CN105173083A - Dropping device for rotor craft - Google Patents
Dropping device for rotor craft Download PDFInfo
- Publication number
- CN105173083A CN105173083A CN201510463277.2A CN201510463277A CN105173083A CN 105173083 A CN105173083 A CN 105173083A CN 201510463277 A CN201510463277 A CN 201510463277A CN 105173083 A CN105173083 A CN 105173083A
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- shell
- rotary table
- inner rotary
- dropping
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Abstract
The invention discloses a dropping device for a rotor craft. The dropping device for the rotor craft comprises a dropping bin body, a fixed support, a motor and a dropping hole. The dropping bin body comprises a shell and an inner rotary table. A sighting device composed of a camera and a laser generator is mounted on the shell. The shell is cylindrical on the whole. The fixed support is mounted on a craft underframe. The shell is kept relatively static during working, and the shell and the inner rotary table are kept concentric. The dropping hole with the diameter being slightly larger than that of a carrying hole of the inner rotary table is distributed in the lower portion of the shell. The laser generator is mounted in the middle of the circle center of the lower bottom surface of the cylindrical shell. The dropping device for the rotor craft is small in size, low in manufacturing cost, capable of being dismounted and mounted conveniently and rapidly, convenient to maintain, capable of carrying a large number of articles, good in safety and stability and capable of achieving accurate air dropping; a large number of dropping devices can be prepared in actual use, unmanned aerial vehicle can move back and forth repeatedly, efficiency is improved, and cost is reduced.
Description
Technical field
The present invention relates to a kind of delivery device, especially relate to a kind of and the matching used sensor delivery device of rotor craft.
Background technology
Unmanned vehicle (UAV) autonomous flight technology is the focus of aviation field research for many years always, and there is a large amount of demands in actual applications, such as: scout and rescue mission, science data are collected, geology, forestry exploration, control of agricultural pest, and video monitoring, production of film and TV etc.Complete above-mentioned task by unmanned vehicle greatly to reduce costs and improve personal security guarantee.The major advantage of unmanned vehicle comprises: system low cost of manufacture, and when executing the task, personnel injure little, has excellent handling and alerting ability etc.Rotary aircraft take off because of it and the requisite space that lands less, handling higher under the intensive environment of obstacle, and the advantage that attitude of flight vehicle hold facility is stronger, all have wide practical use in civilian and military field.And rotary aircraft is compared with Fixed Wing AirVehicle, its advantage also comprises: aircraft takeoff is few with landing requisite space, and the controllability under the intensive environment of obstacle is strong, and attitude of flight vehicle hold facility is high.Small-sized quadrotor, compared with other aircraft, it is advantageous that physical construction is simple, and only can need be realized by the rotating speed changing four motors controlling, and flight maneuver ability is more flexible.On the other hand, small-sized quadrotor has higher handling, and has and take off in small area, spirals, flight, the ability of landing.Aircraft can fly to from target more close to region, and can not closely near target due to its huge single rotor unlike conventional helicopters.Meanwhile, the research of small-sized four rotor wing unmanned aerial vehicles is also for the control fusion of the numerous areas such as automatic control, wireless sensor networks and computer science provides a platform.In the Based Intelligent Control of robot, three-dimensional path planning, the aspects such as the air traffic control of multi-aircraft and collision avoidance, small-sized quadrotor autonomous flight technology all has larger advantage.
Due to traditional air-drop mechanism have that weight is large, carrying capacity is little, cannot the shortcoming such as timesharing air-drop, precision be low.How to research and develop a kind of dropping gear being more applicable to rotor craft carry, make it have that light, timesharing is thrown in, easy to assemble, precision high, and meet and scout and rescue mission, science data are collected, geology, forestry exploration, control of agricultural pest, and video monitoring, the ability of the demands such as production of film and TV has become the problem that current industry is extremely paid close attention to.
Summary of the invention
The present invention researches and develops in view of the foregoing, object be to provide a kind of build light, easy to assemble, can timesharing input, rotor craft sensor delivery device that precision is high.
For achieving the above object, rotor craft sensor delivery device of the present invention comprises throws in storehouse body, fixed support, motor, throw thing hole, throw in storehouse body and comprise shell and inner rotary table, inner rotary table comprises loading hole, shell is provided with back sight, back sight is made up of camera and laser generator, housing integration is cylindrical, fixed support stretches out shell both sides and punches, fixed support is arranged on aircraft underframe by screw, shell operationally keeps geo-stationary, shell is connected with bearing with inner rotary table rotating shaft, shell and inner rotary table is made to keep with one heart, thing hole is thrown in outer casing underpart distribution one, the bore dia throwing thing hole is more bigger than inner rotary table loading hole, in the middle part of the bottom surface center of circle of cylinder blanket, laser generator is installed, the scattering principle of laser is utilized to carry out throwing the calibration of thing, camera is installed on laser generator side, by the image transmission of back sight to ground controller.Shell and inner rotary table material are carbon fibre, are wherein also provided with hole in the middle part of inner rotary table, for installing rotating shaft, rotating shaft by coupler be fixed on carry-on motor and be connected.
Preferably, utilize jackscrew to be connected with rotating shaft by inner rotary table, during work, driven by motor rotating shaft rotates, and inner rotary table keeps and motor same rotational speed, thus contained object is rotated in company with inner rotary table, and launches from the throwing thing hole of shell.
Preferably, the equidistant branch in inner rotary table outer ring 4,6 or 8 loading holes, for loading the object of needs input and completing input.
Preferably, this delivery device is for throwing in scientific research, agricultural, the sensor of detection or living material.
Preferably, rotor craft operationally, by ground remote control device, control the input of the rising and falling of aircraft, flight attitude and sensor, on unmanned plane body, controlling the motion of unmanned plane by controlling brushless motor, ground remote control device reserving a passage and controls unmanned plane bottom control throwing thing device.
Beneficial effect of the present invention is:
Volume of the present invention is little, cost is low, be convenient to fast assembling-disassembling, convenient for maintaining, it is many to carry loading, there is good safety, stability, and can realize dropping accurately, a large amount of delivery device can be prepared in actual use, unmanned plane can be realized and repeatedly come and go operation, improve efficiency, decrease cost.
Accompanying drawing explanation
Fig. 1 is the first block diagram of the delivery device for rotor craft of the present invention.
Fig. 2 is the second block diagram of the delivery device for rotor craft of the present invention.
Fig. 3 is the delivery device birds-eye view for rotor craft of the present invention.
Fig. 4 is the delivery device front view for rotor craft of the present invention.
Fig. 5 is the inner rotary table block diagram of the delivery device for rotor craft of the present invention.
Number in the figure: 1. throw in storehouse body, 2. fixed support, 3. motor, 4. throwing thing hole, 5. shell, 6. inner rotary table, 7. loading hole, 8. back sight.
Detailed description of the invention
Below in conjunction with the drawings and the specific embodiments, the present invention will be further described.
See accompanying drawing 1-5, for the delivery device of rotor craft, comprise and throw in storehouse body 1, fixed support 2, motor 3, throw thing hole 4, throw in storehouse body 1 and comprise shell 5 and inner rotary table 6, inner rotary table comprises loading hole 7, shell 5 is provided with back sight 8, back sight 8 is made up of camera and laser generator, shell 5 entirety is cylindrical, fixed support 2 stretches out shell both sides and punches, fixed support is arranged on aircraft underframe by screw, shell 5 operationally keeps geo-stationary, shell 5 is connected with bearing with rotating shaft with inner rotary table 6, shell 5 and inner rotary table 6 is made to keep concentric, thing hole 4 is thrown in shell 5 bottom distribution one, the bore dia throwing thing hole 4 is more bigger than inner rotary table loading hole 7, in the middle part of the bottom surface center of circle of cylinder blanket 5, laser generator is installed, the scattering principle of laser is utilized to carry out throwing the calibration of thing, camera is installed on laser generator side, by the image transmission of back sight 8 to ground controller.
Shell 5 and inner rotary table 6 material are carbon fibre, are wherein also provided with hole in the middle part of inner rotary table 6, for installing rotating shaft, rotating shaft by coupler be fixed on carry-on motor and be connected 3.
Utilize jackscrew to be connected with rotating shaft by inner rotary table, during work, driven by motor rotating shaft rotates, and inner rotary table keeps and motor same rotational speed, thus contained object is rotated in company with inner rotary table, and launches from the throwing thing hole of shell.
The equidistant branch in inner rotary table 5 outer ring 4,6 or 8 loading holes 7, for loading the object of needs input and completing input.
This delivery device is for throwing in scientific research, agricultural, the sensor of detection or living material.
Rotor craft operationally, by ground remote control device, control the input of the rising and falling of aircraft, flight attitude and sensor, on aircraft body, controlling the motion of aircraft by controlling brushless motor, ground controller reserving a passage and controls unmanned plane bottom control throwing thing device.The sensor that first objects such as loading scientific research, agricultural, detection in inner rotary table will be used, is loaded shell afterwards, and connects inner rotary table with rotating shaft, be fixed on aircraft underframe by shell by hand tighten screw by inner rotary table.Unmanned plane flies to objective afterwards, and back sight is assigned after roughly aiming at the place will throwing thing and thrown thing instruction.After assigning the instruction of throwing thing, the electric machine rotation of unmanned plane underframe, the inner rotary table hole of loading sensor is gone to the throwing thing hole of shell it, sensor will fall to objective by Action of Gravity Field afterwards, in like manner cast other sensor successively, after sensor is all cast, all sensors completes MANET and aircraft makes a return voyage after terminal carries out communication.If also have next group sensor to need to throw in, hand tighten screw rapid removal can be utilized to throw thing device, change another and throw thing device or in inner rotary table, insert new sensor, just can realize repeatedly coming and going operation.
The practicality of this delivery device is described below by simulation environment
Example 1, at volcano, marsh, crag etc. concerning very rugged environment the mankind, people self may be difficult to arrive at, or have for personal safety after arriving at and to threaten or harmful.Therefore be difficult to obtain scientific research accurately, detection data, at this moment just can carry carry delivery device under unmanned plane, sensor is placed in inner rotary table, and sensor is thrown in appropriate place, obtain scientific data accurately.
Example 2, at generation tsunami, earthquake, after the disasteies such as big fire, ground base station is serious, when traffic severe paralysis, the disaster-stricken situation in disaster area and the information such as article of relieving the people in stricken areas of urgent need are difficult to outwardly pass on, and have the factors such as aftershock and can threaten to the safety of personnel, at this moment this device can be used to load the communication apparatus such as satellite phone, and by the moving camera on unmanned plane, first-class imaging device of making a video recording search disaster affected people, communication device is sent in time in disaster affected people hand, they can be contacted with extraneous generation in time, react disaster-stricken situation, thus make accurately, correct reaction and Disaster Relief Measures.
Claims (4)
1. the delivery device for rotor craft, comprise and throw in storehouse body (1), fixed support (2), motor (3), throw thing hole (4), it is characterized in that: throw in storehouse body and comprise shell (5) and inner rotary table (6), inner rotary table comprises loading hole (7), shell (5) is provided with back sight (8), back sight (8) is made up of camera and laser generator, shell (5) entirety is cylindrical, fixed support (2) stretches out shell both sides and punches, fixed support is arranged on aircraft underframe by screw, shell (5) operationally keeps geo-stationary, shell (5) is connected with bearing with rotating shaft with inner rotary table (6), shell (5) and inner rotary table (6) is made to keep with one heart, thing hole (4) is thrown in shell (5) bottom distribution one, the bore dia throwing thing hole (4) is more bigger than inner rotary table loading hole (7), in the middle part of the bottom surface center of circle of cylinder blanket (5), laser generator is installed, the scattering principle of laser is utilized to carry out throwing the calibration of thing, camera is installed on laser generator side, by the image transmission of back sight (8) to ground controller, shell (5) and inner rotary table (6) material are carbon fibre, wherein inner rotary table (6) middle part is also provided with hole, for installing rotating shaft, rotating shaft by coupler be fixed on carry-on motor and be connected (3).
2. delivery device according to claim 1, it is characterized in that: utilize jackscrew to be connected with rotating shaft by inner rotary table, during work, driven by motor rotating shaft rotates, and inner rotary table keeps and motor same rotational speed, thus contained object is rotated in company with inner rotary table, and launch from the throwing thing hole of shell.
3. delivery device according to claim 1, is characterized in that: the equidistant branch in inner rotary table (6) outer ring 4,6 or 8 loading holes (7), for loading the object of needs input and completing input.
4. delivery device according to claim 1, is characterized in that: this delivery device is for throwing in scientific research, agricultural, the sensor of detection or living material.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201510463277.2A CN105173083A (en) | 2015-07-31 | 2015-07-31 | Dropping device for rotor craft |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201510463277.2A CN105173083A (en) | 2015-07-31 | 2015-07-31 | Dropping device for rotor craft |
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| CN105173083A true CN105173083A (en) | 2015-12-23 |
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| CN201510463277.2A Pending CN105173083A (en) | 2015-07-31 | 2015-07-31 | Dropping device for rotor craft |
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| CN105569735A (en) * | 2016-02-25 | 2016-05-11 | 中国矿业大学(北京) | Underground robot communication control system based on Wifi |
| CN105629787A (en) * | 2016-01-09 | 2016-06-01 | 江西新明机械有限公司 | Sound source device automatic dispenser |
| CN105682108A (en) * | 2016-02-25 | 2016-06-15 | 中国矿业大学(北京) | Underground robot communication control system based on wireless sensor network |
| CN106240818A (en) * | 2016-08-22 | 2016-12-21 | 南京理工大学 | Unmanned plane grabs thing device |
| CN106335640A (en) * | 2016-09-28 | 2017-01-18 | 中科新松有限公司 | Unmanned aerial vehicle based continuous dropping device and controller |
| CN106332858A (en) * | 2016-02-03 | 2017-01-18 | 曹萍 | Automatic throwing device |
| CN106364675A (en) * | 2016-07-27 | 2017-02-01 | 曹萍 | Sphere release device |
| CN106516116A (en) * | 2016-09-26 | 2017-03-22 | 江苏大学 | Natural enemy release device used for aircraft |
| CN106643293A (en) * | 2016-05-24 | 2017-05-10 | 李宁 | Wheel type automatic launching device for guided missile and other weapons |
| CN106628182A (en) * | 2016-12-08 | 2017-05-10 | 中国科学院长春光学精密机械与物理研究所 | Automatic feeding cylinder device |
| CN107140212A (en) * | 2017-05-22 | 2017-09-08 | 中国原子能科学研究院 | A kind of throwing device on unmanned vehicle |
| CN107426739A (en) * | 2017-08-19 | 2017-12-01 | 中国矿业大学 | A kind of delivery device and its method of mine detecting airplane wireless communication node |
| CN107600413A (en) * | 2017-09-08 | 2018-01-19 | 厦门大学 | The rotor of multi-chamber microminiature container-type four transports unmanned plane |
| CN108007276A (en) * | 2017-10-27 | 2018-05-08 | 哈尔滨理工大学 | A kind of novel air drops a bomb automatic Land mine removing apparatus |
| CN108377977A (en) * | 2018-03-07 | 2018-08-10 | 华南农业大学 | A kind of optical frequency formula mosquito dispenser based on unmanned plane |
| CN108583891A (en) * | 2018-05-24 | 2018-09-28 | 安徽工程大学 | A kind of fire extinguisher bomb delivery device in multi-rotor unmanned aerial vehicle |
| CN109229410A (en) * | 2018-10-23 | 2019-01-18 | 西北工业大学 | A kind of rotary unmanned plane air-launching method and device |
| CN109292093A (en) * | 2018-11-16 | 2019-02-01 | 中国气象局气象探测中心 | A kind of drum-type Dropsonde instrument catapult-launching gear and sonde put-on method |
| CN109533334A (en) * | 2018-12-29 | 2019-03-29 | 成都紫瑞青云航空宇航技术有限公司 | Launch sensor conveying device and application method in high-altitude |
| CN109573039A (en) * | 2019-01-23 | 2019-04-05 | 沈阳金丰春航空科技有限公司 | It is a kind of for launching the jettison system of honeycomb |
| CN109573485A (en) * | 2018-12-29 | 2019-04-05 | 成都紫瑞青云航空宇航技术有限公司 | Launch sensor conveying mechanism and application method in high-altitude |
| CN109625278A (en) * | 2018-12-27 | 2019-04-16 | 中国科学院长春光学精密机械与物理研究所 | A kind of unmanned aerial vehicle ejecting device |
| CN109649656A (en) * | 2019-01-25 | 2019-04-19 | 华南农业大学 | A kind of mosquito delivery device and unmanned plane |
| CN109677610A (en) * | 2018-12-29 | 2019-04-26 | 成都紫瑞青云航空宇航技术有限公司 | Launch sensing system and application method in high-altitude |
| CN109747830A (en) * | 2018-12-27 | 2019-05-14 | 中国航空工业集团公司西安飞机设计研究所 | A kind of single group wheel link-type unmanned plane delivery device and put-on method |
| CN109987227A (en) * | 2017-12-30 | 2019-07-09 | 广州刀锋智能科技有限公司 | A kind of goods and materials jettison system based on unmanned plane |
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| CN105629787A (en) * | 2016-01-09 | 2016-06-01 | 江西新明机械有限公司 | Sound source device automatic dispenser |
| CN105629787B (en) * | 2016-01-09 | 2018-07-17 | 江西新明机械有限公司 | A kind of sonic source device automatic feeder |
| CN106332858A (en) * | 2016-02-03 | 2017-01-18 | 曹萍 | Automatic throwing device |
| CN105682108A (en) * | 2016-02-25 | 2016-06-15 | 中国矿业大学(北京) | Underground robot communication control system based on wireless sensor network |
| CN105569735A (en) * | 2016-02-25 | 2016-05-11 | 中国矿业大学(北京) | Underground robot communication control system based on Wifi |
| CN106643293A (en) * | 2016-05-24 | 2017-05-10 | 李宁 | Wheel type automatic launching device for guided missile and other weapons |
| CN106364675B (en) * | 2016-07-27 | 2018-12-14 | 曹萍 | A kind of ball-throwing apparatus |
| CN106364675A (en) * | 2016-07-27 | 2017-02-01 | 曹萍 | Sphere release device |
| CN106240818A (en) * | 2016-08-22 | 2016-12-21 | 南京理工大学 | Unmanned plane grabs thing device |
| CN106240818B (en) * | 2016-08-22 | 2018-06-26 | 南京理工大学 | Unmanned plane grabs object device |
| CN106516116A (en) * | 2016-09-26 | 2017-03-22 | 江苏大学 | Natural enemy release device used for aircraft |
| CN106335640B (en) * | 2016-09-28 | 2021-04-09 | 中科新松有限公司 | Unmanned aerial vehicle continuous throwing device and controller |
| CN106335640A (en) * | 2016-09-28 | 2017-01-18 | 中科新松有限公司 | Unmanned aerial vehicle based continuous dropping device and controller |
| CN106628182A (en) * | 2016-12-08 | 2017-05-10 | 中国科学院长春光学精密机械与物理研究所 | Automatic feeding cylinder device |
| CN107140212A (en) * | 2017-05-22 | 2017-09-08 | 中国原子能科学研究院 | A kind of throwing device on unmanned vehicle |
| CN107140212B (en) * | 2017-05-22 | 2024-02-20 | 中国原子能科学研究院 | Throwing device on unmanned vehicles |
| CN107426739A (en) * | 2017-08-19 | 2017-12-01 | 中国矿业大学 | A kind of delivery device and its method of mine detecting airplane wireless communication node |
| CN107600413A (en) * | 2017-09-08 | 2018-01-19 | 厦门大学 | The rotor of multi-chamber microminiature container-type four transports unmanned plane |
| CN108007276A (en) * | 2017-10-27 | 2018-05-08 | 哈尔滨理工大学 | A kind of novel air drops a bomb automatic Land mine removing apparatus |
| CN109987227A (en) * | 2017-12-30 | 2019-07-09 | 广州刀锋智能科技有限公司 | A kind of goods and materials jettison system based on unmanned plane |
| CN108377977A (en) * | 2018-03-07 | 2018-08-10 | 华南农业大学 | A kind of optical frequency formula mosquito dispenser based on unmanned plane |
| CN108377977B (en) * | 2018-03-07 | 2023-05-19 | 华南农业大学 | Unmanned aerial vehicle-based optical frequency type mosquito dispenser |
| CN108583891A (en) * | 2018-05-24 | 2018-09-28 | 安徽工程大学 | A kind of fire extinguisher bomb delivery device in multi-rotor unmanned aerial vehicle |
| CN109229410A (en) * | 2018-10-23 | 2019-01-18 | 西北工业大学 | A kind of rotary unmanned plane air-launching method and device |
| CN109292093A (en) * | 2018-11-16 | 2019-02-01 | 中国气象局气象探测中心 | A kind of drum-type Dropsonde instrument catapult-launching gear and sonde put-on method |
| CN109747830A (en) * | 2018-12-27 | 2019-05-14 | 中国航空工业集团公司西安飞机设计研究所 | A kind of single group wheel link-type unmanned plane delivery device and put-on method |
| CN109625278A (en) * | 2018-12-27 | 2019-04-16 | 中国科学院长春光学精密机械与物理研究所 | A kind of unmanned aerial vehicle ejecting device |
| CN109747830B (en) * | 2018-12-27 | 2022-04-19 | 中国航空工业集团公司西安飞机设计研究所 | Single-group wheel connecting rod type unmanned aerial vehicle throwing device and throwing method |
| CN109533334A (en) * | 2018-12-29 | 2019-03-29 | 成都紫瑞青云航空宇航技术有限公司 | Launch sensor conveying device and application method in high-altitude |
| CN109677610A (en) * | 2018-12-29 | 2019-04-26 | 成都紫瑞青云航空宇航技术有限公司 | Launch sensing system and application method in high-altitude |
| CN109573485B (en) * | 2018-12-29 | 2020-12-29 | 成都紫瑞青云航空宇航技术有限公司 | High-altitude drop sensor conveying mechanism and using method |
| CN109573485A (en) * | 2018-12-29 | 2019-04-05 | 成都紫瑞青云航空宇航技术有限公司 | Launch sensor conveying mechanism and application method in high-altitude |
| CN109573039A (en) * | 2019-01-23 | 2019-04-05 | 沈阳金丰春航空科技有限公司 | It is a kind of for launching the jettison system of honeycomb |
| CN109649656A (en) * | 2019-01-25 | 2019-04-19 | 华南农业大学 | A kind of mosquito delivery device and unmanned plane |
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| CN113511337A (en) * | 2021-05-20 | 2021-10-19 | 华南理工大学 | Multi-material transportation aircraft and control method thereof |
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