CN206155796U - Unmanned aerial vehicle freight transportation device - Google Patents
Unmanned aerial vehicle freight transportation device Download PDFInfo
- Publication number
- CN206155796U CN206155796U CN201621205831.3U CN201621205831U CN206155796U CN 206155796 U CN206155796 U CN 206155796U CN 201621205831 U CN201621205831 U CN 201621205831U CN 206155796 U CN206155796 U CN 206155796U
- Authority
- CN
- China
- Prior art keywords
- guide rail
- fixed mount
- upper bracket
- gusset
- seat
- 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.)
- Expired - Fee Related
Links
Abstract
The utility model belongs to transportation machinery especially relates to an unmanned aerial vehicle freight transportation device, the utility model discloses realize that unmanned aerial vehicle does not descend under the condition on ground, gives the addressee through wireless control's mode with the accurate air -drop of mail to the scheme that the mail handing -over is confirmed has been designed, the utility model discloses it is main including height sensor (1), controller (2), wireless transceiver (3), left mount (4), upper bracket (5), pressure spring (6), clamp plate (7), micro motor (8), right bogie (9), gyro wheel (10), parachute bag (11), transport case (12), lamp area (13).
Description
Technical field
The utility model belongs to field of transport machinery, more particularly to a kind of unmanned plane cargo instrument.
Background technology
Development and the prosperity of express transportation industry with unmanned air vehicle technique, using unmanned plane the quick throwing of Small Mail is carried out
Passing becomes the focus of electric business and express company's research, and result of the test shows：Small Mail is delivered to into some using unmanned plane inclined
Remote address, can actually save manpower and logistics cost, greatly improve and send efficiency, but when mail is transferred to into client, nothing
It is man-machine to need ground of landing, mail is voluntarily removed by addressee, then unmanned plane put back to again, two kinds of wind are there are among these
Danger, first technical risk, unmanned plane in long-range landing and take-off process, in the case where can not visually manipulate, it is aerial or
The external environmental factors such as jump area affect very big on the landing of unmanned plane, land the unstable damage that can cause unmanned plane and cannot
Go around；And unmanned plane finds under the low speed landing place and again take-off process, the consumption to electric energy is very big, causes unmanned plane
Endurance distance shorten dramatically.It two is moral hazard, unmanned plane by way of landing by mail delivery to addressee, but nothing
The programs such as man-machine return, the handing-over confirmation of mail are affected very big by the individual factor of courier or addressee, because of moral element
Produce the very risky of dispute.Based on above reason, a kind of unmanned plane cargo instrument is devised, realize that unmanned plane does not land ground
And mail is dropped to addressee, and devise the scheme that mail handing-over confirms.
The content of the invention
Based on object above, the utility model mainly includes：Height sensor 1, controller 2, wireless transceiver 3, Zuo Gu
Determine frame 4, upper bracket 5, stage clip 6, pressing plate 7, micromachine 8, right bogie 9, roller 10, landing pack 11, transport case 12, light bar
13；Wherein the structure of upper bracket 5 as shown in Figure 4 and Figure 5, including guide rail 5-1, fix bar 5-2, gusset 5-3, slide rail 5-4, guide rail
5-1 and slide rail 5-4 are arranged in parallel, are fixedly connected by two fix bars 5-2 in left and right, are rectangle, the parallel gusset 5-3's of two panels
Left and right two ends are in circular arc convex, and left and right two ends are separately fixed in two fix bars 5-2 in left and right, on two panels gusset 5-3 respectively
Open up multiple screwed holes；The structure of left fixed mount 4 as shown in fig. 6, outward appearance such as bench-like, by many rigid cylindrical rods connections
Into chair back place plane, seat place plane, three planes of handrail place plane are each other 90 °；The knot of right bogie 9
Structure on the cylindrical rod of composition seat, installs multiple rollers 10 as shown in fig. 7, essentially identical with the shape of left fixed mount 4,
On the vertical cylinder rod of left and right armrest positions, a roller 10 is respectively installed, it is fixed on the top of the upside cylindrical rod of seat-back position
One annulus 9-1 of connection, on the top of the downside cylindrical rod of seat-back position, installs guide rail wheel 9-2, the electricity of micromachine 8
Arbor and guide rail wheel 9-2 couple；Space structure is：The cylinder club head at the chair back two ends of left fixed mount 4 is fixed respectively to be joined
It is connected on the guide rail 5-1 and slide rail 5-4 of upper bracket 5, the left side setting height(from bottom) sensor 1, controller 2 of left fixed mount 4, wireless receipts
Send out device 3；Annulus 9-1 on right bogie 9 penetrates slide rail 5-4, and guide rail wheel 9-2 loads on guide rail 5-1；In the gusset of upper bracket 5
5-3 downsides, install multiple stage clips 6, form stage clip group, and a block pressur plate 7 is coupled below stage clip group；Transport case 12 is hollow box body,
Box outer surface fixedly mounts a light bar 13, and the left end of casing installs a landing pack 11.
Description of the drawings
Accompanying drawing 1 is general structure schematic diagram of the present utility model；
Accompanying drawing 2 is A of the present utility model to surface structure schematic diagram；
Accompanying drawing 3 is landing pack 11, transport storehouse 12, the connection diagram of light bar 13；
Accompanying drawing 4 is the schematic appearance of upper bracket 5；
Accompanying drawing 5 is the B of upper bracket 5 to structural representation；
Accompanying drawing 6 is the structural representation of left fixed mount 4；
Accompanying drawing 7 is the structural representation of right bogie 9；
Accompanying drawing 8 is the B of pressing plate 7 to schematic diagram.
Specific embodiment
With reference to the accompanying drawing in the utility model embodiment, the technical scheme in the utility model embodiment is carried out it is clear,
It is fully described by, it is clear that described embodiment is only a part of embodiment of the present utility model, rather than the enforcement of whole
Example.Based on the embodiment in the utility model, those of ordinary skill in the art are obtained under the premise of creative work is not made
The every other embodiment for obtaining, belongs to the scope of the utility model protection.
The utility model mainly includes：Height sensor 1, controller 2, wireless transceiver 3, left fixed mount 4, upper bracket 5,
Stage clip 6, pressing plate 7, micromachine 8, right bogie 9, roller 10, landing pack 11, transport case 12, light bar 13；Wherein upper bracket 5
Structure as shown in Figure 4 and Figure 5, including guide rail 5-1, fix bar 5-2, gusset 5-3, slide rail 5-4, guide rail 5-1 and slide rail 5-4 puts down
Row arrangement, is fixedly connected by two fix bars 5-2 in left and right, is rectangle, and the left and right two ends of the parallel gusset 5-3 of two panels are in circular arc
Convex, left and right two ends are separately fixed in two fix bars 5-2 in left and right, and on two panels gusset 5-3 multiple screwed holes are opened up respectively；
The structure of left fixed mount 4 as shown in fig. 6, outward appearance such as bench-like, is formed by many rigid cylindrical rods connections, chair back place plane,
Seat place plane, three planes of handrail place plane are each other 90 °；The structure of right bogie 9 as shown in fig. 7, with a left side
The shape of fixed mount 4 is essentially identical, on the cylindrical rod of composition seat, installs multiple rollers 10, and in left and right, armrest positions is perpendicular
On straight cylinder rod, a roller 10 is respectively installed, on the top of the upside cylindrical rod of seat-back position, be fixedly connected an annulus 9-1,
On the top of the downside cylindrical rod of seat-back position, guide rail wheel 9-2 is installed, the motor shaft of micromachine 8 and guide rail wheel 9-2 join
Connect；Space structure is：The cylinder club head at the chair back two ends of left fixed mount 4 is fixedly connected respectively in the guide rail of upper bracket 5
On 5-1 and slide rail 5-4, the left side setting height(from bottom) sensor 1, controller 2 of left fixed mount 4, wireless transceiver 3；On right bogie 9
Annulus 9-1 penetrate slide rail 5-4, guide rail wheel 9-2 loads on guide rail 5-1；On the downside of the gusset 5-3 of upper bracket 5, multiple pressures are installed
Spring 6, forms stage clip group, and a block pressur plate 7 is coupled below stage clip group；Transport case 12 is hollow box body, and box outer surface is fixedly mounted
One light bar 13, the left end of casing installs a landing pack 11.
When the utility model is used, upper bracket 5 is fixed on by the plug-in of unmanned motor spindle by the screwed hole on gusset 5-3
On bolt, the mail being delivered is loaded in transport case 12, then by box sealing, the left end of casing installs a landing pack
11, box outer surface installs a light bar 13, and then transport case 12 is put between left fixed mount 4 and right bogie 9, wireless to receive
After sending out the signal that device 3 receives controllers transmission, controller 2 is transmitted a signal to, the control micromachine 8 of controller 2 is rotated,
Guide rail wheel 9-2 is driven to rotate in guide rail 5-1, right bogie 9 to left movement, now slide rail 5-4 pass through annulus 9-1 to right driving
Auxiliary support effect is erected, so that transport case 12 is clamped in the lateral direction by left fixed mount 4 and right bogie 9, is passed through
Stage clip 6 regulates and controls the height of pressing plate 7 processed makes transport case 12 be compressed by above-below direction；After confirmation is linked up by express company and addressee,
Unmanned plane takes off and according to default navigation coordinate to addressee place autonomous flight, and after arriving at overhead, addressee sees
After unmanned plane, addressee instruction, nothing are sent to wireless transceiver 3 by the mobile phone with positioning function or other wireless launchers
The instruction for receiving is passed to controller 2 by line transceiver 3, after customer information and positional information has been examined, in height sensor 1
Drop to default safe drop altitude under control, then control micromachine 8 and invert, move right right bogie 9, release
The stationary state of transport case 12, transport case 12 departs from after unmanned plane, and landing pack 11 is opened, the slow drop ground of transport case 12, transport
The sparkling prompting addressee of light bar 13 on case 12 independently receives mail；Multiple rollers 10 are installed, it is ensured that right driving on right bogie 9
Friction between frame 9 and transport case 12 during relative motion is less, and relative motion is smooth.
Advantage
The utility model simple structure, production cost is very low；Mail joins and confirms that formal science is ingenious, uses and promotes
Value is obvious.
Claims (1)
1. a kind of unmanned plane cargo instrument, including height sensor（1）, controller（2）, wireless transceiver（3）, left fixed mount
（4）, upper bracket（5）, stage clip（6）, pressing plate（7）, micromachine（8）, right bogie（9）, roller（10）, landing pack（11）、
Transport case（12）, light bar（13）；
The upper bracket（5）Including guide rail（5-1）, fix bar（5-2）, gusset（5-3）, slide rail（5-4）；Guide rail（5-1）And cunning
Rail（5-4）It is arranged in parallel, by two fix bars in left and right（5-2）It is fixedly connected, is rectangle；The parallel gusset of two panels（5-3）'s
Left and right two ends are in circular arc convex, and left and right two ends are separately fixed at two fix bars in left and right（5-2）On, two panels gusset（5-3）On
Multiple screwed holes are opened up respectively；
The left fixed mount（4）Outward appearance such as bench-like, is formed, chair back place plane, seat institute by many rigid cylindrical rod connections
It it is each other 90 ° in plane, three planes of handrail place plane；
The right bogie（9）With left fixed mount（4）Shape it is essentially identical, composition seat cylindrical rod on, install it is multiple
Roller（10）, on the vertical cylinder rod of left and right armrest positions, a roller is respectively installed（10）, in the upside cylinder of seat-back position
The top of rod, be fixedly connected an annulus（9-1）, on the top of the downside cylindrical rod of seat-back position, a guide rail wheel is installed（9-
2）, micromachine（8）Motor shaft and guide rail wheel（9-2）Connection；
The unmanned plane cargo instrument, it is characterised in that：Left fixed mount（4）Chair back two ends cylinder club head fixed connection respectively
It is connected on upper bracket（5）Guide rail（5-1）And slide rail（5-4）On, left fixed mount（4）Left side setting height(from bottom) sensor（1）, control
Device（2）, wireless transceiver（3）；Right bogie（9）On annulus（9-1）Penetrate slide rail（5-4）, guide rail wheel（9-2）Load guide rail
（5-1）On；In upper bracket（5）Gusset（5-3）Downside, installs multiple stage clips（6）, stage clip group is formed, couple below stage clip group
One block pressur plate（7）；Transport case（12）For hollow box body, box outer surface one light bar of fixed installation（13）, the left end peace of casing
Fill a landing pack（11）.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201621205831.3U CN206155796U (en) | 2016-11-09 | 2016-11-09 | Unmanned aerial vehicle freight transportation device |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201621205831.3U CN206155796U (en) | 2016-11-09 | 2016-11-09 | Unmanned aerial vehicle freight transportation device |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN206155796U true CN206155796U (en) | 2017-05-10 |
Family
ID=58659531
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201621205831.3U Expired - Fee Related CN206155796U (en) | 2016-11-09 | 2016-11-09 | Unmanned aerial vehicle freight transportation device |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN206155796U (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109552627A (en) * | 2018-10-24 | 2019-04-02 | 国网山东省电力公司龙口市供电公司 | A kind of unmanned plane delivery case |
| CN113031475A (en) * | 2021-03-01 | 2021-06-25 | 南京航空航天大学 | Parafoil track tail end real-time prediction device |
-
2016
- 2016-11-09 CN CN201621205831.3U patent/CN206155796U/en not_active Expired - Fee Related
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109552627A (en) * | 2018-10-24 | 2019-04-02 | 国网山东省电力公司龙口市供电公司 | A kind of unmanned plane delivery case |
| CN113031475A (en) * | 2021-03-01 | 2021-06-25 | 南京航空航天大学 | Parafoil track tail end real-time prediction device |
| CN113031475B (en) * | 2021-03-01 | 2022-09-30 | 南京航空航天大学 | Parafoil track tail end real-time prediction device |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CN102092471B (en) | Floating platform for mooring hot air airship | |
| CN206155796U (en) | Unmanned aerial vehicle freight transportation device | |
| CN201678040U (en) | Unmanned helicopter applicable to engineering | |
| CN108163220B (en) | General type unmanned aerial vehicle launches platform | |
| CN105438460A (en) | Dual-power synergistically driven unmanned aerial vehicle | |
| CN103318406A (en) | Composite rotor craft | |
| CN106006101B (en) | A kind of unmanned aerial vehicle complementary goods loading attachment | |
| CN207683774U (en) | A kind of unmanned plane having air bag of saving oneself | |
| CN203958614U (en) | Integral type multi-rotor aerocraft | |
| CN201553298U (en) | Floating platform for mooring hot airship | |
| CN206417651U (en) | A kind of unmanned aerial vehicle complementary goods loading attachment | |
| CN203112095U (en) | Vertical distribution conveying device for tire automatic production line | |
| CN108216629A (en) | A kind of combination transport unmanned plane | |
| CN104608917A (en) | Tail wing structure of fixed wing unmanned aerial vehicle | |
| CN207257991U (en) | Land buffer-type transport unmanned plane | |
| CN207876000U (en) | A kind of combination transport unmanned plane | |
| CN208828081U (en) | The huge pollution-free transhipment of dirigible synchronizes the system of letting fly away | |
| CN205820344U (en) | A kind of for carry-on jaw | |
| CN205602131U (en) | Small -size load compartment dispensing device of many rotor unmanned aerial vehicle | |
| CN102530260A (en) | Method and system for short-distance taking off of unmanned aerial vehicles | |
| CN205801509U (en) | Parallel unmanned plane is used in a kind of building pipe fitting transport | |
| CN205293057U (en) | Airship | |
| CN207311838U (en) | A kind of unmanned plane airdrop platform | |
| CN107651196A (en) | A kind of double folding multi-rotor aerocraft | |
| CN106314780A (en) | Unmanned aerial vehicle (UAV) for logistics |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20170510 Termination date: 20171109 |
|
| CF01 | Termination of patent right due to non-payment of annual fee |