CN1107113A - Disc shape flight device - Google Patents
Disc shape flight device Download PDFInfo
- Publication number
- CN1107113A CN1107113A CN 93118239 CN93118239A CN1107113A CN 1107113 A CN1107113 A CN 1107113A CN 93118239 CN93118239 CN 93118239 CN 93118239 A CN93118239 A CN 93118239A CN 1107113 A CN1107113 A CN 1107113A
- Authority
- CN
- China
- Prior art keywords
- compression chamber
- fixed
- electromagnet
- housing
- winding
- 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.)
- Pending
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- Connection Of Motors, Electrical Generators, Mechanical Devices, And The Like (AREA)
Abstract
The space disc relates to the spacecraft field and is composed of housing, generator, motor, and annular compressor which is composed of stator winding, electromagnet, blade wheel, sealing ring, compression chamber, spraying tube and switch. The winding and compression chamber are fixed on the housing, the electromagnet is put on the corresponding position of the winding, on the electromagnet is fixed a blade wheel whose outlet is connected to inlet of the compression chamber, the sealing ring is fixed on the housing and blade wheel respectively, the spraying tube is fixed on the autlet of the compression chamber, the switch is installed on the juncture of compression chamber and spraying tube, when the winding is powered by the generator, the annular electromagnet is drived to rotate, the blade wheel fixed on the electromaget is driven to press the water or air into the compression chamber, the produced high pressure water or air is gprayed out from sporaying tube to produce thrust.
Description
The present invention relates to the aircraft field.
Present various space vehicle all is the autogyro of the jet plane that adopts fuel oil, rotary wing aircraft or propeller type that can vertical lift.Jet-propelled and rotary wing aircraft speed is fast, but can not vertical lift, and the autogyro of propeller type can vertical lift, but speed is unhappy, and they can not do long-distance flight.
The present invention is exactly the deficiency at above-mentioned various aircraft, and a kind of brand-new omnibearing aircraft is provided.This flying saucer is vertical lift fast, energy is forward flight fast, can hover for a long time in any place, various spaces, more peculiar is can be aloft with water in the quick flight of freely coming in and going out or adopt large-scale flying saucer to be combined as a huge cartridge type outer space vehicle through many superpositions, have huge propelling thrust, and the quick flight that can between atmospheric envelope and space, freely come in and go out.
The integral structure of flying saucer is made up of housing (1), electrical generator (2), driving engine (3) and annular compressor.Annular compressor is made up of stator coil (4), ring-shaped rotor electromagnet (5), outflow wheel (6), seal ring (7), compression chamber (8), jet pipe (9) and switch (10).Coil (4) and compression chamber (8) are fixed on the housing (1), electromagnet (5) is placed on and coil (4) corresponding section, seal ring (7) is separately fixed on housing (1) and the impeller (6), impeller (6) is fixed on the electromagnet (5), its outlet communicates with the import of compression chamber (8), jet pipe (9) is fixed on the compression chamber (8), and communicates with the outlet of compression chamber; Switch (10) is placed in the junction of jet pipe (9) and compression chamber (8).
When driving engine (3) drives electrical generator (2) rotation, promptly produce electric current, and feeding coil (4) drives ring-shaped rotor (5), the impeller (6) that is fixed on the ring-shaped rotor (5) promptly produces centnifugal force, air or hydraulic pressure are gone in the compression chamber (8), produce high pressure,, promote flying saucer flight from jet pipe (9) ejection.
The invention has the advantages that simple in structure, in light weight, load capacity is big, flying speed is fast, capacity usage ratio is high, flying distance is far away, and quick vertical lift can be done comprehensive quick flight in various spaces.
Accompanying drawing 1 is a main cutaway view of the present invention.
Accompanying drawing 2 is the A-A cutaway view of accompanying drawing 1.
Below in conjunction with description of drawings embodiment:
Stator coil (4), ring-shaped rotor electromagnet (5) are made with superconductor.Housing (1) and outflow wheel (6) are made with composite material.At housing (1) inner bottom part electrical generator (2) and driving engine (3) are housed, (4) two groups of stator coils are fixed on the top and the medial surface at housing (1) outer wall medial recess place respectively, seal ring (7) is separately fixed on housing (1) and the impeller (6).Compression chamber (8) is fixed on the depression bottom, impeller (6) is fixed on the toroidal magnet rotor (5), rotor (5) is placed on and coil (4) corresponding section, when impeller (6) transfixion, impeller (6) is shelved on the outer wall of compression chamber (8), jet pipe (9) is fixed on the exit of compression chamber (8), jet pipe (9) has 10, be fixed with 4 in the bottom of compression chamber (8), be used for this flying saucer lifting, the side of compression chamber is fixed with 6, is used for advancing, turn to and stopping of flying saucer.Junction at jet pipe (9) and compression chamber is provided with electromagnetic switch (10), is used to control the folding of spout.Establish in the flying saucer automatically, M/C platform and other accessory equipment.
Claims (1)
1, a kind of disc shape flight device is made up of housing (1), electrical generator (2), driving engine (3) and annular compressor; It is characterized in that annular compressor is by stator coil (4), ring-shaped rotor electromagnet (5), outflow wheel (6), seal ring (7), compression chamber (8), jet pipe (9) and switch (10) are formed, coil (4) and compression chamber (8) are fixed on the housing (1), electromagnet (5) is placed on and coil (4) corresponding section, seal ring (7) is separately fixed on housing (1) and the impeller (6), impeller (6) is fixed on the electromagnet (5), its outlet communicates with the import of compression chamber (8), jet pipe (9) is fixed on the compression chamber (8), and communicate with the outlet of compression chamber (8), switch (10) is installed in the junction of jet pipe (9) and compression chamber (8).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN 93118239 CN1107113A (en) | 1993-10-01 | 1993-10-01 | Disc shape flight device |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN 93118239 CN1107113A (en) | 1993-10-01 | 1993-10-01 | Disc shape flight device |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN1107113A true CN1107113A (en) | 1995-08-23 |
Family
ID=4992386
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN 93118239 Pending CN1107113A (en) | 1993-10-01 | 1993-10-01 | Disc shape flight device |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN1107113A (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN103158880A (en) * | 2013-03-04 | 2013-06-19 | 陆建收 | Aerospace motor-driven helicopter |
| CN106428559A (en) * | 2016-11-30 | 2017-02-22 | 吴锜 | Disc type aircraft |
-
1993
- 1993-10-01 CN CN 93118239 patent/CN1107113A/en active Pending
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN103158880A (en) * | 2013-03-04 | 2013-06-19 | 陆建收 | Aerospace motor-driven helicopter |
| CN103158880B (en) * | 2013-03-04 | 2015-12-23 | 陆建收 | Empty sky electric helicopter |
| CN106428559A (en) * | 2016-11-30 | 2017-02-22 | 吴锜 | Disc type aircraft |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C06 | Publication | ||
| PB01 | Publication | ||
| C01 | Deemed withdrawal of patent application (patent law 1993) | ||
| WD01 | Invention patent application deemed withdrawn after publication |