CN214420697U - A adjusting device for unmanned aerial vehicle - Google Patents
A adjusting device for unmanned aerial vehicle Download PDFInfo
- Publication number
- CN214420697U CN214420697U CN202120491002.0U CN202120491002U CN214420697U CN 214420697 U CN214420697 U CN 214420697U CN 202120491002 U CN202120491002 U CN 202120491002U CN 214420697 U CN214420697 U CN 214420697U
- Authority
- CN
- China
- Prior art keywords
- aerial vehicle
- unmanned aerial
- fixed
- plate
- stabilizer blade
- 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.)
- Active
Links
Images
Landscapes
- Forklifts And Lifting Vehicles (AREA)
Abstract
The utility model discloses an adjusting device for unmanned aerial vehicle, including fuselage, stabilizer blade and adjustment mechanism, the fuselage bottom is rotated and is installed two "U" shape stabilizer blades, be provided with adjustment mechanism between stabilizer blade and the fuselage, adjustment mechanism includes mounting panel, slide rail, drive actuating cylinder and coupling assembling, the mounting panel is vertically fixed at the fuselage lower surface, the slide rail is fixed at the stabilizer blade front surface, drive actuating cylinder is fixed perpendicularly in the mounting panel side, and drive actuating cylinder inside piston rod and slide rail through the coupling assembling sliding connection that sets up, coupling assembling includes sliding sleeve, connecting plate and fixed column; the utility model discloses a be provided with adjustment mechanism, neither influence the descending of unmanned aerial vehicle on ground, can adjust two stabilizer blade work angles and distance between the two as required again to adjust the focus that unmanned aerial vehicle fell to the ground, increase the steadiness that unmanned aerial vehicle fell to the ground, reduce the probability that unmanned aerial vehicle emptys.
Description
Technical Field
The utility model belongs to the technical field of unmanned aerial vehicle adjusting device, concretely relates to an adjusting device for unmanned aerial vehicle is an adjusting device for taking photo by plane unmanned aerial vehicle stabilizer blade 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 aerial photography unmanned aerial vehicle comprises an aerial vehicle, a flight control device, a gyro holder, a video transmission device, a ground station, a communication system and the like, wherein the flight height of the aerial photography unmanned aerial vehicle is generally more than 500 meters, and the aerial photography unmanned aerial vehicle is suitable for shooting of movie and television propaganda films and aerial views. The aircraft is flexible and convenient, and can quickly complete shooting of the lens.
Distance is fixed between two stabilizer blades on the unmanned aerial vehicle of taking photo by plane some now, and the inconvenient distance of adjusting between the two for when unmanned aerial vehicle fell on uneven ground, the problem of empting probably appeared in unmanned aerial vehicle, and we propose a adjusting device for unmanned aerial vehicle for this reason.
SUMMERY OF THE UTILITY MODEL
An object of the utility model is to provide an adjusting device for unmanned aerial vehicle to solve some aerial photography unmanned aerial vehicle that propose among the above-mentioned background and go up between two stabilizer blades apart from fixed, inconvenient regulation distance between the two for when unmanned aerial vehicle fell on uneven ground, the problem that unmanned aerial vehicle probably appeared empting.
In order to achieve the above object, the utility model provides a following technical scheme: the utility model provides an adjusting device for unmanned aerial vehicle, includes fuselage, stabilizer blade and adjustment mechanism, the fuselage bottom is rotated and is installed the stabilizer blade of two "U" shapes, be provided with adjustment mechanism between stabilizer blade and the fuselage, adjustment mechanism includes mounting panel, slide rail, drives actuating cylinder and coupling assembling, the vertical fixing of mounting panel is at the fuselage lower surface, the slide rail is fixed at the stabilizer blade front surface, it fixes in the mounting panel side to drive actuating cylinder vertical fixation, just it passes through the coupling assembling sliding connection who sets up with the slide rail to drive the inside piston rod of actuating cylinder, coupling assembling includes sliding sleeve, connecting plate and fixed column.
Preferably, the slide rail is overlooked to be T-shaped, the sliding sleeve is sleeved on the slide rail in a sliding manner, a fixed column is fixed on the front surface of the sliding sleeve, one end of the connecting plate is fixed at the end part of the piston rod, and the other end of the connecting plate is sleeved on the fixed column in a rotating manner.
Preferably, the sliding sleeve is internally and rotatably provided with a ball, and the ball is in rolling contact with the surface of the sliding rail.
Preferably, be provided with the firm frame of "U" shape between actuating cylinder and the mounting panel, be provided with the reinforcing plate between mounting panel and the fuselage.
Preferably, the lower surface of the machine body is fixed with a convex plate, and the upper ends of the support legs are rotatably connected with the convex plate through rotating shafts.
Preferably, the lower end of the support leg is provided with a buffer assembly, the buffer assembly comprises a bottom plate, an arc-shaped plate and a supporting plate, the bottom plate is fixed on the inner surface of the lower end of the support leg, and the two S-shaped arc-shaped plates are symmetrically fixed at two ends of the bottom plate.
Preferably, the free end of the arc-shaped plate tilts downwards, a supporting plate is fixed between the arc-shaped plate and the supporting legs, and the arc-shaped plate is a rubber plate.
Preferably, the top of the machine body is provided with a propeller, and the bottom of the machine body is provided with a camera.
Compared with the prior art, the beneficial effects of the utility model are that:
(1) the utility model discloses a be provided with adjustment mechanism, neither influence the descending of unmanned aerial vehicle on ground, can adjust two stabilizer blade work angles and distance between the two as required again to adjust the focus that unmanned aerial vehicle fell to the ground, increase the steadiness that unmanned aerial vehicle fell to the ground, reduce the probability that unmanned aerial vehicle emptys.
(2) The utility model discloses a be provided with the buffering subassembly, neither influence unmanned aerial vehicle flight and fall to the ground, can play the buffering supporting role again when unmanned aerial vehicle appears empting, reduce unmanned aerial vehicle and empty the probability that bumps ground damage at the ground screw, increase unmanned aerial vehicle and fall to the ground stability.
Drawings
Fig. 1 is a schematic structural view of the present invention;
FIG. 2 is a schematic structural diagram of the adjusting 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 structural view of the cushion assembly of the present invention;
in the figure: 1. a body; 2. a support leg; 3. an adjustment mechanism; 31. mounting a plate; 32. a slide rail; 33. a driving cylinder; 4. a buffer assembly; 41. a base plate; 42. an arc-shaped plate; 43. a support plate; 5. a stabilizing frame; 6. a sliding sleeve; 7. a connecting plate; 8. and (5) fixing the column.
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: an adjusting device for an unmanned aerial vehicle comprises a machine body 1, two U-shaped support legs 2 and an adjusting mechanism 3, wherein the two U-shaped support legs 2 are rotatably installed at the bottom of the machine body 1, the adjusting mechanism 3 is arranged between the support legs 2 and the machine body 1, the adjusting mechanism 3 comprises a mounting plate 31, a slide rail 32, a driving cylinder 33 and a connecting assembly, the mounting plate 31 is vertically fixed on the lower surface of the machine body 1, the slide rail 32 is fixed on the front surface of each support leg 2, the driving cylinder 33 is vertically fixed on the side surface of the mounting plate 31, a piston rod inside the driving cylinder 33 is in sliding connection with the slide rail 32 through the arranged connecting assembly, the connecting assembly comprises a sliding sleeve 6, a connecting plate 7 and a fixed column 8, the adjusting mechanism 3 is arranged, the unmanned aerial vehicle can not only land on the ground, but also the working angles of the two support legs 2 and the distance between the two support legs can be adjusted according to requirements, thereby adjusting the center of gravity of the unmanned aerial vehicle when the unmanned aerial vehicle lands, and increasing the stability of the unmanned aerial vehicle when the unmanned aerial vehicle lands, reduce the probability that unmanned aerial vehicle emptys.
In this embodiment, it is preferred, slide rail 32 is overlooked and is regarded as "T" shape, sliding sleeve 6 sliding sleeve establishes on slide rail 32, sliding sleeve 6 front surface is fixed with fixed column 8, connecting plate 7 one end is fixed at the piston rod tip, the other end rotating sleeve establishes on fixed column 8, sliding sleeve 6 internally rotates installs the ball, ball and slide rail 32 surface rolling contact, utilize the frictional resistance between the reducible sliding sleeve 6 of ball and the slide rail 32, utilize coupling assembling to realize being connected of stabilizer blade 2 and piston rod, do not influence the rotation of stabilizer blade 2 simultaneously.
In this embodiment, preferably, a "U" shaped stabilizing frame 5 is disposed between the driving cylinder 33 and the mounting plate 31 to increase the mounting strength of the driving cylinder 33, and a reinforcing plate is disposed between the mounting plate 31 and the body 1.
In this embodiment, preferably, the lower surface of the machine body 1 is fixed with a convex plate, and the upper ends of the support legs 2 are rotatably connected with the convex plate through rotating shafts, so that the angles of the support legs 2 can be conveniently adjusted.
In this embodiment, it is preferred, 2 lower extremes of stabilizer blade are provided with buffering subassembly 4, buffering subassembly 4 includes bottom plate 41, arc 42 and backup pad 43, bottom plate 41 is fixed at 2 lower extreme internal surfaces of stabilizer blade, the arc 42 symmetry of two "S" shapes is fixed at bottom plate 41 both ends, the downward perk of arc 42 free end, be fixed with backup pad 43 between arc 42 and the stabilizer blade 2, arc 42 is the rubber slab, through being provided with buffering subassembly 4, neither influence unmanned aerial vehicle flight and fall to the ground, can play the buffering supporting role again when unmanned aerial vehicle appears empting, reduce unmanned aerial vehicle and empty the probability that damages in the ground screw touchhing ground, increase unmanned aerial vehicle and fall to the ground stability.
In this embodiment, preferably, a propeller is disposed at the top of the body 1, and a camera is disposed at the bottom of the body 1.
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, two drive cylinders 33 work simultaneously, the inside piston rod is carried on back of the body or relative movement simultaneously, drive connecting plate 7 and move, connecting plate 7 drives sliding sleeve 6 and slides on slide rail 32, the ball atress appears rolling, two stabilizer blade 2 working angles appear changing at this moment, until two stabilizer blade 2 angles are suitable, drive cylinder 33 stop work, the distance is suitable between two stabilizer blades 2, and unmanned aerial vehicle's focus changes, through being provided with adjustment mechanism 3, neither influence unmanned aerial vehicle to descend on the ground, can adjust two stabilizer blade 2 working angles and the distance between the two as required again, thereby adjust the focus that unmanned aerial vehicle fell to the ground, increase the steadiness that unmanned aerial vehicle fell to the ground, reduce the probability that unmanned aerial vehicle topples; when unmanned aerial vehicle appearance trend of empting simultaneously, utilize arc 42 and backup pad 43 to play the buffering supporting role to empting of unmanned aerial vehicle, increase unmanned aerial vehicle and place stability.
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 (8)
1. The utility model provides an adjusting device for unmanned aerial vehicle, includes fuselage (1), stabilizer blade (2) and adjustment mechanism (3), its characterized in that: fuselage (1) bottom is rotated and is installed stabilizer blade (2) of two "U" shapes, be provided with adjustment mechanism (3) between stabilizer blade (2) and fuselage (1), adjustment mechanism (3) include mounting panel (31), slide rail (32), drive actuating cylinder (33) and coupling assembling, mounting panel (31) vertical fixing is at fuselage (1) lower surface, slide rail (32) are fixed at stabilizer blade (2) front surface, drive actuating cylinder (33) vertical fixation in mounting panel (31) side, just drive actuating cylinder (33) inside piston rod and slide rail (32) coupling assembling sliding connection through setting up, coupling assembling includes sliding sleeve (6), connecting plate (7) and fixed column (8).
2. An adjustment device for unmanned aerial vehicle according to claim 1, characterized in that: the sliding rail (32) is overlooked to be T-shaped, the sliding sleeve (6) is sleeved on the sliding rail (32) in a sliding mode, a fixing column (8) is fixed on the front surface of the sliding sleeve (6), one end of the connecting plate (7) is fixed to the end portion of the piston rod, and the other end of the connecting plate is rotatably sleeved on the fixing column (8).
3. An adjustment device for unmanned aerial vehicle according to claim 1, characterized in that: the sliding sleeve (6) is internally and rotatably provided with a ball, and the ball is in surface rolling contact with the sliding rail (32).
4. An adjustment device for unmanned aerial vehicle according to claim 1, characterized in that: a U-shaped stabilizing frame (5) is arranged between the driving cylinder (33) and the mounting plate (31), and a reinforcing plate is arranged between the mounting plate (31) and the machine body (1).
5. An adjustment device for unmanned aerial vehicle according to claim 1, characterized in that: the lower surface of the machine body (1) is fixed with a convex plate, and the upper ends of the support legs (2) are rotatably connected with the convex plate through rotating shafts.
6. An adjustment device for unmanned aerial vehicle according to claim 1, characterized in that: the lower end of the supporting leg (2) is provided with a buffer assembly (4), the buffer assembly (4) comprises a bottom plate (41), an arc-shaped plate (42) and a supporting plate (43), the bottom plate (41) is fixed on the inner surface of the lower end of the supporting leg (2), and the two S-shaped arc-shaped plates (42) are symmetrically fixed at two ends of the bottom plate (41).
7. An adjustment device for unmanned aerial vehicle according to claim 6, characterized in that: the arc (42) free end perk downwards, be fixed with backup pad (43) between arc (42) and stabilizer blade (2), arc (42) are the rubber slab.
8. An adjustment device for unmanned aerial vehicle according to claim 1, characterized in that: the top of the machine body (1) is provided with a propeller, and the bottom of the machine body (1) is provided with a camera.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202120491002.0U CN214420697U (en) | 2021-03-08 | 2021-03-08 | A adjusting device for unmanned aerial vehicle |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202120491002.0U CN214420697U (en) | 2021-03-08 | 2021-03-08 | A adjusting device for unmanned aerial vehicle |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN214420697U true CN214420697U (en) | 2021-10-19 |
Family
ID=78072794
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202120491002.0U Active CN214420697U (en) | 2021-03-08 | 2021-03-08 | A adjusting device for unmanned aerial vehicle |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN214420697U (en) |
-
2021
- 2021-03-08 CN CN202120491002.0U patent/CN214420697U/en active Active
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CN207181918U (en) | A kind of single-lens single-axis tilt camera for airborne vehicle | |
| CN214420697U (en) | A adjusting device for unmanned aerial vehicle | |
| CN110823188A (en) | Full-automatic topographic map surveying and mapping device and surveying and mapping method | |
| CN110285296A (en) | A kind of rotation screen camera lifting linkage structure | |
| CN115783331B (en) | Unmanned aerial vehicle-based intelligent mapping device for building engineering | |
| CN217893216U (en) | Unmanned aerial vehicle undercarriage | |
| CN207777990U (en) | Holder is stablized in hand-held ultralight photography | |
| CN109178311B (en) | Shooting visual angle is wide two cloud platform unmanned aerial vehicle | |
| CN215794494U (en) | Aerial photography unmanned aerial vehicle is from steady cloud platform | |
| CN212251965U (en) | Indoor interactive LED display screen | |
| CN211667553U (en) | Handheld camera shooting support | |
| CN213862661U (en) | High-precision mapping unmanned aerial vehicle | |
| CN210890779U (en) | Rotation and sweep oblique photography cloud platform of pendulum combination | |
| CN210600752U (en) | Swing screen camera lift linkage structure | |
| CN110594545B (en) | Swing screen camera lifting linkage structure | |
| CN219857636U (en) | Unmanned aerial vehicle tilting camera device | |
| CN221660979U (en) | Unmanned aerial vehicle capable of stably shooting | |
| CN214524437U (en) | Actual combat type unmanned aerial vehicle supports location structure | |
| CN214451889U (en) | Unmanned aerial vehicle triaxial increases steady cloud platform | |
| CN216360023U (en) | Visual angle adjusting mechanism for unmanned aerial vehicle surveying and mapping | |
| CN214372443U (en) | Three-dimensional topography unmanned aerial vehicle aerial photography device | |
| CN211281459U (en) | Multispectral imaging system of portable unmanned aerial vehicle | |
| CN215826995U (en) | Multi-rotor aerial photography unmanned aerial vehicle three-axis self-stabilizing cradle head | |
| CN218751377U (en) | Unmanned aerial vehicle floor stand | |
| CN116729667A (en) | Unmanned aerial vehicle shoots support damping device |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| TR01 | Transfer of patent right |
Effective date of registration: 20230425 Address after: 163000 New Area Technology Incubator Phase I Project No. 2 Incubator in Daqing City, Heilongjiang Province Patentee after: Ma Jiazheng Address before: 163000 room 223, block A2, No. 101, 102, 2-10, 1115-1119, 1214-1219, No. 2 incubator of phase I project of science and technology incubator in Daqing high tech Zone, Heilongjiang Province Patentee before: Daqing junchuang Hefei Technology Development Co.,Ltd. |
|
| TR01 | Transfer of patent right |