CN117416546A - Unmanned aerial vehicle cluster throwing device, aerial cluster throwing system and unmanned aerial vehicle - Google Patents
Unmanned aerial vehicle cluster throwing device, aerial cluster throwing system and unmanned aerial vehicle Download PDFInfo
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- CN117416546A CN117416546A CN202311396416.5A CN202311396416A CN117416546A CN 117416546 A CN117416546 A CN 117416546A CN 202311396416 A CN202311396416 A CN 202311396416A CN 117416546 A CN117416546 A CN 117416546A
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- 230000001360 synchronised effect Effects 0.000 claims abstract description 5
- 238000004804 winding Methods 0.000 claims description 12
- 230000002457 bidirectional effect Effects 0.000 claims description 10
- 238000006073 displacement reaction Methods 0.000 claims description 9
- 238000009434 installation Methods 0.000 claims description 8
- 238000006243 chemical reaction Methods 0.000 claims description 6
- 230000000694 effects Effects 0.000 abstract description 4
- 238000010586 diagram Methods 0.000 description 5
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- 230000005484 gravity Effects 0.000 description 4
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- 238000000034 method Methods 0.000 description 3
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- 230000009286 beneficial effect Effects 0.000 description 1
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Classifications
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U80/00—Transport or storage specially adapted for UAVs
- B64U80/40—Transport or storage specially adapted for UAVs for two or more UAVs
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U70/00—Launching, take-off or landing arrangements
- B64U70/90—Launching from or landing on platforms
- B64U70/99—Means for retaining the UAV on the platform, e.g. dogs or magnets
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U80/00—Transport or storage specially adapted for UAVs
- B64U80/10—Transport or storage specially adapted for UAVs with means for moving the UAV to a supply or launch location, e.g. robotic arms or carousels
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U80/00—Transport or storage specially adapted for UAVs
- B64U80/80—Transport or storage specially adapted for UAVs by vehicles
- B64U80/86—Land vehicles
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- Engineering & Computer Science (AREA)
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- Aviation & Aerospace Engineering (AREA)
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- Mechanical Engineering (AREA)
- Robotics (AREA)
- Forklifts And Lifting Vehicles (AREA)
Abstract
The invention is applicable to the technical field of unmanned aerial vehicle cluster launching, and provides an unmanned aerial vehicle cluster launching device, an air cluster launching system and an unmanned aerial vehicle, wherein the device comprises: a storage tank; moving the supporting seat; the fixing frame is provided with two groups; the open slot is arranged at the bottom of the storage box; the first rotating shafts are provided with two groups and are rotatably arranged on the fixing frame, each group of the first rotating shafts are vertically distributed on the fixing frame, one first rotating shaft in each group of the first rotating shafts is connected with a second driving motor for driving the first rotating shaft to rotate, and the running states of the two second driving motors are synchronous; the driving wheel is arranged on the first rotating shaft; a surrounding flexible member connected to the same set of opposing drive wheels; the movable supporting plate is uniformly fixed on the surrounding flexible piece; the adjusting mechanism is used for adjusting the distance between the two fixing frames; the automatic fixing unit is used for fixing the unmanned aerial vehicle matched with the automatic fixing unit; the invention has good throwing effect.
Description
Technical Field
The invention belongs to the technical field of unmanned aerial vehicle cluster launching, and particularly relates to an unmanned aerial vehicle cluster launching device, an aerial cluster launching system and an unmanned aerial vehicle.
Background
The existing unmanned aerial vehicle batch release mainly comprises two modes, wherein one mode is that the unmanned aerial vehicle is transported to a target area by adopting a vehicle, and then the unmanned aerial vehicles are flown from the ground one by one in the target area; in another mode, an ejection mechanism is arranged on a conveyor, the unmanned aerial vehicle is arranged in the ejection mechanism, and the conveyor horizontally emits the unmanned aerial vehicle through the ejection mechanism after conveying the unmanned aerial vehicle to a target area.
However, in the prior art, in the transportation process, collision is easy to occur between the unmanned aerial vehicle cluster and the throwing device, so that unmanned aerial vehicle is damaged.
Therefore, how to provide an unmanned aerial vehicle cluster throwing device, an air cluster throwing system and an unmanned aerial vehicle is a problem to be solved by those skilled in the art.
Disclosure of Invention
The invention aims to provide an unmanned aerial vehicle cluster throwing device, an air cluster throwing system and an unmanned aerial vehicle, and aims to solve the problems in the background art.
The invention is realized in such a way that an unmanned aerial vehicle cluster throwing device comprises:
the storage box is used for storing the unmanned aerial vehicle;
the movable supporting seat is fixed on the storage box;
the fixing frames are provided with two groups and are symmetrically distributed;
the open slot is arranged at the bottom of the storage box and is positioned between the two fixing frames;
the first rotating shafts are provided with two groups and are rotatably arranged on the fixing frame, each group of the first rotating shafts are vertically distributed on the fixing frame, one first rotating shaft in each group of the first rotating shafts is connected with a second driving motor for driving the first rotating shaft to rotate, and the running states of the two second driving motors are synchronous;
the driving wheel is arranged on the first rotating shaft;
a surrounding flexible member connected to the same set of opposing drive wheels;
the movable supporting plate is uniformly fixed on the surrounding flexible piece;
the adjusting mechanism is used for adjusting the distance between the two fixing frames;
the automatic fixing unit is arranged on the movable supporting plate and is used for fixing the unmanned aerial vehicle matched with the automatic fixing unit.
Preferably, the adjusting mechanism includes:
the bidirectional screw is rotationally connected with the storage box and is in threaded connection with the fixing frame;
the first driving motor is arranged on the outer wall of the storage box, and the output end of the first driving motor is fixedly connected with the bidirectional screw rod;
the protection shell is sleeved on the outer side of the first driving motor and is fixed with the outer wall of the storage box.
Preferably, the automatic fixing unit includes:
the elastic telescopic mechanism is arranged on the movable supporting plate, and one side, close to the unmanned aerial vehicle, of the elastic telescopic mechanism is provided with a pressed inclined plane matched with the unmanned aerial vehicle;
the driving mechanism is arranged on the movable supporting plate and is used for automatically adjusting the distance between the elastic telescopic mechanism and the movable supporting plate;
the connecting mechanism is arranged on the movable supporting plate and used for supporting the unmanned aerial vehicle in an auxiliary mode, so that the driving mechanism is driven to operate through displacement of the unmanned aerial vehicle.
Preferably, the elastic telescopic mechanism comprises:
a first mounting sleeve;
the first limiting slide block is arranged in the first mounting sleeve in a sliding manner;
the two ends of the first elastic piece are fixedly connected with the first limit sliding block and the inner wall of the first installation sleeve respectively, and the first elastic piece is positioned on one side, close to the surrounding flexible piece, of the first limit sliding block;
the first connecting sliding rod penetrates through the first mounting sleeve and is fixed on the first limiting sliding block;
the inclined wedge seat is fixed at one end of the first connecting sliding rod, which is far away from the first mounting sleeve.
Preferably, the driving mechanism includes:
the second connecting sliding rod penetrates through the movable supporting plate and is fixedly connected with the elastic telescopic mechanism;
the second limiting slide block is fixed at one end of the second connecting slide rod far away from the elastic telescopic mechanism, and the outer diameter of the second limiting slide block is larger than that of the second connecting slide rod;
the second mounting sleeve is in sliding connection with the second limiting slide block and the second connecting slide bar;
the two ends of the second elastic piece are fixedly connected with the second limit sliding block and the inner wall of the second installation sleeve respectively;
the traction rope penetrates through the second mounting sleeve, the second elastic piece and the second limiting slide block and is fixedly connected with the second limiting slide block;
one end of the traction rope, which is positioned outside the second installation sleeve, is connected with the connecting mechanism.
Preferably, the connection mechanism comprises:
the upper end of the support slide rod is positioned at one side of the movable support plate, which is close to the elastic telescopic mechanism;
the elastic support assembly is used for elastically supporting the support slide bar;
the conversion assembly is connected with the traction rope and the support sliding rod respectively and used for converting the linear displacement of the support sliding rod into coiling and uncoiling power for the traction rope.
Preferably, the elastic support assembly includes:
the positioning block is fixed on the side surface of the support sliding rod;
and two ends of the third elastic piece are fixedly connected with the movable supporting plate and the positioning block respectively.
Preferably, the conversion assembly comprises:
the second rotating shaft is arranged on the movable supporting plate through the first supporting frame;
the winding wheel is arranged on the second rotating shaft and winds the traction rope;
the guide wheel is arranged on the second installation sleeve and used for guiding the traction rope;
the driving gear is fixed on the second rotating shaft and is connected with a tooth group arranged on the side surface of the winding wheel in a meshed mode.
The utility model provides an unmanned aerial vehicle aerial cluster puts in system, includes the unmanned aerial vehicle cluster puts in device that the above-mentioned arbitrary embodiment disclosed in, the bottom of conveyer is provided with the unmanned aerial vehicle that can open and shut and throws the mouth.
An unmanned aerial vehicle, the unmanned aerial vehicle comprising:
an unmanned aerial vehicle body;
the mounting plate is mounted on the bottom of the unmanned aerial vehicle body;
the connecting base is fixedly connected with the mounting plate;
the bottom plate is fixed on the connecting base;
and the elastic frame is fixed on the bottom of the bottom plate.
Compared with the prior art, the invention has the beneficial effects that: through setting up bin, remove the supporting seat, the mount, first pivot, the drive wheel, encircle the flexible piece, remove the backup pad, adjustment mechanism and automatic fixation unit, when using, according to the unmanned aerial vehicle specification of throwing in, thereby start adjustment mechanism operation, thereby the distance between two mounts has been adjusted to adjustment mechanism, thereby the shortest distance between two sets of flexible pieces of encircleing has been adjusted, so as to satisfy both sides and encircle the removal backup pad on the flexible piece and can support unmanned aerial vehicle, then put into unmanned aerial vehicle in proper order in the removal backup pad between two sets of flexible pieces, the automatic fixation unit in the rethread removes the backup pad is fixed to it, then through starting second driving motor, two second driving motor synchronous operation, thereby drive first pivot rotation thereby the drive encircle the flexible piece and encircle the operation, encircle flexible piece drive removal backup pad, automatic fixation unit removes, when unmanned aerial vehicle's below removes to the drive wheel department of lower extreme, thereby it need encircle and move the backup pad and drive automatic fixation unit and break away from unmanned aerial vehicle, thereby unmanned aerial vehicle has passed on the bin under the action of gravity and has reached automatic fixation unit, and can also have good effect in proper order through the transportation, can not take place in the storage device, can also be guaranteed in proper order, the transportation device is easy in the transportation, can not take place.
Drawings
The accompanying drawings are included to provide a further understanding of the invention and are incorporated in and constitute a part of this specification, illustrate the invention and together with the embodiments of the invention, serve to explain the invention.
Fig. 1 is a schematic structural diagram of an unmanned aerial vehicle cluster throwing device according to an embodiment of the present invention.
Fig. 2 is a schematic structural diagram of an automatic fixing unit in an unmanned aerial vehicle cluster delivery device according to an embodiment of the present invention when not in use.
Fig. 3 is a schematic structural diagram of an automatic fixing unit in an unmanned aerial vehicle cluster launching device in use according to an embodiment of the present invention.
Fig. 4 is a schematic structural diagram of an unmanned aerial vehicle according to an embodiment of the present invention.
In the accompanying drawings: 1-a storage tank; 2-moving the supporting seat; 3-fixing frame; 4-open grooves; 5-a first rotating shaft; 6-driving wheels; 7-encircling the flexure; 8-moving the support plate; 9-a bidirectional screw; 10-a first drive motor; 11-protecting shell; 12-a first mounting sleeve; 13-a first limit slide block; 14-a first elastic member; 15-a first connecting slide bar; 16-inclined wedge seat; 17-a second connecting slide bar; 18-a second limit slide block; 19-a second mounting sleeve; 20-a second elastic member; 21-a traction rope; 22-a second rotating shaft; 23-winding wheel; 24-guiding wheels; 25-a drive gear; 26-supporting the slide bar; 27-positioning blocks; 28-a third elastic member; 29-unmanned aerial vehicle body; 30-mounting plates; 31-a connection base; 32-a bottom plate; 100-unmanned aerial vehicle; 200-an adjusting mechanism; 300-elastic telescopic mechanism; 400-a driving mechanism; 500-connection mechanism.
Detailed Description
The present invention will be described in further detail with reference to the drawings and examples, in order to make the objects, technical solutions and advantages of the present invention more apparent. It should be understood that the specific embodiments described herein are for purposes of illustration only and are not intended to limit the scope of the invention.
Specific implementations of the invention are described in detail below in connection with specific embodiments.
As shown in fig. 1 and fig. 2, a schematic structural diagram of an unmanned aerial vehicle cluster launching device according to an embodiment of the present invention includes:
a storage box 1, wherein the storage box 1 is used for storing the unmanned aerial vehicle 100;
a movable supporting seat 2, wherein the movable supporting seat 2 is fixed on the storage box 1;
the fixing frames 3 are provided with two groups and are symmetrically distributed;
an open slot 4, wherein the open slot 4 is arranged at the bottom of the storage box 1 and is positioned between the two fixing frames 3;
the first rotating shafts 5 are provided with two groups and are rotatably arranged on the fixed frame 3, each group of the first rotating shafts 5 is vertically distributed on the fixed frame 3, one first rotating shaft 5 in each group of the first rotating shafts 5 is connected with a second driving motor for driving the first rotating shaft to rotate, and the running states of the two second driving motors are synchronous;
a driving wheel 6, wherein the driving wheel 6 is mounted on the first rotating shaft 5;
a surrounding flexible member 7, said surrounding flexible member 7 being connected to the same set of opposing drive wheels 6;
a movable support plate 8, wherein the movable support plate 8 is uniformly fixed on the surrounding flexible member 7;
an adjusting mechanism 200, wherein the adjusting mechanism 200 is used for adjusting the distance between the two fixing frames 3;
the automatic fixing unit is arranged on the movable supporting plate 8 and is used for fixing the unmanned aerial vehicle 100 matched with the automatic fixing unit.
In the embodiment of the invention, when the unmanned aerial vehicle is used, according to the specifications of the unmanned aerial vehicle put in, the adjusting mechanism 200 is started to operate firstly, so that the distance between the two fixing frames 3 is adjusted, namely the shortest distance between the two groups of surrounding flexible pieces 7 is adjusted, so that the movable supporting plates 8 on the two groups of surrounding flexible pieces 7 can support the unmanned aerial vehicle 100, then the unmanned aerial vehicle 100 is sequentially put on the movable supporting plates 8 between the two groups of surrounding flexible pieces 7, then the unmanned aerial vehicle 100 is fixed by an automatic fixing unit on the movable supporting plates 8, then the two second driving motors are started to operate synchronously, thereby driving the first rotating shaft 5 to rotate, the first rotating shaft 5 drives the driving wheels 6 to rotate, thereby driving the surrounding flexible pieces 7 to operate in a surrounding manner, the movable supporting plate 8 is driven by the encircling flexible piece 7, the automatic fixing unit moves, when the lowest movable supporting plate 8 of the supporting unmanned aerial vehicle 100 moves to the driving wheel 6 of the lower end, the automatic fixing unit is driven by the movable supporting plate 8 to be away from the unmanned aerial vehicle 100 due to the encircling back movement, at the moment, the unmanned aerial vehicle 100 automatically passes through the opening groove 4 on the storage box 1 under the action of gravity, the purpose of throwing is achieved, the unmanned aerial vehicle 100 can be sequentially stored in the storage box 1, the storage effect is good, the automatic fixing unit on the movable supporting plate 8 of the supporting unmanned aerial vehicle 100 can be easily thrown in sequence, the unmanned aerial vehicle 100 can be prevented from colliding with other devices and equipment in the transportation process, and the transportation is safe and efficient.
The automatic fixing unit is used for fixing the unmanned aerial vehicle with special characteristics, such as a plate shape or other characteristics, and is matched with the specific structure of the unmanned aerial vehicle.
As shown in fig. 1, as a preferred embodiment of the present invention, the adjusting mechanism 200 includes:
the bidirectional screw rod 9 is rotationally connected with the storage box 1, and the bidirectional screw rod 9 is in threaded connection with the fixing frame 3;
the first driving motor 10 is arranged on the outer wall of the storage box 1, and the output end of the first driving motor 10 is fixedly connected with the bidirectional screw 9;
the protection shell 11 is sleeved outside the first driving motor 10 and is fixed with the outer wall of the storage box 1.
In the embodiment of the invention, when the unmanned aerial vehicle is used, the first driving motor 10 is started, so that the first driving motor 10 drives the bidirectional screw rod 9 to rotate, and the bidirectional screw rod 9 drives the two fixing frames 3 to be close to or far away from each other, so that the distance between the two groups of surrounding flexible pieces 7 is adjusted, and the unmanned aerial vehicle is matched with unmanned aerial vehicles 100 in different size ranges.
As shown in fig. 2 and 3, as another preferred embodiment of the present invention, the automatic fixing unit includes:
the elastic telescopic mechanism 300 is arranged on the movable supporting plate 8, and a pressed inclined plane matched with the unmanned aerial vehicle 100 is arranged on one side, close to the unmanned aerial vehicle 100, of the elastic telescopic mechanism 300;
a driving mechanism 400, wherein the driving mechanism 400 is arranged on the movable supporting plate 8, and the driving mechanism 400 is used for automatically adjusting the distance between the elastic telescopic mechanism 300 and the movable supporting plate 8;
the connection mechanism 500 is arranged on the movable support plate 8, and the connection mechanism 500 is used for supporting the unmanned aerial vehicle 100 in an auxiliary manner so as to drive the driving mechanism 400 to operate through the displacement thereof.
In the embodiment of the invention, after the distance between the two fixing frames 3 is adjusted, the unmanned aerial vehicle 100 is placed on the movable supporting plate 8, at this time, the unmanned aerial vehicle 100 firstly extrudes a pressed inclined plane, the pressed inclined plane is extruded so as to drive the elastic telescopic mechanism 300 to shrink, after the unmanned aerial vehicle 100 spans the elastic telescopic mechanism 300, the unmanned aerial vehicle 100 extrudes the connecting mechanism 500 until the unmanned aerial vehicle 100 moves to the surface of the movable supporting plate 8, and at the same time, the connecting mechanism 500 drives the driving mechanism 400 to operate through extrusion displacement received by the connecting mechanism 500, and the driving mechanism 400 drives the elastic telescopic mechanism 300 to move downwards so as to match the movable supporting plate 8 to automatically fix the unmanned aerial vehicle 100; it should be stated that when the movable support plate 8 rotates to the position of the driving wheel 6 below, that is, the predetermined position, the surrounding flexible member 7 drives the movable support plate 8 and the automatic fixing unit to move, and the unmanned aerial vehicle 100 limits the elastic telescopic mechanism 300, and the elastic telescopic mechanism 300 contracts, so that the unmanned aerial vehicle 100 is separated from the movable support plate 8 and the automatic fixing unit, and automatically falls under the action of gravity.
As shown in fig. 2 and 3, as another preferred embodiment of the present invention, the elastic telescopic mechanism 300 includes:
a first mounting sleeve 12;
the first limit sliding block 13 is arranged in the first mounting sleeve 12 in a sliding manner;
the two ends of the first elastic piece 14 are fixedly connected with the first limit sliding block 13 and the inner wall of the first mounting sleeve 12 respectively, and the first elastic piece 14 is positioned on one side of the first limit sliding block 13, which is close to the surrounding flexible piece 7;
the first connecting sliding rod 15 penetrates through the first mounting sleeve 12 and is fixed on the first limit sliding block 13;
the inclined wedge seat 16, the inclined wedge seat 16 is fixed on one end of the first connecting sliding rod 15 away from the first mounting sleeve 12.
In the embodiment of the invention, when the unmanned aerial vehicle 100 is used, the unmanned aerial vehicle 100 extrudes the pressed inclined plane, so that the inclined wedge seat 16 is driven to move towards the surrounding flexible piece 7, the inclined wedge seat 16 drives the first connecting sliding rod 15 and the first limiting sliding rod 13 to move, the first limiting sliding rod 13 slides along the first mounting sleeve 12 and extrudes the first elastic piece 14 until the unmanned aerial vehicle 100 moves below the inclined wedge seat 16, at the moment, the connecting mechanism 500 drives the driving mechanism 400 to operate through extrusion displacement received by the connecting mechanism, the driving mechanism 400 drives the first mounting sleeve 12 to move downwards, and the first mounting sleeve 12 drives the first limiting sliding rod 13, the first connecting sliding rod 15 and the inclined wedge seat 16 to move, so that the unmanned aerial vehicle 100 is automatically fixed by matching with the movable supporting plate 8.
As shown in fig. 2 and 3, as another preferred embodiment of the present invention, the driving mechanism 400 includes:
the second connecting slide bar 17 penetrates through the movable supporting plate 8 and is fixedly connected with the elastic telescopic mechanism 300;
the second limiting slide block 18 is fixed at one end of the second connecting slide bar 17 far away from the elastic telescopic mechanism 300, and the outer diameter of the second limiting slide block 18 is larger than that of the second connecting slide bar 17;
the second mounting sleeve 19 is in sliding connection with the second limiting slide block 18 and the second connecting slide bar 17;
the two ends of the second elastic piece 20 are fixedly connected with the second limit sliding block 18 and the inner wall of the second mounting sleeve 19 respectively;
the traction rope 21 penetrates through the second mounting sleeve 19, penetrates through the second elastic piece 20 and is fixedly connected with the second limit sliding block 18;
one end of the traction rope 21, which is positioned outside the second mounting sleeve 19, is connected with the connecting mechanism 500.
In the embodiment of the present invention, when the unmanned aerial vehicle 100 moves to the surface of the movable support plate 8, the displacement generated by the extrusion of the connection mechanism 500 is used as power at this time, so that the traction rope 21 is wound, the traction rope 21 pulls the second limiting slide block 18 to move, the second limiting slide block 18 slides downwards along the second mounting sleeve 19 and extrudes the second elastic member 20, and at this time, the second limiting slide block 18 drives the second connection slide bar 17 and the elastic telescopic mechanism 300 to move, so that the elastic telescopic mechanism 300 cooperates with the movable support plate 8 to automatically fix the unmanned aerial vehicle 100.
As shown in fig. 2 and 3, as another preferred embodiment of the present invention, the connection mechanism 500 includes:
a support slide bar 26, wherein the support slide bar 26 is in sliding connection with the movable support plate 8, and the upper end of the support slide bar 26 is positioned at one side of the movable support plate 8 close to the elastic telescopic mechanism 300;
an elastic support assembly for elastically supporting the support slide bar 26;
the conversion assembly is respectively connected with the traction rope 21 and the support slide rod 26 and is used for converting the linear displacement of the support slide rod 26 into the winding and unwinding power for the traction rope 21;
the elastic support assembly includes:
a positioning block 27, the positioning block 27 being fixed to a side surface of the support slide bar 26;
the two ends of the third elastic piece 28 are fixedly connected with the movable supporting plate 8 and the positioning block 27 respectively;
the conversion assembly includes:
the second rotating shaft 22 is arranged on the movable supporting plate 8 through the first supporting frame;
a winding wheel 23, the winding wheel 23 is mounted on the second rotating shaft 22, and the winding wheel 23 winds the traction rope 21;
a guiding wheel 24, the guiding wheel 24 being mounted on the second mounting sleeve 19 and being used for guiding the traction rope 21;
a driving gear 25, the driving gear 25 is fixed on the second rotating shaft 22, and the driving gear 25 is connected with a tooth group installed on the side surface of the winding wheel 23 in a meshing manner.
In the embodiment of the invention, when the unmanned aerial vehicle 100 is used, the supporting slide bar 26 is extruded to move, the supporting slide bar 26 drives the positioning block 27 to move on one hand, the positioning block 27 stretches the third elastic piece 28, so that the third elastic piece 28 generates pulling force to facilitate subsequent resetting, the supporting slide bar 26 drives the tooth set to move on the other hand, the tooth set drives the driving gear 25 to rotate, the driving gear 25 drives the second rotating shaft 22 to rotate, the second rotating shaft 22 drives the winding wheel 23 to rotate, the winding wheel 23 winds the traction rope 21, the traction rope 21 pulls the second limiting slide block 18 to move, the second limiting slide block 18 slides downwards along the second mounting sleeve 19 and extrudes the second elastic piece 20, and at the moment, the second limiting slide block 18 drives the second connecting slide bar 17 and the elastic telescopic mechanism 300 to move, so that the elastic telescopic mechanism 300 is matched with the moving support plate 8 to automatically fix the unmanned aerial vehicle 100.
According to the embodiment of the invention, the storage box 1, the movable supporting seat 2, the fixed frames 3, the open slot 4, the first rotating shaft 5, the driving wheel 6, the encircling flexible piece 7, the movable supporting plate 8, the adjusting mechanism 200 and the automatic fixing unit are arranged, when the unmanned aerial vehicle cluster throwing device is used, according to the specifications of the thrown unmanned aerial vehicle, the adjusting mechanism 200 is started to operate firstly, the distance between the two fixed frames 3 is adjusted by the adjusting mechanism 200, namely the shortest distance between the two encircling flexible pieces 7 is adjusted, so that the movable supporting plates 8 on the encircling flexible pieces 7 at two sides can support the unmanned aerial vehicle 100, then the unmanned aerial vehicle 100 is sequentially placed on the movable supporting plates 8 between the encircling flexible pieces 7, then the unmanned aerial vehicle 100 is fixed by the automatic fixing unit on the movable supporting plate 8, and then the unmanned aerial vehicle is started to operate by the second driving motor, the two second driving motors synchronously run, thereby driving the first rotating shaft 5 to rotate, the first rotating shaft 5 drives the driving wheel 6 to rotate, thereby driving the surrounding flexible piece 7 to run around, the surrounding flexible piece 7 drives the movable supporting plate 8 and the automatic fixing unit to move, when the lowest movable supporting plate 8 of the bearing unmanned aerial vehicle 100 moves to the driving wheel 6 at the lower end, the movable supporting plate 8 drives the automatic fixing unit to separate from the unmanned aerial vehicle 100 because the surrounding is required to move back, at this moment, the unmanned aerial vehicle 100 automatically passes through the opening groove 4 on the storage box 1 under the action of gravity, thereby achieving the throwing purpose, and the unmanned aerial vehicle 100 can be sequentially stored up and down in the storage box 1, not only has good storage effect, but also can be easily thrown in turn, and the automatic fixing unit on the movable supporting plate 8 of the bearing unmanned aerial vehicle 100, it can also be ensured that the unmanned aerial vehicle 100 can not collide with other devices and equipment in the transportation process, and the transportation is safe and efficient.
The invention also provides an unmanned aerial vehicle air cluster throwing system, which comprises a conveyor and the unmanned aerial vehicle cluster throwing device disclosed in any embodiment, wherein in the unmanned aerial vehicle air cluster throwing system, as the surrounding flexible piece 7 drives the movable supporting plate 8 to move from top to bottom, when the movable supporting plate 8 moves to a preset position (at a driving wheel 6 at the lower end) along with the surrounding flexible piece 7, the movable supporting plate 8, the automatic fixing unit and the unmanned aerial vehicle 100 are separated, the unmanned aerial vehicle 100 falls and is released, and an openable unmanned aerial vehicle throwing port is arranged at the bottom of the conveyor so as to release the unmanned aerial vehicle 3 falling from the movable supporting plate 8.
The unmanned aerial vehicle cluster throwing devices can be arranged at a plurality of positions of the conveyor as long as space allows, and the number and arrangement modes of the unmanned aerial vehicle cluster throwing devices placed at each position can be the same or different, and are required to be flexibly arranged according to the cabin space in the conveyor.
As shown in fig. 4, the present invention further provides an unmanned aerial vehicle, which is applied to the above unmanned aerial vehicle air cluster launching system, where the unmanned aerial vehicle 100 includes:
a drone body 29;
a mounting plate 30, the mounting plate 30 being mounted on the bottom of the unmanned aerial vehicle body 29;
a connection base 31, wherein the connection base 31 is fixedly connected with the mounting plate 30;
a bottom plate 32, the bottom plate 32 being fixed to the connection base 31;
and an elastic frame 33, wherein the elastic frame 33 is fixed on the bottom of the bottom plate 32.
The unmanned aerial vehicle 100 does not limit the shape thereof, but the width of the unmanned aerial vehicle 100 is not greater than the distance between the two elastic frames 33, so that unmanned aerial vehicles 100 with different specifications and models can be conveniently put in different high-altitude environments, the unmanned aerial vehicle 100 can be matched with the unmanned aerial vehicle cluster putting device by arranging the mounting plate 30, the connecting base 31, the bottom plate 32 and the elastic frames 33, as shown in fig. 3, the bottom plate 32 can be fixed by matching the adjusting mechanism 200 with the movable supporting plate 8, the distance between the two fixing frames 3 can be adjusted by the adjusting mechanism 200, and then unmanned aerial vehicles 100 with different size ranges can be used, the unmanned aerial vehicles 100 with different specifications and models are avoided, and the problem that different putting devices are required to be matched due to the shape difference of the unmanned aerial vehicles is solved.
The foregoing description of the preferred embodiments of the invention is not intended to be limiting, but rather is intended to cover all modifications, equivalents, and alternatives falling within the spirit and principles of the invention.
Claims (10)
1. Unmanned aerial vehicle cluster puts in device, a serial communication port includes:
the storage box is used for storing the unmanned aerial vehicle;
the movable supporting seat is fixed on the storage box;
the fixing frames are provided with two groups and are symmetrically distributed;
the open slot is arranged at the bottom of the storage box and is positioned between the two fixing frames;
the first rotating shafts are provided with two groups and are rotatably arranged on the fixing frame, each group of the first rotating shafts are vertically distributed on the fixing frame, one first rotating shaft in each group of the first rotating shafts is connected with a second driving motor for driving the first rotating shaft to rotate, and the running states of the two second driving motors are synchronous;
the driving wheel is arranged on the first rotating shaft;
a surrounding flexible member connected to the same set of opposing drive wheels;
the movable supporting plate is uniformly fixed on the surrounding flexible piece;
the adjusting mechanism is used for adjusting the distance between the two fixing frames;
the automatic fixing unit is arranged on the movable supporting plate and is used for fixing the unmanned aerial vehicle matched with the automatic fixing unit.
2. The unmanned aerial vehicle cluster delivery device of claim 1, wherein the adjustment mechanism comprises:
the bidirectional screw is rotationally connected with the storage box and is in threaded connection with the fixing frame;
the first driving motor is arranged on the outer wall of the storage box, and the output end of the first driving motor is fixedly connected with the bidirectional screw rod;
the protection shell is sleeved on the outer side of the first driving motor and is fixed with the outer wall of the storage box.
3. The unmanned aerial vehicle cluster delivery device of claim 1, wherein the automatic fixing unit comprises:
the elastic telescopic mechanism is arranged on the movable supporting plate, and one side, close to the unmanned aerial vehicle, of the elastic telescopic mechanism is provided with a pressed inclined plane matched with the unmanned aerial vehicle;
the driving mechanism is arranged on the movable supporting plate and is used for automatically adjusting the distance between the elastic telescopic mechanism and the movable supporting plate;
the connecting mechanism is arranged on the movable supporting plate and used for supporting the unmanned aerial vehicle in an auxiliary mode, so that the driving mechanism is driven to operate through displacement of the unmanned aerial vehicle.
4. A drone cluster launch device according to claim 3 wherein said elastic telescopic mechanism comprises:
a first mounting sleeve;
the first limiting slide block is arranged in the first mounting sleeve in a sliding manner;
the two ends of the first elastic piece are fixedly connected with the first limit sliding block and the inner wall of the first installation sleeve respectively, and the first elastic piece is positioned on one side, close to the surrounding flexible piece, of the first limit sliding block;
the first connecting sliding rod penetrates through the first mounting sleeve and is fixed on the first limiting sliding block;
the inclined wedge seat is fixed at one end of the first connecting sliding rod, which is far away from the first mounting sleeve.
5. A drone cluster launch apparatus according to claim 3 wherein said drive mechanism comprises:
the second connecting sliding rod penetrates through the movable supporting plate and is fixedly connected with the elastic telescopic mechanism;
the second limiting slide block is fixed at one end of the second connecting slide rod far away from the elastic telescopic mechanism, and the outer diameter of the second limiting slide block is larger than that of the second connecting slide rod;
the second mounting sleeve is in sliding connection with the second limiting slide block and the second connecting slide bar;
the two ends of the second elastic piece are fixedly connected with the second limit sliding block and the inner wall of the second installation sleeve respectively;
the traction rope penetrates through the second mounting sleeve, the second elastic piece and the second limiting slide block and is fixedly connected with the second limiting slide block;
one end of the traction rope, which is positioned outside the second installation sleeve, is connected with the connecting mechanism.
6. The unmanned aerial vehicle cluster delivery device of claim 5, wherein the connection mechanism comprises:
the upper end of the support slide rod is positioned at one side of the movable support plate, which is close to the elastic telescopic mechanism;
the elastic support assembly is used for elastically supporting the support slide bar;
the conversion assembly is connected with the traction rope and the support sliding rod respectively and used for converting the linear displacement of the support sliding rod into coiling and uncoiling power for the traction rope.
7. The unmanned aerial vehicle cluster delivery device of claim 6, wherein the resilient support assembly comprises:
the positioning block is fixed on the side surface of the support sliding rod;
and two ends of the third elastic piece are fixedly connected with the movable supporting plate and the positioning block respectively.
8. The unmanned aerial vehicle cluster delivery device of claim 6, wherein the conversion assembly comprises:
the second rotating shaft is arranged on the movable supporting plate through the first supporting frame;
the winding wheel is arranged on the second rotating shaft and winds the traction rope;
the guide wheel is arranged on the second installation sleeve and used for guiding the traction rope;
the driving gear is fixed on the second rotating shaft and is connected with a tooth group arranged on the side surface of the winding wheel in a meshed mode.
9. An unmanned aerial vehicle air cluster throwing system, which comprises a conveyor and an unmanned aerial vehicle cluster throwing device as claimed in any one of claims 1-8, wherein an openable unmanned aerial vehicle throwing port is arranged at the bottom of the conveyor.
10. An unmanned aerial vehicle, characterized in that the unmanned aerial vehicle comprises:
an unmanned aerial vehicle body;
the mounting plate is mounted on the bottom of the unmanned aerial vehicle body;
the connecting base is fixedly connected with the mounting plate;
the bottom plate is fixed on the connecting base;
and the elastic frame is fixed on the bottom of the bottom plate.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202311396416.5A CN117416546A (en) | 2023-10-26 | 2023-10-26 | Unmanned aerial vehicle cluster throwing device, aerial cluster throwing system and unmanned aerial vehicle |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202311396416.5A CN117416546A (en) | 2023-10-26 | 2023-10-26 | Unmanned aerial vehicle cluster throwing device, aerial cluster throwing system and unmanned aerial vehicle |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN117416546A true CN117416546A (en) | 2024-01-19 |
Family
ID=89532088
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202311396416.5A Pending CN117416546A (en) | 2023-10-26 | 2023-10-26 | Unmanned aerial vehicle cluster throwing device, aerial cluster throwing system and unmanned aerial vehicle |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN117416546A (en) |
-
2023
- 2023-10-26 CN CN202311396416.5A patent/CN117416546A/en active Pending
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