CN106335640B - Unmanned aerial vehicle continuous throwing device and controller - Google Patents
Unmanned aerial vehicle continuous throwing device and controller Download PDFInfo
- Publication number
- CN106335640B CN106335640B CN201610860865.4A CN201610860865A CN106335640B CN 106335640 B CN106335640 B CN 106335640B CN 201610860865 A CN201610860865 A CN 201610860865A CN 106335640 B CN106335640 B CN 106335640B
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- clamping plate
- plate
- aerial vehicle
- unmanned aerial
- lower clamping
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- 238000003860 storage Methods 0.000 claims abstract description 22
- 238000009749 continuous casting Methods 0.000 claims description 6
- 230000000694 effects Effects 0.000 description 2
- 238000000034 method Methods 0.000 description 2
- 230000002411 adverse Effects 0.000 description 1
- 238000004519 manufacturing process Methods 0.000 description 1
- 239000000725 suspension Substances 0.000 description 1
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Classifications
-
- 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
- B64D1/00—Dropping, ejecting, releasing, or receiving articles, liquids, or the like, in flight
- B64D1/02—Dropping, ejecting, or releasing articles
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U10/00—Type of UAV
- B64U10/10—Rotorcrafts
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- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Mechanical Engineering (AREA)
- Remote Sensing (AREA)
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Abstract
The invention relates to the technical field of unmanned aerial vehicle throwing equipment, in particular to a continuous throwing device and a controller for an unmanned aerial vehicle, wherein the device comprises an upper clamping plate and a lower clamping plate, a plurality of through holes are formed in the lower clamping plate, a plurality of storage containers are arranged between the upper clamping plate and the lower clamping plate, openings are formed in the bottom ends of the storage containers, and the openings and the through holes are arranged oppositely; one side that the punch holder was kept away from to the lower plate is equipped with the rotor plate, is equipped with a hourglass thing hole on the rotor plate, and the rotor plate is connected with drive arrangement, and drive arrangement includes the steering wheel, and the rotation axis is connected to the steering wheel, and the rotation axis is connected with the rotor plate. The continuous throwing device and the controller of the unmanned aerial vehicle can realize continuous throwing by controlling the rotation of the rotating plate through the steering engine, the thrown objects are loaded through the storage container, and the rotation angle of the steering engine can be accurately controlled through the PWM wave duty ratio.
Description
Technical Field
The invention relates to the technical field of unmanned aerial vehicle throwing equipment, in particular to an unmanned aerial vehicle continuous throwing device and a controller.
Background
With the rapid development of the unmanned aerial vehicle technology and the maturity of the market, the unmanned aerial vehicle is widely applied in society. However, the technology and the product for utilizing the unmanned aerial vehicle to throw articles in the air are very few, at present, only a throwing mode is a one-time throwing mode, and the throwing articles adopt a simple suspension mode without a container for loading the throwing articles, so that continuous throwing cannot be realized, and the flight safety of the unmanned aerial vehicle is influenced in the throwing process.
Disclosure of Invention
The invention aims to provide a continuous throwing device and a controller for an unmanned aerial vehicle, and aims to solve the technical problem that the unmanned aerial vehicle in the prior art cannot realize continuous throwing.
In order to achieve the purpose, the invention adopts the following technical scheme:
an unmanned aerial vehicle continuous throwing device comprises an upper clamping plate and a lower clamping plate, wherein the upper clamping plate is fixedly connected with the lower clamping plate, a plurality of through holes are formed in the lower clamping plate and are distributed in a circumferential manner, a plurality of storage containers are arranged between the upper clamping plate and the lower clamping plate, openings are formed in the bottom ends of the storage containers, and the openings are opposite to the through holes;
one side that the punch holder was kept away from to the lower plate is equipped with the rotor plate, the rotor plate with the lower plate is parallel to each other, be equipped with a hourglass thing hole on the rotor plate, it is not less than to leak the thing hole the through-hole, the rotor plate is connected with drive arrangement, drive arrangement includes the steering wheel, the steering wheel is located on the lower plate, the steering wheel is connected with the rotation axis, the rotation axis with the rotor plate is connected, the rotation orbit at hourglass thing hole center overlaps the coincidence with a plurality of the circle that the center of through-hole formed each other.
Furthermore, the upper clamping plate, the lower clamping plate and the rotating plate are all round plates, the steering engine and the rotating shaft are arranged at the centers of the lower clamping plate and the rotating plate, and the through holes and the center of the lower clamping plate are uniformly distributed as the circle center.
Furthermore, a plurality of sliding grooves which are uniformly distributed are arranged at the edge of the rotating plate, the notches of the sliding grooves face to the center of the rotating plate, and the sliding grooves are buckled at the edge of the lower clamping plate.
Further, its characterized in that, the top of punch holder is equipped with the connecting piece, the one end of connecting piece with punch holder fixed connection, the connecting piece is equipped with the connecting hole.
Further, the upper clamping plate and the lower clamping plate are connected through bolts.
Further, the steering engine is a 360-degree steering engine.
Furthermore, the through hole and the object leaking hole are both round holes.
The invention also provides a controller of the continuous throwing device of the unmanned aerial vehicle, which comprises a remote control end and a receiving end, wherein the remote control end comprises a control button, the control button is connected with a first processor, and the first processor is connected with a transmitting module;
the receiving end comprises a receiving module, the receiving module is connected with a second processor, and the second processor is connected with a steering engine of the continuous throwing device of the unmanned aerial vehicle according to any one of claims 1 to 7.
Further, the first processor and the second processor are STC15W408AS single-chip microcomputers.
Further, the transmitting module is a 2.4G radio frequency module.
When the unmanned aerial vehicle continuous throwing device is used, the steering engine rotates to drive the rotating plate to move, when the object leaking hole in the rotating plate is opposite to the through hole in the lower clamping plate, an object leaking channel is formed at the moment, objects to be thrown in the storage container can smoothly fall down, and then the steering engine continues to drive the rotating plate to rotate, so that the corresponding objects to be thrown can be thrown down at one time. This continuous casting device, when throwing with article on the unmanned aerial vehicle many times, in batches to needs, can realize continuous casting through the rotation of steering wheel control rotor plate. The thing of jettisoninging passes through the storing container and loads, and jettisoninging device and unmanned aerial vehicle frame are fixed simultaneously, and unmanned aerial vehicle flight in-process focus can not change, also does not receive the strong wind influence that the unmanned aerial vehicle screw produced, can not produce the wind-load that the horizontal direction changes to can not lead to the fact adverse effect for unmanned aerial vehicle flight safety.
When the controller of the continuous throwing device of the unmanned aerial vehicle is used, the first processor continuously acquires information of the control buttons, the acquired signals generate corresponding control commands, the commands are sent out through the transmitting module, the receiving module receives corresponding data and sends the data to the second processor, and the second processor decodes the commands, generates and outputs corresponding PWM waves to drive the steering engine to rotate. By adopting the control mode, the rotation angle of the steering engine can be accurately controlled, and the unmanned aerial vehicle can complete the parabolic operation.
Drawings
Fig. 1 is a front view of a continuous casting device of an unmanned aerial vehicle provided in embodiment 1 of the present invention;
fig. 2 is a top view of a lower plate of a continuous throwing device of an unmanned aerial vehicle provided in embodiment 1 of the present invention;
fig. 3 is a bottom view of a rotating plate of a continuous throwing device of an unmanned aerial vehicle according to embodiment 1 of the present invention.
In the figure:
1. an upper splint; 2. a lower splint; 3. a through hole; 4. a storage container; 5. a rotating plate; 6. an object leaking hole; 7. a steering engine; 8. a rotating shaft; 9. a chute; 10. a connecting member; 11. and (4) bolts.
Detailed Description
The technical scheme of the invention is further explained by the specific implementation mode in combination with the attached drawings.
Example 1
As shown in fig. 1-3, an unmanned aerial vehicle continuous throwing device comprises an upper clamp plate 1 and a lower clamp plate 2, wherein the upper clamp plate 1 is fixedly connected with the lower clamp plate 2, a plurality of through holes 3 are formed in the lower clamp plate 2, the through holes 3 are distributed in a circumferential manner, a plurality of storage containers 4 are arranged between the upper clamp plate 1 and the lower clamp plate 2, openings are formed in the bottom ends of the storage containers 4, and the openings are opposite to the through holes 3;
one side that upper plate 1 was kept away from to lower plate 2 is equipped with rotor plate 5, rotor plate 5 is parallel to each other with lower plate 2, be equipped with one on the rotor plate 5 and leak thing hole 6, it is not less than through-hole 3 to leak thing hole 6, rotor plate 5 is connected with drive arrangement, drive arrangement includes steering wheel 7, steering wheel 7 is located on lower plate 2, steering wheel 7 is connected with rotation axis 8, rotation axis 8 is connected with rotor plate 5, the rotation orbit at hourglass thing hole 6 center overlaps the coincidence each other with the circle that the center of a plurality of through-holes 3 formed.
Fig. 1 illustrates four storage containers 4, and one storage container 4 is hidden in a front view to show a steering gear 7. The space between the upper clamp plate 1 and the lower clamp plate 2 is used for placing a storage container 4, a to-be-thrown object is placed in the storage container 4, and the upper clamp plate 1 and the lower clamp plate 2 have a certain fixing effect on the storage container 4.
The through hole 3 on the lower clamping plate 2 is equal to or slightly larger than the opening of the storage container 4, and the object leaking hole 6 is also equal to or slightly larger than the through hole 3, so as to ensure that the object to be thrown in the storage container 4 can be smoothly thrown out.
When the object is thrown, the steering engine 7 drives the rotating plate 5 to rotate, the object leaking hole 6 in the rotating plate 5 is aligned to one through hole 3, the object to be thrown in the storage container 4 corresponding to the through hole 3 is thrown out, the rotating plate 5 continuously rotates, and when the object to be thrown is aligned to the next through hole 3, the object to be thrown is continuously thrown out, so that continuous throwing is formed.
The upper clamping plate 1, the lower clamping plate 2 and the rotating plate 5 are all circular plates, the steering engine 7 and the rotating shaft 8 are arranged at the centers of the lower clamping plate 2 and the rotating plate, and the centers of the through holes 3 and the lower clamping plate 2 are uniformly distributed as the circle center.
Because the rotating plate 5 needs to rotate when in use, the rotating track is circular, and therefore, the rotating plate is arranged to be circular in structure, and is convenient to produce, manufacture, disassemble and assemble.
The edge of rotor plate 5 is equipped with a plurality of evenly distributed's spout 9, and the notch of spout 9 is located towards the center of rotor plate 5, and spout 9 lock joint is in the edge of lower plate 2.
The rotor plate 5 is rotatory in the below of lower plate 2, in order to improve the stability of rotor plate 5, links together rotor plate 5 and lower plate 2 through spout 9, and when rotor plate 5 rotated, spout 9 rotated along the edge of lower plate 2, and the effort of avoiding rotor plate 5 to produce all uses on rotation axis 8, makes overall structure more stable.
The novel clamping device is characterized in that a connecting piece 10 is arranged at the top of the upper clamping plate 1, one end of the connecting piece 10 is fixedly connected with the upper clamping plate 1, and the connecting piece 10 is provided with a connecting hole.
Whole jettison device is connected to unmanned aerial vehicle's frame through connecting piece 10 on, sets up a plurality of connecting pieces 10 at the top of punch holder 1, wherein, is equipped with the connecting hole on connecting piece 10, is connected with unmanned aerial vehicle's frame through the connecting hole, and then when making unmanned aerial vehicle flight, jettison device can combine as an organic wholely with the frame, and jettison device can not receive the influence of external world and unmanned aerial vehicle screw etc..
The upper and lower clamping plates 1 and 2 are connected by bolts 11. The bolt 11 is adopted for connecting and dismounting, and meanwhile, the distance between the bolt and the container is adjustable, so that the universality of the throwing device is improved, and the throwing device is suitable for the use of the storage containers 4 with different heights.
Preferably, the steering engine 7 is a 360 ° steering engine. The through hole 3 and the leakage hole 6 are both round holes. The through holes 3 are generally circular holes, but may be holes of other shapes according to the requirement of an actual parabola.
Example 2
A controller of an unmanned aerial vehicle continuous throwing device comprises a remote control end and a receiving end, wherein the remote control end comprises a control button, the control button is connected with a first processor, and the first processor is connected with a transmitting module;
the receiving terminal includes receiving module, and receiving module is connected with the second treater, and the steering wheel 7 of the continuous jettison device of unmanned aerial vehicle in embodiment 1 is connected to the second treater.
Preferably, the first processor and the second processor are STC15W408AS single-chip microcomputer. The transmitting module is a 2.4G radio frequency module.
During the specific use, be connected this continuous casting device and unmanned aerial vehicle's frame through connecting piece 10, place in storing container 4 and treat the parabola, unmanned aerial vehicle takes off the back, through control button operation unmanned aerial vehicle's flight orbit and parabolic opening, unmanned aerial vehicle begins to throw the thing after flying to the assigned position, and the emission module sends the instruction, and receiving module receives the instruction, second treater control steering wheel 7's rotation angle.
The rotating plate 5 rotates under the driving of the steering engine 7, the object leakage hole 6 in the steering engine 7 is aligned to one through hole 3, objects to be thrown in the storage container 4 at the through hole 3 fall down through the object leakage hole 6, and then the rotating plate 5 continuously rotates to continuously throw out the rest objects to be thrown one by one.
The technical principle of the present invention is described above in connection with specific embodiments. The description is made for the purpose of illustrating the principles of the invention and should not be construed in any way as limiting the scope of the invention. Based on the explanations herein, those skilled in the art will be able to conceive of other embodiments of the present invention without inventive effort, which would fall within the scope of the present invention.
Claims (7)
1. The continuous throwing device of the unmanned aerial vehicle is characterized by comprising an upper clamping plate (1) and a lower clamping plate (2), wherein the upper clamping plate (1) is fixedly connected with the lower clamping plate (2), a plurality of through holes (3) are formed in the lower clamping plate (2), the through holes (3) are circumferentially distributed, a plurality of storage containers (4) are arranged between the upper clamping plate (1) and the lower clamping plate (2), openings are formed in the bottom ends of the storage containers (4), and the openings are opposite to the through holes (3);
a rotating plate (5) is arranged on one side, away from the upper clamping plate (1), of the lower clamping plate (2), the rotating plate (5) is parallel to the lower clamping plate (2), an object leaking hole (6) is formed in the rotating plate (5), the object leaking hole (6) is not smaller than the through hole (3), the rotating plate (5) is connected with a driving device, the driving device comprises a steering engine (7), the steering engine (7) is arranged on the lower clamping plate (2), the steering engine (7) is connected with a rotating shaft (8), the rotating shaft (8) is connected with the rotating plate (5), and the rotating track of the center of the object leaking hole (6) and the circle formed by the centers of the through holes (3) are overlapped;
a plurality of uniformly distributed sliding grooves (9) are formed in the edge of the rotating plate (5), the notches of the sliding grooves (9) face the center of the rotating plate (5), and the sliding grooves (9) are buckled on the edge of the lower clamping plate (2);
the upper clamping plate (1) and the lower clamping plate (2) are detachably connected through a bolt (11), so that the distance between the upper clamping plate (1) and the lower clamping plate (2) is adjustable, and the storage containers with different heights can be accommodated;
the upper plate (1), the lower plate (2) and the rotating plate (5) are circular plates, the steering engine (7) and the rotating shaft (8) are arranged at the centers of the lower plate (2) and the rotating plate (5), and the through holes (3) are uniformly distributed around the center of the lower plate (2).
2. The continuous throwing device of unmanned aerial vehicle according to claim 1, wherein a connecting piece (10) is arranged at the top of the upper clamping plate (1), one end of the connecting piece (10) is fixedly connected with the upper clamping plate (1), and the connecting piece (10) is provided with a connecting hole.
3. The continuous casting device of unmanned aerial vehicle according to claim 1, wherein the steering engine (7) is a 360 ° steering engine.
4. The continuous throwing device of unmanned aerial vehicle according to claim 1, wherein the through hole (3) and the object leaking hole (6) are both circular holes.
5. The continuous unmanned aerial vehicle throwing device of claim 1, further comprising a controller, wherein the controller comprises a remote control end and a receiving end, the remote control end comprises a control button, the control button is connected with a first processor, and the first processor is connected with a transmitting module;
the receiving end comprises a receiving module, the receiving module is connected with a second processor, and the second processor is connected with the steering engine.
6. The continuous casting apparatus of claim 5, wherein the first processor and the second processor are STC15W408AS single-chip microcomputer.
7. The continuous throwing device of unmanned aerial vehicle of claim 5 wherein the transmitting module is a 2.4G radio frequency module.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201610860865.4A CN106335640B (en) | 2016-09-28 | 2016-09-28 | Unmanned aerial vehicle continuous throwing device and controller |
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| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201610860865.4A CN106335640B (en) | 2016-09-28 | 2016-09-28 | Unmanned aerial vehicle continuous throwing device and controller |
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| Publication Number | Publication Date |
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| CN106335640A CN106335640A (en) | 2017-01-18 |
| CN106335640B true CN106335640B (en) | 2021-04-09 |
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| CN201610860865.4A Active CN106335640B (en) | 2016-09-28 | 2016-09-28 | Unmanned aerial vehicle continuous throwing device and controller |
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| CN107600413B (en) * | 2017-09-08 | 2019-12-31 | 厦门大学 | Multi-cabin type microminiature container type four-rotor transportation unmanned aerial vehicle |
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| CN110239717B (en) * | 2019-07-23 | 2024-05-07 | 安徽天路航空科技股份有限公司 | Cabin type article throwing device in aircraft |
| CN110510120A (en) * | 2019-09-29 | 2019-11-29 | 长沙幻飞科技有限公司 | A kind of continuous saving casting device |
| CN111025984B (en) * | 2019-12-23 | 2021-02-26 | 中国科学院光电研究院 | Near space ball carries control device that jettisonings |
| CN111650169A (en) * | 2020-06-28 | 2020-09-11 | 吉林大学 | Fluorescent copper ion sensor based on fracture activity deoxyribozyme |
| CN112607031B (en) * | 2020-12-22 | 2022-02-22 | 西安羚控电子科技有限公司 | Modular unmanned aerial vehicle cluster aerial rapid delivery system |
| CN112960116A (en) * | 2021-01-27 | 2021-06-15 | 湖南迈克森伟电子科技有限公司 | Aerial material delivery platform of close-range unmanned aerial vehicle |
| CN113511337B (en) * | 2021-05-20 | 2023-07-18 | 华南理工大学 | Multi-material transportation aircraft and control method thereof |
| CN113525686A (en) * | 2021-07-20 | 2021-10-22 | 三明学院 | Unmanned aerial vehicle and throwing device thereof |
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| CN205381403U (en) * | 2016-01-19 | 2016-07-13 | 北京象限空间科技有限公司 | Device is put in to centre gripping |
| CN205454519U (en) * | 2016-01-27 | 2016-08-17 | 珠海市皓翔飞行器有限公司 | Material device is spilt in special seeding of unmanned aerial vehicle |
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2016
- 2016-09-28 CN CN201610860865.4A patent/CN106335640B/en active Active
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| CN204452941U (en) * | 2014-12-30 | 2015-07-08 | 王洪洋 | A kind of simple and fast delivery device for model plane load-carrying air-drop |
| CN105173083A (en) * | 2015-07-31 | 2015-12-23 | 北京邮电大学 | Dropping device for rotor craft |
| CN205044969U (en) * | 2015-09-21 | 2016-02-24 | 温州乐享科技信息有限公司 | Device is put in to unmanned aerial vehicle fire extinguishing bomb |
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