CN1305923A - Free-state space vehicle - Google Patents
Free-state space vehicle Download PDFInfo
- Publication number
- CN1305923A CN1305923A CN 00114025 CN00114025A CN1305923A CN 1305923 A CN1305923 A CN 1305923A CN 00114025 CN00114025 CN 00114025 CN 00114025 A CN00114025 A CN 00114025A CN 1305923 A CN1305923 A CN 1305923A
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- main body
- annular turbine
- coil
- gear
- free
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Abstract
A flying vehicle for free space is composed of a truncated spherial main body, external annular turbine linked to the engine in main body via gears, and 8-pole coil with magnetic field arranged at flat botton. It can fly in the free space, such as air and water.
Description
The present invention relates to a kind of can be at the free-state space vehicle of various free state spaceflights or navigation.
In Earth'S atmosphere, aircraft or rocket rely on driving engine to spray high velocity air to afterbody, thereby obtain reaction thrust flight; Autogyro then relies on the propeller high speed revolution at top to produce the vacuum control height, and the propeller controlling party of afterbody is to flight.Steamer on the water surface and water submarine not is by propeller draining navigation.They have a common ground, drive the air of free state or water to reach the purpose of motion by propeller or driving engine [for example: turbo type engine] exactly.
Though autogyro, aircraft, rocket, steamer, the various technology of submarine are along with development in science and technology is constantly perfect, even hydroairplane appearred, in some scientific and technological relatively advanced countries, submarine rocket also begins application implementation, but because the reason of many aspects [for example: hydroairplane involves great expense, rocket is serious etc. to environmental disruption], from popularization and the range of use that has limited them to a great extent.
The objective of the invention is to provide a kind of free-state space vehicle, and it can free state space do flight arbitrarily just in empty G﹠W.
Free-state space vehicle of the present invention is made up of the annular turbine of the main body of a segment shape and an outer button, and a circle ends of the earth coil is arranged at smooth bottom, shields with magnetic medium in the middle of the coil of the ends of the earth, and annular turbine connects with driving engine in the main body by gear.Open driving engine and make the annular turbine rotation, this moment, annular turbine was discharged air-flow or current up or down, control or raising air-flow or water velocity, thereby the purpose that reaches diving or fly.And ends of the earth coil be used for controlling party to.
The present invention is owing to adopt the annular turbine of outer button to advance in conjunction with ends of the earth coil, so the very wide model of its flight range: can move in the water high speed because being equipped with the intrinsic water tank of submarine; It can not need large-scale adrm by vertical lift.Can not produce rocket or jet plane a large amount of tail gas like that.
The present invention is described in further detail below in conjunction with the drawings and specific embodiments.
Fig. 1 is the cross-sectional view of the free-state space vehicle structure of proposition according to the present invention; Fig. 2 is its longitudinal section; Fig. 3 is the cross sectional drawing of the ends of the earth coil of this aircraft bottom.
Structure of the present invention comprises segment shape aircraft body 1, annular turbine 2, ends of the earth coil 3-10, control power supply 11, driving engine 12, transmission shaft 13, gear 14-17, its middle gear 14,15 are fixed in the two ends of transmission shaft 13, and gear 16,17 plays stationary annular turbine 2, magnetic medium screen layer 18.
Start the engine 12, by gear 14,15, transmission shaft 13 rotates annular turbine 2:
Embodiment A: annular turbine 2 slow rotation, make annular turbine 2 upwards drainings, then this aircraft is dived under water downwards.Control driving engine 12 operating speves just can the downward speed of diving under water of controlling aircraft.
Embodiment B: annular turbine 2 slow rotation, make annular turbine 2 downward drainings, this aircraft buoyance lift that makes progress then, when aircraft near the water surface, form vacuum thereby further improve rotating speed, this aircraft will leave the follow-up continuous flight of the water surface.
Embodiment C: in the flight or the process of moving under water of aircraft, open control power supply 11, give symmetric coil 3,6 energisings, make their polarity opposite, so the magnetic field of the as many as one group of coil generation in the magnetic field of coil 3,6 at this moment is coil 3,----aircraft body 1 rotation under geomagnetic field action of having an effect of 6 magnetic fields that produced and geomagnetic field, aircraft body keeps stable, i.e. no longer rotation when the polarity in the polarity of the magnetic field of coil 3,6 and geomagnetic field is opposite.Regulating winding 3,6 magnetic intensity is between the two perhaps given other one group of coil electricity, just can the controlling aircraft heading.
Claims (3)
1, a kind of free-state space vehicle, be made up of the main body 1 of a segment shape and the annular turbine 2 of an outer button, a circle ends of the earth coil 3-10 is arranged at main body 1 smooth bottom, and its power supply is provided by control power supply 11, shield with magnetic medium screen layer 18 in the middle of the coil of the ends of the earth, the gear 14,15 of annular turbine 2 by being fixed in transmission shaft 13 two ends connects transmission shaft 13 and gear 15 with driving engine 12 in the main body 1,16,17 are fixed in annular turbine 2 on the main body 1.
2, aircraft according to claim 1 is characterized in that transmission shaft 13 and gear 15,16,17 are fixed in annular turbine 2 on the main body 1, can only rotate with respect to main body to guarantee annular turbine 2, and the relative motion that can not produce alternate manner.
3, aircraft according to claim 1 is characterized in that controlling the magnetic field properties that power supply 11 is controlled ends of the earth coil 3-10, keeps main body stable.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN 00114025 CN1305923A (en) | 2000-01-19 | 2000-01-19 | Free-state space vehicle |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN 00114025 CN1305923A (en) | 2000-01-19 | 2000-01-19 | Free-state space vehicle |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN1305923A true CN1305923A (en) | 2001-08-01 |
Family
ID=4583750
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN 00114025 Pending CN1305923A (en) | 2000-01-19 | 2000-01-19 | Free-state space vehicle |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN1305923A (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108033009A (en) * | 2017-12-08 | 2018-05-15 | 燕胜 | A kind of magnetomotive inspection aircraft based on magnetic field |
-
2000
- 2000-01-19 CN CN 00114025 patent/CN1305923A/en active Pending
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108033009A (en) * | 2017-12-08 | 2018-05-15 | 燕胜 | A kind of magnetomotive inspection aircraft based on magnetic field |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C06 | Publication | ||
| PB01 | Publication | ||
| C02 | Deemed withdrawal of patent application after publication (patent law 2001) | ||
| WD01 | Invention patent application deemed withdrawn after publication |