CN108275278B - Unmanned aerial vehicle of support terminal charges in area - Google Patents
Unmanned aerial vehicle of support terminal charges in area Download PDFInfo
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- CN108275278B CN108275278B CN201810046260.0A CN201810046260A CN108275278B CN 108275278 B CN108275278 B CN 108275278B CN 201810046260 A CN201810046260 A CN 201810046260A CN 108275278 B CN108275278 B CN 108275278B
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- 230000002093 peripheral effect Effects 0.000 claims abstract description 12
- 238000000034 method Methods 0.000 claims 1
- 230000008878 coupling Effects 0.000 description 2
- 238000010168 coupling process Methods 0.000 description 2
- 238000005859 coupling reaction Methods 0.000 description 2
- 239000000463 material Substances 0.000 description 2
- 208000035473 Communicable disease Diseases 0.000 description 1
- 230000009286 beneficial effect Effects 0.000 description 1
- 238000011161 development Methods 0.000 description 1
- 238000010586 diagram Methods 0.000 description 1
- 238000005516 engineering process Methods 0.000 description 1
- 208000015181 infectious disease Diseases 0.000 description 1
- 238000007689 inspection Methods 0.000 description 1
- 238000012423 maintenance Methods 0.000 description 1
- 238000004519 manufacturing process Methods 0.000 description 1
- 238000013507 mapping Methods 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 238000012544 monitoring process Methods 0.000 description 1
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Classifications
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- 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
- B64D27/00—Arrangement or mounting of power plants in aircraft; Aircraft characterised by the type or position of power plants
- B64D27/02—Aircraft characterised by the type or position of power plants
- B64D27/24—Aircraft characterised by the type or position of power plants using steam or spring force
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B60—VEHICLES IN GENERAL
- B60L—PROPULSION OF ELECTRICALLY-PROPELLED VEHICLES; SUPPLYING ELECTRIC POWER FOR AUXILIARY EQUIPMENT OF ELECTRICALLY-PROPELLED VEHICLES; ELECTRODYNAMIC BRAKE SYSTEMS FOR VEHICLES IN GENERAL; MAGNETIC SUSPENSION OR LEVITATION FOR VEHICLES; MONITORING OPERATING VARIABLES OF ELECTRICALLY-PROPELLED VEHICLES; ELECTRIC SAFETY DEVICES FOR ELECTRICALLY-PROPELLED VEHICLES
- B60L53/00—Methods of charging batteries, specially adapted for electric vehicles; Charging stations or on-board charging equipment therefor; Exchange of energy storage elements in electric vehicles
- B60L53/10—Methods of charging batteries, specially adapted for electric vehicles; Charging stations or on-board charging equipment therefor; Exchange of energy storage elements in electric vehicles characterised by the energy transfer between the charging station and the vehicle
- B60L53/14—Conductive energy transfer
- B60L53/16—Connectors, e.g. plugs or sockets, specially adapted for charging electric vehicles
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B60—VEHICLES IN GENERAL
- B60L—PROPULSION OF ELECTRICALLY-PROPELLED VEHICLES; SUPPLYING ELECTRIC POWER FOR AUXILIARY EQUIPMENT OF ELECTRICALLY-PROPELLED VEHICLES; ELECTRODYNAMIC BRAKE SYSTEMS FOR VEHICLES IN GENERAL; MAGNETIC SUSPENSION OR LEVITATION FOR VEHICLES; MONITORING OPERATING VARIABLES OF ELECTRICALLY-PROPELLED VEHICLES; ELECTRIC SAFETY DEVICES FOR ELECTRICALLY-PROPELLED VEHICLES
- B60L2200/00—Type of vehicles
- B60L2200/10—Air crafts
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- 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
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T10/00—Road transport of goods or passengers
- Y02T10/60—Other road transportation technologies with climate change mitigation effect
- Y02T10/70—Energy storage systems for electromobility, e.g. batteries
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- 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
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T10/00—Road transport of goods or passengers
- Y02T10/60—Other road transportation technologies with climate change mitigation effect
- Y02T10/7072—Electromobility specific charging systems or methods for batteries, ultracapacitors, supercapacitors or double-layer capacitors
-
- 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
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T90/00—Enabling technologies or technologies with a potential or indirect contribution to GHG emissions mitigation
- Y02T90/10—Technologies relating to charging of electric vehicles
- Y02T90/14—Plug-in electric vehicles
Landscapes
- Engineering & Computer Science (AREA)
- Power Engineering (AREA)
- Transportation (AREA)
- Mechanical Engineering (AREA)
- Aviation & Aerospace Engineering (AREA)
- Charge And Discharge Circuits For Batteries Or The Like (AREA)
Abstract
The invention discloses an unmanned aerial vehicle with a charging support terminal, and relates to the technical field of unmanned aerial vehicles. The telescopic rod comprises a body, a telescopic rod, a first connecting sleeve, a second connecting sleeve and a terminal; a plurality of first fixing plates are fixed on one end face of the first connecting sleeve; a first groove is formed on one surface of the first fixing plate; the second connecting sleeve comprises a first sleeve and a second sleeve; the first sleeve is fixedly connected with the second sleeve through a connecting plate; a plurality of second fixing plates are fixed on one end face of the first sleeve; a second groove is formed on one surface of the second fixing plate; the terminal comprises a first circular ring and a second circular ring; a first through hole is formed in the peripheral side surface of the first circular ring; one end of the first ring is provided with a plurality of third grooves; a second through hole is formed in the peripheral side surface of the second circular ring; one end of the second ring is provided with a plurality of fourth grooves. According to the invention, by using the telescopic double-ring charging terminal structure, the charging terminal can automatically feed, and the problem that the existing unmanned aerial vehicle needs manual operation for charging is solved.
Description
Technical Field
The invention belongs to the technical field of unmanned aerial vehicles, and particularly relates to an unmanned aerial vehicle with a charging support terminal.
Background
An unmanned aircraft, abbreviated as "drone", and abbreviated in english as "UAV", is an unmanned aircraft that is operated by a radio remote control device and a self-contained program control device, or is operated autonomously, either completely or intermittently, by an onboard computer.
Unmanned aerial vehicles can be classified into military and civil applications according to the application field. For military use, unmanned aerial vehicles divide into reconnaissance aircraft and target drone. In the civil aspect, the unmanned aerial vehicle + the industry application is really just needed by the unmanned aerial vehicle; at present, the unmanned aerial vehicle is applied to the fields of aerial photography, agriculture, plant protection, miniature self-timer, express transportation, disaster relief, wild animal observation, infectious disease monitoring, surveying and mapping, news reporting, power inspection, disaster relief, film and television shooting, romantic manufacturing and the like, the application of the unmanned aerial vehicle is greatly expanded, and developed countries actively expand industrial application and develop unmanned aerial vehicle technology.
Along with unmanned aerial vehicle's rapid development, also higher and higher to the requirement that unmanned aerial vehicle charges, the wired charging of current unmanned aerial vehicle needs manual operation, not only extravagant manpower, reduce efficiency moreover.
Disclosure of Invention
The invention aims to provide an unmanned aerial vehicle with a charging support terminal, which solves the problem that the existing unmanned aerial vehicle needs manual operation for charging through a telescopic double-ring charging terminal structure.
In order to solve the technical problems, the invention is realized by the following technical scheme:
the invention relates to an unmanned aerial vehicle with a charging support terminal, which comprises a body, a telescopic rod, a first connecting sleeve, a second connecting sleeve and a terminal, wherein the telescopic rod is arranged on the body; a plurality of fixed seats are fixed on the inner surface of the body; a telescopic rod is fixed on one surface of the fixed seat; a seventh groove is formed in the peripheral side surface of the telescopic rod; a plurality of first fixing plates are fixed on one end face of the first connecting sleeve; a first groove is formed in one surface of the first fixing plate; a plurality of first limiting blocks are fixed on the inner surface of the first groove; the second connecting sleeve comprises a first sleeve and a second sleeve; the first sleeve and the second sleeve are fixedly connected through a connecting plate; a plurality of second fixing plates are fixed on one end face of the first sleeve; a second groove is formed in one surface of the second fixing plate; a plurality of second limiting blocks are fixed on the inner surface of the second groove; the terminal comprises a first circular ring and a second circular ring; a first through hole is formed in the peripheral side surface of the first circular ring; one end of the first ring is provided with a plurality of third grooves; a second through hole is formed in the peripheral side surface of the second circular ring; one end of the second ring is provided with a plurality of fourth grooves; one end of the telescopic rod is matched with the first connecting sleeve; one end of the telescopic rod is matched with the second sleeve; the first limiting block is matched with the first through hole; the second limiting block is matched with the second through hole.
Further, a rubber layer is arranged between the outer surface of the first circular ring and the inner surface of the second circular ring, and the first circular ring is prevented from being in contact with the second circular ring to cause short circuit.
Further, the third groove is of an L-shaped structure; the fourth groove is of an L-shaped structure, so that the charging terminal is more firmly contacted with a power supply.
Furthermore, a first binding post is fixed at one end of the first circular ring; and a second binding post is fixed at one end of the second circular ring.
Furthermore, the fixing seat is of a clamping groove structure, so that the fixing seat is convenient to disassemble, assemble and maintain.
Further, the first connecting sleeve is of a cylindrical structure; a fifth groove is formed in the inner surface of the first connecting sleeve; and a sixth groove is formed on the inner surface of the second sleeve.
The invention has the following beneficial effects:
1. the invention uses the buckle connection, so that the whole mechanism is simpler to disassemble and assemble and is convenient to maintain.
2. According to the invention, by using the telescopic double-ring charging terminal structure, the charging terminal can automatically feed, and the unmanned aerial vehicle can autonomously charge, so that the working efficiency is improved, the cost is reduced, and the problem that the existing unmanned aerial vehicle needs manual operation for charging is solved.
Of course, it is not necessary for any product in which the invention is practiced to achieve all of the above-described advantages at the same time.
Drawings
In order to more clearly illustrate the technical solutions of the embodiments of the present invention, the drawings used in the description of the embodiments will be briefly introduced below, and it is obvious that the drawings in the following description are only some embodiments of the present invention, and it is obvious for those skilled in the art that other drawings can be obtained according to the drawings without creative efforts.
Fig. 1 is a schematic structural diagram of an unmanned aerial vehicle with a charging support terminal according to the present invention;
FIG. 2 is a schematic structural view of the body;
FIG. 3 is a schematic structural view of the telescopic rod;
FIG. 4 is a schematic structural view of the first coupling sleeve;
FIG. 5 is a bottom view of the first coupling sleeve;
fig. 6 is a structural bottom view of the second connecting sleeve;
fig. 7 is a schematic structural view of the second connecting sleeve;
FIG. 8 is a schematic view of a terminal structure;
fig. 9 is a structural bottom view of the terminal;
in the drawings, the components represented by the respective reference numerals are listed below:
1-body, 2-telescopic rod, 3-first connecting sleeve, 4-second connecting sleeve, 5-terminal, 101-fixed seat, 201-seventh groove, 301-fifth groove, 302-first fixing plate, 303-first groove, 304-first limiting block, 401-first sleeve, 402-second sleeve, 403-connecting plate, 404-second fixing plate, 405-second groove, 406-second limiting block, 407-sixth groove, 501-first ring, 502-second ring, 503-rubber layer, 5011-first through hole, 5012-first binding post, 5013-third groove, 5021-second through hole, 5022-second binding post and 5023-fourth groove.
Detailed Description
The technical solutions in the embodiments of the present invention will be clearly and completely described below with reference to the drawings in the embodiments of the present invention, and it is obvious that the described embodiments are only a part of the embodiments of the present invention, and not all of the embodiments. All other embodiments, which can be derived by a person skilled in the art from the embodiments given herein without making any creative effort, shall fall within the protection scope of the present invention.
In the description of the present invention, it is to be understood that the terms "opening," "upper," "lower," "thickness," "top," "middle," "length," "inner," "peripheral," and the like are used in an orientation or positional relationship that is merely for convenience in describing and simplifying the description, and do not indicate or imply that the referenced component or element must have a particular orientation, be constructed and operated in a particular orientation, and thus should not be considered as limiting the present invention.
Referring to fig. 1-9, the present invention relates to an unmanned aerial vehicle with a charging support terminal, which comprises a main body 1, a telescopic rod 2, a first connecting sleeve 3, a second connecting sleeve 4 and a terminal 5;
two fixed seats 101 are fixed on the inner surface of the body 1; a telescopic rod 2 is fixed on one surface of the fixed seat 101; a seventh groove 201 is formed on the peripheral side surface of the telescopic rod 2;
two first fixing plates 302 are oppositely fixed on one end surface of the first connecting sleeve 3; a first groove 303 is formed on one surface of the first fixing plate 302; two first limiting blocks 304 are oppositely fixed on the inner surface of the first groove 303;
the second connecting sleeve 4 comprises a first sleeve 401 and a second sleeve 402; the first sleeve 401 and the second sleeve 402 are fixedly connected through a connecting plate 403; two second fixing plates 404 are oppositely fixed on one end face of the first sleeve 401; a second groove 405 is formed on one surface of the second fixing plate 404; two second limiting blocks 406 are relatively fixed on the inner surface of the second groove 405;
the terminal 5 includes a first ring 501 and a second ring 502; a first through hole 5011 is formed in the peripheral side surface of the first ring 501; one end of the first ring 501 is provided with two third grooves 5013; a second through hole 5021 is formed on the peripheral side surface of the second ring 502; one end of the second ring 502 is provided with two fourth grooves 5023;
one end of the telescopic rod 2 is in threaded fit with the first connecting sleeve 3; one end of the other telescopic rod 2 is in threaded fit with the second sleeve 402; the first stopper 304 is matched with the first through hole 5011; the second stopper 406 is engaged with the second through hole 5021.
A rubber layer 503 is arranged between the outer surface of the first ring 501 and the inner surface of the second ring 502 to prevent the first ring from contacting with the second ring to generate short circuit.
Wherein, the third slot 5013 is of an L-shaped structure; the fourth groove 5023 is an L-shaped structure, so that the charging terminal is more firmly contacted with a power supply.
Wherein, one end of the first ring 501 is fixed with a first terminal 5012; a second terminal 5022 is fixed at one end of the second ring 502.
Wherein, fixing base 101 is the draw-in groove structure, makes things convenient for dismouting and maintenance.
Wherein, the first connecting sleeve 3 is a cylinder structure; a fifth groove 301 is formed in the inner surface of the first connecting sleeve 3; the inner surface of the second sleeve 402 is provided with a sixth concave groove 407, and the concave groove is internally provided with internal threads.
In the description herein, references to the description of "one embodiment," "an example," "a specific example" or the like are intended to mean that a particular feature, structure, material, or characteristic described in connection with the embodiment or example is included in at least one embodiment or example of the invention. In this specification, the schematic representations of the terms used above do not necessarily refer to the same embodiment or example. Furthermore, the particular features, structures, materials, or characteristics described may be combined in any suitable manner in any one or more embodiments or examples.
The preferred embodiments of the invention disclosed above are intended to be illustrative only. The preferred embodiments are not intended to be exhaustive or to limit the invention to the precise embodiments disclosed. Obviously, many modifications and variations are possible in light of the above teaching. The embodiments were chosen and described in order to best explain the principles of the invention and the practical application, to thereby enable others skilled in the art to best utilize the invention. The invention is limited only by the claims and their full scope and equivalents.
Claims (3)
1. An unmanned aerial vehicle with a charging support terminal comprises a body (1), an expansion link (2), a first connecting sleeve (3), a second connecting sleeve (4) and a terminal (5); a plurality of fixed seats (101) are fixed on the inner surface of the body (1); a telescopic rod (2) is fixed on one surface of the fixed seat (101); a seventh groove (201) is formed in the peripheral side surface of the telescopic rod (2); a plurality of first fixing plates (302) are fixed on one end face of the first connecting sleeve (3); a first groove (303) is formed on one surface of the first fixing plate (302); a plurality of first limiting blocks (304) are fixed on the inner surface of the first groove (303); the second connecting sleeve (4) comprises a first sleeve (401) and a second sleeve (402); the first sleeve (401) and the second sleeve (402) are fixedly connected through a connecting plate (403); a plurality of second fixing plates (404) are fixed on one end face of the first sleeve (401); a second groove (405) is formed on one surface of the second fixing plate (404); a plurality of second limiting blocks (406) are fixed on the inner surface of the second groove (405); one end of the telescopic rod (2) is matched with the first connecting sleeve (3); one end of the telescopic rod (2) is matched with the second sleeve (402); the first limiting block (304) is matched with the first through hole (5011); the second limiting block (406) is matched with the second through hole (5021);
the method is characterized in that:
the terminal (5) comprises a first circular ring (501) and a second circular ring (502); a first through hole (5011) is formed in the peripheral side face of the first circular ring (501); one end of the first circular ring (501) is provided with a plurality of third grooves (5013); a second through hole (5021) is formed in the peripheral side face of the second circular ring (502); one end of the second circular ring (502) is provided with a plurality of fourth grooves (5023); a rubber layer (503) is arranged between the outer surface of the first circular ring (501) and the inner surface of the second circular ring (502); the third groove (5013) is of an L-shaped structure; the fourth groove (5023) is of an L-shaped structure; one end of the first ring (501) is fixed with a first binding post (5012); one end of the second circular ring (502) is fixed with a second binding post (5022).
2. The unmanned aerial vehicle of claim 1, wherein the fixing base (101) is a slot structure.
3. The unmanned aerial vehicle with the charging support terminal as claimed in claim 1, wherein the first connecting sleeve (3) is of a cylindrical structure; a fifth groove (301) is formed in the inner surface of the first connecting sleeve (3); the inner surface of the second sleeve (402) is provided with a sixth groove (407).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201810046260.0A CN108275278B (en) | 2018-01-17 | 2018-01-17 | Unmanned aerial vehicle of support terminal charges in area |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201810046260.0A CN108275278B (en) | 2018-01-17 | 2018-01-17 | Unmanned aerial vehicle of support terminal charges in area |
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| Publication Number | Publication Date |
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| CN108275278A CN108275278A (en) | 2018-07-13 |
| CN108275278B true CN108275278B (en) | 2021-07-27 |
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| Application Number | Title | Priority Date | Filing Date |
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| CN201810046260.0A Active CN108275278B (en) | 2018-01-17 | 2018-01-17 | Unmanned aerial vehicle of support terminal charges in area |
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Families Citing this family (1)
| Publication number | Priority date | Publication date | Assignee | Title |
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| CN110103748A (en) * | 2019-05-24 | 2019-08-09 | 中国科学院地理科学与资源研究所 | A kind of magnetic-type charging unit of small drone |
Citations (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106043725A (en) * | 2016-06-30 | 2016-10-26 | 张春生 | Shipborne unmanned plane charging device |
| CN205811594U (en) * | 2016-06-24 | 2016-12-14 | 国网安徽省电力公司黄山供电公司 | Electric power remote line walking unmanned plane charging station |
| JP6179687B1 (en) * | 2016-07-12 | 2017-08-16 | 中国電力株式会社 | Unmanned air vehicle, power receiving coil unit, and charging system |
| CN107128490A (en) * | 2017-05-03 | 2017-09-05 | 国网青海省电力公司海南供电公司 | Electric inspection process automatic charging unmanned plane |
Family Cites Families (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US20170282734A1 (en) * | 2016-04-04 | 2017-10-05 | Skycatch, Inc. | Unmanned aerial vehicle self-aligning battery assembly |
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2018
- 2018-01-17 CN CN201810046260.0A patent/CN108275278B/en active Active
Patent Citations (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN205811594U (en) * | 2016-06-24 | 2016-12-14 | 国网安徽省电力公司黄山供电公司 | Electric power remote line walking unmanned plane charging station |
| CN106043725A (en) * | 2016-06-30 | 2016-10-26 | 张春生 | Shipborne unmanned plane charging device |
| JP6179687B1 (en) * | 2016-07-12 | 2017-08-16 | 中国電力株式会社 | Unmanned air vehicle, power receiving coil unit, and charging system |
| CN107128490A (en) * | 2017-05-03 | 2017-09-05 | 国网青海省电力公司海南供电公司 | Electric inspection process automatic charging unmanned plane |
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| CN108275278A (en) | 2018-07-13 |
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Effective date of registration: 20240527 Address after: 230000, Future Center Building, Advanced Technology Research Institute, University of Science and Technology of China, No. 5089 Wangjiang West Road, High tech Zone, Hefei City, Anhui Province Patentee after: Wang Xingsheng Country or region after: China Address before: 230000 702, building 19, Yifang city garden, 426 Songlin Road, Hefei Economic and Technological Development Zone, Anhui Province Patentee before: ANHUI ZHONGJIANG ENVIRONMENTAL TECHNOLOGY Co.,Ltd. Country or region before: China |