slot 17, servo cylinder 18 is installed through the screw at the top in the fixed slot 17, the montant 21 has all been welded at fixed disc 11 top both ends.
In this embodiment, as shown in fig. 4, the servo cylinder 18 is conveniently mounted through the fixing groove 17.
Wherein, locating hole 22 has been run through to montant 21 one end, the power take off end of servo electricity jar 18 is connected with the locating lever, the locating lever tip runs through locating hole 22 and is located horizontal constant head tank 20.
In this embodiment, as shown in fig. 1, the positioning hole 22 is matched with the transverse positioning groove 20, so that the position of the vertical rod 21 in the vertical reserved groove 19 is conveniently fixed, and the position of the fixed disc 11 in the height direction is conveniently fixed.
Wherein, the mounting hole 5 has been run through at L shape riser 4 top.
In this embodiment, as shown in fig. 1, the external bolts pass through the mounting holes 5, so that the L-shaped vertical plate 4 and the bottom of the unmanned aerial vehicle are conveniently fixed, and the vision device is mounted.
It should be noted that, the utility model is an electric vertical take-off and landing aircraft vision device, during operation, pass mounting hole 5 through the outside bolt, conveniently fix L shape riser 4 and unmanned aerial vehicle bottom, thereby install this vision device, servo motor 8, auxiliary camera 14, distance sensor 15 and panorama camera 16 all connect unmanned aerial vehicle from the power supply that takes, servo motor 8 conveniently drives gear 9 rotation during operation, thereby make rack 7 and sliding plate 6 reciprocate along the direction of guide rail 2, and then can adjust auxiliary camera 14 as required, distance sensor 15 and panorama camera 16's height, when auxiliary camera 14, distance sensor 15 and panorama camera 16 bottom expose the fixed storehouse 10 bottom, conveniently synthesize visual detection to surrounding environment, when auxiliary camera 14, distance sensor 15 and panorama camera 16 rise, 21 top gets into in the vertical reserve tank 19, servo motor 18 during operation drives locating lever and passes locating hole 22 that one end was seted up of montant 21, and lie in transverse locating slot 20, thereby can carry out the fixed position to the fixed position of auxiliary camera 14, the fixed position of panorama camera 16 is convenient for carrying out the visual detection, and when this visual device is convenient for carrying out, the high-level protection device is realized at the fixed position of panorama camera 16.
The foregoing has shown and described the basic principles and main features of the present utility model and the advantages of the present utility model. It will be understood by those skilled in the art that the present utility model is not limited to the embodiments described above, and that the above embodiments and descriptions are merely illustrative of the principles of the present utility model, and various changes and modifications may be made without departing from the spirit and scope of the utility model, which is defined in the appended claims. The scope of the utility model is defined by the appended claims and equivalents thereof.
Claims (5)
1. The utility model provides an electronic perpendicular aircraft vision device that takes off and land, includes bottom plate (1), L shape riser (4), fixed storehouse (10), fixed disc (11), mount pad (12), distance sensor (15) and panoramic camera (16), its characterized in that: the utility model discloses a camera, including fixed storehouse (10), fixed storehouse (10) top, fixed storehouse (8) are provided with servo motor (8) through the fixing base, servo motor (8) are connected with gear (9) power take off end, fixed storehouse (10) top is provided with the through groove, be provided with sliding plate (6) in the through groove, sliding plate (6) one end is connected with rack (7), rack (7) and gear (9) meshing, sliding plate (6) bottom welding has fixed disc (11), fixed disc (11) are located fixed storehouse (10), fixed disc (11) bottom is provided with mount pad (12), the mount pad (12) bottom is close to central authorities department and is provided with panoramic camera (16), mount pad (12) bottom is close to panoramic camera (16) one side department installs distance sensor (15) through the mounting groove, mount pad (12) bottom periphery is provided with ramp surface (13), install supplementary camera (14) through the screw on the ramp surface (13).
2. An electric vertical takeoff and landing aircraft visual equipment as defined in claim 1, wherein: the bottom of the bottom plate (1) is close to the center and provided with a guide rail (2) through a connecting bolt (3), and one end of the sliding plate (6) is positioned in the guide rail (2).
3. An electric vertical takeoff and landing aircraft visual equipment as defined in claim 1, wherein: the top is provided with vertical reservation groove (19) near both ends department in fixed storehouse (10), is close to vertical reservation groove (19) both ends department all is provided with transverse positioning groove (20) and fixed slot (17), servo electric jar (18) are installed through the screw in top in fixed slot (17), montant (21) have all been welded at fixed disc (11) top both ends.
4. An electric vertical takeoff and landing aircraft visual means as defined in claim 3, wherein: the locating device is characterized in that a locating hole (22) is formed in one end of the vertical rod (21) in a penetrating mode, a locating rod is connected to the power output end of the servo electric cylinder (18), and the end portion of the locating rod penetrates through the locating hole (22) and is located in the transverse locating groove (20).
5. An electric vertical takeoff and landing aircraft visual equipment as defined in claim 1, wherein: the top of the L-shaped vertical plate (4) is provided with a mounting hole (5) in a penetrating way.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202321750907.0U CN220263092U (en) | 2023-07-05 | 2023-07-05 | Electric vertical take-off and landing aircraft vision device |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202321750907.0U CN220263092U (en) | 2023-07-05 | 2023-07-05 | Electric vertical take-off and landing aircraft vision device |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN220263092U true CN220263092U (en) | 2023-12-29 |
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ID=89311122
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202321750907.0U Active CN220263092U (en) | 2023-07-05 | 2023-07-05 | Electric vertical take-off and landing aircraft vision device |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN220263092U (en) |
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2023
- 2023-07-05 CN CN202321750907.0U patent/CN220263092U/en active Active
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