CN218493530U - A decoupling type work ladder for unmanned aerial vehicle maintains - Google Patents
A decoupling type work ladder for unmanned aerial vehicle maintains Download PDFInfo
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- CN218493530U CN218493530U CN202222394362.6U CN202222394362U CN218493530U CN 218493530 U CN218493530 U CN 218493530U CN 202222394362 U CN202222394362 U CN 202222394362U CN 218493530 U CN218493530 U CN 218493530U
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Abstract
The utility model relates to an unmanned aerial vehicle maintains technical field, discloses a decoupling zero formula work ladder for unmanned aerial vehicle maintains, including first work ladder, detachable connect in the second work ladder at first work ladder top. The utility model provides a guarantee that prior art exists big, the function singleness, availability factor low, packing cost of transportation scheduling problem.
Description
Technical Field
The utility model relates to an unmanned aerial vehicle maintains technical field, specifically is a decoupling type work ladder for unmanned aerial vehicle maintains.
Background
Unmanned aerial vehicle belongs to the precision apparatus, and the flight state and life can all be influenced to the slight change of any part. Therefore, drones should be careful during routine use and should be maintained and inspected regularly.
Among the prior art, when accomplishing large-scale unmanned aerial vehicle maintenance work, need the work ladder of different specifications supplementary, lead to that the guarantee scale is big, the function is single, the availability factor is low, packing cost of transportation is high.
SUMMERY OF THE UTILITY MODEL
For overcoming the not enough of prior art, the utility model provides a decoupling zero formula work ladder for unmanned aerial vehicle maintains solves that the guarantee scale that prior art exists is big, the function singleness, the availability factor is low, packing cost of transportation scheduling problem.
The utility model provides a technical scheme that above-mentioned problem adopted is:
the utility model provides a decoupling type work ladder for unmanned aerial vehicle maintains, includes first work ladder, detachable connect in the second work ladder at first work ladder top.
As a preferable technical solution, the top of the first working ladder is detachably connected with a safety support frame, and the safety support frame can be unfolded or folded relative to the first working ladder.
As a preferred technical scheme, the top of the first working ladder and the top of the safe supporting frame are provided with mounting holes, and the second working ladder is detachably connected with the first working ladder through the mounting holes.
As a preferable technical scheme, special support legs matched with the mounting holes are arranged at the bottom of the second working ladder.
As a preferable technical solution, a locking/releasing mechanism is disposed at the bottom of the dedicated support leg, the locking/releasing mechanism is detachably connected to a fixing base, and the fixing base can sleeve the locking/releasing mechanism therein.
As a preferable technical solution, the number of the mounting holes, the dedicated support legs, the locking/releasing mechanism, and the fixing base is four.
In a preferred embodiment, the second working ladder is provided with a moving wheel and a switching mechanism, and the moving wheel can be unfolded or folded by operating the switching mechanism.
In a preferred embodiment, the conversion mechanism is a rotary mechanism, and rotating the conversion mechanism can unfold or fold the movable wheel.
As a preferred technical scheme, the number of steps of the first working ladder is three, and the number of steps of the second working ladder is two.
Compared with the prior art, the utility model, following beneficial effect has:
the utility model discloses it is easy and simple to handle, improved and equipped availability factor, reduced packing, storage, cost of transportation, reached a ladder number usefulness, satisfied different use and maintain the demand and reduce life-span expense purpose.
Drawings
Fig. 1 is a schematic structural view of the present invention;
FIG. 2 is a schematic structural view of a first working ladder with a safety support;
FIG. 3 is a schematic structural view of a second working ladder;
FIG. 4 is a schematic diagram of a five-step working ladder mode;
FIG. 5 is a schematic view of the primary and secondary work benches and work platform modes;
fig. 6 is a schematic view of the mobile working ladder mode (90 degrees counterclockwise rotation).
Reference numbers and corresponding part names in the drawings: 1. the working ladder comprises a first working ladder body, a second working ladder body, a safety supporting frame body, 4 mounting holes, 5 special supporting legs, 6 locking/releasing mechanisms, 7 fixing seats, 8 moving wheels, 9 and a switching mechanism.
Detailed Description
The present invention will be described in further detail with reference to the following examples and drawings, but the present invention is not limited thereto.
Example 1
As shown in fig. 1 to 6, when the maintenance work of the medium-large unmanned aerial vehicle is completed, the requirements of different working heights and movement need to be solved. The fully-functional working ladder with the decoupling design is combined dynamically and statically, is random in height and height, and meets general requirements of use and maintenance.
The utility model provides a decoupling type work ladder for unmanned aerial vehicle maintains, makes up according to the user demand at will, realizes multiple mode, no longer need dispose other supplementary work ladders and workstation. Social resources are saved, and the service cost in the life cycle is reduced. The second-level fixed step is provided with a movable wheel for switching the speed at the highest speed, a second-level movable working stool and a working platform. The freely-detachable and pleasurable combined working ladder is widely applied to the use and maintenance of all medium and large unmanned aerial vehicles.
The decoupling type working ladder for unmanned aerial vehicle maintenance shown in fig. 1 is composed of a first working ladder 1 (working ladder with three-level fixed steps) and a second working ladder 2 (working ladder with two-level fixed steps) with safety supports. The reverse direction of the step surface at the top of the first working ladder 1 shown in fig. 2 is provided with a fast unfolding or folding safety supporting frame 3 which is provided with a mounting hole 4; the bottom of the second working ladder 2 shown in fig. 3 is provided with four special support legs 5, and the bottom of the special support legs 5 is provided with a locking/releasing mechanism 6 and a fixing seat 7 which can be locked or released quickly, so as to form a safe fixing structure.
The special support legs of the second working ladder 2 shown in fig. 4 are inserted into the mounting holes 4 of the first working ladder 1 and the safety support frame 3; the quick locking/releasing mechanism 6 and the fixed seat 7 are matched to fix the ladder with the three-stage working ladder; fig. 5 shows a state in which the second working ladder 2 is moved by rotating the direction of the moving wheel 8 by the speed switching mechanism 9 with four built-in moving wheels 8 provided in the second working ladder 2.
A decoupled work ladder application mode for drone maintenance described as follows:
the second working ladder 2 is used independently, the middle part of the machine body is maintained, and the working ladder or the working platform is moved, as shown in fig. 5 and 6;
a three-level working ladder mode 1 independent use mode, as shown in fig. 2; the first-stage step and the second-stage step maintain the low and middle parts of the airplane, and the third-stage step maintains the top parts of the airplane body and the wings; a safety supporting frame 3 which can be unfolded or folded quickly is designed in the opposite direction of the step; mounting holes 4 connected with the second-level fixed steps are designed on the surfaces of the third-level steps and the top of the safe supporting frame;
five-stage working ladder mode: a second working ladder 2 is superposed on the first working ladder 1 to realize the function of a five-level working ladder and meet the maintenance of a horizontal tail and a vertical tail of an airplane. As shown in fig. 4.
The utility model discloses it is easy and simple to handle, improved and equipped availability factor, reduced packing, storage, cost of transportation, reached a ladder number usefulness, satisfied different use and maintain the demand and reduce life-span expense purpose.
As described above, the present invention can be preferably realized.
The above description is only a preferred embodiment of the present invention, and is not intended to limit the present invention in any way, and the technical essence of the present invention is that any simple modification, equivalent replacement, and improvement made to the above embodiments, within the spirit and principle of the present invention, all still belong to the protection scope of the technical solution of the present invention.
Claims (9)
1. The utility model provides a decoupling type work ladder for unmanned aerial vehicle maintains, its characterized in that includes first work ladder (1), detachable connect in second work ladder (2) at first work ladder (1) top.
2. A decoupled working ladder for unmanned aerial vehicle maintenance according to claim 1, characterized in that the top of the first working ladder (1) is detachably connected with a safety support frame (3), and the safety support frame (3) can be unfolded or folded relative to the first working ladder (1).
3. The decoupling type working ladder for unmanned aerial vehicle maintenance according to claim 2, characterized in that the top of the first working ladder (1) and the top of the safety support frame (3) are provided with mounting holes (4), and the second working ladder (2) is detachably connected with the first working ladder (1) through the mounting holes (4).
4. A decoupled working ladder for unmanned aerial vehicle maintenance according to claim 3, characterized in that the bottom of the second working ladder (2) is provided with special support legs (5) cooperating with the mounting holes (4).
5. The decoupling working ladder for unmanned aerial vehicle maintenance according to claim 4, wherein a locking/releasing mechanism (6) is arranged at the bottom of the special supporting leg (5), the locking/releasing mechanism (6) is detachably connected with a fixing base (7), and the fixing base (7) can sleeve the locking/releasing mechanism (6) therein.
6. A decoupled working ladder for unmanned aerial vehicle maintenance, according to claim 5, characterized in that the number of mounting holes (4), dedicated legs (5), locking/releasing mechanisms (6), fixing seats (7) is four.
7. A decoupled working ladder for unmanned aerial vehicle maintenance according to claim 6, characterized in that the second working ladder (2) is provided with moving wheels (8), a switching mechanism (9), and the moving wheels (8) can be unfolded or folded by operating the switching mechanism (9).
8. A decoupled working ladder for unmanned aerial vehicle maintenance according to claim 7, characterized in that the switching mechanism (9) is a rotary structure, rotating the switching mechanism (9) enabling unfolding or folding of the moving wheels (8).
9. A decoupled work ladder for unmanned aerial vehicle maintenance according to any of claims 1 to 8, characterized in that the first work ladder (1) has three steps and the second work ladder (2) has two steps.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202222394362.6U CN218493530U (en) | 2022-09-08 | 2022-09-08 | A decoupling type work ladder for unmanned aerial vehicle maintains |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202222394362.6U CN218493530U (en) | 2022-09-08 | 2022-09-08 | A decoupling type work ladder for unmanned aerial vehicle maintains |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN218493530U true CN218493530U (en) | 2023-02-17 |
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Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202222394362.6U Active CN218493530U (en) | 2022-09-08 | 2022-09-08 | A decoupling type work ladder for unmanned aerial vehicle maintains |
Country Status (1)
| Country | Link |
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| CN (1) | CN218493530U (en) |
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- 2022-09-08 CN CN202222394362.6U patent/CN218493530U/en active Active
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