CN2528706Y - Manned craft - Google Patents
Manned craft Download PDFInfo
- Publication number
- CN2528706Y CN2528706Y CN 02203371 CN02203371U CN2528706Y CN 2528706 Y CN2528706 Y CN 2528706Y CN 02203371 CN02203371 CN 02203371 CN 02203371 U CN02203371 U CN 02203371U CN 2528706 Y CN2528706 Y CN 2528706Y
- Authority
- CN
- China
- Prior art keywords
- manned craft
- open top
- top roll
- manned
- craft
- 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
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Abstract
The utility model relates to a manned craft with a shape that is like a disk flying object. An open frame is internally provided with a closed bearing cabin and a horizontal rotor driven by a maglev superconductive electric motor. A jet engine with a circumrotating nozzle may be arranged under the bearing cabin. A solar cell plate and a vertical rubber are arranged on the open frame. The manner craft of flying object type of the utility model overcomes the disadvantages of the existing helicopters, fire balloons, airships and other crafts and has the advantages of low cost, good flying performance, saving energy, long flying and hang time, wide application and great exploitation prospect.
Description
Technical field
The utility model relates to manned craft.
Background technology
Existing aircraft has aircraft, dirigible, fire balloon etc.Aircraft flight speed is fast, and voyage is long, but energy consumption is big, the hang time short; Dirigible is simple in structure, and manufacturing cost and use cost is low, but the speed of a ship or plane is low, and flight control is dumb; The fire balloon range of use is limited, generally is used for exploring and sports.
Summary of the invention
The utility model is exactly to overcome the shortcoming that existing multiple aircraft exists, and provides a kind of cost low, saves the energy, and flight maneuver is flexible, flight, long manned craft of hang time.
The utility model manned craft shape such as disk flying saucer adopt open top roll housing, and its centre is closed carrying storehouse and electrical motor, and the rotor of electrical motor links to each other with main rotor, and aircraft has the vertical direction rudder on the top.
This flying disc type manned craft relies on huge main rotor landing, by vertical direction rudder control heading, and maneuverability, the aircraft time is long, and it is aerial also can to hover, and purposes is very extensive.
For reducing expenditure of energy, the driving engine of this manned craft can adopt the magnetic suspension superconducting motor, to increase the flight time, prolongs the fixed point hang time.Also can solar panel be set on frame, make full use of inexhaustible solar power.
For improving airworthiness, can adopt major diameter, high amount of deflection main rotor, and on the frame under the main rotor, establish annular magnetic suspension support slideway, sagging when avoiding the main rotor low-speed running, the touching frame.
For improving the takeoff data and the manoevreability of manned craft, the jet engine with rotatable nozzle can be set under manned craft open top roll housing centre also.
Description of drawings
Fig. 1 is the utility model flying disc type manned craft structural representation.
Fig. 2 is Fig. 1 manned craft schematic top plan view.
Among the figure, 1 landing pad, 2 rotatable nozzles, 3 jet engines, 4 annular brace slideways, 5 open top roll housings, 6 solar panels, 7 main rotors, 8 levitating electromagnets, 9 motor rotors, 10 motor stators, 11 electrical motors, 12 carrying storehouses, 13 vertical direction rudders.
The specific embodiment
As Fig. 1, shown in Figure 2, the utility model manned craft shape such as disk flying saucer, the centre of its open top roll housing 5 is osed top carrying storehouse 12, the electrical motor 11 of warehouse middle part for being made of motor rotor 9 and motor stator 10.Electrical motor 11 adopts and surpasses, leads material, divides into magnetic suspension electromagnet 8 on the motor rotor 9, and it is extremely low to constitute energy consumption, the magnetic suspension superconducting motor that efficient is high.The fuel cell that carries except that manned craft provides the electric energy, on the open top roll housing 5 of manned craft large-area solar panel 6 can be installed, to make full use of high aerial inexhaustible solar power, keep the running of superconducting motor, the utility model manned craft relies on huge relatively main rotor 7 to produce lift, and it is aerial that aircraft lift-off flight or fixed point are detained.Vertical direction rudder 13 on the open top roll housing 5 is in order to the heading of control and stabilized flight device.Annular magnetic suspension support slideway 4 is arranged on the open top roll housing 5 under the main rotor 7 of manned craft,, prevent that main rotor 7 from touching open top roll housing 5 to support the main rotor 7 of low-speed running and stall.Jet engine 3 with rotatable nozzle 2 is arranged under open top roll housing 5 centres.The nozzle mouth goes up to the air manned craft towards ground fast when taking off; During flight, handle the jet direction of nozzle 2, can controlling aircraft heading and acceleration flight.
Claims (5)
1, a kind of manned craft, it is characterized in that said aircraft shape such as disk flying saucer, adopt open top roll housing (5), its centre is closed carrying storehouse (12) and electrical motor (11), the motor rotor (9) of electrical motor (11) links to each other with main rotor (7), and go up on the aircraft top also has vertical direction rudder (13).
2, manned craft according to claim 1 is characterized in that said electrical motor (11) is the magnetic suspension superconducting motor.
3, manned craft according to claim 1 and 2 is characterized in that having under said open top roll housing (5) centre jet engine (3) with rotatable nozzle (2).
4, manned craft according to claim 1 and 2 is characterized in that being provided with on the said open top roll housing (5) solar panel (6).
5, manned craft according to claim 1 and 2 is characterized in that on the open top roll housing (5) under the said main rotor (7) annular magnetic suspension support slideway (4) being arranged.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN 02203371 CN2528706Y (en) | 2002-01-25 | 2002-01-25 | Manned craft |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN 02203371 CN2528706Y (en) | 2002-01-25 | 2002-01-25 | Manned craft |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN2528706Y true CN2528706Y (en) | 2003-01-01 |
Family
ID=33685578
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN 02203371 Expired - Fee Related CN2528706Y (en) | 2002-01-25 | 2002-01-25 | Manned craft |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN2528706Y (en) |
Cited By (8)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| WO2009143669A1 (en) * | 2008-05-27 | 2009-12-03 | Tian Yu | Aircraft and the power driving system thereof |
| CN101913428A (en) * | 2010-07-26 | 2010-12-15 | 李进朋 | Flying disk |
| CN103507954A (en) * | 2013-02-05 | 2014-01-15 | 李贤明 | Air injection flying saucer |
| CN104908955A (en) * | 2015-05-22 | 2015-09-16 | 中国科学院物理研究所 | Multi-shaft unmanned aerial vehicle |
| CN106892115A (en) * | 2017-04-01 | 2017-06-27 | 李宣南 | A kind of dish-shaped manned craft |
| CN108100209A (en) * | 2017-12-15 | 2018-06-01 | 厦门立思科技股份有限公司 | Magnetic suspension butterfly aircraft |
| CN109018381A (en) * | 2018-08-23 | 2018-12-18 | 陈国宝 | Jet-propelled Electric aircraft |
| CN109018379A (en) * | 2018-08-23 | 2018-12-18 | 陈国宝 | Jet external-rotor electric helicopter |
-
2002
- 2002-01-25 CN CN 02203371 patent/CN2528706Y/en not_active Expired - Fee Related
Cited By (9)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| WO2009143669A1 (en) * | 2008-05-27 | 2009-12-03 | Tian Yu | Aircraft and the power driving system thereof |
| CN101913428A (en) * | 2010-07-26 | 2010-12-15 | 李进朋 | Flying disk |
| CN103507954A (en) * | 2013-02-05 | 2014-01-15 | 李贤明 | Air injection flying saucer |
| CN104908955A (en) * | 2015-05-22 | 2015-09-16 | 中国科学院物理研究所 | Multi-shaft unmanned aerial vehicle |
| CN104908955B (en) * | 2015-05-22 | 2017-04-12 | 中国科学院物理研究所 | Multi-shaft unmanned aerial vehicle |
| CN106892115A (en) * | 2017-04-01 | 2017-06-27 | 李宣南 | A kind of dish-shaped manned craft |
| CN108100209A (en) * | 2017-12-15 | 2018-06-01 | 厦门立思科技股份有限公司 | Magnetic suspension butterfly aircraft |
| CN109018381A (en) * | 2018-08-23 | 2018-12-18 | 陈国宝 | Jet-propelled Electric aircraft |
| CN109018379A (en) * | 2018-08-23 | 2018-12-18 | 陈国宝 | Jet external-rotor electric helicopter |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| C19 | Lapse of patent right due to non-payment of the annual fee | ||
| CF01 | Termination of patent right due to non-payment of annual fee |