CN211086588U - Unmanned aerial vehicle location is with machine-mounted laser radar - Google Patents
Unmanned aerial vehicle location is with machine-mounted laser radar Download PDFInfo
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- CN211086588U CN211086588U CN201921441053.1U CN201921441053U CN211086588U CN 211086588 U CN211086588 U CN 211086588U CN 201921441053 U CN201921441053 U CN 201921441053U CN 211086588 U CN211086588 U CN 211086588U
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Abstract
The utility model discloses an unmanned aerial vehicle location is with machine-carried laser radar, which comprises an outer shell, shell one side surface is provided with the laser instrument, and the lower extreme outer fixed surface of shell is connected with the mounting panel, the lower extreme outer surface of mounting panel has the protection pad to glue, and the inside of mounting panel has seted up the slotted hole, the inside swing joint of slotted hole has the screw rod, the quantity of slotted hole is two, the inside of shell is provided with the detector, the surface swing joint of shell has second go-between and first go-between, and the second go-between is located the top of first go-between, fixedly connected with connecting rod between first go-between and the second go-between. The utility model discloses, can adjust laser radar's position to can avoid the shell to cause the damage at the in-process of collision, can prolong the life of shell, the person of facilitating the use adjusts the angle of shell, the person of facilitating the use's operation, and is comparatively practical.
Description
Technical Field
The utility model relates to an airborne laser radar technical field specifically is an unmanned aerial vehicle location is with airborne laser radar.
Background
The laser radar is an active modern optical remote sensing technology, is a product of combining a traditional radar technology and a modern laser technology, and has the characteristics of high brightness, high directivity, high coherence and high peak power, so the laser radar has the advantages of high angular resolution, high distance resolution, high time resolution, high measurement precision, long detection distance, multi-target detection and strong anti-interference.
Compare chinese patent CN201821795037.8 an airborne laser radar system based on unmanned aerial vehicle, wherein it is described: laser radar system includes shell body, passive optical module, laser light source, detector, data acquisition module, host system and temperature control module, and whole process does not consume laser radar and even whole unmanned aerial vehicle's battery completely, has solved the contradiction of the limited battery power supply of unmanned aerial vehicle and the strict control by temperature change of laser radar ingeniously.
Current airborne laser radar can not be better when installing laser radar on unmanned aerial vehicle adjust laser radar's position, and can't carry out better protection to laser radar in the use, practical inadequately.
Therefore, an airborne laser radar for positioning the unmanned aerial vehicle is provided.
SUMMERY OF THE UTILITY MODEL
An object of the utility model is to provide an unmanned aerial vehicle location is with machine carries laser radar can adjust laser radar's position to can avoid the shell to cause the damage at the in-process of collision, can prolong the life of shell, convenient to use person adjusts the angle of shell, convenient to use person's operation, and is comparatively practical, with the problem of proposing in solving above-mentioned background art.
In order to achieve the above object, the utility model provides a following technical scheme: the utility model provides an unmanned aerial vehicle location is with machine-carried laser radar, includes the shell, shell one side surface is provided with the laser instrument, and the lower extreme external surface fixedly connected with mounting panel of shell, the lower extreme outer surface veneer of mounting panel has the protection to fill up, and the inside of mounting panel has seted up the slotted hole, the inside swing joint of slotted hole has the screw rod, the quantity of slotted hole is two, the inside of shell is provided with the detector.
The screw rod can support the rotation of shell under the state of unscrewing, the mounting panel can be through slotted hole and screw rod swing joint, the slotted hole is the arc hole, and two slotted holes are concentric, consequently, can make the shell rotate, just can screw up the screw rod after confirming the position, convenient to use person adjusts the angle of shell, then the mounting panel just can fix, inevitable meeting collides with the foreign object at the in-process of unmanned aerial vehicle flight, the surface of shell has set up first go-between, connecting rod and second go-between, and it is the rubber material, at first go-between, can protect the shell under the effect of connecting rod and second go-between, can avoid the shell to cause the damage at the in-process of collision, can prolong the life of shell, convenient to use person's operation, and is comparatively practical.
Preferably, the outer surface of the housing is movably connected with a second connecting ring and a first connecting ring, and the second connecting ring is located above the first connecting ring.
The damage to the shell in the collision process can be avoided, and the service life of the shell can be prolonged.
Preferably, a connecting rod is fixedly connected between the first connecting ring and the second connecting ring, and the first connecting ring and the second connecting ring have the same size and specification.
The shell can be protected, and the effect is better.
Preferably, the connecting rod, the first connecting ring and the second connecting ring are all made of rubber.
The surface of shell has set up first go-between, connecting rod and second go-between, and it is the rubber material, can protect the shell under the effect of first go-between, connecting rod and second go-between.
Preferably, the slotted hole is arc-shaped, and the two slotted holes are concentric.
The mounting plate can be movably connected with the screw rod through the slotted holes, the slotted holes are arc-shaped holes, and the two slotted holes are concentric, so that the shell can rotate.
Preferably, a power interface is arranged on the outer surface of one side of the shell, and the output end of the power interface is electrically connected with the input ends of the laser and the detector.
Be connected through power source and external power source, can provide the power for laser instrument and detector, laser radar just can use.
Compared with the prior art, the beneficial effects of the utility model are that:
the utility model discloses, the screw rod can support the rotation of shell under the state of unscrewing, the mounting panel can be through slotted hole and screw rod swing joint, the slotted hole is the arc hole, and two slotted hole centre of a circle, consequently, can make the shell rotate, just can screw up the screw rod after confirming the position, convenient to use person adjusts the angle of shell, then the mounting panel just can fix, inevitable meeting collides with the foreign object at the in-process of unmanned aerial vehicle flight, the surface of shell has set up first go-between, connecting rod and second go-between, and it is the rubber material, at first go-between, can protect the shell under the effect of connecting rod and second go-between, can avoid the shell to cause the damage at the in-process of collision, can prolong the life of shell, convenient to use person's operation, and is comparatively practical.
Drawings
Fig. 1 is a schematic structural view of the present invention;
FIG. 2 is a combination view of the mounting plate and the slot of the present invention;
FIG. 3 is a view showing the combination of the screw and the slot of the present invention;
fig. 4 is a combination view of the first connecting ring and the connecting rod of the present invention.
In the figure: 1. a housing; 2. a laser; 3. mounting a plate; 4. a slot; 5. a screw; 6. a protective pad; 7. a first connecting ring; 8. a connecting rod; 9. a second connecting ring.
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 to 4, the present invention provides a technical solution: an airborne laser radar for positioning an unmanned aerial vehicle is shown in figure 1 and comprises a shell 1, wherein a laser 2 is arranged on the outer surface of one side of the shell 1, a mounting plate 3 is fixedly connected to the outer surface of the lower end of the shell 1, and a protective pad 6 is glued to the outer surface of the lower end of the mounting plate 3;
as shown in fig. 2 and 3, a slot 4 is formed in the mounting plate 3, a screw 5 is movably connected in the slot 4, the number of the slot 4 is two, and a detector is arranged in the housing 1.
By adopting the technical scheme, the screw 5 can support the rotation of the shell 1 in the unscrewing state, the mounting plate 3 can be movably connected with the screw 5 through the slotted hole 4, the slotted hole 4 is an arc-shaped hole, and the two slotted holes 4 are concentric, so that the shell 1 can rotate, after the position has been established, the screw 5 can be tightened, so that the mounting plate 3 can be fixed, the unmanned aerial vehicle inevitably collides with foreign objects in the flying process, the outer surface of the shell 1 is provided with a first connecting ring 7, a connecting rod 8 and a second connecting ring 9 which are all made of rubber materials, can protect shell 1 under the effect of first go-between 7, connecting rod 8 and second go-between 9, can avoid shell 1 to cause the damage at the in-process of collision, can prolong shell 1's life, convenient to use person's operation, it is comparatively practical.
Specifically, as shown in fig. 4, a second connection ring 9 and a first connection ring 7 are movably connected to the outer surface of the housing 1, and the second connection ring 9 is located above the first connection ring 7.
Through adopting above-mentioned technical scheme, can avoid shell 1 to cause the damage at the in-process of collision, can prolong shell 1's life.
Specifically, as shown in fig. 4, a connecting rod 8 is fixedly connected between the first connecting ring 7 and the second connecting ring 9, and the first connecting ring 7 and the second connecting ring 9 have the same size and specification.
Through adopting above-mentioned technical scheme, can protect shell 1, the effect is better.
Specifically, as shown in fig. 4, the connecting rod 8, the first connecting ring 7 and the second connecting ring 9 are made of rubber.
Through adopting above-mentioned technical scheme, the surface of shell 1 has set up first go-between 7, connecting rod 8 and second go-between 9, and it is the rubber material, can protect shell 1 under the effect of first go-between 7, connecting rod 8 and second go-between 9.
Specifically, as shown in fig. 2 and 3, the slot 4 is arc-shaped, and the two slot 4 are concentric.
Through adopting above-mentioned technical scheme, mounting panel 3 can be through slotted hole 4 and 5 swing joint of screw rod, and slotted hole 4 is the arc hole, and two slotted holes 4 centre of a circle, consequently can make shell 1 rotate.
Specifically, as shown in fig. 1, a power interface is disposed on an outer surface of one side of the housing 1, and an output end of the power interface is electrically connected to the laser 2 and an input end of the detector.
Through adopting above-mentioned technical scheme, be connected through power source and external power source, can provide the power for laser instrument 2 and detector, laser radar just can use.
The working principle is as follows: the user can install laser radar on unmanned aerial vehicle, it is fixed to be connected mounting panel 3 through screw rod 5 and unmanned aerial vehicle, when installing laser radar, the user can finely tune shell 1, screw rod 5 can support the rotation of shell 1 under the state of unscrewing, mounting panel 3 can be through slotted hole 4 and screw rod 5 swing joint, slotted hole 4 is the arc hole, and two slotted holes 4 are concentric, therefore can make shell 1 rotate, just can screw up screw rod 5 after confirming the position, so mounting panel 3 just can fix, later when using laser radar, be connected with external power source through power source interface, can provide the power for laser 2 and detector, laser radar just can use, inevitable meeting collides with the foreign object in the in-process of unmanned aerial vehicle flight, the surface of shell 1 has set up first connecting ring 7, Connecting rod 8 and second go-between 9, and it is the rubber material, can protect shell 1 under the effect of first go-between 7, connecting rod 8 and second go-between 9.
The using method comprises the following steps: firstly, a user can install the laser radar on the unmanned aerial vehicle, the mounting plate 3 can be protected through the protective pad 6, the mounting plate 3 is fixedly connected with the unmanned aerial vehicle through the screw rod 5, when the laser radar is installed, the user can finely adjust the shell 1, the screw rod 5 can support the rotation of the shell 1 in an unscrewing state, the mounting plate 3 can be movably connected with the screw rod 5 through the slotted hole 4, the slotted hole 4 is an arc-shaped hole, and the two slotted holes 4 are concentric, so that the shell 1 can rotate, the screw rod 5 can be screwed up after the position is determined, the user can conveniently adjust the angle of the shell 1, the mounting plate 3 can be fixed, when the laser radar is used, the laser radar is connected with an external power supply through a power interface, the laser 2 and a detector can be provided with power, and the laser radar can be used, unavoidable meeting collides with the foreign object at the in-process that unmanned aerial vehicle flies, the surface of shell 1 has set up first go-between 7, connecting rod 8 and second go-between 9, and it is the rubber material, can protect shell 1 under the effect of first go-between 7, connecting rod 8 and second go-between 9, can avoid shell 1 to cause the damage at the in-process of collision, can prolong shell 1's life, convenient to use person's operation, and is comparatively practical.
The above-mentioned laser 2 and detector and their use are the prior art disclosed and well known by those skilled in the art provided in the background, and those skilled in the art can achieve the corresponding use effect by providing this technical solution, so it is not described one by one.
The installation method comprises the following steps:
firstly, forming a slotted hole 4 in an installation plate 3, and connecting and fixing the slotted hole through a screw rod 5;
secondly, connecting the first connecting ring 7, the connecting rod 8 and the second connecting ring 9;
and thirdly, sleeving the first connecting ring 7, the connecting rod 8 and the second connecting ring 9 on the outer surface of the shell 1 to finish the installation.
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 (6)
1. The utility model provides an unmanned aerial vehicle location is with machine carries laser radar, includes shell (1), its characterized in that: the utility model discloses a laser instrument, including shell (1), mounting panel (3), slotted hole (4), the inside swing joint of slotted hole (4) has screw rod (5), the quantity of slotted hole (4) is two, the inside of shell (1) is provided with the detector, and the lower extreme outer fixed surface of shell (1) is connected with mounting panel (3), the lower extreme outer surface veneer of mounting panel (3) has protection pad (6), and mounting panel (3) has seted up slotted hole (4), the inside swing joint of slotted hole (4).
2. The airborne lidar of claim 1, wherein: the outer surface of the shell (1) is movably connected with a second connecting ring (9) and a first connecting ring (7), and the second connecting ring (9) is positioned above the first connecting ring (7).
3. The airborne lidar of claim 2, wherein: a connecting rod (8) is fixedly connected between the first connecting ring (7) and the second connecting ring (9), and the first connecting ring (7) and the second connecting ring (9) are identical in size and specification.
4. The airborne lidar of claim 3, wherein the airborne lidar further comprises: the connecting rod (8), the first connecting ring (7) and the second connecting ring (9) are all made of rubber materials.
5. The airborne lidar of claim 1, wherein: the slotted holes (4) are arc-shaped, and the two slotted holes (4) are concentric.
6. The airborne lidar of claim 1, wherein: the outer surface of one side of shell (1) is provided with power source, and power source's output electric connection laser instrument (2) and the input of detector.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201921441053.1U CN211086588U (en) | 2019-09-02 | 2019-09-02 | Unmanned aerial vehicle location is with machine-mounted laser radar |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201921441053.1U CN211086588U (en) | 2019-09-02 | 2019-09-02 | Unmanned aerial vehicle location is with machine-mounted laser radar |
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| Publication Number | Publication Date |
|---|---|
| CN211086588U true CN211086588U (en) | 2020-07-24 |
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| Application Number | Title | Priority Date | Filing Date |
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| CN201921441053.1U Active CN211086588U (en) | 2019-09-02 | 2019-09-02 | Unmanned aerial vehicle location is with machine-mounted laser radar |
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Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN115902828A (en) * | 2022-11-08 | 2023-04-04 | 武汉新烽光电股份有限公司 | Combined laser radar device with strong anti-interference performance |
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2019
- 2019-09-02 CN CN201921441053.1U patent/CN211086588U/en active Active
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN115902828A (en) * | 2022-11-08 | 2023-04-04 | 武汉新烽光电股份有限公司 | Combined laser radar device with strong anti-interference performance |
| CN115902828B (en) * | 2022-11-08 | 2024-06-14 | 武汉新烽光电股份有限公司 | Combined laser radar device with high anti-interference performance |
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