CN109131916B - Quick plug mounting platform of unmanned aerial vehicle - Google Patents
Quick plug mounting platform of unmanned aerial vehicle Download PDFInfo
- Publication number
- CN109131916B CN109131916B CN201811108401.3A CN201811108401A CN109131916B CN 109131916 B CN109131916 B CN 109131916B CN 201811108401 A CN201811108401 A CN 201811108401A CN 109131916 B CN109131916 B CN 109131916B
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- plug
- trapezoid
- supporting plate
- mounting
- unmanned aerial
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- 230000007246 mechanism Effects 0.000 claims abstract description 35
- 238000010586 diagram Methods 0.000 description 3
- 238000009434 installation Methods 0.000 description 2
- 238000000034 method Methods 0.000 description 2
- 238000004891 communication Methods 0.000 description 1
- 238000011161 development Methods 0.000 description 1
- 230000008030 elimination Effects 0.000 description 1
- 238000003379 elimination reaction Methods 0.000 description 1
- 238000005516 engineering process Methods 0.000 description 1
- 238000004880 explosion Methods 0.000 description 1
- 238000011835 investigation Methods 0.000 description 1
- 238000013507 mapping Methods 0.000 description 1
- 238000005457 optimization Methods 0.000 description 1
- 230000008092 positive effect Effects 0.000 description 1
Classifications
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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
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U2101/00—UAVs specially adapted for particular uses or applications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U2101/00—UAVs specially adapted for particular uses or applications
- B64U2101/30—UAVs specially adapted for particular uses or applications for imaging, photography or videography
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- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Battery Mounting, Suspending (AREA)
Abstract
The rapid plugging and unplugging mounting platform for the unmanned aerial vehicle comprises a battery supporting plate, a mounting base hinged below the battery supporting plate, clamping mechanisms symmetrically hinged at two sides of the battery supporting plate, angle adjusting arms symmetrically connected at two sides of the battery supporting plate, a trapezoid plugging block connected below the mounting base, a spring locking mechanism arranged at the front end of the trapezoid plugging block, and a trapezoid plugging seat matched with the trapezoid plugging block; the angle adjusting arm is fixedly connected with the battery supporting plate, is of an arc-shaped sheet structure and is provided with an arc-shaped adjusting hole; an adjusting locking bolt is arranged in the arc-shaped adjusting hole; one end of the adjusting locking bolt is in threaded connection with a threaded hole on the mounting base; the trapezoidal socket is inserted into the trapezoidal plug block, the trapezoidal plug block is fixedly connected with the trapezoidal socket through the spring locking mechanism, and the mounting device is arranged below the trapezoidal socket. The mounting platform can realize quick replacement of the mounting device and has strong universality.
Description
Technical Field
The invention relates to the technical field of unmanned aerial vehicle mounting, in particular to a rapid plug-in mounting platform of an unmanned aerial vehicle.
Background
Unmanned aircraft is abbreviated as "unmanned aircraft", and is an unmanned aircraft which is operated by using radio remote control equipment and a self-contained program control device, and the unmanned aircraft is actually a collective term of unmanned aircraft. Compared with manned aircraft, it has the advantages of small size, low cost, convenient use, low requirement for battle environment, strong battlefield survivability, etc. Because the unmanned aerial vehicle has important significance for future air combat, all the main military countries in the world are tightening to develop the unmanned aerial vehicle.
Along with the rapid development of unmanned aerial vehicle technology, the unmanned aerial vehicle has wide application in the fields of military, civil use and the like as a small robot tool with strong maneuverability and simple operation, and has wide application in the aspects of investigation, explosion elimination, search and rescue and the like at present.
Unmanned aerial vehicles are classified according to purposes and can be classified into military unmanned aerial vehicles and civilian unmanned aerial vehicles. Military unmanned aerial vehicles can be classified into reconnaissance unmanned aerial vehicles, bait unmanned aerial vehicles, electronic countermeasure unmanned aerial vehicles, communication relay unmanned aerial vehicles, unmanned fighter aircraft, target aircraft, and the like; the civil unmanned aerial vehicle can be divided into a patrol/monitor unmanned aerial vehicle, an agricultural unmanned aerial vehicle, a meteorological unmanned aerial vehicle, an exploration unmanned aerial vehicle, a mapping unmanned aerial vehicle and the like.
Unmanned aerial vehicle as a carrier its usage depends on unmanned aerial vehicle's mounting platform, and the different tasks can be accomplished to the different modules of mount, and the task such as take photo by plane can be accomplished to the mount camera, and the electric power that can be accomplished to the mount infrared camera is patrolled line etc. tasks, and the military equipment of mount can accomplish the battle task such as aerial accurate battle, and at present, unmanned aerial vehicle mounting platform mostly is single fixed, installs inconveniently, can't be general, can not satisfy multiple hanging device and switch the use fast.
Disclosure of Invention
The invention aims to provide a rapid plugging and unplugging mounting platform for an unmanned aerial vehicle, which not only can adjust the angle of a mounting device, but also can meet the requirements of rapid switching and use of various unmanned aerial vehicle mounting devices, and realizes the purposes of universality, rapid installation and rapid switching of all devices on the platform.
In order to achieve the above purpose, the invention is realized by adopting the following technical scheme:
The rapid plugging and unplugging mounting platform for the unmanned aerial vehicle comprises a battery supporting plate, a mounting base hinged below the battery supporting plate, clamping mechanisms symmetrically hinged at two sides of the battery supporting plate, angle adjusting arms symmetrically connected at two sides of the battery supporting plate, a trapezoid plugging block connected below the mounting base, a spring locking mechanism arranged at the front end of the trapezoid plugging block, and a trapezoid plugging seat matched with the trapezoid plugging block; the battery supporting plate is used for placing the unmanned aerial vehicle storage battery, and four foot frames of the unmanned aerial vehicle are fixed on the clamping mechanism; the angle adjusting arm is fixedly connected with the battery supporting plate, is of an arc-shaped sheet structure and is provided with an arc-shaped adjusting hole; an adjusting locking bolt is arranged in the arc-shaped adjusting hole; one end of the adjusting locking bolt is in threaded connection with a threaded hole on the mounting base; the trapezoidal socket is inserted into the trapezoidal plug block, the trapezoidal plug block is fixedly connected with the trapezoidal socket through the spring locking mechanism, and the mounting device is arranged below the trapezoidal socket.
As the optimization of the invention, one side of the battery supporting plate connected with the mounting base is symmetrically and fixedly connected with two connecting shaft seats, and the first hinging shaft penetrates through the two connecting shaft seats and the mounting base to hinge the battery supporting plate with the mounting base; the battery support plate is characterized in that two sides of the battery support plate are also provided with two connecting lugs, the connecting lugs are provided with hinge holes, and the second hinge shaft penetrates through the hinge holes and the clamping mechanism to hinge the clamping mechanism with the battery support plate.
As the preferable choice of the invention, the said clamping mechanism includes the fixed card that is hinged with the battery pallet and the movable card that is connected with the fixed card through the fast-assembling bolt; the fixed card and the movable card form two clamping holes after being connected.
As the preferable choice of the invention, the said trapezoid plug-in block connects under the mounting base through a plurality of screws, the front end of the trapezoid plug-in block processes a first bump; the first bulge is provided with a mounting hole for mounting the spring locking mechanism; the two side surfaces of the trapezoid plug-in block are inclined surfaces which are symmetrically inclined outwards; the trapezoid plug-in seat is provided with a plurality of connecting holes for connecting the mounting objects, and is provided with a trapezoid plug-in groove matched with the trapezoid plug-in block; the front end of the trapezoid plug-in seat is provided with a second bulge; a locking groove is formed in the second bulge; the locking groove corresponds to the mounting hole.
As the preferable choice of the invention, a stop block is fixedly connected with the back of the trapezoid plug-in block below the mounting base; the stop block is used for limiting after the trapezoidal inserting block is inserted into the trapezoidal inserting seat.
As a further preferable mode of the invention, two connecting lugs of the battery supporting plate are also provided with limiting blocks, the limiting blocks are arranged on the second hinge shaft, and the limiting blocks are of L-shaped structures and are used for limiting the upward rotation angle of the clamping mechanism.
As a further preferable aspect of the present invention, the battery support plate is provided with two lightening holes, the mounting base is provided with two lightening holes, and the fixing clip and the movable clip are respectively provided with lightening holes.
As a further preferred aspect of the present invention, the spring locking mechanism has a spring locking plug at the bottom, and a pull ring at the top, the spring locking plug is retracted when the pull ring is pulled up, and the spring locking plug is extended when the pull ring is put down, and is snapped into a locking groove on the trapezoidal socket.
The invention has the following advantages and positive effects:
1. the mounting platform provided by the invention has the advantages that the structure is simple, the use is convenient, the platform and the unmanned aerial vehicle foot frame are fixed through the clamping mechanism, and the mounting and the fixing are firm; in addition, through inserting trapezoidal bayonet socket or extracting trapezoidal plug block fast, can realize the quick replacement to the mounting device, make it can satisfy multiple mounting device quick switch and use, this mounting platform commonality is strong, and application scope is wide.
2. The mounting platform provided by the invention can realize the platform sharing, the quick mounting and the quick switching of various mounting systems; in addition, the inclination angle of the mounting device can be adjusted through the angle adjusting fixing bolt, so that the requirements under various environments are met.
3. The mounting platform provided by the invention is provided with the plurality of lightening holes, and the whole weight of the mounting platform is lighter, so that the unmanned aerial vehicle can bear the mounting device with larger weight for taking off.
Drawings
FIG. 1 is a schematic diagram of the overall structure of the present invention.
Fig. 2 is an exploded view of fig. 1 of the present invention.
FIG. 3 is a second schematic diagram of the overall structure of the present invention.
Fig. 4 is a schematic diagram showing the connection of the battery tray and the mounting base.
Fig. 5 is a second schematic view of the connection between the battery tray and the mounting base.
Detailed Description
The following detailed description of the application, taken in conjunction with the accompanying drawings, is not intended to limit the scope of the application, so that those skilled in the art may better understand the technical solutions of the application and their advantages.
As shown in fig. 1 and 2: the invention provides a rapid plugging and unplugging mounting platform of an unmanned aerial vehicle, which comprises the following components: the battery support plate 1, a mounting base 3 hinged below the battery support plate 1 through a first hinge shaft 2, clamping mechanisms 5 symmetrically hinged on two sides of the battery support plate 1 through a second hinge shaft 4, angle adjusting arms 6 symmetrically connected on two sides of the battery support plate 1, a trapezoid inserting block 7 connected below the mounting base 3, a spring locking mechanism 8 arranged at the front end of the trapezoid inserting block 7, and a trapezoid inserting seat 9 matched with the trapezoid inserting block for use; the battery supporting plate 1 is used for placing an unmanned aerial vehicle storage battery, and four foot frames of the unmanned aerial vehicle are fixed on the clamping mechanism 5; the angle adjusting arm 6 is fixedly connected with the battery supporting plate 1 through a fixing bolt 6-2, the angle adjusting arm 6 is of an arc-shaped sheet structure, and an arc-shaped adjusting hole 6-1 is formed in the angle adjusting arm 6; an adjusting locking bolt 6-3 is arranged in the arc-shaped adjusting hole 6-1; one end of the adjusting locking bolt 6-3 is in threaded connection with the threaded hole 3-2 on the mounting base 3; the trapezoid inserting seat 9 is inserted into the trapezoid inserting block 7, the trapezoid inserting block 7 is fixedly connected with the trapezoid inserting seat 9 through the spring locking mechanism 8, and a mounting device is arranged below the trapezoid inserting seat 9;
Two lightening holes 1-1 are formed in the battery supporting plate 1, and two connecting shaft seats 1-2 are symmetrically and fixedly connected to one side, connected with the mounting base 3, of the battery supporting plate 1; the first hinge shaft 2 passes through the two connecting shaft bases 1-2 and the mounting base 3, and the battery supporting plate 1 is hinged with the mounting base 3; two sides of the battery supporting plate 1 are also provided with two connecting lugs 1-3, the connecting lugs 1-3 are provided with hinge holes 1-4, and the second hinge shaft 4 passes through the hinge holes 1-4 and the clamping mechanism 5 to hinge the clamping mechanism 5 with the battery supporting plate 1; the two connecting lugs 1-3 of the battery supporting plate 1 are also provided with limiting blocks 1-5, the limiting blocks 1-5 are arranged on the second hinge shaft 4, and the limiting blocks 1-5 are of L-shaped structures and are used for limiting the upward rotation angle of the clamping mechanism 5;
Two lightening holes 3-1 are formed in the mounting base 3, threaded holes 3-2 are formed in two side faces of the mounting base 3 respectively, and one end of an adjusting locking bolt 6-3 is in threaded connection with the threaded holes 3-2 in the mounting base 3;
The clamping mechanism 5 comprises a fixed card 5-1 hinged with the battery supporting plate 1 and a movable card 5-3 connected with the fixed card 5-1 through a fast-assembling bolt 5-2; the fixed card 5-1 and the movable card 5-3 are connected to form two clamping holes 5-4; the fixed card 5-1 and the movable card 5-3 are respectively provided with a lightening hole 5-5;
The trapezoid inserting block 7 is connected below the mounting base 3 through a plurality of screws, and a first protrusion 7-1 is machined at the front end of the trapezoid inserting block 7; the first bulge 7-1 is provided with a mounting hole 7-2 for mounting a spring locking mechanism 8; the two side surfaces of the trapezoid inserting block 7 are inclined surfaces 7-3 which are symmetrically inclined outwards;
the trapezoid plug seat 9 is provided with a plurality of connecting holes 9-1 for connecting the mounting objects, and the trapezoid plug seat 9 is provided with a trapezoid plug groove 9-2 matched with the trapezoid plug block 7; the front end of the trapezoid plug-in seat 9 is provided with a second bulge 9-3; the second bulge 9-3 is provided with a locking groove 9-4; the locking groove 9-4 corresponds to the mounting hole 7-2;
The lower surface of the spring locking mechanism 8 is provided with a spring locking plug 8-1, the upper surface of the spring locking plug 8-1 is provided with a pull ring 8-2, the spring locking plug 8-1 is retracted when the pull ring 8-2 is pulled up, the spring locking plug 8-1 extends out when the pull ring 8-2 is put down, and the spring locking plug is clamped into a locking groove 9-4 on the trapezoid plug seat 9;
a stop block 10 is fixedly connected to the rear of the trapezoid plug-in block 7 below the mounting base 3; the stop block 10 is used for limiting after the trapezoidal inserting seat 9 is inserted into the trapezoidal inserting block 7.
The working process comprises the following steps: during installation, the quick-mounting bolts 5-2 are detached firstly, four leg frames of the unmanned aerial vehicle are fixed in the clamping holes 5-4 of the fixed card 5-1 and the movable card 5-3, then the quick-mounting bolts 5-2 are screwed down, and the mounting platform is connected with the unmanned aerial vehicle;
Then placing a storage battery used by the unmanned aerial vehicle on the battery supporting plate 1, connecting and fixing the trapezoid inserting seat 9 with the mounting device, then inserting the trapezoid inserting seat 9 together with the mounting device on the trapezoid inserting block 7, and connecting and fixing the trapezoid inserting seat 9 with the trapezoid inserting block 7 through the spring locking mechanism 8;
then the angle of the mounting device is adjusted through the adjusting locking bolt 6-3, the adjusting locking bolt 6-3 is screwed down after the angle is determined, and the unmanned aerial vehicle drives the mounting platform and the mounting device to take off; when the mounting device needs to be replaced, only the pull ring 8-2 is pulled upwards to detach the trapezoid plug-in seat 9, and then another mounting device with the trapezoid plug-in seat 9 is replaced, so that the operation is simple, convenient, time-saving and labor-saving.
Claims (6)
1. Quick plug mounting platform of unmanned aerial vehicle, its characterized in that: the device comprises a battery supporting plate, a mounting base hinged below the battery supporting plate, clamping mechanisms symmetrically hinged at two sides of the battery supporting plate, angle adjusting arms symmetrically connected at two sides of the battery supporting plate, a trapezoid plug-in block connected below the mounting base, a spring locking mechanism arranged at the front end of the trapezoid plug-in block, and a trapezoid plug-in seat matched with the trapezoid plug-in block for use; the battery supporting plate is used for placing the unmanned aerial vehicle storage battery, and four foot frames of the unmanned aerial vehicle are fixed on the clamping mechanism; the angle adjusting arm is fixedly connected with the battery supporting plate, is of an arc-shaped sheet structure and is provided with an arc-shaped adjusting hole; an adjusting locking bolt is arranged in the arc-shaped adjusting hole; one end of the adjusting locking bolt is in threaded connection with a threaded hole on the mounting base; the trapezoidal inserting seat is inserted into the trapezoidal inserting block, the trapezoidal inserting block is fixedly connected with the trapezoidal inserting seat through the spring locking mechanism, and the mounting device is arranged below the trapezoidal inserting seat;
two connecting shaft seats are symmetrically and fixedly connected to one side, connected with the mounting base, of the battery supporting plate, and the first hinging shaft penetrates through the two connecting shaft seats and the mounting base to hinge the battery supporting plate and the mounting base; two sides of the battery supporting plate are also provided with two connecting lugs, the connecting lugs are provided with hinge holes, and the second hinge shaft penetrates through the hinge holes and the clamping mechanism to hinge the clamping mechanism with the battery supporting plate;
the trapezoid inserting block is connected below the mounting base through a plurality of screws, and a first bulge is formed at the front end of the trapezoid inserting block; the first bulge is provided with a mounting hole for mounting the spring locking mechanism; the two side surfaces of the trapezoid plug-in block are inclined surfaces which are symmetrically inclined outwards; the trapezoid plug-in seat is provided with a plurality of connecting holes for connecting the mounting objects, and is provided with a trapezoid plug-in groove matched with the trapezoid plug-in block; the front end of the trapezoid plug-in seat is provided with a second bulge; a locking groove is formed in the second bulge; the locking groove corresponds to the mounting hole.
2. The unmanned aerial vehicle rapid plug-and-pull mounting platform according to claim 1, wherein: the clamping mechanism comprises a fixed card hinged with the battery supporting plate and a movable card connected with the fixed card through a fast-assembling bolt; the fixed card and the movable card form two clamping holes after being connected.
3. The unmanned aerial vehicle rapid plug-and-pull mounting platform according to claim 1, wherein: a stop block is fixedly connected to the rear of the trapezoid plug-in block below the mounting base; the stop block is used for limiting after the trapezoidal inserting block is inserted into the trapezoidal inserting seat.
4. The unmanned aerial vehicle rapid plug-and-pull mounting platform according to claim 1, wherein: the battery support plate is characterized in that limiting blocks are further arranged on the two connecting lugs of the battery support plate, the limiting blocks are arranged on the second hinge shaft and are of L-shaped structures and used for limiting the upward rotation angle of the clamping mechanism.
5. The unmanned aerial vehicle rapid plug-and-pull mounting platform according to claim 2, wherein: the battery support plate is provided with two lightening holes, the mounting base is provided with two lightening holes, and the fixing clamp and the movable clamp are respectively provided with lightening holes.
6. The unmanned aerial vehicle rapid plug-and-pull mounting platform according to claim 1, wherein: the lower side of the spring locking mechanism is provided with a spring locking plug, the upper side of the spring locking plug is provided with a pull ring, the spring locking plug is retracted when the pull ring is pulled up, and the spring locking plug extends out and is clamped into a locking groove on the trapezoid plug seat when the pull ring is put down.
Applications Claiming Priority (2)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201811067696 | 2018-09-13 | ||
| CN2018110676964 | 2018-09-13 |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CN109131916A CN109131916A (en) | 2019-01-04 |
| CN109131916B true CN109131916B (en) | 2024-05-10 |
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ID=64823344
Family Applications (2)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201821550874.4U Active CN208868306U (en) | 2018-09-13 | 2018-09-21 | A kind of unmanned plane fast insert-pull carry platform |
| CN201811108401.3A Active CN109131916B (en) | 2018-09-13 | 2018-09-21 | Quick plug mounting platform of unmanned aerial vehicle |
Family Applications Before (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201821550874.4U Active CN208868306U (en) | 2018-09-13 | 2018-09-21 | A kind of unmanned plane fast insert-pull carry platform |
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| CN (2) | CN208868306U (en) |
Families Citing this family (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN208868306U (en) * | 2018-09-13 | 2019-05-17 | 吉林省翼启飞科技有限公司 | A kind of unmanned plane fast insert-pull carry platform |
| CN111114786B (en) * | 2020-01-14 | 2021-08-31 | 吉林省翼启飞科技有限公司 | Grenade and grenade throwing device |
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| CN104512556A (en) * | 2013-09-30 | 2015-04-15 | 哈尔滨飞机工业集团有限责任公司 | Four-link opening mechanism of radar cover of airplane |
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Also Published As
| Publication number | Publication date |
|---|---|
| CN109131916A (en) | 2019-01-04 |
| CN208868306U (en) | 2019-05-17 |
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