CN111252249B - Unmanned aerial vehicle transportation delivery equipment - Google Patents
Unmanned aerial vehicle transportation delivery equipment Download PDFInfo
- Publication number
- CN111252249B CN111252249B CN202010246912.2A CN202010246912A CN111252249B CN 111252249 B CN111252249 B CN 111252249B CN 202010246912 A CN202010246912 A CN 202010246912A CN 111252249 B CN111252249 B CN 111252249B
- Authority
- CN
- China
- Prior art keywords
- connecting rod
- unmanned aerial
- aerial vehicle
- rotating shaft
- gear
- 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.)
- Active
Links
- 230000005540 biological transmission Effects 0.000 claims description 16
- 230000010354 integration Effects 0.000 abstract description 2
- 238000009434 installation Methods 0.000 description 5
- 238000010586 diagram Methods 0.000 description 2
- 230000009286 beneficial effect Effects 0.000 description 1
- 230000007547 defect Effects 0.000 description 1
- 238000000034 method Methods 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 230000001502 supplementing effect Effects 0.000 description 1
- 230000032258 transport Effects 0.000 description 1
Images
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
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C25/00—Alighting gear
- B64C25/02—Undercarriages
- B64C25/08—Undercarriages non-fixed, e.g. jettisonable
- B64C25/10—Undercarriages non-fixed, e.g. jettisonable retractable, foldable, or the like
- B64C25/18—Operating mechanisms
- B64C25/20—Operating mechanisms mechanical
-
- 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
- B64D9/00—Equipment for handling freight; Equipment for facilitating passenger embarkation or the like
-
- H—ELECTRICITY
- H02—GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
- H02S—GENERATION OF ELECTRIC POWER BY CONVERSION OF INFRARED RADIATION, VISIBLE LIGHT OR ULTRAVIOLET LIGHT, e.g. USING PHOTOVOLTAIC [PV] MODULES
- H02S20/00—Supporting structures for PV modules
- H02S20/30—Supporting structures being movable or adjustable, e.g. for angle adjustment
-
- 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
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02E—REDUCTION OF GREENHOUSE GAS [GHG] EMISSIONS, RELATED TO ENERGY GENERATION, TRANSMISSION OR DISTRIBUTION
- Y02E10/00—Energy generation through renewable energy sources
- Y02E10/50—Photovoltaic [PV] energy
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Mechanical Engineering (AREA)
- Forklifts And Lifting Vehicles (AREA)
Abstract
The invention discloses unmanned aerial vehicle transportation and distribution equipment, which comprises an unmanned aerial vehicle body, wherein the unmanned aerial vehicle body comprises a first chute, a first slide block is arranged in the first chute in a sliding manner, a first rotating shaft is arranged at the rear side of the first slide block in a rotating manner, a rotating wheel is fixedly arranged on the first rotating shaft, a first connecting rod is fixedly arranged on the front end surface of the rotating wheel, a first open slot is formed in the first slide block, the first connecting rod can extend into the first open slot, a second connecting rod is fixedly arranged at the left end of the unmanned aerial vehicle body, a clamping block is arranged on the second connecting rod in a sliding manner, and the right end surface of the clamping block is fixedly connected with the first slide block. Integration degree is high, and is safe in utilization, can improve unmanned aerial vehicle's freight efficiency greatly.
Description
Technical Field
The invention relates to the field of unmanned aerial vehicles, in particular to unmanned aerial vehicle transportation and distribution equipment.
Background
As is well known, along with the development of science and technology, the unmanned aerial vehicle of china develops rapidly, and the technique of the first unmanned aerial vehicle of present stage has developed maturity for unmanned aerial vehicle is in the transportation, measures, all has very big use in the aspect of military project etc., but unmanned aerial vehicle is because the reason of the volume of self and power, retrieves a lot of restrictions, and unmanned simultaneously getting the material also is the problem that needs to solve, consequently need design an unmanned aerial vehicle transportation delivery equipment and solve above-mentioned problem.
Disclosure of Invention
The invention aims to provide unmanned aerial vehicle transportation and distribution equipment which is used for overcoming the defects in the prior art.
The invention is realized by the following technical scheme.
An unmanned aerial vehicle transportation and distribution device comprises an unmanned aerial vehicle body, wherein the unmanned aerial vehicle body comprises a first sliding chute;
a first sliding block is arranged in the first sliding groove in a sliding manner, a first rotating shaft is arranged on the rear side of the first sliding block in a rotating manner, a rotating wheel is fixedly arranged on the first rotating shaft, a first connecting rod is fixedly arranged on the front end face of the rotating wheel, a first open slot is formed in the first sliding block, the first connecting rod can extend into the first open slot, a second connecting rod is fixedly arranged on the left end of the unmanned aerial vehicle body, a clamping block is arranged on the second connecting rod in a sliding manner, the right end face of the clamping block is fixedly connected with the first sliding block, a second open slot is formed in the lower side of the clamping block, a second rotating shaft is symmetrically arranged on the second connecting rod in the second open slot in a rotating manner, a first gear is fixedly arranged on the second rotating shaft, a first rack capable of being meshed with the first gear is fixedly arranged on the lower side of the second connecting rod, and a first rotating rod is fixedly arranged, a third connecting rod is hinged at the lower end of the first rotating rod, a third rotating shaft is rotatably arranged outside the second rotating shaft, a second rotating rod is fixedly arranged on the third rotating shaft, a fourth connecting rod is hinged at the bottom end of the second rotating rod, a clamping block is fixedly arranged on the fourth connecting rod and the third connecting rod, a groove is arranged in the clamping block, a third opening groove is formed in the upper end of the clamping block, the fourth connecting rod and the third connecting rod are fixed in the third opening groove, a second sliding groove is formed in the upper side of the second connecting rod, a second sliding block is slidably arranged in the second sliding groove, a spring is connected between the right end wall of the second sliding block and the right end wall of the second sliding groove, a fourth opening groove is formed in the left end of the second sliding block, a fifth connecting rod is fixedly arranged outside the fourth opening groove, a fifth opening groove is formed in the left end of the clamping block, a sixth connecting rod is fixedly arranged in the fifth opening groove, a seventh connecting rod is hinged between the sixth connecting rod and the fifth connecting rod, and an eighth connecting rod is fixedly arranged on the inner side of the fourth opening groove.
Further, the fixed backup pad that is equipped with in unmanned aerial vehicle fuselage top, it is equipped with the fourth pivot to rotate in the backup pad, the fixed connecting block that is equipped with in the fourth pivot, the fixed slurcam that is equipped with of connecting block up end, slurcam left side bottom face is equipped with first outer fishplate bar, first outer fishplate bar internal fixation is equipped with the ninth connecting rod, the ninth connecting rod with it is equipped with the tenth connecting rod to articulate between the eighth connecting rod, backup pad top longitudinal symmetry rotates and is equipped with the fifth pivot, the fixed mounting gear that is equipped with intermeshing in the fifth pivot, the slurcam right-hand member be equipped with can with mounting gear engagement's second rack, the fixed solar cell panel that is equipped with on the mounting gear.
Further, unmanned aerial vehicle fuselage rear side is equipped with the transmission chamber, transmission chamber rear end wall is equipped with the third spout, it is equipped with the third slider to slide in the third spout, the third slider internal fixation is equipped with the motor, the fixed controller that is equipped with of third spout right-hand member, the terminal surface rotates before the motor and is equipped with the sixth pivot, the fixed second gear that is equipped with of terminal surface before the sixth pivot.
Furthermore, a third gear is fixedly arranged on the first rotating shaft in the transmission cavity, a seventh rotating shaft is rotatably arranged between the sixth rotating shaft and the first rotating shaft, a fourth gear is fixedly arranged on the seventh rotating shaft, a chain is arranged between the fourth gear and the third gear, and the chain can be meshed with the second gear.
Further, the transmission chamber downside the fixed second outer joint plate that is equipped with of unmanned aerial vehicle fuselage bottom face, the second outer joint plate internal rotation is equipped with the eighth pivot, the fixed support frame that is equipped with in the eighth pivot, the fixed third outer joint plate that is equipped with of terminal surface in the support frame, the fixed first catch bar that is equipped with of third outer joint plate internal fixation, transmission chamber right-hand member slides from top to bottom and is equipped with the sliding block, sliding block left end face be equipped with can with the third rack of second gear engagement, the fixed power block that is equipped with of sliding block bottom face, the symmetry is equipped with the outer joint plate of fourth on the power block, the outer joint plate internal fixation of fourth is equipped with the second catch bar, the second catch bar with it is equipped with the third catch bar to articulate between the first catch bar.
The invention has the beneficial effects that: the device is simple in structure and easy and convenient to operate, the unmanned aerial vehicle can be assisted to pick up and deliver goods, the solar panel can be opened when the device transports the goods, power can be improved by supplementing power energy, and meanwhile, the device is convenient and rapid to use, high in integration degree and safe to use, and the goods delivery efficiency of the unmanned aerial vehicle can be greatly improved.
Drawings
In order to more clearly illustrate the embodiments of the invention or the technical solutions in the prior art, the drawings used in the description of the embodiments or the prior art will be briefly described below, and it is obvious that the drawings in the following description are only some embodiments of the invention, and it is obvious for those skilled in the art that other drawings can be obtained based on these drawings without creative efforts.
FIG. 1 is a schematic structural diagram of an embodiment of the present invention;
FIG. 2 is a schematic view of the structure A-A of FIG. 1;
FIG. 3 is a schematic diagram of B-B in FIG. 1.
Detailed Description
The invention will now be described in detail with reference to fig. 1-3, for the sake of convenience, the orientations described hereinafter being defined as follows: the up, down, left, right, and front-back directions described below correspond to the up, down, left, right, and front-back directions in the projection relationship of fig. 1 itself.
With reference to fig. 1-3, an unmanned aerial vehicle transportation and distribution apparatus includes an unmanned aerial vehicle body 10, the unmanned aerial vehicle body 10 includes a first sliding groove 11, a first sliding block 16 is slidably disposed in the first sliding groove 11, a first rotating shaft 12 is rotatably disposed at the rear side of the first sliding block 16, a rotating wheel 13 is fixedly disposed on the first rotating shaft 12, a first connecting rod 15 is fixedly disposed on the front end face of the rotating wheel 13, a first open slot 14 is disposed in the first sliding block 16, the first connecting rod 15 can extend into the first open slot 14, a second connecting rod 75 is fixedly disposed at the left end of the unmanned aerial vehicle body 10, a clamping block 17 is slidably disposed on the second connecting rod 75, the right end face of the clamping block 17 is fixedly connected with the first sliding block 16, a second open slot 29 is disposed at the lower side of the clamping block 17, and a second rotating shaft 26 is symmetrically rotatably disposed on the second connecting rod 75 in the second open slot 29, a first gear 27 is fixedly arranged on the second rotating shaft 26, a first rack 18 capable of being meshed with the first gear 27 is fixedly arranged on the lower side of the second connecting rod 75, a first rotating rod 22 is fixedly arranged on the first gear 27, a third connecting rod 21 is hinged to the lower end of the first rotating rod 22, a third rotating shaft 28 is rotatably arranged on the outer side of the second rotating shaft 26, a second rotating rod 25 is fixedly arranged on the third rotating shaft 28, a fourth connecting rod 24 is hinged to the bottom end of the second rotating rod 25, a clamping block 23 is fixedly arranged on the fourth connecting rod 24 and the third connecting rod 21, a groove 19 is formed in the clamping block 23, a third opening groove 20 is formed in the upper end of the clamping block 23, the fourth connecting rod 24 and the third connecting rod 21 are fixed in the third opening groove 20, a second sliding groove 50 is formed in the upper side of the second connecting rod 75, and a second sliding block 51 is slidably arranged in the second sliding groove 50, second slider 51 right-hand member wall with it is equipped with spring 49 to connect between the 50 right-hand member walls of second spout, second slider 51 left end is equipped with fourth open slot 35, the fixed fifth connecting rod 34 that is equipped with in fourth open slot 35 outside, the clamp is got 17 the left end and is equipped with fifth open slot 30, fifth open slot 30 internal fixation is equipped with sixth connecting rod 31, sixth connecting rod 31 with it is equipped with seventh connecting rod 32 to articulate between the fifth connecting rod 34, fourth open slot 35 inboard is fixed and is equipped with eighth connecting rod 33.
Fixed backup pad 48 that is equipped with in unmanned aerial vehicle fuselage 10 top, it is equipped with fourth pivot 47 to rotate in the backup pad 48, the fixed connecting block 46 that is equipped with in the fourth pivot 47, the fixed slurcam 38 that is equipped with of connecting block 46 up end, the bottom face is equipped with first outer fishplate bar 37 in the slurcam 38 left side, first outer fishplate bar 37 internal fixation is equipped with ninth connecting rod 36, ninth connecting rod 36 with it is equipped with tenth connecting rod 76 to articulate between the eighth connecting rod 33, the rotation of the 48 top longitudinal symmetry in backup pad is equipped with fifth pivot 43, the fixed installation gear 44 that is equipped with intermeshing in the fifth pivot 43, slurcam 38 right-hand member be equipped with can with installation gear 44 meshed second rack 45, the fixed solar cell panel 39 that is equipped with on the installation gear 44.
The unmanned aerial vehicle fuselage 10 rear side is equipped with transmission chamber 72, transmission chamber 72 rear end wall is equipped with third spout 66, it is equipped with third slider 65 to slide in the third spout 66, third slider 65 internal fixation is equipped with motor 64, the fixed controller 67 that is equipped with of third spout 66 right-hand member, the terminal surface rotates before the motor 64 is equipped with sixth pivot 69, the fixed second gear 70 that is equipped with of terminal surface before the sixth pivot 69 is located in the transmission chamber 72 the fixed third gear 74 that is equipped with in the first pivot 12, sixth pivot 69 with it is equipped with seventh pivot 71 to rotate between the first pivot 12, the fixed fourth gear 77 that is equipped with in seventh pivot 71, fourth gear 77 with be equipped with chain 73 between the third gear 74, chain 73 can with the meshing of second gear 70.
The fixed second outer joint plate 55 that is equipped with of transmission chamber 72 downside unmanned aerial vehicle fuselage 10 bottom face, the second outer joint plate 55 internal rotation is equipped with eighth pivot 56, the fixed support frame 57 that is equipped with in the eighth pivot 56, the fixed third outer joint plate 58 that is equipped with of support frame 57 interior terminal surface, the third outer joint plate 58 internal fixation is equipped with first catch bar 59, the transmission chamber 72 right-hand member slides from top to bottom and is equipped with sliding block 53, sliding block 53 left end face be equipped with can with the third rack 68 of second gear 70 meshing, the fixed power block 63 that is equipped with of sliding block 53 bottom face, the symmetry is equipped with the fourth outer joint plate 62 on the power block 63, fourth outer joint plate 62 internal fixation is equipped with second catch bar 61, second catch bar 61 with it is equipped with third catch bar 60 to articulate between the first catch bar 59.
The working state is as follows:
when the goods need to be transported, the unmanned house is stopped above the goods, the motor 64 is turned on to drive the sixth rotating shaft 69 to rotate, the sixth rotating shaft 69 rotates to drive the second gear 70 to rotate, the second gear 70 rotates to drive the chain 73 to rotate, the chain 73 rotates to drive the third gear 74 to rotate, the third gear 74 rotates to drive the first rotating shaft 12 to rotate, the first rotating shaft 12 rotates to drive the rotating wheel 13 to rotate, the rotating wheel 13 rotates to drive the first sliding block 16 to slide downwards through the first connecting rod 15, the first sliding block 16 slides downwards to drive the clamping block 17 to slide downwards, the clamping block 17 slides downwards to drive the first gear 27 to rotate through the matching of the first gear 27 and the first rack 18, the first gear 27 rotates to drive the first rotating rod 22 to rotate, the first rotating rod 22 rotates to pass through the fourth connecting rod 24 and the third connecting rod 21 to make the clamping block 23 slide downwards, the clamping block 23 slides downwards to pass through the groove 19 to clamp the goods, the clamping block 17 slides downwards to pass through the sixth connecting rod 31 to drive the seventh connecting rod 32 to slide downwards, the seventh connecting rod 32 slides downwards to drive the fourth opening groove 35 to slide rightwards, the fourth opening groove 35 slides rightwards to pass through the eighth connecting rod 33 to drive the ninth connecting rod 36 to slide rightwards, the ninth connecting rod 36 slides rightwards to drive the pushing plate 38 to rotate, the pushing plate 38 rotates to drive the installation gear 44 to rotate through the second rack 45, the installation gear 44 rotates to drive the solar cell panel 39 to open, the solar cell panel 39 is opened to provide larger flight power through solar energy, when the equipment needs to fall, the controller 67 is opened and is driven the third slider 65 slides to the right, the third slider 65 slides to the right and makes the second gear 70 with the meshing of third rack 68, the second gear 70 rotates and passes through the third rack 68 drives the sliding block 53 slides downwards, the sliding block 53 slides downwards and drives the power block 63 slides downwards, the power block 63 slides downwards and passes through the third catch bar 60 makes the support frame 57 open, support equipment.
The above embodiments are merely illustrative of the technical ideas and features of the present invention, and the purpose thereof is to enable those skilled in the art to understand the contents of the present invention and implement the present invention, and not to limit the protection scope of the present invention. All equivalent changes and modifications made according to the spirit of the present invention should be covered within the protection scope of the present invention.
Claims (5)
1. The utility model provides an unmanned aerial vehicle transportation delivery equipment, includes the unmanned aerial vehicle fuselage, its characterized in that: the unmanned aerial vehicle body comprises a first sliding chute;
a first sliding block is arranged in the first sliding groove in a sliding manner, a first rotating shaft is arranged on the rear side of the first sliding block in a rotating manner, a rotating wheel is fixedly arranged on the first rotating shaft, a first connecting rod is fixedly arranged on the front end face of the rotating wheel, a first open slot is formed in the first sliding block, the first connecting rod can extend into the first open slot, a second connecting rod is fixedly arranged on the left end of the unmanned aerial vehicle body, a clamping block is arranged on the second connecting rod in a sliding manner, the right end face of the clamping block is fixedly connected with the first sliding block, a second open slot is formed in the lower side of the clamping block, a second rotating shaft is symmetrically arranged on the second connecting rod in the second open slot in a rotating manner, a first gear is fixedly arranged on the second rotating shaft, a first rack capable of being meshed with the first gear is fixedly arranged on the lower side of the second connecting rod, and a first rotating rod is fixedly arranged, a third connecting rod is hinged at the lower end of the first rotating rod, a third rotating shaft is rotatably arranged outside the second rotating shaft, a second rotating rod is fixedly arranged on the third rotating shaft, a fourth connecting rod is hinged at the bottom end of the second rotating rod, a clamping block is fixedly arranged on the fourth connecting rod and the third connecting rod, a groove is arranged in the clamping block, a third opening groove is formed in the upper end of the clamping block, the fourth connecting rod and the third connecting rod are fixed in the third opening groove, a second sliding groove is formed in the upper side of the second connecting rod, a second sliding block is slidably arranged in the second sliding groove, a spring is connected between the right end wall of the second sliding block and the right end wall of the second sliding groove, a fourth opening groove is formed in the left end of the second sliding block, a fifth connecting rod is fixedly arranged outside the fourth opening groove, a fifth opening groove is formed in the left end of the clamping block, a sixth connecting rod is fixedly arranged in the fifth opening groove, a seventh connecting rod is hinged between the sixth connecting rod and the fifth connecting rod, and an eighth connecting rod is fixedly arranged on the inner side of the fourth opening groove.
2. An unmanned aerial vehicle transportation distribution apparatus as claimed in claim 1, wherein: the fixed backup pad that is equipped with in unmanned aerial vehicle fuselage top, it is equipped with the fourth pivot to rotate in the backup pad, the fixed connecting block that is equipped with in the fourth pivot, the fixed slurcam that is equipped with of connecting block up end, slurcam left side bottom face is equipped with first outer fishplate bar, first outer fishplate bar internal fixation is equipped with the ninth connecting rod, the ninth connecting rod with it is equipped with the tenth connecting rod to articulate between the eighth connecting rod, backup pad top longitudinal symmetry rotates and is equipped with the fifth pivot, the fixed mounting gear that is equipped with intermeshing in the fifth pivot, the slurcam right-hand member be equipped with can with mounting gear engagement's second rack, the fixed solar cell panel that is equipped with on the mounting gear.
3. An unmanned aerial vehicle transportation distribution apparatus as claimed in claim 2, wherein: the unmanned aerial vehicle fuselage rear side is equipped with the transmission chamber, transmission chamber rear end wall is equipped with the third spout, it is equipped with the third slider to slide in the third spout, the third slider internal fixation is equipped with the motor, the fixed controller that is equipped with of third spout right-hand member, the terminal surface rotates before the motor and is equipped with the sixth pivot, the terminal surface is fixed and is equipped with the second gear before the sixth pivot.
4. An unmanned aerial vehicle transportation distribution apparatus as claimed in claim 3, wherein: the transmission cavity is internally provided with a first rotating shaft, a second rotating shaft is arranged in the transmission cavity, a third gear is fixedly arranged on the first rotating shaft, a seventh rotating shaft is rotatably arranged between the sixth rotating shaft and the first rotating shaft, a fourth gear is fixedly arranged on the seventh rotating shaft, a chain is arranged between the fourth gear and the third gear, and the chain can be meshed with the second gear.
5. An unmanned aerial vehicle transportation distribution apparatus as claimed in claim 4, wherein: the transmission chamber downside the fixed second outer joint plate that is equipped with of unmanned aerial vehicle fuselage bottom end face, the second outer joint plate internal rotation is equipped with the eighth pivot, the fixed support frame that is equipped with in the eighth pivot, the fixed third outer joint plate that is equipped with of end face in the support frame, the fixed first catch bar that is equipped with in the third outer joint plate, the transmission chamber right-hand member slides from top to bottom and is equipped with the sliding block, sliding block left end face be equipped with can with the third rack of second gear engagement, the fixed power piece that is equipped with of sliding block bottom end face, the symmetry is equipped with the fourth outer joint plate on the power piece, the fourth outer joint plate internal fixation is equipped with the second catch bar, the second catch bar with it is equipped with the third catch bar to articulate between the first catch bar.
Priority Applications (2)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202010246912.2A CN111252249B (en) | 2020-03-31 | 2020-03-31 | Unmanned aerial vehicle transportation delivery equipment |
| GBGB2009850.5A GB202009850D0 (en) | 2020-03-31 | 2020-06-29 | A drone transportation and distribution equipment |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202010246912.2A CN111252249B (en) | 2020-03-31 | 2020-03-31 | Unmanned aerial vehicle transportation delivery equipment |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CN111252249A CN111252249A (en) | 2020-06-09 |
| CN111252249B true CN111252249B (en) | 2020-11-17 |
Family
ID=70942223
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202010246912.2A Active CN111252249B (en) | 2020-03-31 | 2020-03-31 | Unmanned aerial vehicle transportation delivery equipment |
Country Status (2)
| Country | Link |
|---|---|
| CN (1) | CN111252249B (en) |
| GB (1) | GB202009850D0 (en) |
Families Citing this family (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN112793792A (en) * | 2021-02-26 | 2021-05-14 | 上海润璋智能科技股份有限公司 | Unmanned aerial vehicle for delivering light and handy goods |
Family Cites Families (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| EP3385162A1 (en) * | 2017-04-07 | 2018-10-10 | Antony Pfoertzsch | Basis vehicle for a scout car and method for same, and system including same |
| CN109693789A (en) * | 2017-10-24 | 2019-04-30 | 南京菱亚汽车技术研究院 | A kind of intelligent unmanned machine for being used to take out dispatching based on Internet of Things |
| JP2019166965A (en) * | 2018-03-23 | 2019-10-03 | 株式会社荏原製作所 | System for transporting object to high place |
| CN110341975A (en) * | 2019-07-22 | 2019-10-18 | 金陵科技学院 | A kind of solar energy containing unmanned plane is with fortune station |
-
2020
- 2020-03-31 CN CN202010246912.2A patent/CN111252249B/en active Active
- 2020-06-29 GB GBGB2009850.5A patent/GB202009850D0/en not_active Ceased
Also Published As
| Publication number | Publication date |
|---|---|
| CN111252249A (en) | 2020-06-09 |
| GB202009850D0 (en) | 2020-08-12 |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CN110435910A (en) | A kind of multi-rotor unmanned aerial vehicle landing-gear | |
| CN111252249B (en) | Unmanned aerial vehicle transportation delivery equipment | |
| CN203937650U (en) | A kind of battery of electric vehicle fast replacing device | |
| CN110094134A (en) | A kind of advancing slip sliding door system of big aperture of car | |
| CN217598424U (en) | Top cover adjusting device for sludge cleaning and transporting vehicle | |
| CN215752555U (en) | New energy automobile is handling device for battery | |
| CN215552793U (en) | Improved green emergency charging vehicle | |
| CN203496898U (en) | Worm and gear type bottom-discharging type mine car | |
| CN212894494U (en) | Special turning and throwing device for production of biological organic fertilizer | |
| CN208715170U (en) | Lithium battery passenger car changes electric system | |
| CN210554384U (en) | New forms of energy self-discharging formula mine car carriage | |
| CN205970784U (en) | Big top cap of meteorological radar car mechanism that opens and shuts | |
| CN112026511A (en) | Vehicle-mounted solar power generation equipment capable of being automatically stored | |
| CN212828585U (en) | Graphite thoughtlessly holds between fingers workshop and uses raw and other materials conveyer | |
| CN111470336A (en) | Material conveyor in subway tunnel and use method thereof | |
| CN216660073U (en) | Guide cover for van-type semitrailer and van-type semitrailer | |
| CN212921624U (en) | Carrying device of lithium battery pack | |
| CN220594615U (en) | Light-weight rear cover of pickup truck | |
| CN203026563U (en) | Battery fastening device of electric automobile | |
| CN211837675U (en) | Graphite raw material mixing device for lithium battery production | |
| CN215877047U (en) | Material mixing device is used in fodder yeast production of low-power consumption | |
| CN216861216U (en) | High-integration wireless battery replacement robot | |
| CN211544599U (en) | Metal container with door convenient for loading and unloading goods | |
| CN217999269U (en) | Locking structure for preventing self-opening flying wing carriage | |
| CN213384554U (en) | Novel electric motor car lithium cell storage device |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| PB01 | Publication | ||
| PB01 | Publication | ||
| SE01 | Entry into force of request for substantive examination | ||
| SE01 | Entry into force of request for substantive examination | ||
| TA01 | Transfer of patent application right |
Effective date of registration: 20201029 Address after: 252000 No.5 Lushan South Road, high tech Industrial Development Zone, Liaocheng City, Shandong Province Applicant after: Liaocheng innovation Real Estate Co., Ltd Address before: 361000 Haifa Building, Huli District, Xiamen City, Fujian Province Applicant before: Xiamen Cha Re-injection Packaging Co.,Ltd. |
|
| TA01 | Transfer of patent application right | ||
| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| TR01 | Transfer of patent right |
Effective date of registration: 20210706 Address after: 252000 room 307, building 8, high tech city, No.5, Lushan South Road, Jiuzhou street, high tech Zone, Liaocheng City, Shandong Province Patentee after: Liaocheng Quantum Technology Group Co.,Ltd. Address before: 252000 No.5, Lushan South Road, Liaocheng hi tech Industrial Development Zone, Shandong Province Patentee before: Liaocheng innovation Real Estate Co., Ltd |
|
| TR01 | Transfer of patent right |