Rotor wing unmanned aerial vehicle recycling platform for building construction measurement
By designing a rotary-wing drone recovery platform with a rotatable storage box lid and a buffer mechanism, the portability and shock absorption issues of drone recovery platforms at construction sites have been solved, achieving stable and convenient drone recovery.
Patent Information
- Application Number
- CN202520032376.4
- Authority / Receiving Office
- CN · China
- Patent Type
- Utility models(China)
- Current Assignee / Owner
- Filing Date
- 2025-01-07
- Publication Date
- 2025-11-18
- Estimated Expiration
- 2035-01-07
AI Technical Summary
Existing drone recovery platforms are difficult to carry conveniently at construction sites and cannot effectively reduce the vibration and impact during drone recovery, making them particularly inconvenient to use in complex environments.
A rotary-wing drone recovery platform was designed, which includes No. 1 and No. 2 storage box covers. The box covers are rotatably connected, and the bottom is equipped with support legs and a buffer mechanism. The support legs are connected by a damping pivot, and the buffer mechanism consists of a column and a buffer spring for support and shock absorption.
It enables convenient carrying and stable recovery of drones, reduces vibration and impact during recovery, and improves practicality and safety.
Smart Images
Figure CN223559873U_ABST
Abstract
Description
TECHNICAL FIELD
[0001] The utility model relates to unmanned plane recycling platform technical field, concretely relates to a rotor unmanned plane recycling platform for construction survey. BACKGROUND
[0002] Unmanned aircraft is called "drone" for short, which is a kind of aircraft without crew, controlled by radio remote control equipment and self-provided program control device, or operated by on-board computer completely or intermittently.
[0003] Nowadays, drones are widely used in various fields. In the field of construction, some drones can replace manual work to measure and survey buildings. After the completion of unmanned aerial vehicle measurement, the unmanned aerial vehicle needs to be recycled. Although the unmanned aerial vehicle has a support frame, the construction site environment is complex, and there is often accumulated water and mud on the ground, which makes it inconvenient for the normal recycling of the unmanned aerial vehicle.
[0004] The existing method is to place a wooden board on the ground to make the unmanned aerial vehicle stop on the wooden board. However, it is troublesome to carry the wooden board, and the operator needs to find a suitable wooden board on the construction site every time, which is troublesome. UTILITY MODEL CONTENT
[0005] In order to solve the above technical problems, the utility model embodiment provides a rotor unmanned plane recycling platform for construction survey, which comprises a first storage box cover and a second storage box cover, the first storage box cover and the second storage box cover are rotationally connected, the first storage box cover and the second storage box cover can be rotated to a flush state, symmetrically distributed support legs are arranged at the bottom of the first storage box cover and the second storage box cover, a buffer mechanism is further included, the buffer mechanism is installed in the first storage box cover and the second storage box cover, and is used for buffering and preventing collision.
[0006] Further, the bottom of the first storage box cover and the second storage box cover is provided with symmetrically distributed rotating seats, the rotating seats are provided with damping shafts, and the support legs are rotationally connected with the rotating seats through the damping shafts.
[0007] Further, a limiting plate is arranged on the rotating seat, and the support leg can be rotated and attached to the limiting plate.
[0008] Further, the first storage box cover and the second storage box cover are provided with a handle that can be attached.
[0009] Further, the first storage box cover and the second storage box cover are provided with a handle that can be attached.
[0010] Further, the buffer mechanism comprises columns arranged in the first storage box cover and the second storage box cover, a plurality of the columns are symmetrically distributed, a supporting plate is sleeved on the columns, and a buffer spring is annularly sleeved outside the columns, and the buffer spring is located at the bottom of the supporting plate.
[0011] Further, screw holes are formed in the top surface of the columns, mounting holes matched with the columns are formed in the supporting plate, and hand screws are connected in the screw holes and are pressed on the supporting plate.
[0012] Compared with the prior art, the utility model has the advantages that:
[0013] By arranging the first storage box cover and the second storage box cover which are rotationally connected with each other, the first storage box cover and the second storage box cover can be stored as a hand luggage to facilitate carrying and storage, supporting legs for supporting the first storage box cover and the second storage box cover from the ground are arranged at the bottom of the first storage box cover and the second storage box cover, and a buffer mechanism is further arranged to reduce the impact force generated when the unmanned aerial vehicle falls on the supporting plate, thereby playing a protection role and improving the practicability. BRIEF DESCRIPTION OF DRAWINGS
[0014] In order to more clearly illustrate the specific embodiments of the utility model or the technical solutions in the prior art, the following will briefly introduce the drawings needed to be used in the specific embodiments or the prior art description, and obviously, the drawings in the following description are some embodiments of the utility model, and those skilled in the art can also obtain other drawings according to these drawings without creating any creative labor.
[0015] Figure 1 It is the three-dimensional structure schematic diagram of the utility model;
[0016] Figure 2 It is the axonometric structure schematic diagram of the utility model;
[0017] Figure 3 It is Figure 2 the enlarged structure schematic diagram of A in the figure;
[0018] Figure 4 It is the split structure schematic diagram of the utility model;
[0019] Figure 5 It is Figure 4 the enlarged structure schematic diagram of B in the figure.
[0020] Figure: 1, the first storage box cover; 2, the second storage box cover; 3, the supporting plate; 4, the lock catch; 5, the handle; 6, the supporting leg; 7, the rotating seat; 8, the damping rotating shaft; 9, the limiting plate; 10, the hand screw; 11, the mounting hole; 12, the column; 13, the screw hole; 14, the buffer spring. DETAILED DESCRIPTION
[0021] The technical solutions of the utility model will be described clearly and completely in conjunction with the drawings. Obviously, the described embodiments are some of the embodiments of the utility model, rather than all the embodiments. Based on the embodiments in the utility model, all other embodiments obtained by those skilled in the art without creative labor fall within the protection scope of the utility model. In the case of no conflict, the following embodiments and the features in the embodiments can be combined with each other.
[0022] As Figures 1-5 , the embodiment provides a rotor unmanned aerial vehicle recovery platform for building construction measurement, which comprises a first storage box cover 1 and a second storage box cover 2, the first storage box cover 1 and the second storage box cover 2 are rotationally connected, and the first storage box cover 1 and the second storage box cover 2 can be rotated to a flush state; symmetrically distributed supporting legs 6 are arranged at the bottom of the first storage box cover 1 and the second storage box cover 2; further comprising a buffer mechanism; the buffer mechanism is installed in the first storage box cover 1 and the second storage box cover 2 and is used for buffering and preventing collision.
[0023] In the embodiment, as Figure 2 and Figure 3 shown, the bottom of the first storage box cover 1 and the second storage box cover 2 is provided with symmetrically distributed rotating seats 7, the rotating seats 7 are provided with damping shafts 8, the supporting legs 6 are rotationally connected with the rotating seats 7 through the damping shafts 8, the rotating seats 7 are provided with limiting plates 9, the supporting legs 6 can be rotated and attached to the limiting plates 9, the damping can make the supporting legs 6 have stability, and the supporting legs 6 can be kept stable after rotation, thereby better supporting.
[0024] In the embodiment, as Figure 1 and Figure 2 shown, the first storage box cover 1 and the second storage box cover 2 are provided with attachable handles 5, the first storage box cover 1 and the second storage box cover 2 are provided with adaptive lock buckles 4, the lock buckles 4 are similar to the buckling components on the existing common suitcase, and the buckling fixation can facilitate hand carrying.
[0025] In the embodiment, as Figure 3 and Figure 4 shown, the buffer mechanism comprises vertical columns 12 arranged in the first storage box cover 1 and the second storage box cover 2, the plurality of vertical columns 12 are symmetrically distributed, supporting plates 3 are sleeved on the vertical columns 12, buffer springs 14 are annularly sleeved outside the vertical columns 12, the buffer springs 14 are located at the bottom of the supporting plates 3, the buffer characteristics of the buffer springs 14 can play a protection role, reduce the jolt force generated by the unmanned aerial vehicle falling to contact the supporting plates 3, and further make the unmanned aerial vehicle stably recover.
[0026] In the embodiment, asFigure 3 and Figure 4 As shown in the figure, the top surface of the column 12 is provided with a threaded hole 13, the support plate 3 is provided with a mounting hole 11 matched with the column 12, a hand screw bolt 10 is connected in the threaded hole 13 and is pressed on the support plate 3, the hand screw bolt 10 can be screwed and disassembled, the support plate 3 and the buffer spring 14 can be removed, damaged parts can be replaced after long-term use, and practicality is improved.
[0027] The implementation principle of the embodiment of the rotor unmanned aerial vehicle recovery platform for building construction measurement is as follows: in use, the lock buckle 4 is opened, and the first storage box cover 1 and the second storage box cover 2 are opened to be horizontally aligned, then the first storage box cover 1 and the second storage box cover 2 are placed on the ground through the support legs 6, and the unmanned aerial vehicle falls on the support plate 3, so that the unmanned aerial vehicle can be recovered, and use is facilitated.
[0028] In the description of the utility model, it needs to be explained that the orientation or position relationship indicated by the terms "center", "upper", "lower", "left", "right", "vertical", "horizontal", "inner", "outer" and the like is based on the orientation or position relationship shown in the drawings, or is the orientation or position relationship commonly placed when the utility model product is used, and is only for the convenience of describing the utility model and simplifying the description, and therefore cannot be understood as indicating or implying that the indicated device or element must have a specific orientation, be constructed and operated in a specific orientation, and therefore cannot be understood as limiting the utility model. In addition, the terms "first", "second", "third" and the like are only used for differentiation in description and cannot be understood as indicating or implying relative importance.
[0029] In the description of the utility model, it also needs to be explained that, unless otherwise explicitly specified and limited, the terms "setting", "mounting", "connecting", "connecting" should be broadly understood, for example, it can be fixedly connected, or it can be detachably connected, or integrally connected; it can be mechanically connected, or it can be electrically connected; it can be directly connected, or it can be indirectly connected through an intermediate medium, or it can be connected inside two elements. For ordinary skilled persons in the art, the specific meaning of the above terms in the utility model can be understood according to the specific circumstances.
[0030] The above is only the preferred embodiment of the utility model, and is not used to limit the utility model. For those skilled in the art, the utility model can have various changes and variations. Any modification, equivalent replacement, improvement and the like made within the spirit and principle of the utility model shall be included in the protection scope of the utility model.
Claims
1. A rotary-wing unmanned aerial vehicle recovery platform for construction surveying, comprising a first storage box cover (1) and a second storage box cover (2), characterized in that: The first storage box cover (1) and the second storage box cover (2) are rotationally connected, and the first storage box cover (1) and the second storage box cover (2) can be rotated to a flush state. Supporting legs (6) are symmetrically arranged at the bottom of the first storage box cover (1) and the second storage box cover (2). It also includes a buffer mechanism. The buffer mechanism is installed in the first storage box cover (1) and the second storage box cover (2) for buffering and preventing collision.
2. The rotary-wing UAV recovery platform for construction surveying according to claim 1, characterized in that: Rotating seats (7) are symmetrically arranged at the bottom of the first storage box cover (1) and the second storage box cover (2), damping rotating shafts (8) are arranged on the rotating seats (7), and the supporting legs (6) are rotationally connected with the rotating seats (7) through the damping rotating shafts (8).
3. The rotary-wing UAV recovery platform for construction surveying according to claim 2, characterized in that: Limiting plates (9) are arranged on the rotating seats (7), and the supporting legs (6) can be rotationally attached to the limiting plates (9).
4. The rotary wing drone recovery platform for construction surveying of claim 1, wherein: A handle (5) is arranged on the first storage box cover (1) and the second storage box cover (2) and can be attached thereto.
5. The rotary wing drone recovery platform for construction surveying of claim 1, wherein: Locks (4) are arranged on the first storage box cover (1) and the second storage box cover (2) and are adapted thereto.
6. The rotary wing drone recovery platform for construction surveying of claim 1, wherein: The buffer mechanism includes a plurality of columns (12) arranged in the first storage box cover (1) and the second storage box cover (2), the columns (12) are symmetrically arranged, a supporting plate (3) is sleeved on the columns (12), a buffer spring (14) is annularly arranged outside the columns (12), and the buffer spring (14) is located at the bottom of the supporting plate (3).
7. The rotary-wing UAV recovery platform for construction surveying according to claim 6, characterized in that: Screw holes (13) are formed in the top surface of the column (12), mounting holes (11) adapted to the column (12) are formed in the supporting plate (3), hand screws (10) are connected in the screw holes (13), and the hand screws (10) are pressed on the supporting plate (3).