CN105235905A - External power-supply ground-effect craft method and equipment - Google Patents
External power-supply ground-effect craft method and equipment Download PDFInfo
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- CN105235905A CN105235905A CN201510595129.6A CN201510595129A CN105235905A CN 105235905 A CN105235905 A CN 105235905A CN 201510595129 A CN201510595129 A CN 201510595129A CN 105235905 A CN105235905 A CN 105235905A
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- external power
- power supply
- supply ground
- effect craft
- craft
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Abstract
An external power-supply ground-effect craft employs an external power-supply ground-effect craft method described in the claim 1, and is characterized in that the craft comprises a fuselage, multiple motor-driven turbines, a propeller, an external power supply, an external power-supply ground-effect craft computer control system and a transmission line; the external power-supply ground-effect craft contains a load platform; and the external power supply supplies power for the ground-effect craft via the transmission line. By employing the external power supply, an internal combustion engine and a fuel tank are saved, weight is reduced by 50%, cost is reduced to 20%, turning movement is facilitated, the speed can reach 200 Km/h, the wind power of the craft usually does not detonate antitank land mine, and the unloaded ground-effect craft directly carries explosive for attacking an enemy target. For commercial application, the external power-supply ground-effect craft directly carries materials and spans water surface and finishes conveying without erecting a floating bridge, and helps to win time for do rescue and relief work. Usage of regenerable electric power accords with the sustainable development idea; and the work continuous time is long up to a few weeks.
Description
Technical field
The present invention relates to external power supply ground effect vehicle method and apparatus.
Background technology
Existing a kind of ground effect vehicle and air cushion vehicle, utilize screw propeller export the antagonistic force of gas generation downwards and depart from ground, directly can comprise armored personnel carrier flight on smooth meadow and water surface loading, but cost be very high.
Summary of the invention
The object of the invention is to provide external power supply ground effect vehicle method and apparatus.
External power supply ground effect vehicle method of the present invention: manufacture an external power supply ground effect vehicle, comprise fuselage, some electric turbines, propelling unit, external power supply, external power supply ground effect vehicle computer control system and power transmission line; External power supply ground effect vehicle contains a load platform; The placement location of external power supply comprises on ground, vehicle and naval vessel; External power supply is by power transmission line supply place effect aircraft.
The present invention realizes the technical scheme of its object according to said external power supply ground effect vehicle method: manufacture an external power supply ground effect vehicle, comprise fuselage, some electric turbines, propelling unit, external power supply, external power supply ground effect vehicle computer control system and power transmission line; External power supply ground effect vehicle contains a load platform; The placement location of external power supply comprises on ground, vehicle and naval vessel; External power supply is by power transmission line supply place effect aircraft.
Beneficial effect: external power supply ground effect vehicle of the present invention adopts external power supply.Can save combustion engine and fuel tank, own wt minimizing 50%, cost are reduced to 20%; Effective load rate is high, simultaneously due to Mass lost facilitate turning movement, running velocity can reach 200 kms/time; There is no combustion engine and electric drive more easily decentralized output and the load real-time matching namely facilitating screw propeller, little on the impact of toning equipment, more easily find that enemy has the firing point of sound and carries out counterattack in the very first time; Also because the low easy miniaturization of cost comprises, a ground effect vehicle is configured to each battlebus as load, dispose military strength and more easily expand depth and area; The wind-force of aircraft is unlikely to ignite antitank mine usually; Ground effect vehicle after unloading directly can carry explosive and attack unfriendly target.
In commercial, external power supply ground effect vehicle, when rescue and relief work, need not set up pontoon bridge, directly goods and materials can be crossed over the water surface and complete conveying, gains time for rescuing; The electric power that can regenerate is used to meet the theory of sustainable development.Run duration can reach several weeks.
Accompanying drawing explanation
Fig. 1 is the fundamental diagram that gully crossed over by an external power supply ground effect vehicle conveying equipment.
Fig. 2 is the fundamental diagram that an external power supply ground effect vehicle makes beach landings.
In figure, 1. external power supply ground effect vehicle; 2. fuselage; 3. electric turbine; 4. propelling unit; 5. external power supply; 6. power transmission line; 7. battlefield robot; 8. logistics car; 9. automatic wire winding device; 10. electric reel; 11. pedestals; 12. amphibious tanks; 14. battleships.
Detailed description of the invention
Fig. 1 provides embodiment 1.
Embodiment 1, manufactures an external power supply ground effect vehicle 1, comprises fuselage 2, some electric turbines 3, propelling unit 4, external power supply 5, external power supply ground effect vehicle computer control system and power transmission line 6.Fuselage 2, as a load platform, loads a battlefield robot 7; Logistics car 8 below by power transmission line 6 and automatic wire winding device 9 externally power supply ground effect vehicle 1 electric energy is provided.Owing to adopting external power supply ground effect vehicle, the obstacle in on-the-spot gully, marshy area and minefield can be overcome, with 200 kms/time speed and snakelike route swoop enemy position.
Automatic wire winding device 9 comprises the pedestal 11 of an electric reel 10 and support electric reel 10.
Fig. 2 provides embodiment 2.
Embodiment 2, external power supply ground effect vehicle 1, comprises fuselage 2, some electric turbines 3, propelling unit 4, external power supply, external power supply ground effect vehicle computer control system and power transmission line 6.Fuselage 2, as a load platform, loads a battlefield robot 7; One's own side's amphibious tank 12 below and battleship 14 all by power transmission line 3 externally power supply ground effect vehicle 1 electric energy is provided.Owing to adopting external power supply ground effect vehicle, on-the-spot sea and the obstacle in beachhead minefield can be overcome, with 200 kms/time speed and snakelike route swoop enemy position.
After making beach landings, battlefield robot 7 drives off from external power supply ground effect vehicle 1 and goes into battle.Now, external power supply ground effect vehicle 1 returns or implements clearance task or directly clashes into the target of enemy.
Claims (2)
1. external power supply ground effect vehicle method: manufacture an external power supply ground effect vehicle, comprise fuselage, some electric turbines, propelling unit, external power supply, external power supply ground effect vehicle computer control system and power transmission line; External power supply ground effect vehicle contains a load platform; The placement location of external power supply comprises on ground, vehicle and naval vessel; External power supply is by power transmission line supply place effect aircraft.
2. external power supply ground effect vehicle, uses the external power supply ground effect vehicle method described in claim 1, it is characterized in that comprising fuselage, some electric turbines, propelling unit, external power supply, external power supply ground effect vehicle computer control system and power transmission line; External power supply ground effect vehicle contains a load platform; External power supply is by power transmission line supply place effect aircraft.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201510595129.6A CN105235905A (en) | 2015-09-18 | 2015-09-18 | External power-supply ground-effect craft method and equipment |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201510595129.6A CN105235905A (en) | 2015-09-18 | 2015-09-18 | External power-supply ground-effect craft method and equipment |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN105235905A true CN105235905A (en) | 2016-01-13 |
Family
ID=55033820
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201510595129.6A Withdrawn CN105235905A (en) | 2015-09-18 | 2015-09-18 | External power-supply ground-effect craft method and equipment |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN105235905A (en) |
Citations (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN101385903A (en) * | 2007-09-14 | 2009-03-18 | 北京德庐影像技术有限责任公司 | Hitching type electric self-service helicopter and system thereof |
| CN101590915A (en) * | 2008-05-27 | 2009-12-02 | 葛振志 | Utilize electric motor driven ground effect vehicle and electric power system |
| US20130233964A1 (en) * | 2012-03-07 | 2013-09-12 | Aurora Flight Sciences Corporation | Tethered aerial system for data gathering |
| WO2014203593A1 (en) * | 2013-06-21 | 2014-12-24 | 株式会社エルム | Control system for remote-control unmanned flight vehicle |
| CN104470804A (en) * | 2012-04-05 | 2015-03-25 | 奥图马股份公司 | Device and method for automatically controlling a winch device and vehicle equipped with said device |
| CN104908928A (en) * | 2015-06-23 | 2015-09-16 | 白立安 | Ground effect aircraft |
-
2015
- 2015-09-18 CN CN201510595129.6A patent/CN105235905A/en not_active Withdrawn
Patent Citations (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN101385903A (en) * | 2007-09-14 | 2009-03-18 | 北京德庐影像技术有限责任公司 | Hitching type electric self-service helicopter and system thereof |
| CN101590915A (en) * | 2008-05-27 | 2009-12-02 | 葛振志 | Utilize electric motor driven ground effect vehicle and electric power system |
| US20130233964A1 (en) * | 2012-03-07 | 2013-09-12 | Aurora Flight Sciences Corporation | Tethered aerial system for data gathering |
| CN104470804A (en) * | 2012-04-05 | 2015-03-25 | 奥图马股份公司 | Device and method for automatically controlling a winch device and vehicle equipped with said device |
| WO2014203593A1 (en) * | 2013-06-21 | 2014-12-24 | 株式会社エルム | Control system for remote-control unmanned flight vehicle |
| CN104908928A (en) * | 2015-06-23 | 2015-09-16 | 白立安 | Ground effect aircraft |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C06 | Publication | ||
| PB01 | Publication | ||
| 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: 20160113 |