Double-shaft linkage unmanned aerial vehicle laser anti-shake holder and unmanned aerial vehicle

Abstract

The utility model provides a double-shaft linkage unmanned aerial vehicle laser anti-shake holder and an unmanned aerial vehicle, and the laser anti-shake holder comprises a fixed plate and a laser emitter. A longitudinal driver, a driving rod connected to the longitudinal driver, a mounting seat rotatably connected to the upper end of the driving rod, a transverse driver arranged on the driving rod, a winding roller connected to the transverse driver, and a driving rope wound on the winding roller are arranged on the fixed plate; two ends of the driving rope are respectively connected to two opposite ends of the mounting seat; and the laser transmitter is arranged on the mounting seat. The driving rod is driven through the longitudinal drive, the mounting base is driven to rotate, the longitudinal angle of the laser transmitter is adjusted, the winding roller is driven through the transverse drive, the posture of the mounting base is changed through winding and unwinding of the driving rope, and the transverse angle of the laser transmitter is adjusted. The effect of accurately and flexibly adjusting the angle of the laser transmitter is achieved, the laser transmitter can quickly and accurately aim at targets in different directions, and the precision and efficiency of laser operation of the unmanned aerial vehicle are improved.

Description

TECHNICAL FIELD

[0001] The utility model relates to unmanned aerial vehicle laser holder technology field, specifically, it relates to a double -shaft linkage's unmanned aerial vehicle laser anti -shake holder and unmanned aerial vehicle. BACKGROUND

[0002] The unmanned aerial vehicle laser anti -shake holder is installed on the unmanned aerial vehicle, is used for stabilizing laser emission device and the component of accurate control its angle. The existing unmanned aerial vehicle adopts single -shaft anti -shake design, sets up shock absorber or stabilizing device in a certain axial direction, to avoid the shaking of laser emitter in this axial direction too violent, can reduce the influence of this axial vibration on laser emission to a certain extent.

[0003] But when the unmanned aerial vehicle flies in complex environment, meets the air flow instability or unmanned aerial vehicle posture frequently changes, in addition to the direction controlled by single -shaft, laser emitter still can be influenced by big vibration in other directions, the component of single -shaft anti -shake device is only adjusted to single -shaft vibration, when other axial vibration appears, lack corresponding response mechanism, this leads to laser emitter under the action of multidirectional vibration, cannot stably point to target, seriously influence the precision of laser emission, when carrying out high -precision laser surveying or scanning task, the decline of such precision can make the data deviation that obtains, reduce the quality of task execution, in laser communication, also can lead to signal transmission instability, influence communication effect. SUMMARY

[0004] Therefore, the utility model discloses a double -shaft linkage's unmanned aerial vehicle laser anti -shake holder and unmanned aerial vehicle to solve the above -mentioned problems.

[0005] The utility model discloses the following scheme:

[0006] The application provides a double -shaft linkage's unmanned aerial vehicle laser anti -shake holder, including fixed plate and laser emitter, be provided with longitudinal drive on the fixed plate, be connected to the drive rod of longitudinal drive, rotatablely be connected to the mounting seat of drive rod upper end, set up on the drive rod transverse drive, be connected to the winding roller of transverse drive, drive rope is wound on the winding roller.

[0007] The longitudinal drive is used for driving the laser emitter to rotate longitudinally along the axis of the drive rod, and the transverse drive drives the laser emitter to flip transversely through the drive rope.

[0008] Further, the upper end of the driving rod is formed with a Y-shaped branch arm; the mounting seat is rotatably connected between the two branch arms; the driving rod is provided with a notch; the winding roller is arranged on the notch; and the driving rope is wound on the winding roller arranged in the notch.

[0009] Further, a first damping plug arranged on the branch arm is further included for adjusting the pre-tightening force of the rotation of the mounting seat.

[0010] Further, the bottom of the mounting seat is provided with a lifting ring at each end; and the two ends of the driving rope are connected to the lifting rings.

[0011] Further, a limiting cylinder arranged on the fixing plate is further included; and the driving rod is rotatably connected to the limiting cylinder.

[0012] Further, a second damping plug arranged on the limiting cylinder is further included for adjusting the pre-tightening force of the rotation of the driving rod.

[0013] Further, a mounting plate connected to the corresponding position of the unmanned aerial vehicle is further included; and the fixing plate is mounted on the mounting plate through a plurality of damping assemblies.

[0014] Further, the damping assembly includes a damping sleeve connected to the mounting plate and a compression rod connected to the fixing plate; the compression rod is slidably arranged in the damping sleeve; and an elastic member is arranged between the bottom of the compression rod and the inner bottom of the damping sleeve.

[0015] An unmanned aerial vehicle includes a machine laser anti-shake holder, which is a double-shaft linkage unmanned aerial vehicle laser anti-shake holder and is mounted on the corresponding position of the unmanned aerial vehicle through the mounting plate.

[0016] By adopting the above technical scheme, the following technical effects can be achieved.

[0017] 1. The driving rod is driven through longitudinal driving to drive the mounting seat to rotate, thereby realizing longitudinal angle adjustment of the laser emitter; and the winding roller is driven through transverse driving to change the posture of the mounting seat by winding and unwinding the driving rope, thereby adjusting the transverse angle of the laser emitter; the effects of accurately and flexibly adjusting the angle of the laser emitter are achieved, the laser emitter can quickly and accurately aim at different target directions, and the precision and efficiency of the laser operation of the unmanned aerial vehicle are greatly improved.

[0018] 2. The mounting plate and the damping assembly are arranged, thereby realizing the effects of stably mounting the holder and effectively damping; and the mounting plate is firmly connected to the unmanned aerial vehicle, thereby reducing the influence of the flight vibration of the unmanned aerial vehicle on the holder assembly. BRIEF DESCRIPTION OF DRAWINGS

[0019] In order to more clearly illustrate the technical scheme of the embodiments of the present application, the drawings needed in the embodiments will be briefly introduced as follows. It should be understood that the following drawings only show some embodiments of the present application, and therefore should not be considered as limiting the scope. For those skilled in the art, other related drawings can also be obtained from these drawings without creative labor.

[0020] Figure 1 is a three-dimensional structure schematic diagram of a double-shaft linkage unmanned aerial vehicle laser anti-shake holder according to an embodiment of the present application;

[0021] Figure 2 is an exploded structure schematic diagram of a first damping plug in a double-shaft linkage unmanned aerial vehicle laser anti-shake holder according to an embodiment of the present application;

[0022] Figure 3 is an exploded structure schematic diagram of a second damping plug in a double-shaft linkage unmanned aerial vehicle laser anti-shake holder according to an embodiment of the present application;

[0023] Figure 4 is an exploded structure schematic diagram of a mounting plate part of a double-shaft linkage unmanned aerial vehicle laser anti-shake holder according to an embodiment of the present application;

[0024] Figure 5 is a cross-sectional structure schematic diagram of a vibration reduction assembly of a double-shaft linkage unmanned aerial vehicle laser anti-shake holder according to an embodiment of the present application;

[0025] Figure: fixed plate 1, vibration reduction assembly 2, limiting cylinder 3, longitudinal drive 4, drive rod 5, support arm 6, mounting seat 7, laser emitter 8, transverse drive 9, winding roller 10, lifting ring 11, drive rope 12, second damping plug 13, first damping plug 14, slot 15, cross slot 16, fixed bolt one 201, compression rod 202, damping sleeve 203, elastic member 204, fixed bolt two 205, mounting plate 206, tapered slot 207, mounting screw 208. DETAILED DESCRIPTION

[0026] In order to make the purpose, technical scheme and advantages of the embodiments of the present application clearer, the technical scheme of the embodiments of the present application will be described clearly and completely below in conjunction with the drawings of the embodiments of the present application. Obviously, the described embodiments are some but not all of the embodiments of the present application. Based on the embodiments of the present application, all other embodiments obtained by those of ordinary skill in the art without creative work fall within the scope of protection of the present application. Therefore, the following detailed description of the embodiments of the present application provided in the drawings is not intended to limit the scope of the claimed present application, but only represents selected embodiments of the present application. Based on the embodiments of the present application, all other embodiments obtained by those of ordinary skill in the art without creative work fall within the scope of protection of the present application.

[0027] Embodiment

[0028] In conjunction with Figures 1 to 5 The embodiment provides a double-shaft linkage unmanned aerial vehicle laser anti-shake holder, which comprises a fixed plate 1 and a laser emitter 8, the fixed plate 1 is provided with a longitudinal drive 4, a drive rod 5 connected to the longitudinal drive 4, a mounting seat 7 rotatably connected to the upper end of the drive rod 5, a transverse drive 9 arranged on the drive rod 5, a winding roller 10 connected to the transverse drive 9, and a drive rope 12 wound on the winding roller 10; the two ends of the drive rope 12 are respectively connected to the opposite two ends of the mounting seat 7; the laser emitter 8 is arranged on the mounting seat 7.

[0029] The longitudinal drive 4 is used for driving the laser emitter 8 to rotate longitudinally along the axis of the drive rod 5; the transverse drive 9 drives the laser emitter 8 to overturn transversely through the drive rope 12.

[0030] The drive rod 5 is driven by the longitudinal drive 4, the mounting seat 7 is driven to rotate, the laser emitter 8 is longitudinally adjusted, the winding roller 10 is driven by the transverse drive 9, the posture of the mounting seat 7 is changed by winding and unwinding the drive rope 12, and the transverse angle of the laser emitter 8 is adjusted; the effect of accurately and flexibly adjusting the angle of the laser emitter 8 is realized, the laser emitter 8 can quickly and accurately aim at different direction targets, and the precision and efficiency of the laser operation of the unmanned aerial vehicle are greatly improved.

[0031] Specifically, in the embodiment, as Figure 1 and Figure 2As shown, the longitudinal drive 4 and the transverse drive 9 both adopt motors. The fixed plate 1 is provided with a limiting cylinder 3. The bottom of the fixed plate 1 is fixedly provided with the longitudinal drive 4, the output end of which is connected with the driving rod 5, and the driving rod 5 is rotatably connected to the limiting cylinder 3, thereby ensuring the stability of the driving rod 5 in the rotating process, so that it can only rotate around its own axis inside the limiting cylinder 3.

[0032] In the embodiment, the upper end of the driving rod 5 is formed with a Y-shaped branch arm 6, the mounting seat 7 is rotatably connected between the two branch arms 6, and a notch is arranged at the upper end of the driving rod 5. The transverse drive 9 is fixedly arranged on the side of one of the branch arms 6, the winding roller 10 is connected to the output end of the transverse drive 9 and passes through the branch arm 6 and is arranged on the notch, and the driving rope 12 is wound on the winding roller 10 arranged in the notch. The notch can limit the driving rope 12. The bottom of the mounting seat 7 is provided with a lifting ring 11 at each end, and the two ends of the driving rope 12 are connected to the lifting rings 11 respectively.

[0033] When the longitudinal angle of the laser emitter 8 needs to be adjusted, the longitudinal drive 4 starts to work, the power output by the longitudinal drive 4 drives the driving rod 5 to rotate inside the limiting cylinder 3, thereby driving the branch arm 6 to rotate around the longitudinal axis, further driving the mounting seat 7 to change the longitudinal angle, so as to realize the adjustment of the longitudinal angle of the laser emitter 8 and meet the needs of longitudinal scanning or irradiation of the target in different task scenarios.

[0034] When the transverse angle of the laser emitter 8 needs to be adjusted, since the output end of the transverse drive 9 is fixedly connected with the winding roller 10, the winding roller 10 starts to rotate after the transverse drive 9 is started, thereby winding or unwinding the driving rope 12. When the winding roller 10 rotates clockwise, the right side of the driving rope 12 is wound, so that the left side of the mounting seat 7 is pulled up, the mounting seat 7 rotates transversely around the rotating shaft, thereby driving the laser emitter 8 to be lifted to the left side, so as to realize the adjustment of the transverse angle. Conversely, when the winding roller 10 rotates the driving rope 12 counterclockwise, the left side of the mounting seat 7 descends, and the laser emitter 8 is lifted to the right side.

[0035] The longitudinal drive 4 and the transverse drive 9 drive the driving rod 5 and the winding roller 10 respectively, so that the laser emitter 8 can be flexibly adjusted in the longitudinal and transverse directions. Meanwhile, the limiting cylinder 3, the branch arm 6, the mounting seat 7, the lifting ring 11 and the driving rope 12 cooperate with each other to ensure the stability of the laser emitter 8 in the rotating process, so as to meet the needs of accurate laser emission of the target in different directions during the flight of the unmanned aerial vehicle.

[0036] In the embodiment, as shown in Figure 2 and Figure 3 The first damping plug 14 is arranged on the support arm 6, and the mounting rotating shaft is screwed on the support arm 6; one end abuts against the rotating shaft of the mounting seat 7, and the other end is provided with a slot 15, which is convenient for adjusting by a screwdriver. By adjusting the close degree of one end of the first damping plug 14 to the rotating shaft of the mounting seat 7, the pre-tightening force adjustment of the rotation of the mounting seat 7 is realized, and then the stability, accuracy and flexibility of the mounting seat 7 driven by the transverse drive 9 are adjusted. The side wall of the limiting cylinder 3 is also provided with a second damping plug 13 screwed thereon, one end of which abuts against the side wall of the drive rod 5, and the other end is also provided with a slot 15 or a cross slot 16. By adjusting the close degree of one end of the second damping plug 13 to the drive rod 5, the pre-tightening force adjustment of the rotation of the drive rod 5 is realized, and then the stability, accuracy and flexibility of the drive rod 5 driven by the longitudinal drive 4 are adjusted.

[0037] In the embodiment, as shown in Figure 1 and Figure 4 The mounting plate 206 is used for connecting to the corresponding position of the unmanned aerial vehicle, and the fixing plate 1 is mounted on the mounting plate 206 through a plurality of damping assemblies. The mounting plate 206 is connected with the unmanned aerial vehicle through a plurality of mounting screws 208, the mounting screws 208 respectively penetrate the tapered grooves 207 opened at the four corners of the top of the mounting plate 206, the tapered design of the top of the mounting screw 208 matches the internal size of the tapered groove 207, and when the mounting screw 208 is tightened, the tapered part of the top of the screw gradually embeds into the tapered groove 207, so that the connection between the mounting plate 206 and the unmanned aerial vehicle is more closely, and the stability of the mounting plate 206 on the unmanned aerial vehicle is ensured. The top of the mounting screw 208 is provided with a cross slot 16, and the inside is provided with an anti-skid design. When the mounting screw 208 is installed or disassembled, the cross slot 16 is matched with a cross screwdriver, and the anti-skid design can ensure that the screwdriver stably exerts force in the cross slot 16, so as to avoid the screwdriver head from slipping when rotating the mounting screw 208.

[0038] In the embodiment, as shown in Figure 4 and Figure 5As shown, the damping assembly includes a damping sleeve 203 connected to the mounting plate 206, a compression rod 202 connected to the fixed plate 1; the compression rod 202 is slidably arranged in the damping sleeve 203, and an elastic member 204 is arranged between the bottom of the compression rod 202 and the inner bottom of the damping sleeve 203. Specifically, a plurality of fixing bolts one 201 respectively penetrate the four corners of the top of the fixed plate 1, preliminarily positioning the fixed plate 1 above the mounting plate 206, the fixing bolts one 201 are threadedly connected to the compression rod 202, the other end of the compression rod 202 is slidably connected in the damping sleeve 203, the damping sleeve 203 is internally provided with the elastic member 204, and the elastic member 204 is a spring; when the compression rod 202 moves up and down in the damping sleeve 203, the spring generates a corresponding elastic force; when the compression rod 202 moves downward, the spring is compressed to generate an upward elastic force; when the compression rod 202 moves upward, the spring is stretched to generate a downward elastic force, which can play a role in buffering and damping, reducing the influence of the vibration generated during the flight of the unmanned aerial vehicle on the fixed plate 1 and the entire gimbal assembly, and a plurality of the damping sleeves 203 are threadedly connected with fixing bolts two 205 at the bottom, the fixing bolts two 205 respectively penetrate the four corners of the bottom of the mounting plate 206 and are threadedly connected to the bottom of the damping sleeve 203, by tightening the fixing bolts two 205, the damping sleeve 203 and the mounting plate 206 can be firmly connected together, after installation, when the unmanned aerial vehicle flies and generates vibration, the vibration is transmitted to the mounting plate 206, the vibration of the mounting plate 206 is transmitted to the damping sleeve 203 through the fixing bolts two 205, the spring in the damping sleeve 203 absorbs part of the vibration energy, at the same time, the sliding connection between the damping sleeve 203 and the compression rod 202 can also consume part of the vibration energy, the compression rod 202 transmits the buffered vibration to the fixed plate 1, greatly reducing the vibration amplitude transmitted to the fixed plate 1, thereby ensuring the stability of the laser stabilization gimbal assembly, ensuring that the laser emitter 8 can work stably, and improving the precision of laser emission.

[0039] The utility model also provides a kind of unmanned plane, including machine laser anti-shake holder, the machine laser anti-shake holder is the double-shaft linkage's unmanned plane laser anti-shake holder, it is installed on the corresponding position of the unmanned plane by the mounting plate 206.It is realized that the unmanned plane laser anti-shake holder of double-shaft linkage is set, realizes the effect that unmanned plane accurately flexible adjustment laser emitter 8 angle, can let laser emitter 8 quickly, accurately aim at different direction target, greatly improves the precision and efficiency of unmanned plane laser operation.

[0040] The above is only the preferred embodiment of the utility model, and the protection scope of the utility model is not limited to the above-mentioned examples, and any technical solution falling within the concept of the utility model belongs to the protection scope of the utility model.

[0041] In the description of the utility model, it should be understood that the orientation or positional relationship indicated by the terms "center", "longitudinal", "lateral", "length", "width", "thickness", "upper", "lower", "front", "rear", "left", "right", "vertical", "horizontal", "top", "bottom", "inner", "outer", "clockwise", "counterclockwise" and the like is based on the orientation or positional relationship shown in the drawings, and is only for the convenience of describing the utility model and simplifying the description, and does not indicate or imply that the devices or elements referred to must have a particular orientation, be constructed and operated in a particular orientation, and therefore cannot be understood as a limitation on the utility model.

[0042] In addition, the terms "first" and "second" are only for descriptive purposes, and cannot be understood as indicating or implying relative importance or implicitly indicating the number of the indicated technical features. Therefore, the features defined as "first" and "second" can explicitly or implicitly include one or more of the features. In the description of the utility model, the meaning of "multiple" is two or more, unless otherwise specifically limited.

[0043] In the utility model, unless otherwise specifically defined and limited, the terms "mounting", "connection", "connection", "fixing" and the like should be broadly understood, for example, it can be fixedly connected, or it can be detachably connected, or it can be integrated; 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; it can be the communication or interaction relationship between two elements. For ordinary skilled in the art, the specific meaning of the above terms in the utility model can be understood according to the specific circumstances.

[0044] In the utility model, unless another definite provision and limitation, first feature is "on" or "under" second feature can include that first and second features are in direct contact, also can include that first and second features are not in direct contact but are in contact through other features between them. Moreover, first feature "on", "above" and "upper side" of second feature includes that first feature is directly above and obliquely above second feature, or only indicates that horizontal height of first feature is higher than second feature. First feature "under", "below" and "lower side" of second feature includes that first feature is directly below and obliquely below second feature, or only indicates that horizontal height of first feature is less than second feature.

Claims

1. A dual-axis linkage unmanned aerial vehicle laser anti-shake holder, comprising a fixed plate and a laser emitter, characterized in that, The fixed plate is provided with a longitudinal drive, a drive rod connected to the longitudinal drive, a mounting seat rotatably connected to the upper end of the drive rod, a transverse drive provided on the drive rod, a winding roller connected to the transverse drive, and a drive rope wound on the winding roller; the two ends of the drive rope are respectively connected to the opposite ends of the mounting seat; the laser emitter is arranged on the mounting seat; The longitudinal drive is used to drive the laser emitter to rotate longitudinally along the axis of the drive rod; the transverse drive drives the laser emitter to flip transversely through the drive rope.

2. The dual-axis gimbalized drone laser stabilization gimbal of claim 1, wherein, The upper end of the drive rod is formed with a Y-shaped branch; the mounting seat is rotatably connected between the two branches; the upper end of the drive rod is provided with a notch; the winding roller is arranged in the notch; the drive rope is wound on the winding roller arranged in the notch.

3. The dual-axis gimbalized drone laser stabilization gimbal of claim 2, wherein, A first damping plug arranged on the branch is further included for adjusting the pre-tightening force of the rotation of the mounting seat.

4. The dual-axis gimbalized drone laser stabilization gimbal of claim 1, wherein, The bottom ends of the mounting seat are respectively provided with lifting rings; the two ends of the drive rope are respectively connected to the lifting rings.

5. The dual-axis gimbal system of claim 1, wherein, A limiting cylinder arranged on the fixed plate is further included; the drive rod is rotatably connected to the limiting cylinder.

6. The dual-axis gimbal of claim 5, wherein, A second damping plug arranged on the limiting cylinder is further included for adjusting the pre-tightening force of the rotation of the drive rod.

7. The dual-axis gimbal of any one of claims 1-6, wherein the first and second axes are perpendicular to each other. An installation plate for being connected to the corresponding position of the unmanned aerial vehicle is further included; the fixed plate is mounted on the installation plate through a plurality of damping assemblies.

8. The dual-axis gimbal system of claim 7, wherein the first and second motors are configured to rotate the first and second motorized gimbals about the first and second axes, respectively, in response to a first and second motor control signal, respectively. The damping assembly includes a damping sleeve connected to the installation plate and a compression rod connected to the fixed plate; the compression rod is slidably arranged in the damping sleeve, and an elastic member is arranged between the bottom of the compression rod and the inner bottom of the damping sleeve.

9. A drone comprising an organic laser stabilization gimbal, characterized in that, The machine laser anti-shake holder is a dual-axis linkage unmanned aerial vehicle laser anti-shake holder as claimed in claim 7 or 8, which is mounted on the corresponding position of the unmanned aerial vehicle through the installation plate.

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