CN107963217A - Carry the small drone of parcel delivery device - Google Patents
Carry the small drone of parcel delivery device Download PDFInfo
- Publication number
- CN107963217A CN107963217A CN201711378876.XA CN201711378876A CN107963217A CN 107963217 A CN107963217 A CN 107963217A CN 201711378876 A CN201711378876 A CN 201711378876A CN 107963217 A CN107963217 A CN 107963217A
- Authority
- CN
- China
- Prior art keywords
- gas
- motor
- arranging box
- charging connection
- unmanned plane
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
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Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C39/00—Aircraft not otherwise provided for
- B64C39/02—Aircraft not otherwise provided for characterised by special use
- B64C39/024—Aircraft not otherwise provided for characterised by special use of the remote controlled vehicle type, i.e. RPV
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENTS 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
- B64D1/08—Dropping, ejecting, or releasing articles the articles being load-carrying devices
- B64D1/12—Releasing
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENTS 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
- B64D1/08—Dropping, ejecting, or releasing articles the articles being load-carrying devices
- B64D1/14—Absorbing landing shocks
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U2101/00—UAVs specially adapted for particular uses or applications
- B64U2101/60—UAVs specially adapted for particular uses or applications for transporting passengers; for transporting goods other than weapons
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U2201/00—UAVs characterised by their flight controls
- B64U2201/20—Remote controls
Abstract
The small drone of parcel delivery device is carried, belongs to unmanned air vehicle technique field, including unmanned plane body and parcel delivery device；Wrapping up delivery device includes wireless remote control module, wireless communication module, GPS positioning module, arranging box A, arranging box B, supporting plate, swivel plate, motor A, parcel buffer gear and control chip；Parcel buffer gear includes air accumulator, electromagnetic gas valve, air bag, gas-charging connection B, gas-charging connection A, gas flowmeter and reciprocal drive component；Control chip is electrically connected with wireless communication module, GPS positioning module, electromagnetic gas valve, motor A and motor B.The present invention, which can carry cargo and fly to, appointed place and to be launched, and can be applied to disaster area disaster relief work, its is simple in structure compact, easy to control, reliable and stable.
Description
Technical field
The present invention relates to unmanned air vehicle technique field, particularly a kind of small drone for carrying parcel delivery device.
Background technology
Referred to as " unmanned plane ", english abbreviation is " UAV " to UAV, using radio robot and is provided for oneself
The not manned aircraft that presetting apparatus manipulates.It can be divided into from technical standpoint definition：Unmanned fixed-wing aircraft, unmanned VTOL
Machine, unmanned airship, unmanned helicopter, unmanned multi-rotor aerocraft, unmanned parasol etc..Unmanned plane presses application field, can be divided into
It is military with it is civilian.Military aspect, unmanned plane are divided into reconnaissance plane and target drone.Civilian aspect, unmanned plane+sector application, is unmanned plane
Really just need；At present take photo by plane, agricultural, plant protection, self-timer, express transportation, disaster relief, observation wild animal, monitoring infect
The application in disease, mapping, news report, electric inspection process, the disaster relief, movies-making, manufacture romance etc. field, has greatly expanded nothing
The man-machine purposes of itself, developed country is also in actively extension sector application and development unmanned air vehicle technique.Unmanned plane is most early in 20 generation
Record and occur the twenties, the World War I just carries out like a raging fire within 1914, and the card Dare and Pi Qieer two of Britain will
Army, a suggestion is proposed to military aviation association of Britain：Develop a kind of not employment to drive, and flown with the small-sized of radio control
Machine, enables it to fly to a certain target area overhead of enemy, and the bombs sway in advance on flivver is gone.This bold sets
Want to be instantly available Britain's military aviation association president at that time and wear Martin Henderson jazz appreciation.He specifies and is led by A.M. Lip rivers professor
Members of a squad horse is developed.Unmanned plane was used as the target drone trained at that time.It is that many countries are used to describe most
The term of UAV of new generation.From literal, this term can be described from kite, and drone, is arrived
The cruise missile that V-1 fly bombs come from development, but reusable heavier-than-air flight is only limitted in the term of the military
Device.
With developing rapidly for science and technology, unmanned plane is gradually applied in the rescue work of geological disaster, how to utilize nobody
The medicine and food that the disaster area air-drop masses that machine is difficult to arrive in the short time to disaster assistance personnel are badly in need of become one it is non-often with
There is the problem of research significance, at present, have no has the function of the aircraft of fixed point air-drop parcel on the market.
The content of the invention
The purpose of the present invention is overcome the deficiencies in the prior art, and provide a kind of miniature self-service for carrying parcel delivery device
Machine, it provides one kind and can be applicable in the rescue work of disaster area, can remote control fixed point air-drop parcel aircraft.
The technical scheme is that：Carry the small drone of parcel delivery device, including unmanned plane body；It is also wrapped
Include parcel delivery device；Wrap up delivery device include wireless remote control module, wireless communication module, GPS positioning module, arranging box A,
Arranging box B, supporting plate, swivel plate, motor A, parcel buffer gear and control chip；
Wireless communication module is installed on unmanned plane body, it is connected with wireless remote control module telecommunication；
GPS positioning module is installed on unmanned plane body；
Arranging box A is fixedly mounted on unmanned plane body lower end, its lower end is open；
Arranging box B is fixed on the lateral wall of arranging box A；
Supporting plate is fixed on swivel plate, and it is open that it is used to open or close the lower end of lower end arranging box A；
Swivel plate is fixed on the arbor of motor A；
Motor A is fixed in the lower end of unmanned plane body, and the arbor of motor A, which rotates, drives swivel plate to rotate, and then drives supporting plate to turn
It is dynamic, to open or close the lower end of arranging box A opening；
Wrapping up buffer gear includes air accumulator, electromagnetic gas valve, air bag, gas-charging connection B, gas-charging connection A, gas flowmeter and reciprocal
Drive component；Air accumulator is located at the air path elements intracavitary of arranging box, which is provided with air inlet and gas outlet；The air inlet of electromagnetic gas valve
End is connected with the gas outlet of compression gas accumulator, and the gas outlet of electromagnetic gas valve is connected with gas-charging connection A；Air bag is located at arranging box
In A, and it is placed on supporting plate, which is provided with inflating port；Gas-charging connection B sealings are fixed on the inflating port of air bag and face inflation
Connector A, is equipped with check valve in it；Gas-charging connection A is associated with reciprocal drive component, and is done under the driving of reciprocal drive component past
Linear motion, and then realize and dock or separate with gas-charging connection B；Gas flowmeter is installed between electromagnetic gas valve and air accumulator
Pipeline on；
Reciprocal drive component includes motor B, leading screw, nut and clamping piece；Motor B is installed on the side wall of arranging box B inner cavities, silk
Thick stick one end is connected to by shaft coupling on the arbor of motor B, and the other end is movably arranged on by axle sleeve on the side wall of arranging box B,
Nut thread is connected on leading screw, and clamping piece one end is clamped on gas-charging connection A, and the other end is fixed with nut-welding；
Control chip is installed in arranging box A, itself and wireless communication module, GPS positioning module, electromagnetic gas valve, motor A and motor
B is electrically connected.
The present invention has the following advantages that compared with prior art：
The present invention, which can carry cargo and fly to, appointed place and to be launched, and can be applied to disaster area disaster relief work, its is simple in structure small
Ingeniously, it is easy to control, it is reliable and stable.
Below in conjunction with figure, the invention will be further described with embodiment.
Brief description of the drawings
Fig. 1 is the structure diagram when present invention carries parcel；
Fig. 2 is the structure diagram when present invention launches parcel.
Embodiment
Embodiment 1：
As shown in Figs. 1-2, the small drone of parcel delivery device, including unmanned plane body 100 and parcel delivery device are carried.
Wrapping up delivery device includes wireless remote control module, wireless communication module 1, GPS positioning module 2, arranging box A3, placement
Case B4, supporting plate 5, swivel plate 6, motor A7, parcel buffer gear and control chip.
Wireless communication module 1 is installed on unmanned plane body 100, it is connected with wireless remote control module telecommunication.
GPS positioning module 2 is installed on unmanned plane body 100.
Arranging box A3 is fixedly mounted on 100 lower end of unmanned plane body, its lower end is open.
Arranging box B4 is fixed on the lateral wall of arranging box A3.
Supporting plate 5 is fixed on swivel plate 6, and it is open that it is used to open or close the lower end of lower end arranging box A3.
Swivel plate 6 is fixed on the arbor of motor A7.
Motor A7 is fixed in the lower end of unmanned plane body 100, and the arbor of motor A7, which rotates, drives swivel plate 6 to rotate, and then
Supporting plate 5 is driven to rotate, to open or close the lower end of arranging box A3 opening.
Wrapping up buffer gear includes air accumulator 81, electromagnetic gas valve 82, air bag 83, gas-charging connection B84, gas-charging connection A85, gas
Flowmeter body 86 and reciprocal drive component.Air accumulator is located at the air path elements intracavitary of arranging box, which is provided with air inlet and outlet
Mouthful.The inlet end of electromagnetic gas valve is connected with the gas outlet of compression gas accumulator, and gas outlet and the gas-charging connection A of electromagnetic gas valve connect
It is logical.Air bag is located in arranging box A, and is placed on supporting plate, which is provided with inflating port.Gas-charging connection B sealings are fixed in air bag
Check valve is equipped with inflating port and face gas-charging connection A, in it.Gas-charging connection A is associated with reciprocal drive component, and is back and forth being driven
Linear reciprocating motion is done under the driving of dynamic component, and then is realized and is docked or separate with gas-charging connection B.Gas flowmeter is installed on electricity
On pipeline between magnetism valve and air accumulator.
Reciprocal drive component includes motor B87, leading screw 88, nut 89 and clamping piece 80.Motor B87 is installed on arranging box B4
On the side wall of inner cavity, 88 one end of leading screw is connected to by shaft coupling on the arbor of motor B87, and the other end is installed by axle sleeve activity
On the side wall of arranging box B4, nut 89 is threaded on leading screw 88, and 80 one end of clamping piece is clamped on gas-charging connection A85,
The other end is welded and fixed with nut 89.
Control chip 9 is in arranging box A3, itself and wireless communication module 1, GPS positioning module 2, electromagnetic gas valve 82, motor
A7 and motor B87 is electrically connected.
Sketch the use of the present invention：Parcel 101 is first put into arranging box A3 by operating personnel, passes through wireless remote control module control
Electromagnetic gas valve 82 processed is opened, and the gas in air accumulator 81 enters air bag 83, struts air bag 83, when gas flowmeter 86 detects
After aeration quantity reaches predetermined value, control chip 9 controls reciprocal drive component generation to act, by gas-charging connection A85 and gas-charging connection
B84 is separated, and due to being equipped with check valve in gas-charging connection B84, the gas that both are separated in rear gasbag 83 will not leak.
Destination coordinate is inputted by wireless remote control module, sends to unmanned plane body 100, wireless communication module 1 and receives
After command adapted thereto, control chip 9 is sent data to, control chip 9 is calculated according to current position coordinates and destination coordinate
Go out flight path, then control unmanned plane body 100 to fly to appointed place.After arriving at, control chip 9 controls motor A7
Arbor rotate and drive swivel plate 6 to rotate, and then drive supporting plate 5 to rotate, to open the lower end of arranging box A3 opening, air bag 83 connects
Fall and discharge together with parcel 101, from vibrations when air bag 83 protects the landing of parcel 101.
Claims (1)
1. the small drone of parcel delivery device is carried, including unmanned plane body；It further includes parcel delivery device；Parcel is thrown
Put device include wireless remote control module, wireless communication module, GPS positioning module, arranging box A, arranging box B, supporting plate, swivel plate,
Motor A, parcel buffer gear and control chip；
Wireless communication module is installed on unmanned plane body, it is connected with wireless remote control module telecommunication；
GPS positioning module is installed on unmanned plane body；
Arranging box A is fixedly mounted on unmanned plane body lower end, its lower end is open；
Arranging box B is fixed on the lateral wall of arranging box A；
Supporting plate is fixed on swivel plate, and it is open that it is used to open or close the lower end of lower end arranging box A；
Swivel plate is fixed on the arbor of motor A；
Motor A is fixed in the lower end of unmanned plane body, and the arbor of motor A, which rotates, drives swivel plate to rotate, and then drives supporting plate to turn
It is dynamic, to open or close the lower end of arranging box A opening；
Wrapping up buffer gear includes air accumulator, electromagnetic gas valve, air bag, gas-charging connection B, gas-charging connection A, gas flowmeter and reciprocal
Drive component；Air accumulator is located at the air path elements intracavitary of arranging box, which is provided with air inlet and gas outlet；The air inlet of electromagnetic gas valve
End is connected with the gas outlet of compression gas accumulator, and the gas outlet of electromagnetic gas valve is connected with gas-charging connection A；Air bag is located at arranging box
In A, and it is placed on supporting plate, which is provided with inflating port；Gas-charging connection B sealings are fixed on the inflating port of air bag and face inflation
Connector A, is equipped with check valve in it；Gas-charging connection A is associated with reciprocal drive component, and is done under the driving of reciprocal drive component past
Linear motion, and then realize and dock or separate with gas-charging connection B；Gas flowmeter is installed between electromagnetic gas valve and air accumulator
Pipeline on；
Reciprocal drive component includes motor B, leading screw, nut and clamping piece；Motor B is installed on the side wall of arranging box B inner cavities, silk
Thick stick one end is connected to by shaft coupling on the arbor of motor B, and the other end is movably arranged on by axle sleeve on the side wall of arranging box B,
Nut thread is connected on leading screw, and clamping piece one end is clamped on gas-charging connection A, and the other end is fixed with nut-welding；
Control chip is installed in arranging box A, itself and wireless communication module, GPS positioning module, electromagnetic gas valve, motor A and motor
B is electrically connected.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201711378876.XA CN107963217B (en) | 2017-12-19 | 2017-12-19 | Carry on small-size unmanned aerial vehicle who puts in device of parcel |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201711378876.XA CN107963217B (en) | 2017-12-19 | 2017-12-19 | Carry on small-size unmanned aerial vehicle who puts in device of parcel |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CN107963217A true CN107963217A (en) | 2018-04-27 |
| CN107963217B CN107963217B (en) | 2021-02-19 |
Family
ID=61995697
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201711378876.XA Active CN107963217B (en) | 2017-12-19 | 2017-12-19 | Carry on small-size unmanned aerial vehicle who puts in device of parcel |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN107963217B (en) |
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN110271670A (en) * | 2019-06-18 | 2019-09-24 | 深圳高度创新技术有限公司 | Rescue unmanned plane and its lifebuoy loading device in waters |
| US20200023972A1 (en) * | 2018-07-19 | 2020-01-23 | Arthur J. Olsen | Drone payload release assembly |
| CN112078797A (en) * | 2020-08-28 | 2020-12-15 | 重庆工程职业技术学院 | Fixed point air-drop device based on unmanned aerial vehicle |
| CN112591093A (en) * | 2020-12-24 | 2021-04-02 | 嘉创飞航(苏州)智能科技有限公司 | Air-drop type unmanned aerial vehicle based on remote positioning |
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| CN107097961A (en) * | 2017-05-12 | 2017-08-29 | 河南省酷农航空植保科技有限公司 | A kind of anti-crash unmanned plane |
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| US20130037650A1 (en) * | 2011-03-15 | 2013-02-14 | Stephen B. Heppe | Systems and Methods for Long Endurance Airship Operations |
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Cited By (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US20200023972A1 (en) * | 2018-07-19 | 2020-01-23 | Arthur J. Olsen | Drone payload release assembly |
| CN110271670A (en) * | 2019-06-18 | 2019-09-24 | 深圳高度创新技术有限公司 | Rescue unmanned plane and its lifebuoy loading device in waters |
| CN110271670B (en) * | 2019-06-18 | 2024-02-20 | 深圳高度创新技术有限公司 | Water area rescue unmanned aerial vehicle and life buoy carrying device thereof |
| CN112078797A (en) * | 2020-08-28 | 2020-12-15 | 重庆工程职业技术学院 | Fixed point air-drop device based on unmanned aerial vehicle |
| CN112591093A (en) * | 2020-12-24 | 2021-04-02 | 嘉创飞航(苏州)智能科技有限公司 | Air-drop type unmanned aerial vehicle based on remote positioning |
| CN112591093B (en) * | 2020-12-24 | 2023-07-04 | 嘉创飞航(苏州)智能科技有限公司 | Air-drop type unmanned aerial vehicle based on remote positioning |
Also Published As
| Publication number | Publication date |
|---|---|
| CN107963217B (en) | 2021-02-19 |
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