CN114590415A - A connection structure, unmanned aerial vehicle and laser radar system for unmanned aerial vehicle - Google Patents
A connection structure, unmanned aerial vehicle and laser radar system for unmanned aerial vehicle Download PDFInfo
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- CN114590415A CN114590415A CN202011399213.8A CN202011399213A CN114590415A CN 114590415 A CN114590415 A CN 114590415A CN 202011399213 A CN202011399213 A CN 202011399213A CN 114590415 A CN114590415 A CN 114590415A
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- 238000001179 sorption measurement Methods 0.000 claims abstract description 21
- 238000013016 damping Methods 0.000 claims description 16
- 238000010521 absorption reaction Methods 0.000 claims description 9
- 230000007246 mechanism Effects 0.000 claims description 9
- 238000000034 method Methods 0.000 abstract description 13
- 230000008569 process Effects 0.000 abstract description 11
- 238000011900 installation process Methods 0.000 abstract description 3
- SZVJSHCCFOBDDC-UHFFFAOYSA-N iron(II,III) oxide Inorganic materials O=[Fe]O[Fe]O[Fe]=O SZVJSHCCFOBDDC-UHFFFAOYSA-N 0.000 description 11
- 238000010586 diagram Methods 0.000 description 6
- 230000000694 effects Effects 0.000 description 2
- 238000009434 installation Methods 0.000 description 2
- 230000004308 accommodation Effects 0.000 description 1
- 230000004888 barrier function Effects 0.000 description 1
- 230000009286 beneficial effect Effects 0.000 description 1
- 230000008859 change Effects 0.000 description 1
- 230000008878 coupling Effects 0.000 description 1
- 238000010168 coupling process Methods 0.000 description 1
- 238000005859 coupling reaction Methods 0.000 description 1
- 238000005516 engineering process Methods 0.000 description 1
- 230000010354 integration Effects 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
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- 238000012827 research and development Methods 0.000 description 1
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D47/00—Equipment not otherwise provided for
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D47/00—Equipment not otherwise provided for
- B64D47/08—Arrangements of cameras
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Abstract
The invention discloses a connecting structure for an unmanned aerial vehicle, the unmanned aerial vehicle and a laser radar system, which comprise: the connecting bracket comprises a power supply bracket and a side fixing bracket; the two side fixing brackets are oppositely arranged, and the power supply bracket and the side fixing brackets jointly form a space for accommodating the carrying equipment; the power supply support and the side fixing support are respectively provided with a first adsorption part, and the first adsorption part is in adsorption fit with a second adsorption part arranged at a corresponding position on the carrying equipment, so that the carrying equipment is fixed. According to the laser radar device, the first fixed magnet and the second fixed magnet are mutually adsorbed and fixed, and the first power supply magnet and the second power supply magnet are mutually adsorbed and fixed, so that the laser radar device can be directly installed and removed from the connecting bracket when in use, and the technical problem that the laser radar device in the prior art is complicated in installation process and inconvenient to detach in the process of being installed on the unmanned aerial vehicle is solved.
Description
Technical Field
The invention relates to the technical field of unmanned aerial vehicle equipment, in particular to a connecting structure for an unmanned aerial vehicle, the unmanned aerial vehicle and a laser radar system.
Background
The statements in this section merely provide background information related to the present disclosure and may not necessarily constitute prior art.
The unmanned plane is called unmanned plane for short, and is an unmanned aerial vehicle operated by radio remote control equipment and a self-contained program control device. Unmanned aerial vehicles are in fact a general term for unmanned aerial vehicles, and can be defined from a technical perspective as follows: unmanned fixed wing aircraft, unmanned VTOL aircraft, unmanned airship, unmanned helicopter, unmanned multi-rotor aircraft, unmanned paravane, etc. Compared with manned aircraft, it has the advantages of small volume, low cost, convenient use, low requirement on the operational environment, strong battlefield viability and the like. Since the unmanned aircraft has important significance for future air battles, the research and development work of the unmanned aircraft is carried out in all major military countries in the world.
In order to improve the performance and the effect of the unmanned aerial vehicle, loads such as a laser radar or a visible light infrared camera need to be connected to the unmanned aerial vehicle; the prior art generally makes the following:
(1) set relevant load and unmanned aerial vehicle to the form of integration, this kind of structural style can guarantee that loads such as laser radar can connect on unmanned aerial vehicle absolutely stably, but this kind of mode can't realize the change to loads such as laser radar, has limited unmanned aerial vehicle's effect to a certain extent.
(2) Arranging a mounting mechanism for loads such as a laser radar and the like, and fixing the mounting mechanism on the unmanned aerial vehicle; however, when the mounting mechanisms are used for mounting and dismounting loads such as laser radars, the operation process is very complicated, and if the mounting mechanisms are not fastened in the connection process, the loads such as the laser radars fall and are damaged in the operation process.
Disclosure of Invention
In view of this, the invention provides a connection structure for an unmanned aerial vehicle, the unmanned aerial vehicle and a laser radar system, wherein the mounting equipment and the unmanned aerial vehicle are fixed in an adsorption manner by the fixed magnets, so that the dismounting process is simplified, and the functionality and the operation convenience of the unmanned aerial vehicle are improved.
According to a first aspect of embodiments of the present invention, there is provided a connection structure for a drone, including: the connecting bracket comprises a power supply bracket and a side fixing bracket; the two side fixing brackets are oppositely arranged, and the power supply bracket and the side fixing brackets jointly form a space for accommodating the carrying equipment; the power supply support and the side fixing support are respectively provided with a first adsorption part, and the first adsorption part is in adsorption fit with a second adsorption part arranged at a corresponding position on the carrying equipment, so that the carrying equipment is fixed.
According to a second aspect of the embodiments of the present invention, there is provided an unmanned aerial vehicle, including: the unmanned aerial vehicle body and foretell linking bridge, this body coupling of linking bridge and unmanned aerial vehicle.
According to a third aspect of the embodiments of the present invention, there is provided a laser radar system of an unmanned aerial vehicle, including: the above-mentioned unmanned aerial vehicle; the laser radar equipment is carried on the connecting support; the laser radar equipment is provided with a second adsorption piece, and the setting position of the second adsorption piece corresponds to the setting position of the first adsorption piece on the connecting bracket; through the absorption cooperation of first absorption piece and second absorption piece, it is fixed with laser radar equipment and linking bridge.
Compared with the prior art, the invention has the beneficial effects that:
(1) the invention provides a double-adsorption type fixing technology of an unmanned aerial vehicle, develops a related system, and solves the technical problems that in the prior art, laser radar equipment is complex in installation process and inconvenient to detach in the process of being installed on the unmanned aerial vehicle.
(2) According to the laser radar device, the first fixed magnet and the second fixed magnet are mutually adsorbed and fixed, and the first power supply magnet and the second power supply magnet are mutually adsorbed and fixed, so that the laser radar device can be directly installed and removed from the connecting support when the laser radar device is used, and the technical problem that the laser radar device in the prior art is complicated in installation process and inconvenient to detach when the laser radar device is installed on an unmanned aerial vehicle is effectively solved.
(3) According to the invention, the limiting clamping block is arranged on the inner side arm of the side fixing support, and the laser radar equipment can transversely move into the side fixing support along the chamfer angle of the limiting clamping block to be contacted with the first fixing magnet and the first power supply magnet to form a fit, so that the fixing strength of the side fixing support to the laser radar equipment is increased, and the installation convenience of the equipment is also increased.
(4) According to the unmanned aerial vehicle body, the space for accommodating the carrying equipment is divided into at least two subspaces through the limiting clamping block, the first fixed magnet and the first power supply magnet are arranged in each subspace to fix the carrying equipment, so that the unmanned aerial vehicle body can carry different equipment (such as laser radar equipment and a camera) simultaneously according to flight requirements, and the practicability and convenience of the structure are improved.
Advantages of additional aspects of the invention will be set forth in part in the description which follows, and in part will be obvious from the description, or may be learned by practice of the invention.
Drawings
FIG. 1 is a schematic view of a first angle configuration of a connecting bracket according to an embodiment of the present invention;
FIG. 2 is a schematic view of a second angle of the connecting bracket according to the embodiment of the invention;
FIG. 3 is a schematic structural diagram of a mounting apparatus according to an embodiment of the present invention;
FIG. 4 is a schematic diagram of a mounting device and a power supply bracket according to an embodiment of the invention;
fig. 5 is a schematic structural diagram of a first angle of the unmanned aerial vehicle with the connecting structure according to the embodiment of the invention;
fig. 6 is a schematic structural diagram of a second angle of the unmanned aerial vehicle with the connecting structure according to the embodiment of the invention;
fig. 7 is a schematic structural diagram of a third angle of the unmanned aerial vehicle with the connecting structure according to the embodiment of the invention;
the unmanned aerial vehicle comprises an unmanned aerial vehicle body 1, a connecting support 2, a power supply support 21, a power supply socket 211, a first power supply magnet 212, a side fixing support 22, a first fixing magnet 221, a limiting clamping block 222, a carrying device 3, a second fixing magnet 31, a power supply plug 32, a second power supply magnet 33, a damping mechanism 4, a damping support 41, a damping gasket 42, a rotating motor 5 and a flying support 6.
Detailed Description
It should be noted that the following detailed description is exemplary and is intended to provide further explanation of the disclosure. Unless defined otherwise, all technical and scientific terms used herein have the same meaning as commonly understood by one of ordinary skill in the art to which this application belongs.
It is noted that the terminology used herein is for the purpose of describing particular embodiments only and is not intended to be limiting of example embodiments according to the present application. As used herein, the singular forms "a", "an", and "the" are intended to include the plural forms as well, unless the context clearly indicates otherwise, and it should be understood that the terms "comprises" and "comprising", and any variation thereof, are intended to cover a non-exclusive inclusion, such that a process, method, system, article, or apparatus that comprises a list of steps or elements is not necessarily limited to those steps or elements expressly listed, but may include other steps or elements not expressly listed or inherent to such process, method, article, or apparatus.
The embodiments and features of the embodiments of the present invention may be combined with each other without conflict.
Example one
According to an embodiment of the present invention, there is provided an embodiment of a connection structure for an unmanned aerial vehicle, including: the connecting bracket 2, the connecting bracket 2 includes the power supply bracket 21 and side fixed bolster 22; the two side fixing brackets 22 are oppositely arranged, and the power supply bracket 21 and the side fixing brackets 22 jointly form a space for accommodating the embarkation equipment 3; the power supply support 21 and the side fixing support 22 are respectively provided with a first suction part, and the first suction part is in suction fit with a second suction part arranged at a corresponding position on the carrying equipment 3, so that the carrying equipment 3 is fixed.
Specifically, referring to fig. 1 and 2, the connection bracket 2 includes two power supply brackets 21 and two side fixing brackets 22, where the two side fixing brackets 22 are symmetrically disposed, the upper ends of the power supply brackets 21 are connected to the two side fixing brackets 22, and the upper portions of the power supply brackets 21 are inclined outward to increase the accommodation space; the lower part is vertically arranged and is provided with a power supply socket 211;
a first fixed magnet 221 is arranged at the opposite position of the two side fixed brackets 22, and a ring of first power supply magnets 212 are also arranged at the periphery of the power supply socket 211;
referring to fig. 3, the two sides of the carrying device 3 are respectively provided with a second fixed magnet 31, meanwhile, the carrying device 3 is provided with a power supply plug 32 matched with the power supply socket 211, and the periphery of the power supply plug 32 is also provided with a circle of second power supply magnets 33;
the positions of the second fixed magnet 31 and the second power supply magnet 33 on the mounting device 3 correspond to the positions of the first fixed magnet 221 and the first power supply magnet 212 on the connecting bracket 2; the mounting device 3 can be fixed by the attraction and engagement of the first fixed magnet 221 and the second fixed magnet 31, and the power supply plug 32 can be smoothly inserted into the power supply socket 211 while the mounting device 3 is fixed by the attraction and engagement of the first power supply magnet 212 and the second power supply magnet 33.
The power supply plug 32 of the onboard apparatus 3 can obtain a power supply from the unmanned aerial vehicle body 1 by being inserted into the power supply socket 211.
As an optional implementation manner, data lines may be added to the power supply plug 32 and the power supply socket 211, so that the onboard device 3 and the unmanned aerial vehicle body 1 are connected to each other to realize information exchange.
Use carrying equipment 3 as the laser radar equipment for the example, refer to fig. 4, when needs install laser radar equipment on unmanned aerial vehicle, only need with two second power supply magnetite 33 on the laser radar equipment aim at the first power supply magnetite 212 that sets up on the power supply support 21, make power supply plug 32 insert in the power supply socket 211, then aim at the first fixed magnetite 221 on two lateral part fixed bolsters 22 with two fixed magnetite 31 of second on the laser radar equipment, through the absorption of magnetite, accomplish the fixed to laser radar equipment.
Needless to say, the mounting device 3 in the present embodiment is not limited to the laser radar device, and may be a load such as infrared light or visible light.
As an alternative embodiment, the limiting blocks 222 are respectively and oppositely arranged on the inner side walls of the two side fixing brackets 22, and the limiting blocks 222 can divide the space for accommodating the carrying device 3 into at least two subspaces for accommodating the carrying device 3; a first fixed magnet 221 is arranged on the side fixed bracket 22 in each subspace; the power supply bracket 21 in each subspace is provided with a power supply socket 211, and the periphery of each power supply socket 211 is provided with a circle of first power supply magnets 212.
The purpose that sets up like this, homoenergetic places one in each subspace and carries on equipment 3 for linking bridge 2 can carry on different equipment simultaneously according to the flight demand, has increased linking bridge 2's practicality. Referring to the structural diagram of the connecting bracket 2 shown in fig. 2, the accommodating space is divided into two subspaces by the limiting fixture block 222, and each subspace can be respectively loaded with a laser radar device and a camera.
Of course, the second fixed magnet 31 and the second power supply magnet 33 need to be provided at the same positions on the mounted devices.
In addition, the outer end (the end far away from the side fixing bracket 22) of each limiting fixture block 222 is provided with a chamfer, when the mounting device 3 is mounted, the mounting device 3 can be directly inserted into the limiting fixture block 222, and the mounting device 3 can transversely move to the position, in the side fixing bracket 22, where the first fixing magnet 221 and the first power supply magnet 212 are in contact with each other along the chamfer of the limiting fixture block 222, and is in adsorption fit, so that the fixing strength of the side fixing bracket 22 on the mounting device 3 is increased, and the mounting convenience of the device is increased.
Example two
According to an embodiment of the present invention, an embodiment of an unmanned aerial vehicle is provided, with reference to fig. 5 to 7, including: unmanned aerial vehicle body 1 and the linking bridge 2 disclosed in embodiment one.
Wherein, linking bridge 2 is connected with rotating electrical machines 5's output, can realize rotatoryly for unmanned aerial vehicle body 1 under rotating electrical machines 5's drive to this orientation of adjusting the equipment carried on.
As an optional implementation manner, referring to fig. 1-4 and fig. 7, a damping mechanism 4 is arranged between the connecting bracket 2 and the unmanned aerial vehicle body 1, the damping mechanism 4 is composed of two damping brackets 41 and two damping gaskets 42, the two damping brackets 41 are provided, a plurality of damping gaskets 42 are installed between the two damping brackets 41, during use, unstable force generated in the flight and collision processes of the unmanned aerial vehicle is damped through the damping gaskets 42, so that the installation stability of the carrying device 3 is increased, and the carrying device 3 is prevented from being damaged in the oscillation process.
As an optional implementation manner, refer to fig. 5-7, the bottom of unmanned aerial vehicle body 1 is equipped with flight support 6, flight support 6 is equipped with two, two flight support 6 are installed in the both sides of unmanned aerial vehicle body 1, flight support 6 highly is greater than the height of linking bridge 2, flight support 6 through setting up supports unmanned aerial vehicle body 1, can be through flight support 6 with the whole steady placing of unmanned aerial vehicle subaerial when taking off, be convenient for taking off of unmanned aerial vehicle more, simultaneously, flight support 6 through setting up can prevent that unmanned aerial vehicle body 1 from producing the equipment damage that the striking leads to on linking bridge 2 in flight process bottom and ground or barrier.
EXAMPLE III
According to an embodiment of the present invention, there is provided an embodiment of a lidar system for an unmanned aerial vehicle, including: the unmanned aerial vehicle disclosed in embodiment two and the linking bridge 2 disclosed in embodiment one. Wherein, the connecting bracket 2 is provided with at least one laser radar device; the both sides of laser radar equipment are equipped with the fixed magnetite 31 of second respectively, and simultaneously, be equipped with on the laser radar equipment with power supply socket 211 assorted power plug 32, the periphery of power plug 32 also is equipped with round second power supply magnetite 33.
The arrangement positions of the second fixed magnet 31 and the second power supply magnet 33 on the laser radar device correspond to the arrangement positions of the first fixed magnet 221 and the first power supply magnet 212 on the connecting bracket 2; through the absorption cooperation of first fixed magnetite 221 and second fixed magnetite 31, can fix laser radar equipment, through the absorption cooperation of first power supply magnetite 212 and second power supply magnetite 33, can realize fixing laser radar equipment the time, make power supply plug 32 insert smoothly in power supply socket 211.
Although the embodiments of the present invention have been described with reference to the accompanying drawings, it is not intended to limit the scope of the present invention, and it should be understood by those skilled in the art that various modifications and variations can be made without inventive efforts by those skilled in the art based on the technical solution of the present invention.
Claims (13)
1. A connection structure for unmanned aerial vehicle, its characterized in that includes: the connecting bracket comprises a power supply bracket and a side fixing bracket; the two side fixing brackets are oppositely arranged, and the power supply bracket and the side fixing brackets jointly form a space for accommodating the carrying equipment; the power supply support and the side fixing support are respectively provided with a first adsorption part, and the first adsorption part is in adsorption fit with a second adsorption part arranged at a corresponding position on the carrying equipment, so that the carrying equipment is fixed.
2. The connection structure for the unmanned aerial vehicle of claim 1, wherein a power supply socket is arranged on the power supply bracket, and the power supply socket is matched with a power supply plug arranged on the carrying equipment to supply power to the carrying equipment.
3. The connection structure for the unmanned aerial vehicle of claim 2, wherein the first suction piece is disposed at a periphery of the power supply socket, and the first suction piece is in suction fit with the second suction piece disposed at a corresponding position of the power supply plug, so as to fix the carrying device.
4. The connecting structure for the unmanned aerial vehicle as claimed in claim 1, wherein the inner side walls of the two side fixing brackets are oppositely provided with limiting blocks, and the limiting blocks can divide the space for accommodating the embarkation equipment into at least two subspaces for accommodating the embarkation equipment.
5. A connection structure for unmanned aerial vehicle as claimed in claim 4, wherein the power supply bracket and the side fixing bracket in each sub-space are respectively provided with a first suction attachment.
6. A connection arrangement for unmanned aerial vehicle as claimed in claim 4, wherein a power supply socket is provided on the power supply support in each subspace.
7. The connecting structure for the unmanned aerial vehicle as claimed in claim 4, wherein an end of the limiting fixture block away from the side fixing bracket is provided with a chamfer.
8. A connection structure for unmanned aerial vehicle of claim 1 or 4, wherein, the embarkation equipment is: lidar load apparatus.
9. An unmanned aerial vehicle, comprising: the linking bridge of any one of claims 1-8, the linking bridge is connected with the unmanned aerial vehicle body.
10. The unmanned aerial vehicle of claim 9, wherein the connecting bracket is connected with the unmanned aerial vehicle body through a damping mechanism; the damping mechanism comprises two damping supports and a damping gasket arranged between the two damping supports.
11. An unmanned aerial vehicle as claimed in claim 9, wherein the connecting bracket is capable of performing rotary motion relative to the unmanned aerial vehicle body under the driving of a rotary motor.
12. The drone of claim 9, further comprising: set up the flight support in unmanned aerial vehicle body bottom both sides respectively, the height of flight support is greater than the height of linking bridge.
13. A lidar system for an unmanned aerial vehicle, comprising: the drone of any one of claims 9-12; the laser radar equipment is carried on the connecting support; the laser radar equipment is provided with a second adsorption piece, and the setting position of the second adsorption piece corresponds to the setting position of the first adsorption piece on the connecting bracket; through the absorption cooperation of first absorption piece and second absorption piece, it is fixed with laser radar equipment and linking bridge.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202011399213.8A CN114590415A (en) | 2020-12-04 | 2020-12-04 | A connection structure, unmanned aerial vehicle and laser radar system for unmanned aerial vehicle |
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| Application Number | Priority Date | Filing Date | Title |
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| CN202011399213.8A CN114590415A (en) | 2020-12-04 | 2020-12-04 | A connection structure, unmanned aerial vehicle and laser radar system for unmanned aerial vehicle |
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| CN211167408U (en) * | 2019-07-18 | 2020-08-04 | 东北林业大学 | Unmanned aerial vehicle nacelle for forest fire monitoring |
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|---|---|---|---|---|
| CN203658576U (en) * | 2013-12-31 | 2014-06-18 | 国家电网公司 | Unmanned plane laser radar overhead power transmission corridor mapping system |
| CN205424349U (en) * | 2015-12-18 | 2016-08-03 | 深圳市华海技术有限公司 | Universal fixed knot of camera constructs |
| WO2017185621A1 (en) * | 2016-04-28 | 2017-11-02 | 乐视控股（北京）有限公司 | Foldable unmanned aerial vehicle and use method thereof |
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