CN217575630U - Big load unmanned aerial vehicle flight platform that stability is good - Google Patents
Big load unmanned aerial vehicle flight platform that stability is good Download PDFInfo
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- CN217575630U CN217575630U CN202221883646.5U CN202221883646U CN217575630U CN 217575630 U CN217575630 U CN 217575630U CN 202221883646 U CN202221883646 U CN 202221883646U CN 217575630 U CN217575630 U CN 217575630U
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Abstract
The utility model discloses a high-load unmanned aerial vehicle flight platform with good stability, which comprises a platform shell, wherein the bottom inside the platform shell is provided with an electric push rod, the output end of the electric push rod is provided with a shutdown platform, two sides of the top of the shutdown platform are provided with straps, racks are symmetrically arranged on two sides of the shutdown platform, and the middle parts of two sides inside the platform shell are provided with rotating shafts; the utility model discloses an electric push rod drive shut-down platform places unmanned aerial vehicle to bind the unmanned aerial vehicle organism through the tie, in order to keep unmanned aerial vehicle stable when shifting, improve its security performance, avoid unmanned aerial vehicle crooked, collide with, make unmanned aerial vehicle inner part appear damaging; and when the shutdown platform moves, through mutual cooperation of rack, gear, rope sheave, stay cord, follow driving wheel, opening, realize two sets of baffles in step and to the inside sealed effect of platform casing, need not external drive power and carry out relevant sealed setting.
Description
Technical Field
The utility model relates to an unmanned aerial vehicle flight platform technical field specifically is a big load unmanned aerial vehicle flight platform that stability is good.
Background
In the field of existing rotor unmanned aerial vehicles, the types of heavy-load aircrafts are few, most of the loads cannot exceed 3KG, and a suitable flight platform is lacked for some heavy-mass mounting; and big load unmanned aerial vehicle places the face unevenness because its loading capacity is big, the stability of accomodating is relatively poor and the difference of the environment that flight platform is located, all can play great influence to taking off, descending of unmanned aerial vehicle.
SUMMERY OF THE UTILITY MODEL
An object of the utility model is to provide a big load unmanned aerial vehicle flight platform that stability is good to propose current problem in solving above-mentioned background art.
In order to achieve the above object, the utility model provides a following technical scheme: a high-load unmanned aerial vehicle flight platform with good stability comprises a platform shell, wherein an electric push rod is arranged at the bottom inside the platform shell, a shutdown platform is installed at the output end of the electric push rod, binding belts are arranged on two sides of the top of the shutdown platform, racks are symmetrically arranged on two sides of the shutdown platform, rotating shafts are arranged in the middle of two sides inside the platform shell, a rope pulley is arranged at one end of the outer side of each rotating shaft, a gear is sleeved on the other end of the outer side of each rotating shaft, the racks are meshed with the gears, a pull rope is arranged on the outer side of each rope pulley, through holes are formed in the middle of two sides of the platform shell, and the pull rope penetrates through the through holes and extends to the outside of the platform shell;
the roof is installed at the top of platform casing, the through-hole has been seted up to the inside intermediate position department of roof, the holding tank has been seted up to the inside bilateral symmetry of roof, the spout has been seted up at the inside both ends of holding tank, and is two sets of the inside sliding connection of spout has two sets of baffles, the bilateral symmetry of roof is equipped with from the driving wheel, and is two sets of the stay cord passes from the outside of driving wheel and carries on the back one side interconnect with two sets of baffles mutually respectively, and is two sets of the outside of the inside stay cord of holding tank all is equipped with the spring, the bilateral symmetry of platform casing is equipped with supports stabilizing mean.
Preferably, the supporting and stabilizing mechanism comprises two groups of supporting plates, the two groups of supporting plates are respectively positioned at the bottoms of the two sides of the platform shell, threaded holes are formed in the two ends of the top of each supporting plate, adjusting screws are arranged in the threaded holes, supporting rods are arranged at the bottoms of the adjusting screws, supporting blocks are arranged at the bottoms of the supporting rods, and handles are arranged at the tops of the adjusting screws.
Preferably, a control panel is arranged at one end of the front face of the platform shell, and the control panel is electrically connected with the electric push rod through a lead.
Preferably, both sides of the bottom of the platform shell are provided with holes matched with the racks.
Preferably, the driven wheels are arranged on two sides of the top plate through mounting seats.
Preferably, the top plate is provided with through holes at two sides, and the pull rope is erected at the outer side of the driven wheel and penetrates through the through holes to be connected with one side of the baffle.
Compared with the prior art, the beneficial effects of the utility model are that: the high-stability large-load unmanned aerial vehicle flying platform drives the stopping platform to place the unmanned aerial vehicle through the electric push rod, and binds the unmanned aerial vehicle body through the binding belt so as to keep the stability of the unmanned aerial vehicle during transfer, improve the safety performance of the unmanned aerial vehicle, avoid the unmanned aerial vehicle from being inclined and collided and damage internal parts of the unmanned aerial vehicle; when the shutdown platform moves, the two groups of baffles are synchronously sealed inside the platform shell through the mutual matching of the rack, the gear, the rope pulley, the pull rope, the driven wheel and the through opening, and the external driving force is not needed for carrying out related sealing setting; can adjust the position of the supporting shoe of bracing piece bottom through rotating adjusting screw to carry out corresponding adjustment according to unevenness's the environment of placing, make the roof be in the level, with the stability when keeping flight platform to put, and then guarantee big load unmanned aerial vehicle's normal use.
Drawings
Fig. 1 is a perspective view of the present invention;
fig. 2 is a front sectional view of the present invention;
FIG. 3 is a front view of the present invention;
fig. 4 is an enlarged view of fig. 2 a according to the present invention;
fig. 5 is an enlarged view of the position B of fig. 2 according to the present invention.
In the figure: 1. a platform housing; 2. an electric push rod; 3. a support plate; 4. a support stabilizing mechanism; 41. a support block; 42. a support bar; 43. adjusting the screw rod; 5. a port; 6. pulling a rope; 7. a baffle plate; 8. a top plate; 9. a through hole; 10. a chute; 11. a binding band; 12. a shutdown platform; 13. a driven wheel; 14. accommodating grooves; 15. a spring; 16. a rack; 17. a sheave; 18. a rotating shaft; 19. a gear.
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 efforts all belong to the protection scope of the present invention.
Referring to fig. 1-5, the present invention provides an embodiment: a high-load unmanned aerial vehicle flight platform with good stability comprises a platform shell 1, an electric push rod 2 is arranged at the bottom inside the platform shell 1, a shutdown platform 12 is installed at the output end of the electric push rod 2, straps 11 are arranged on two sides of the top of the shutdown platform 12, racks 16 are symmetrically arranged on two sides of the shutdown platform 12, rotating shafts 18 are arranged in the middle of two sides inside the platform shell 1, rope pulleys 17 are arranged at one ends of the outer sides of the rotating shafts 18, gears 19 are sleeved on the other ends of the outer sides of the rotating shafts 18, the racks 16 are meshed with the gears 19, pull ropes 6 are arranged on the outer sides of the rope pulleys 17, through holes 5 are formed in the middle of two sides of the platform shell 1, the pull ropes 6 extend to the outside of the platform shell 1 through the through holes 5, a control panel is arranged at one end of the front side of the platform shell 1 and is electrically connected with the electric push rod 2 through a lead, the electric push rod 2 is controlled by the control panel to move the shutdown platform 12, holes matched with the racks 16 are formed in two sides of the bottom of the platform shell 1, and the racks 16 can be moved out in the holes;
The working principle is as follows: when the flying platform is used conventionally, the two groups of baffles 7 are driven to be mutually closed to serve as a platform through the elastic potential energy of the two groups of springs 15, and the flying platform can be used for performing conventional arrangement on the flying function of the unmanned aerial vehicle;
the stopping platform 12 is driven to move upwards by the driving of the electric push rod 2, the gear rack 16 mounted on the stopping platform 12 is driven to move upwards respectively by the upward movement of the stopping platform 12, so that the gear 19 is driven to rotate, the rope pulley 17 is driven to roll the pull rope 6 by the rotation of the gear 19, the other end of the pull rope 6 pulls the baffle 7, so that the two groups of baffle 7 are separated from each other, and the spring 15 is compressed by the baffle 7, so that the sealing effect on the platform shell 1 is relieved, then the stopping platform 12 can serve as a flying platform, the unmanned aerial vehicle is landed to the top of the stopping platform 12, then the body of the unmanned aerial vehicle can be bound and fixed by the binding belt 11, then the stopping platform 12 is driven to move downwards by the electric push rod 2 again, the unmanned aerial vehicle is moved into the inside of the platform shell 1 to be stored, the rack 16, the gear 19 and the rope pulley 17 are driven to perform paying-off operation while the stopping platform 12 moves downwards, and the two groups of the baffle 7 are driven to approach each other to perform sealing operation by the elastic restoring force of the spring 15;
can adjust the position of the supporting shoe 41 of bracing piece 42 bottom through rotating adjusting screw 43 to carry out corresponding adjustment according to unevenness's the environment of placing, make roof 8 be in the horizontality, stability when guaranteeing unmanned aerial vehicle's lift.
It is obvious to a person skilled in the art that the invention is not restricted to details of the above-described exemplary embodiments, but that it can be implemented in other specific forms without departing from the spirit or essential characteristics of the invention. The present embodiments are therefore to be considered in all respects as illustrative and not restrictive, the scope of the invention being indicated by the appended claims rather than by the foregoing description, and all changes which come within the meaning and range of equivalency of the claims are therefore intended to be embraced therein. Any reference sign in a claim should not be construed as limiting the claim concerned.
In the description of the present invention, "a plurality" means two or more unless otherwise specified; the terms "upper", "lower", "left", "right", "inner", "outer", "front", "rear", "head", "tail", and the like indicate orientations or positional relationships based on the orientations or positional relationships shown in the drawings, and are merely for convenience of description and simplicity of description, and do not indicate or imply that the device or element being referred to must have a particular orientation, be constructed and operated in a particular orientation, and thus, should not be construed as limiting the present invention. Furthermore, the terms "first," "second," "third," and the like are used for descriptive purposes only and are not to be construed as indicating or implying relative importance.
In the description of the present invention, it is to be noted that, unless otherwise explicitly specified or limited, the terms "connected" and "connected" are to be interpreted broadly, e.g., as either a fixed connection or a detachable connection; can be mechanically or electrically connected; may be directly connected or indirectly connected through an intermediate. The specific meaning of the above terms in the present invention can be understood in specific cases to those skilled in the art.
Claims (6)
1. The utility model provides a big load unmanned aerial vehicle flight platform that stability is good, includes platform casing (1), its characterized in that: an electric push rod (2) is arranged at the bottom inside the platform shell (1), a shutdown platform (12) is installed at the output end of the electric push rod (2), binding belts (11) are arranged on two sides of the top of the shutdown platform (12), racks (16) are symmetrically arranged on two sides of the shutdown platform (12), a rotating shaft (18) is arranged in the middle of two sides inside the platform shell (1), a rope pulley (17) is arranged at one end of the outer side of the rotating shaft (18), a gear (19) is sleeved at the other end of the outer side of the rotating shaft (18), the racks (16) are meshed with the gear (19), a pull rope (6) is arranged on the outer side of the rope pulley (17), through holes (5) are formed in the middle of two sides of the platform shell (1), and the pull rope (6) penetrates through the through holes (5) and extends to the outside of the platform shell (1);
roof (8) are installed at the top of platform casing (1), through-hole (9) have been seted up to the inside intermediate position department of roof (8), holding tank (14) have been seted up to the inside bilateral symmetry of roof (8), spout (10), two sets of have been seted up at the inside both ends of holding tank (14) the inside sliding connection of spout (10) has two sets of baffles (7), the bilateral symmetry of roof (8) is equipped with from driving wheel (13), and is two sets of stay cord (6) are passed from the outside of driving wheel (13) and are carried on the back one side interconnect of carrying on the body with two sets of baffles (7) respectively, and are two sets of all the cover in the outside of holding tank (14) inside stay cord (6) is equipped with spring (15), the bilateral symmetry of platform casing (1) is equipped with and supports stabilizing mean (4).
2. The high-load unmanned aerial vehicle flight platform with good stability of claim 1, characterized in that: the supporting and stabilizing mechanism (4) comprises two groups of supporting plates (3), the two groups of supporting plates (3) are respectively located at the bottoms of the two sides of the platform shell (1), threaded holes are formed in the two ends of the top of each supporting plate (3), adjusting screws (43) are arranged inside the threaded holes, supporting rods (42) are arranged at the bottoms of the adjusting screws (43), supporting blocks (41) are arranged at the bottoms of the supporting rods (42), and handles are arranged at the tops of the adjusting screws (43).
3. The high-load unmanned aerial vehicle flight platform with good stability of claim 1, characterized in that: the front end of the platform shell (1) is provided with a control panel, and the control panel is electrically connected with the electric push rod (2) through a lead.
4. The high-load unmanned aerial vehicle flight platform with good stability of claim 1, characterized in that: holes matched with the racks (16) are formed in the two sides of the bottom of the platform shell (1).
5. The high-load unmanned aerial vehicle flight platform that stability is good according to claim 1, characterized in that: the driven wheels (13) are arranged on two sides of the top plate (8) through mounting seats.
6. The high-load unmanned aerial vehicle flight platform with good stability of claim 1, characterized in that: the two sides of the top plate (8) are provided with through holes, and the pull rope (6) is arranged on the outer side of the driven wheel (13) and penetrates through the through holes to be connected with one side of the baffle (7).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202221883646.5U CN217575630U (en) | 2022-07-21 | 2022-07-21 | Big load unmanned aerial vehicle flight platform that stability is good |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202221883646.5U CN217575630U (en) | 2022-07-21 | 2022-07-21 | Big load unmanned aerial vehicle flight platform that stability is good |
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| CN217575630U true CN217575630U (en) | 2022-10-14 |
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| Application Number | Title | Priority Date | Filing Date |
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| CN202221883646.5U Active CN217575630U (en) | 2022-07-21 | 2022-07-21 | Big load unmanned aerial vehicle flight platform that stability is good |
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Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN117550126A (en) * | 2024-01-11 | 2024-02-13 | 华慧科技(长春)有限公司 | Unmanned aerial vehicle is with platform that takes off and land |
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2022
- 2022-07-21 CN CN202221883646.5U patent/CN217575630U/en active Active
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN117550126A (en) * | 2024-01-11 | 2024-02-13 | 华慧科技(长春)有限公司 | Unmanned aerial vehicle is with platform that takes off and land |
| CN117550126B (en) * | 2024-01-11 | 2024-04-02 | 华慧科技(长春)有限公司 | Unmanned aerial vehicle is with platform that takes off and land |
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