CN205150248U - From unmanned aerial vehicle system who takes electric supply cable - Google Patents
From unmanned aerial vehicle system who takes electric supply cable Download PDFInfo
- Publication number
- CN205150248U CN205150248U CN201521001948.5U CN201521001948U CN205150248U CN 205150248 U CN205150248 U CN 205150248U CN 201521001948 U CN201521001948 U CN 201521001948U CN 205150248 U CN205150248 U CN 205150248U
- Authority
- CN
- China
- Prior art keywords
- power cable
- unmanned plane
- uas
- aerial vehicle
- supply device
- 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
Landscapes
- Charge And Discharge Circuits For Batteries Or The Like (AREA)
Abstract
The utility model discloses a from unmanned aerial vehicle system who takes electric supply cable, including main unmanned aerial vehicle, a plurality of unmanned aerial vehicle and ground power supply device of following, it through electric supply cable series connection in proper order, ranks the first to follow unmanned aerial vehicle from unmanned aerial vehicle with main unmanned aerial vehicle connects through the 2nd electric supply cable, arranges at the end from unmanned aerial vehicle through the 3rd electric supply cable with the ground power supply device is connected. The beneficial effects are that: can the long distance, long -time, the low flight of bearing a burden.
Description
Technical field
The utility model relates to a kind of Unmanned Aircraft Systems (UAS) carrying power cable.
Background technology
Robot airplane is called for short " unmanned plane ", and english abbreviation is " UAV ", is the not manned aircraft utilizing radio robot to handle with the process controller provided for oneself.Can be divided into from technical standpoint definition: depopulated helicopter, unmanned fixed-wing aircraft, unmanned multi-rotor aerocraft, unmanned airship, unmanned parasol etc.
Unmanned plane+sector application is the real firm need of unmanned plane.At present taking photo by plane, agricultural plant protection, the field such as mapping application, expanded the purposes of unmanned plane itself greatly.
All there is following problem in existing unmanned plane: power supply duration is limited, flying distance is limited, drag cable bears a heavy burden excessive.
Utility model content
Problem to be solved in the utility model is to provide a kind of Unmanned Aircraft Systems (UAS) carrying power cable can growing distance, long-time, low flight of bearing a heavy burden.
In order to solve the problems of the technologies described above, the technical solution adopted in the utility model is: a kind of Unmanned Aircraft Systems (UAS) carrying power cable, it is characterized in that, comprise main unmanned plane, multiple from unmanned plane and floor power supply device, describedly to be sequentially connected in series from unmanned plane by the first power cable, what rank the first is describedly connected by the second power cable from unmanned plane with described main unmanned plane, comes the described of end and is connected with described floor power supply device by the 3rd power cable from unmanned plane.
Preferably, the above-mentioned Unmanned Aircraft Systems (UAS) carrying power cable, wherein said main unmanned plane comprises main unmanned plane body, is arranged on intrinsic first storage battery of described main unmanned plane, and described second power cable and described first storage battery are electrically connected.
Preferably, the above-mentioned Unmanned Aircraft Systems (UAS) carrying power cable, wherein saidly comprises from unmanned plane body from unmanned plane, is arranged on described from intrinsic second storage battery of unmanned plane, and described first power cable and described second storage battery are electrically connected.
Preferably, the above-mentioned Unmanned Aircraft Systems (UAS) carrying power cable, wherein said first power cable, the second power cable, the 3rd power cable include metal-cored, to be arranged on described metal-cored surface insulating barrier, are provided with reinforced rib in described insulating barrier.
Preferably, the above-mentioned Unmanned Aircraft Systems (UAS) carrying power cable, wherein said 3rd power cable is provided with first interface away from the described termination from unmanned plane, described floor power supply device is provided with the second interface, and described first interface and described second interface removably connect.
Preferably, the above-mentioned Unmanned Aircraft Systems (UAS) carrying power cable, the bottom of wherein said floor power supply device is provided with roller.
Preferably, the above-mentioned Unmanned Aircraft Systems (UAS) carrying power cable, wherein said floor power supply device is rechargeable.
Technique effect of the present utility model is mainly reflected in: electric energy is passed to main unmanned plane by multiple from unmanned plane by floor power supply device successively, and the main unmanned plane therefore in the utility model can be grown distance, fly for a long time; The first power cable can be dragged from unmanned plane up, therefore alleviate the heavy burden of main unmanned plane.
Accompanying drawing explanation
Fig. 1 is structural representation of the present utility model;
Fig. 2 is the structural representation of main unmanned plane in Fig. 1;
Fig. 3 is the structural representation from unmanned plane in Fig. 1;
Fig. 4 is A place partial enlarged drawing in Fig. 1;
Fig. 5 is the transverse sectional view of Fig. 1 first power cable or the second power cable or the 3rd power cable.
Detailed description of the invention
In order to make the purpose of this utility model, technical scheme and advantage clearly understand, below in conjunction with drawings and Examples, the utility model is further elaborated.Should be appreciated that specific embodiment described herein only in order to explain the utility model, and be not used in restriction the utility model.
As shown in Fig. 1,2,3,4,5, a kind of Unmanned Aircraft Systems (UAS) carrying power cable, comprise main unmanned plane 1, multiple from unmanned plane 2 and floor power supply device 3, from unmanned plane 2 by the first power cable according to being connected in series for 4 times, what rank the first is connected from unmanned plane 2 and logical 1 mistake the second power cable 5 of main unmanned plane, comes being connected with floor power supply device 3 by the 3rd power cable 6 from unmanned plane 2 of end.
Main unmanned plane 1 comprises main unmanned plane body 11, be arranged on the first storage battery 12, second power cable 5 in main unmanned plane body 11 and the first storage battery 12 is electrically connected.Comprise from unmanned plane body 21 from unmanned plane 2, be arranged on and be electrically connected from the second storage battery 22, first power cable 4 in unmanned plane body 21 and the second storage battery 22.
During use, main unmanned plane 1 is started, flies in the air from ground forward upward.Main unmanned plane 1 drags the second power cable 5 and flies after n rice, is connected to the second power cable 5 and starts one from unmanned plane 2.The weight of long first power cable 4 of n rice is just equaled, wherein from flying height a little less than main unmanned plane 1 of the flying height of unmanned plane 2 from the rising thrust of unmanned plane 2.
Same, main unmanned plane 1 continues flight forward, just continue mounting upper one from unmanned plane 2.
The first power cable 4, second power cable 5 in the utility model, the 3rd power cable 6 include metal-cored 71, to be arranged on metal-cored 71 surfaces insulating barrier 72, are provided with reinforced rib 73 in insulating barrier 72.Such design makes the resistance to abrasion of the first power cable 4, second power cable 5, the 3rd power cable 6 good, long service life.
Wherein the 3rd power cable 6 is provided with first interface 61 away from the termination from unmanned plane 2, floor power supply device 3 is provided with the second interface 31, first interface 61 and the second interface 31 removably connect, like this design connection that facilitates the 3rd power cable 6 and floor power supply device 3 be separated.
Wherein the bottom of floor power supply device 3 of the present utility model is provided with roller 32, and therefore floor power supply device 3 moves conveniently, and floor power supply device 3 is rechargeable.
Electric energy is passed to main unmanned plane 1 by multiple from unmanned plane 2 by floor power supply device 3 in the utility model successively, and the main unmanned plane 1 therefore in the utility model can be grown distance, fly for a long time; The first power cable 4 can be dragged from unmanned plane 2 up, therefore alleviate the heavy burden of main unmanned plane 1.
Embodiment recited above is described preferred implementation of the present utility model, not limits design of the present utility model and scope.Under the prerequisite not departing from the utility model design concept; the various modification that this area ordinary person makes the technical solution of the utility model and improvement; protection domain of the present utility model all should be dropped into; the technology contents of the utility model request protection, all records in detail in the claims.
Claims (7)
1. one kind carries the Unmanned Aircraft Systems (UAS) of power cable, it is characterized in that: comprise main unmanned plane, multiple from unmanned plane and floor power supply device, describedly to be sequentially connected in series from unmanned plane by the first power cable, what rank the first is describedly connected by the second power cable from unmanned plane with described main unmanned plane, comes the described of end and is connected with described floor power supply device by the 3rd power cable from unmanned plane.
2. the Unmanned Aircraft Systems (UAS) carrying power cable according to claim 1, it is characterized in that: described main unmanned plane comprises main unmanned plane body, is arranged on intrinsic first storage battery of described main unmanned plane, and described second power cable and described first storage battery are electrically connected.
3. the Unmanned Aircraft Systems (UAS) carrying power cable according to claim 1, it is characterized in that: describedly comprise from unmanned plane body from unmanned plane, be arranged on described from intrinsic second storage battery of unmanned plane, described first power cable and described second storage battery are electrically connected.
4. the Unmanned Aircraft Systems (UAS) carrying power cable according to claim 1, it is characterized in that: described first power cable, the second power cable, the 3rd power cable include metal-cored, to be arranged on described metal-cored surface insulating barrier, are provided with reinforced rib in described insulating barrier.
5. the Unmanned Aircraft Systems (UAS) carrying power cable according to claim 1, it is characterized in that: described 3rd power cable is provided with first interface away from the described termination from unmanned plane, described floor power supply device is provided with the second interface, described first interface and described second interface removably connect.
6. carry the Unmanned Aircraft Systems (UAS) of power cable according to claim 1 or 5, it is characterized in that: the bottom of described floor power supply device is provided with roller.
7. carry the Unmanned Aircraft Systems (UAS) of power cable according to claim 1 or 5, it is characterized in that: described floor power supply device is rechargeable.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201521001948.5U CN205150248U (en) | 2015-12-07 | 2015-12-07 | From unmanned aerial vehicle system who takes electric supply cable |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201521001948.5U CN205150248U (en) | 2015-12-07 | 2015-12-07 | From unmanned aerial vehicle system who takes electric supply cable |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN205150248U true CN205150248U (en) | 2016-04-13 |
Family
ID=55685966
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201521001948.5U Expired - Fee Related CN205150248U (en) | 2015-12-07 | 2015-12-07 | From unmanned aerial vehicle system who takes electric supply cable |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN205150248U (en) |
Cited By (9)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106143913A (en) * | 2016-07-20 | 2016-11-23 | 江苏冰城氢能科技有限公司 | Take off vertically electric power system, fixed-wing unmanned plane and method of work |
| CN106506062A (en) * | 2016-11-29 | 2017-03-15 | 中山大学 | The distributed high-speed communication system of cluster unmanned plane and communication means |
| CN106672227A (en) * | 2017-01-07 | 2017-05-17 | 温岭鸿方智能科技有限公司 | Agricultural plant protection system based on multi-rotor UAV (unmanned aerial vehicle) and cross-area plant protection operation method |
| CN106737759A (en) * | 2017-02-27 | 2017-05-31 | *** | A kind of multipurpose overlength flexible aei mechanical arm operating system |
| CN106828901A (en) * | 2017-01-19 | 2017-06-13 | 张万民 | Towing power lead formula multiaxis rotor wing unmanned aerial vehicle extinguishing device and extinguishing method |
| US20190283871A1 (en) * | 2018-03-15 | 2019-09-19 | T-Mobile Usa, Inc. | Inhibiting cable entanglement in tethered drones |
| CN112622657A (en) * | 2020-12-01 | 2021-04-09 | 易瓦特科技股份公司 | Unmanned aerial vehicle formation charging system |
| CN113247256A (en) * | 2021-06-21 | 2021-08-13 | 韩元元 | Aerial passage constructed by unmanned aerial vehicle |
| US11448136B2 (en) | 2020-04-16 | 2022-09-20 | Honeywell International Inc. | Adaptive aircraft electrical power distribution system |
-
2015
- 2015-12-07 CN CN201521001948.5U patent/CN205150248U/en not_active Expired - Fee Related
Cited By (13)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106143913B (en) * | 2016-07-20 | 2019-02-15 | 江苏冰城氢能科技有限公司 | Take off vertically power supply system, fixed-wing unmanned plane and working method |
| CN106143913A (en) * | 2016-07-20 | 2016-11-23 | 江苏冰城氢能科技有限公司 | Take off vertically electric power system, fixed-wing unmanned plane and method of work |
| CN106506062B (en) * | 2016-11-29 | 2020-01-21 | 中山大学 | Distributed rapid communication system and communication method for cluster unmanned aerial vehicle |
| CN106506062A (en) * | 2016-11-29 | 2017-03-15 | 中山大学 | The distributed high-speed communication system of cluster unmanned plane and communication means |
| CN106672227A (en) * | 2017-01-07 | 2017-05-17 | 温岭鸿方智能科技有限公司 | Agricultural plant protection system based on multi-rotor UAV (unmanned aerial vehicle) and cross-area plant protection operation method |
| CN106828901A (en) * | 2017-01-19 | 2017-06-13 | 张万民 | Towing power lead formula multiaxis rotor wing unmanned aerial vehicle extinguishing device and extinguishing method |
| CN106737759A (en) * | 2017-02-27 | 2017-05-31 | *** | A kind of multipurpose overlength flexible aei mechanical arm operating system |
| US20190283871A1 (en) * | 2018-03-15 | 2019-09-19 | T-Mobile Usa, Inc. | Inhibiting cable entanglement in tethered drones |
| WO2019178423A1 (en) * | 2018-03-15 | 2019-09-19 | T-Mobile Usa, Inc. | Inhibiting cable entanglement in tethered drones |
| US10710716B2 (en) | 2018-03-15 | 2020-07-14 | T-Mobile Usa, Inc. | Inhibiting cable entanglement in tethered drones |
| US11448136B2 (en) | 2020-04-16 | 2022-09-20 | Honeywell International Inc. | Adaptive aircraft electrical power distribution system |
| CN112622657A (en) * | 2020-12-01 | 2021-04-09 | 易瓦特科技股份公司 | Unmanned aerial vehicle formation charging system |
| CN113247256A (en) * | 2021-06-21 | 2021-08-13 | 韩元元 | Aerial passage constructed by unmanned aerial vehicle |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CN205150248U (en) | From unmanned aerial vehicle system who takes electric supply cable | |
| JP6810550B2 (en) | Detachment and capture of fixed-wing aircraft | |
| CN104843181B (en) | A kind of oil electric mixed dynamic fixed-wing VUAV system | |
| CN111094131B (en) | System for charging an aircraft | |
| US20140339371A1 (en) | Long Range Electric Aircraft and Method of Operating Same | |
| US11635773B2 (en) | Tilt-frame UAV for agricultural air sampling with a propeller-thrust-governing system that facilitates VTOL capability | |
| CN105966612B (en) | Become posture VTOL unmanned plane | |
| CN202170017U (en) | Unmanned aerial vehicle | |
| CN210634740U (en) | Carry polymorphic type unmanned aerial vehicle's dirigible | |
| CN203544370U (en) | Agricultural multi-rotor unmanned helicopter | |
| US10246185B2 (en) | Aircraft system and method for vertical takeoff and landing | |
| CN110683051A (en) | Power supply system for an aircraft and corresponding aircraft | |
| CN105217033A (en) | Amphibious rotor wing unmanned aerial vehicle | |
| CN104773303A (en) | Long-endurance multi-rotor-wing unmanned aerial vehicle agricultural plant protection method | |
| CN105129097A (en) | Unmanned aerial vehicle capable of taking off and landing vertically | |
| CN204489187U (en) | A kind of vertical takeoff and landing horizontal flight unmanned plane | |
| CN206141833U (en) | Unmanned aerial vehicle system | |
| CN204056287U (en) | A kind of autonomous flight is without active force unmanned plane | |
| CN106005371B (en) | Difference directly drives dynamic three rudder face unmanned planes entirely | |
| CN107554351A (en) | To the aerogenerator device people of high electric air commercial aircraft wireless power | |
| CN111717365A (en) | Carry polymorphic type unmanned aerial vehicle's dirigible | |
| CN203842313U (en) | Novel remote control model with combination of vertical take-off and landing and level fight characteristic of fixed wing | |
| CN202953165U (en) | Mooring rotor lift-off platform system | |
| CN106494604A (en) | Hollow long endurance unmanned aircraft total arrangement | |
| CN104192295B (en) | A kind of autonomous flight is without active force unmanned plane and flying method thereof |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| CF01 | Termination of patent right due to non-payment of annual fee | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20160413 Termination date: 20161207 |