CN103112593A - Ground power supply air vehicle and system thereof - Google Patents
Ground power supply air vehicle and system thereof Download PDFInfo
- Publication number
- CN103112593A CN103112593A CN201310023143XA CN201310023143A CN103112593A CN 103112593 A CN103112593 A CN 103112593A CN 201310023143X A CN201310023143X A CN 201310023143XA CN 201310023143 A CN201310023143 A CN 201310023143A CN 103112593 A CN103112593 A CN 103112593A
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- wire
- power supply
- ground power
- air vehicle
- ground
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Abstract
The invention provides a ground power supply air vehicle which comprises an air vehicle body, a motor, an actuating mechanism which is used for generating flying force, a wire which is used for supplying power and a ground power source. The motor drives the actuating mechanism, and the motor is connected with the ground power source through the wire. The ground power supply air vehicle is characterized in that a wire supporting device is arranged outside the air vehicle, the wire is connected with the ground power supply after the wire is supported by the wire supporting device, and therefore the wire is prevented from contacting wings of the air vehicle. The invention further provides a system of the ground power supply air vehicle. The system of the ground power supply air vehicle mainly comprises the air vehicle body, the motor, the actuating mechanism which is used for generating the flying force, the wire which is used for supplying power, the wire supporting device and the ground power source. The motor drives the actuating mechanism, and the motor is connected with the ground power source through the wire. The system of the ground power supply air vehicle is characterized in that the wire supporting device is arranged outside the air vehicle, and the wire is connected with the ground power supply after the wire is supported by the wire supporting device. The ground power supply air vehicle and the system of the ground power supply air vehicle have the advantage of solving the problem that the wire is contacted with the wings of the air vehicle and barrier on the ground.
Description
Technical field
The present invention relates to aircraft.
Background technology
Adopt surface power supply equipment to carry out wired power supply to aircraft, can effectively improve the load-carrying ability of aircraft, and extend cruise duration.Yet wired power supply mode faces two major issues: one is that electric power conductor is easily encountered wing, affects aircraft flight, even causes wire to be cut off; Another problem is that electric power conductor easily touches ground obstacle.
Summary of the invention
The object of the present invention is to provide the wired scheme for electric aircraft in a kind of ground, to realize carrying out safe power supply by not being loaded in carry-on electric supply installation (as: battery, power transmission line) to aircraft.
The invention provides a kind of aircraft of surface power supply, mainly comprise the actuating unit of aircraft body, electrical motor, generation flight forces, wire and the ground power supply of power supply, the direct motor drive actuating unit, be connected with ground power supply by wire, it is characterized in that: aircraft exterior is provided with the wire support device, wire is connected with ground power supply after the wire support device, in order to avoid wire touches the wing of aircraft.
The present invention also provides a kind of aerocraft system of surface power supply, mainly comprise the actuating unit of aircraft body, electrical motor, generation flight forces, wire and the ground power supply of power supply, the direct motor drive actuating unit, be connected with ground power supply by wire, it is characterized in that: aircraft exterior is provided with the wire support device, and wire is connected with ground power supply after the wire support device.
The aerocraft system of wired power supply provided by the invention, its wire that connects aircraft and surface power supply equipment (as: battery, storage battery, voltage transformer, power transmission line etc.) can be promoted by wire lifting device, to avoid ground obstacle.
The aerocraft system of wired power supply provided by the invention, its wire lifting device can be one or more in ground supporting bar, balloon, small-sized rotor craft.
The aerocraft system of wired power supply provided by the invention, its wire can leave (or on bobbin) in receiver in, and in order to elongating apart from use, wire receiver (or bobbin) can be placed on ground, also can be placed on wire lifting device.
The aerocraft system of wired power supply provided by the invention can be by power transmission line carriage power supply (being similar to the power supply mode of electric locomotive).
The aircraft of wired power supply provided by the invention, its advantage is: the problem of touching that has solved electric power conductor and aircraft wing and ground obstacle.
Description of drawings
Fig. 1 is the structural representation of the aircraft of wired power supply of employing ground support strut and balloon;
Fig. 2 is the structural representation of the aircraft of wired power supply of employing ground support and rotor craft;
Fig. 3 is the structural representation of the aircraft of wired power supply of employing power transmission line carriage.
The specific embodiment
Embodiment 1
the aircraft of wired power supply, its structure as shown in Figure 1, comprise aircraft body 7, surface power supply equipment 1---battery, wire 2 and wire lifting device 3---ground support 3.1 and balloon 3.2, wire 2 leaves 4 li of ground receivers (or being entangled on bobbin under balloon) in, wire 2 one termination surface power supply equipment 1, wire 2 is linked Electric aircraft body 7(rotor craft by wire lifting device 3, Fixed Wing AirVehicle or and flapping wing aircraft) on, by the wire support device 5 on Electric aircraft body 7---the line bar is linked on aircraft body 7 and powered.
Embodiment 2
The aircraft of wired power supply, its structure as shown in Figure 2,---battery, wire 2, wire lifting device 3---ground support 3.1 and the rotor craft 3.3 that comprise aircraft body 7, surface power supply equipment 1, wire 2 one termination surface power supply equipment 1, wire 2 is linked aircraft body 7(rotor craft, Fixed Wing AirVehicle or and flapping wing aircraft by wire lifting device 3) on, by the wire support device 5 on aircraft body 7---the line bar is linked on aircraft body 7 and powered.
The aircraft of wired power supply, its structure as shown in Figure 3,---power transmission line, wire 2 and transition apparatus 3---the power transmission line carriage (being similar to the power supply mode of electric locomotive) that comprises aircraft body 7, surface power supply equipment 1, wire 2 leaves 4 li of ground receivers in, wire 2 one termination surface power supply equipment 1, link on aircraft body 7 by transition apparatus 3, wire 2 is linked carry-on voltage transformer 6 by the line bar 5 on aircraft body 7 and is powered.
Claims (7)
1. the aircraft of a surface power supply, the actuating unit that mainly comprises aircraft body, electrical motor and generation flight forces, the direct motor drive actuating unit, be connected with ground power supply by wire, it is characterized in that: aircraft exterior is provided with the wire support device, is used for the wire of support and connection ground power supply.
2. the aerocraft system of a surface power supply, mainly comprise the actuating unit of aircraft body, electrical motor, generation flight forces, wire and the ground power supply of power supply, the direct motor drive actuating unit, be connected with ground power supply by wire, it is characterized in that: aircraft exterior is provided with the wire support device, and wire is connected with ground power supply after the wire support device.
3. according to the aerocraft system of wired power supply claimed in claim 2, it is characterized in that: the wire of described connection aircraft and surface power supply equipment promotes by wire lifting device.
4. according to the aerocraft system of wired power supply claimed in claim 2, it is characterized in that: described wire lifting device is one or more in ground support, balloon, small-sized rotor craft.
5. according to the aerocraft system of claim 2,3 or 4 described wired power supplies, it is characterized in that: described wire leaves in receiver.
6. according to the aerocraft system of claim 2,3 or 4 described wired power supplies, it is characterized in that: described power equipment supply is power transmission line and relevant carriage.
7. according to the aerocraft system of wired power supply claimed in claim 5, it is characterized in that: described power equipment supply is power transmission line and relevant carriage.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201310023143XA CN103112593A (en) | 2013-01-22 | 2013-01-22 | Ground power supply air vehicle and system thereof |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201310023143XA CN103112593A (en) | 2013-01-22 | 2013-01-22 | Ground power supply air vehicle and system thereof |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN103112593A true CN103112593A (en) | 2013-05-22 |
Family
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Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201310023143XA Pending CN103112593A (en) | 2013-01-22 | 2013-01-22 | Ground power supply air vehicle and system thereof |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN103112593A (en) |
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN105083564A (en) * | 2015-09-18 | 2015-11-25 | 施侃超 | Communicating remote-control flight vehicle system with external power source and power-supply power lines |
| CN107016897A (en) * | 2017-05-02 | 2017-08-04 | 北京信息科技大学 | A kind of electromagnetic power Multi-axis aircraft |
| CN107672797A (en) * | 2017-09-30 | 2018-02-09 | 镇江皮埃纳米科技有限公司 | A kind of fire-fighting aircraft |
Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| FR431362A (en) * | 1911-04-22 | 1911-11-09 | Theodore Theodore Kryshtofovic | System for transmitting electrical energy to air vehicles |
| CN1080609A (en) * | 1992-06-29 | 1994-01-12 | 蔡渤啸 | Electric power helicopter |
| CN1446729A (en) * | 2002-03-26 | 2003-10-08 | 刘毅 | Low altitude aircraft with power supplied by wired electricity |
| CN201102628Y (en) * | 2007-09-10 | 2008-08-20 | 新疆生产建设兵团建筑工程科学技术研究院有限责任公司 | Connecting line power aerial vehicle |
| CN101590915A (en) * | 2008-05-27 | 2009-12-02 | 葛振志 | Utilize electric motor driven ground effect vehicle and electric power system |
-
2013
- 2013-01-22 CN CN201310023143XA patent/CN103112593A/en active Pending
Patent Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| FR431362A (en) * | 1911-04-22 | 1911-11-09 | Theodore Theodore Kryshtofovic | System for transmitting electrical energy to air vehicles |
| CN1080609A (en) * | 1992-06-29 | 1994-01-12 | 蔡渤啸 | Electric power helicopter |
| CN1446729A (en) * | 2002-03-26 | 2003-10-08 | 刘毅 | Low altitude aircraft with power supplied by wired electricity |
| CN201102628Y (en) * | 2007-09-10 | 2008-08-20 | 新疆生产建设兵团建筑工程科学技术研究院有限责任公司 | Connecting line power aerial vehicle |
| CN101590915A (en) * | 2008-05-27 | 2009-12-02 | 葛振志 | Utilize electric motor driven ground effect vehicle and electric power system |
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN105083564A (en) * | 2015-09-18 | 2015-11-25 | 施侃超 | Communicating remote-control flight vehicle system with external power source and power-supply power lines |
| CN107016897A (en) * | 2017-05-02 | 2017-08-04 | 北京信息科技大学 | A kind of electromagnetic power Multi-axis aircraft |
| CN107672797A (en) * | 2017-09-30 | 2018-02-09 | 镇江皮埃纳米科技有限公司 | A kind of fire-fighting aircraft |
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Legal Events
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| C06 | Publication | ||
| PB01 | Publication | ||
| C10 | Entry into substantive examination | ||
| SE01 | Entry into force of request for substantive examination | ||
| C05 | Deemed withdrawal (patent law before 1993) | ||
| WD01 | Invention patent application deemed withdrawn after publication |
Application publication date: 20130522 |