CN214524437U - Actual combat type unmanned aerial vehicle supports location structure - Google Patents
Actual combat type unmanned aerial vehicle supports location structure Download PDFInfo
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- CN214524437U CN214524437U CN202120490982.2U CN202120490982U CN214524437U CN 214524437 U CN214524437 U CN 214524437U CN 202120490982 U CN202120490982 U CN 202120490982U CN 214524437 U CN214524437 U CN 214524437U
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- location structure
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Abstract
The utility model discloses a practical combat type unmanned aerial vehicle supporting and positioning structure, including fuselage, camera shooting instrument and supporting and positioning mechanism, the camera shooting instrument is installed in the bottom of the fuselage through the supporting and positioning mechanism, the supporting and positioning mechanism includes back frame, front frame, driving cylinder and rotating assembly, the "U" shape the front frame and the "L" shape back frame are installed on the lower surface of the fuselage through the adjusting assembly that sets up, the driving cylinder is vertically fixed on the inner surface of the back frame, the rotating assembly includes circular plate, rack and ring gear, the circular plate is fixed with the rear surface of the camera shooting instrument through the extension plate that sets up, the circular plate is installed inside the front frame in a rotating manner; the utility model discloses a be provided with supporting positioning mechanism, both can support the appearance of making a video recording and realize its fastening installation, can adjust the working angle of the appearance of making a video recording again as required and adjust the location to the angle, reduce because the appearance angle of making a video recording is uncomfortable and influence image acquisition's probability, reduce the trouble of artificial regulation location simultaneously.
Description
Technical Field
The utility model belongs to the technical field of unmanned aerial vehicle supports location structure, concretely relates to actual combat type unmanned aerial vehicle supports location structure, is a support location structure that aerial photography unmanned aerial vehicle used for actual combat very much.
Background
Unmanned aerial vehicle takes photo by plane has integrated high definition photography and camera device's remote control aircraft, and the system mainly includes: the system comprises an airborne machine, a flight control machine, a gyro platform, a video transmission machine, a ground station, a communication system and the like.
The appearance mounted position that makes a video recording on unmanned aerial vehicle is fixed for some current, and it is usually inconvenient to adjust the location to the appearance working angle that makes a video recording as required to probably cause the problem of influence to the information acquisition condition, for this reason we propose a real battle type unmanned aerial vehicle support location structure.
SUMMERY OF THE UTILITY MODEL
An object of the utility model is to provide an actual combat type unmanned aerial vehicle supports location structure to it is fixed to solve some of the appearance mounted position of making a video recording on the unmanned aerial vehicle of taking photo by plane that propose among the above-mentioned background art, and it is usually inconvenient to adjust the location to appearance working angle as required, thereby probably causes the problem of influence to the information acquisition condition.
In order to achieve the above object, the utility model provides a following technical scheme: the utility model provides an actual combat type unmanned aerial vehicle supports location structure, includes fuselage, the appearance of making a video recording and supports positioning mechanism, the appearance of making a video recording is installed in the fuselage bottom through supporting positioning mechanism, support positioning mechanism and include after-poppet, fore-stock, drive actuating cylinder and runner assembly, "U" shape the after-poppet of fore-stock and "L" shape is installed at the fuselage lower surface through the adjusting part that sets up, it is vertical fixed at the after-poppet internal surface to drive actuating cylinder, runner assembly includes plectane, rack and ring gear, the plectane is fixed through the extension board that sets up and the appearance after-poppet, the plectane rotates to install inside the fore-stock, the rack is detachable and drive the inside piston rod of actuating cylinder and be connected, the ring gear is fixed at the plectane periphery and is connected with rack toothing.
Preferably, a fixed shaft is vertically fixed inside the front frame, and the circular plate is sleeved on the fixed shaft through a bearing.
Preferably, a convex plate is fixed on the rear surface of the rack, the piston rod penetrates through the convex plate and is exposed outside, two spiral rings are screwed on the piston rod in a threaded manner, and the two spiral rings are respectively in contact with the upper surface and the lower surface of the convex plate for limiting.
Preferably, two connecting plates are arranged between the front frame and the rear frame, and a stabilizing frame is arranged between the driving cylinder and the rear frame.
Preferably, the adjusting component comprises an underframe, fixing rods and a limiting ring, the U-shaped underframe is fixed on the lower surface of the machine body, the lower ends of the two fixing rods are respectively fixed on the upper surfaces of the front frame and the rear frame, and the upper ends of the two fixing rods movably penetrate through the underframe and are exposed outside.
Preferably, the limiting ring is rotatably mounted at the end part of the fixing rod, and the lower surface of the limiting ring is in contact with the inner surface of the bottom frame for limiting.
Preferably, the lower surface of the machine body is provided with a support, and the upper surface of the machine body is provided with a propeller.
Compared with the prior art, the beneficial effects of the utility model are that:
(1) the utility model discloses a be provided with supporting positioning mechanism, both can support the appearance of making a video recording and realize its fastening installation, can adjust the working angle of the appearance of making a video recording again as required and adjust the location to the angle, reduce because the appearance angle of making a video recording is uncomfortable and influence image acquisition's probability, reduce the trouble of artificial regulation location simultaneously.
(2) The utility model discloses a be provided with adjusting part, the whole work height that supports positioning mechanism is adjusted as required to the convenience, increases the appearance work convenience of making a video recording, and the follow-up whole dismantlement that supports positioning mechanism of being convenient for simultaneously takes off.
Drawings
Fig. 1 is a schematic structural view of the present invention;
fig. 2 is a schematic diagram of a right-side view structure of the supporting and positioning mechanism of the present invention;
FIG. 3 is an enlarged view of area A of FIG. 2 according to the present invention;
FIG. 4 is a schematic view of the adjustment assembly of FIG. 2 according to the present invention;
in the figure: 1. a body; 2. a camera; 3. a supporting and positioning mechanism; 31. a rear frame; 32. a front frame; 33. a driving cylinder; 4. an adjustment assembly; 41. a chassis; 42. fixing the rod; 43. a limiting ring; 5. a circular plate; 6. a rack; 7. a ring gear; 8. and fixing the shaft.
Detailed Description
The technical solutions in the embodiments of the present invention will be described clearly and completely with reference to the accompanying drawings in the embodiments of the present invention, and it is obvious that the described embodiments are only some embodiments of the present invention, not all embodiments. Based on the embodiments in the present invention, all other embodiments obtained by a person skilled in the art without creative work belong to the protection scope of the present invention.
Referring to fig. 1-4, the present invention provides a technical solution: a practical combat type unmanned aerial vehicle supporting and positioning structure comprises a machine body 1, a camera 2 and a supporting and positioning mechanism 3, wherein the camera 2 is installed at the bottom of the machine body 1 through the supporting and positioning mechanism 3, the supporting and positioning mechanism 3 comprises a rear frame 31, a front frame 32, a driving cylinder 33 and a rotating assembly, the U-shaped front frame 32 and the L-shaped rear frame 31 are installed at the lower surface of the machine body 1 through an arranged adjusting assembly 4, the driving cylinder 33 is vertically fixed at the inner surface of the rear frame 31, the rotating assembly comprises a circular plate 5, a rack 6 and a gear ring 7, the circular plate 5 is fixed with the rear surface of the camera 2 through an arranged support plate, the circular plate 5 is rotatably installed inside the front frame 32, the rack 6 is detachably connected with a piston rod inside the driving cylinder 33, the gear ring 7 is fixed on the circumferential surface of the circular plate 5 and is meshed with the rack 6, and the supporting and positioning mechanism 3 is arranged, so that the camera 2 can be supported and fixedly installed, the working angle of the camera 2 can be adjusted according to the requirement, the angle can be adjusted and positioned, the probability that the image acquisition is influenced due to the fact that the angle of the camera 2 is not comfortable is reduced, and meanwhile the trouble of manual adjustment and positioning is reduced.
In this embodiment, preferably, the fixed shaft 8 is vertically fixed inside the front frame 32, and the circular plate 5 is sleeved on the fixed shaft 8 through a bearing, which facilitates the circular plate 5 to rotate around the fixed shaft 8.
In this embodiment, preferably, a convex plate is fixed on the rear surface of the rack 6, the piston rod penetrates through the convex plate and is exposed outside, two spiral rings are screwed on the piston rod in a threaded manner, and the two spiral rings are respectively in contact with the upper surface and the lower surface of the convex plate for limiting, so that the subsequent rack 6 is conveniently separated from or connected with the piston rod.
In this embodiment, preferably, two connecting plates are arranged between the front frame 32 and the rear frame 31 to realize the fastening connection between the front frame and the rear frame, and simultaneously avoid the disengagement of the meshed gear ring 7 and the meshed rack 6, and a fixing frame is arranged between the driving cylinder 33 and the rear frame 31 to increase the installation strength of the driving cylinder 33.
In this embodiment, preferably, the adjusting assembly 4 includes a bottom frame 41, fixing rods 42 and a limiting ring 43, the bottom frame 41 in a U shape is fixed on the lower surface of the machine body 1, the lower ends of the two fixing rods 42 are respectively fixed on the upper surfaces of the front frame 32 and the rear frame 31, the upper end of the two fixing rods movably penetrates through the bottom frame 41 and is exposed outside, the limiting ring 43 is rotatably installed at the end portion of the fixing rod 42, the lower surface of the limiting ring 43 is in contact with the inner surface of the bottom frame 41 for limitation, the adjusting assembly 4 is arranged, the working height of the whole supporting and positioning mechanism 3 can be conveniently adjusted as required, the working convenience of the camera 2 is improved, and the whole supporting and positioning mechanism 3 can be conveniently detached.
In this embodiment, preferably, the lower surface of the body 1 is provided with a support, and the upper surface of the body 1 is provided with a propeller.
The model of the middle driving cylinder 33 of the utility model is SC50X 100-50-S-FA.
The utility model discloses a theory of operation and use flow: the utility model discloses when using, can adjust the location to 2 operating positions of appearance of making a video recording as required, drive actuating cylinder 33 work, the inside piston rod upwards or moves downwards, drive rack 6 and move, and ring gear 7 moves along with it and rotates around fixed axle 8, drive appearance of making a video recording 2 and rotate, make it be in suitable operating position, through being provided with support positioning mechanism 3, both can support appearance of making a video recording 2 and realize its fastening installation, can adjust the working angle of appearance of making a video recording 2 as required and adjust the location to the angle, reduce the probability that influences image acquisition because 2 angular discomfort of appearance of making a video recording, reduce the trouble of artificial regulation location simultaneously; meanwhile, the fixing rod 42 and the limiting ring 43 can realize the working height of the whole supporting and positioning mechanism 3, and meanwhile, the supporting and positioning mechanism 3 is convenient to mount and dismount.
Although embodiments of the present invention have been shown and described, it will be appreciated by those skilled in the art that changes, modifications, substitutions and alterations can be made in these embodiments without departing from the principles and spirit of the invention, the scope of which is defined in the appended claims and their equivalents.
Claims (7)
1. The utility model provides an actual combat type unmanned aerial vehicle supports location structure, includes fuselage (1), camera instrument (2) and supports positioning mechanism (3), its characterized in that: the camera (2) is arranged at the bottom of the machine body (1) through a supporting and positioning mechanism (3), the supporting and positioning mechanism (3) comprises a rear frame (31), a front frame (32), a driving cylinder (33) and a rotating assembly, the U-shaped front frame (32) and the L-shaped rear frame (31) are arranged on the lower surface of the machine body (1) through the arranged adjusting assembly (4), the driving cylinder (33) is vertically fixed on the inner surface of the rear frame (31), the rotating assembly comprises a circular plate (5), a rack (6) and a gear ring (7), the circular plate (5) is fixed with the rear surface of the camera (2) through a support plate, the circular plate (5) is rotatably arranged inside the front frame (32), the rack (6) is detachably connected with a piston rod inside the driving cylinder (33), the gear ring (7) is fixed on the circumferential surface of the circular plate (5) and is meshed and connected with the rack (6).
2. The actual combat type unmanned aerial vehicle supports location structure of claim 1, characterized in that: a fixed shaft (8) is vertically fixed inside the front frame (32), and the circular plate (5) is sleeved on the fixed shaft (8) through a bearing.
3. The actual combat type unmanned aerial vehicle supports location structure of claim 1, characterized in that: a convex plate is fixed on the rear surface of the rack (6), the piston rod penetrates through the convex plate and is exposed outside, two spiral rings are screwed on the piston rod in a threaded manner, and the two spiral rings are respectively in contact with the upper surface and the lower surface of the convex plate for limiting.
4. The actual combat type unmanned aerial vehicle supports location structure of claim 1, characterized in that: two connecting plates are arranged between the front frame (32) and the rear frame (31), and a stabilizing frame is arranged between the driving cylinder (33) and the rear frame (31).
5. The actual combat type unmanned aerial vehicle supports location structure of claim 1, characterized in that: the adjusting assembly (4) comprises an underframe (41), fixing rods (42) and a limiting ring (43), the U-shaped underframe (41) is fixed on the lower surface of the machine body (1), the lower ends of the two fixing rods (42) are respectively fixed on the upper surfaces of the front frame (32) and the rear frame (31), and the upper ends of the two fixing rods movably penetrate through the underframe (41) and are exposed outside.
6. The actual combat type unmanned aerial vehicle supports location structure of claim 5, characterized in that: the limiting ring (43) is rotatably mounted at the end part of the fixing rod (42), and the lower surface of the limiting ring (43) is in contact limiting with the inner surface of the bottom frame (41).
7. The actual combat type unmanned aerial vehicle supports location structure of claim 1, characterized in that: the lower surface of the machine body (1) is provided with a support, and the upper surface of the machine body (1) is provided with a propeller.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202120490982.2U CN214524437U (en) | 2021-03-08 | 2021-03-08 | Actual combat type unmanned aerial vehicle supports location structure |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202120490982.2U CN214524437U (en) | 2021-03-08 | 2021-03-08 | Actual combat type unmanned aerial vehicle supports location structure |
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| Publication Number | Publication Date |
|---|---|
| CN214524437U true CN214524437U (en) | 2021-10-29 |
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| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202120490982.2U Active CN214524437U (en) | 2021-03-08 | 2021-03-08 | Actual combat type unmanned aerial vehicle supports location structure |
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| CN (1) | CN214524437U (en) |
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2021
- 2021-03-08 CN CN202120490982.2U patent/CN214524437U/en active Active
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