CN105083564A - Communicating remote-control flight vehicle system with external power source and power-supply power lines - Google Patents
Communicating remote-control flight vehicle system with external power source and power-supply power lines Download PDFInfo
- Publication number
- CN105083564A CN105083564A CN201510595192.XA CN201510595192A CN105083564A CN 105083564 A CN105083564 A CN 105083564A CN 201510595192 A CN201510595192 A CN 201510595192A CN 105083564 A CN105083564 A CN 105083564A
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- China
- Prior art keywords
- external power
- flight vehicle
- power source
- aircraft
- power supply
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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
- Y02T50/00—Aeronautics or air transport
- Y02T50/40—Weight reduction
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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
- Y02T50/00—Aeronautics or air transport
- Y02T50/60—Efficient propulsion technologies, e.g. for aircraft
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- Cable Transmission Systems, Equalization Of Radio And Reduction Of Echo (AREA)
Abstract
The invention provides a communicating remote-control flight vehicle system with an external power source and power-supply power lines. The system is characterized by comprising a flight vehicle, the external power source, the power transmission lines and a remote control unit. The flight vehicle comprises a vehicle body, electric spiral propellers or electric rotor wings, a flight state computer control system and a flight vehicle load. Two or more power transmission lines forming a loop with the external power source and the power utilization load of the flight vehicle are adopted; power line carrier communication modules in signal connection with the power transmission lines are arranged on the flight vehicle and the external power source. When the related flight vehicle only needs to be used at a fixed point or within a small range, the weight of many batteries can be reduced by means of the external power source, and the flight vehicle has an ability to hover and fly for a long time; the power transmission lines are used for transmitting signals, which is beneficial for confidentiality.
Description
Technical field
The present invention relates to external power source power line communication remotely-piloted vehicle system.
Background technology
Existing electric remote control aircraft comprises fixed-wing and rotary wind type, and wherein rotary wind type can be divided into again single rotor and many rotors, and they rely on battery-operated, can free flight within the scope of certain space.But its hang time is subject to capacity of cell restriction, and the mode of transmission of information is wireless, and confidentiality is not strong.
Summary of the invention
The object of the invention is to provide the remotely-piloted vehicle that the hang time is longer, security performance is stronger.
The present invention realizes the technical scheme of its object: manufacture an external power source power line communication remotely-piloted vehicle system, comprise aircraft, external power supply, power transmission line and remote controller; Aircraft comprises fuselage, electric propeller or electronic rotor, state of flight computer control system and aircraft load, state of flight computer control system comprises satellite positioning-terminal, accelerometer, magnetometer, pressure sensor and gyroscope, adopts one group more than two to form the power transmission line in loop with the electricity consumption load of external power supply and described aircraft;
external power supply supplies aircraft continually;the PLC communication module that aircraft is all connected with powerline signal containing one with external power supply place
, utilize power line carrier to realize wire signal transmission.
Can also adopt a power supply unsteady flow module, realizing is the electric energy form that described aircraft needs by the high voltage-small current electric energy morphological transformation of power line transmission, the traditional direct current booster circuit that power supply unsteady flow module comprises voltage transformer, inverter and powers to DC machine.
A Digiplex can also be adopted.
Beneficial effect of the present invention: when only needing attachment point or one to use relevant flight device among a small circle, external power source power line communication remotely-piloted vehicle system of the present invention can be saved the weight of many batteries by means of external power supply facility and be had the ability of long-time stagnant sky flight; Power line transmission signal is utilized more to be conducive to maintaining secrecy.Adopt power supply unsteady flow module the external power supply of high voltage-small current can be transformed to the electric energy form of applicable aircraft work, related content can with reference to prior art.Adopt Digiplex, can enable when power transmission line et out of order, instruct aircraft security to land.
Accompanying drawing explanation
Fig. 1 is that an external power source power line communication remotely-piloted vehicle system utilizes power transmission line to carry out the schematic diagram of wire signal transmission.
Fig. 2 is the structure for amplifying schematic diagram of automatic wire winding device in Fig. 1.
1. aircraft in figure; 2. external power supply; 3. power transmission line; 4. Digiplex; 5. aerocamera; 6. automatic wire winding device; 7. PLC communication module; 8. electric reel; 9. pedestal; 10. logistics car.
Detailed description of the invention
Fig. 1 provides embodiment 1.
In embodiment 1, manufacture an external power source power line communication remotely-piloted vehicle system, comprise aircraft 1, external power supply 2, power transmission line 3 and Digiplex 4; Aircraft 1 comprises fuselage, electric propeller or electronic rotor, state of flight computer control system and aircraft load aerocamera 5, state of flight computer control system comprises satellite positioning-terminal, accelerometer, magnetometer, pressure sensor and gyroscope, and aircraft 1 is connected with external power supply 2 with automatic wire winding device 6 by one group of two power transmission line 3; External power supply 2 supplies aircraft 1 continually; The PLC communication module 7 that aircraft 1 is all connected with power transmission line 3 signal containing one with external power supply 2 place, utilizes power transmission line 3 to realize wire signal transmission, carries out communication.About the content of electric line carrier communication can with reference to existing electric wireline Internet technology.
Automatic wire winding device 6 comprises an electric reel 8 and two pedestals 9 be connected with electric reel 8.
External power supply 2 is loaded on a logistics car 10.
Claims (3)
1. external power source power line communication remotely-piloted vehicle system, is characterized in that comprising aircraft, external power supply, power transmission line and remote controller; Aircraft comprises fuselage, electric propeller or electronic rotor, state of flight computer control system and aircraft load, state of flight computer control system comprises satellite positioning-terminal, accelerometer, magnetometer, pressure sensor and gyroscope, adopts one group more than two to form the power transmission line in loop with the electricity consumption load of external power supply and described aircraft; The PLC communication module that aircraft is all connected with powerline signal containing one with external power supply place.
2. according to external power source power line communication remotely-piloted vehicle system according to claim 1, it is characterized in that containing a power supply unsteady flow module, realizing the high voltage-small current electric energy morphological transformation of power line transmission is the electric energy form that described aircraft needs, the traditional direct current booster circuit that power supply unsteady flow module comprises voltage transformer, inverter and powers to DC machine.
3., according to the external power source power line communication remotely-piloted vehicle system described in claims 1 or 2, it is characterized in that containing a Digiplex.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201510595192.XA CN105083564A (en) | 2015-09-18 | 2015-09-18 | Communicating remote-control flight vehicle system with external power source and power-supply power lines |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201510595192.XA CN105083564A (en) | 2015-09-18 | 2015-09-18 | Communicating remote-control flight vehicle system with external power source and power-supply power lines |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN105083564A true CN105083564A (en) | 2015-11-25 |
Family
ID=54565082
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201510595192.XA Withdrawn CN105083564A (en) | 2015-09-18 | 2015-09-18 | Communicating remote-control flight vehicle system with external power source and power-supply power lines |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN105083564A (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109118873A (en) * | 2018-05-28 | 2019-01-01 | 北京摩诘创新科技股份有限公司 | A kind of aircraft control load simulation system and analogy method |
Citations (8)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN201682494U (en) * | 2010-05-20 | 2010-12-22 | 中国电子科技集团公司第三十八研究所 | Captive balloon communication system based on power line carrier equipment |
| CN103101620A (en) * | 2012-12-31 | 2013-05-15 | 天津曙光敬业科技有限公司 | Heavy-load multi-rotor-wing unmanned helicopter |
| CN103112593A (en) * | 2013-01-22 | 2013-05-22 | 王欢 | Ground power supply air vehicle and system thereof |
| CN103144779A (en) * | 2012-11-30 | 2013-06-12 | 中国电子科技集团公司第七研究所 | Multi-rotor-wing unmanned aerial vehicle mooring system |
| CN203638106U (en) * | 2014-01-10 | 2014-06-11 | 江苏艾锐泰克无人飞行器科技有限公司 | Wired power multi-rotor unmanned aerial vehicle |
| CN204250374U (en) * | 2014-10-11 | 2015-04-08 | 王欢 | A kind of electronic aerial photography aircraft |
| CN104691758A (en) * | 2015-03-01 | 2015-06-10 | 朱幕松 | Rotor wing vertical lift electric unmanned machine of linkage fixed wing |
| CN205060039U (en) * | 2015-09-18 | 2016-03-02 | 邱玉燕 | External power source power supply power line communication remote control flight ware system |
-
2015
- 2015-09-18 CN CN201510595192.XA patent/CN105083564A/en not_active Withdrawn
Patent Citations (8)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN201682494U (en) * | 2010-05-20 | 2010-12-22 | 中国电子科技集团公司第三十八研究所 | Captive balloon communication system based on power line carrier equipment |
| CN103144779A (en) * | 2012-11-30 | 2013-06-12 | 中国电子科技集团公司第七研究所 | Multi-rotor-wing unmanned aerial vehicle mooring system |
| CN103101620A (en) * | 2012-12-31 | 2013-05-15 | 天津曙光敬业科技有限公司 | Heavy-load multi-rotor-wing unmanned helicopter |
| CN103112593A (en) * | 2013-01-22 | 2013-05-22 | 王欢 | Ground power supply air vehicle and system thereof |
| CN203638106U (en) * | 2014-01-10 | 2014-06-11 | 江苏艾锐泰克无人飞行器科技有限公司 | Wired power multi-rotor unmanned aerial vehicle |
| CN204250374U (en) * | 2014-10-11 | 2015-04-08 | 王欢 | A kind of electronic aerial photography aircraft |
| CN104691758A (en) * | 2015-03-01 | 2015-06-10 | 朱幕松 | Rotor wing vertical lift electric unmanned machine of linkage fixed wing |
| CN205060039U (en) * | 2015-09-18 | 2016-03-02 | 邱玉燕 | External power source power supply power line communication remote control flight ware system |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109118873A (en) * | 2018-05-28 | 2019-01-01 | 北京摩诘创新科技股份有限公司 | A kind of aircraft control load simulation system and analogy method |
| CN109118873B (en) * | 2018-05-28 | 2021-07-30 | 北京摩诘创新科技股份有限公司 | Aircraft control load simulation system and simulation method |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C06 | Publication | ||
| PB01 | Publication | ||
| CB02 | Change of applicant information |
Address after: 317500 Zhejiang province Wenling City Taiping Street South Road 109 Lane 9 Applicant after: Shi Kanchao Address before: 200336 Shanghai City, Changning District Xianxia Road, Lane 780 No. 38 Room 302 Applicant before: Shi Kanchao |
|
| COR | Change of bibliographic data | ||
| SE01 | Entry into force of request for substantive examination | ||
| SE01 | Entry into force of request for substantive examination | ||
| WW01 | Invention patent application withdrawn after publication | ||
| WW01 | Invention patent application withdrawn after publication |
Application publication date: 20151125 |