CN1830724A - Self-rotating stable type aircraft - Google Patents
Self-rotating stable type aircraft Download PDFInfo
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- CN1830724A CN1830724A CN 200610012613 CN200610012613A CN1830724A CN 1830724 A CN1830724 A CN 1830724A CN 200610012613 CN200610012613 CN 200610012613 CN 200610012613 A CN200610012613 A CN 200610012613A CN 1830724 A CN1830724 A CN 1830724A
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- aircraft
- self
- stable type
- rotating
- type aircraft
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Abstract
A spin stabilized flying vehicle is disclosed, which is designed on the basis of spin stabilizing principle, so its design principle and flying effect are different from other flying vehicles.
Description
Affiliated technical field
The present invention relates to a kind of self-rotating stable type aircraft, its principle of design and practical flight effect all are different from existing all kinds of aircraft.Be that principle design according to spin stabilization forms.
Background technology
At present, known aircraft all is to utilize the thrust of driving engine and/or machine (revolving) wing etc. to provide lift to reach the purpose of flight.Can be if wish from ground up to space, even extraterrestrially can fly whenever and wherever possible, hover, then there is not a kind of aircraft directly to accomplish at present.
Summary of the invention
In order to be implemented in atmospheric envelope, space even the extraterrestrial aircraft solution plan that all is suitable for, the invention provides a kind of actv. Flight Vehicle Design thinking.
The technical solution adopted for the present invention to solve the technical problems is: with two or the driving engine (vector propeller) of many controlled (change) spray angles aircraft not only can be spinned but also can fly to all directions.Aircraft central authorities then can realize carrying people to fly as adding metastable part.
The invention has the beneficial effects as follows, can take off at an arbitrary position and land, do not need runway.Can stop in the optional position, endoatmosphere, add or the rocket engine that changes the outfit, then can realize space flight, particularly what is interesting is to provide a kind of effective and damage-free landing mode for all kinds of extraterrestrial detectors.
Description of drawings
Below in conjunction with accompanying drawing (being scheme drawing) to the present invention do further wash bright.
Fig. 1 is the aircraft lateral plan.
Fig. 2 is the aircraft birds-eye view.
Fig. 3 is the exploded orthogonal view of vector propeller propulsive force.
Fig. 4 is the self-rotating stable type aircraft section-drawing of the relatively stable part in tool center.
Fig. 5 is the self-rotating stable type aircraft birds-eye view of the relatively stable part in tool center
Among the figure (1). aircraft rotating part, (2). vector propeller, (3). the relatively stable portion in aircraft center, F. vector propeller propulsive force, F
1.F horizontal resolution, F
2.F vertical resolution.
The specific embodiment
Changeable angle that vector propeller sends and big or small power (F among Fig. 3) can be broken down into the power (F among Fig. 3 that promotes the aircraft spin
1) and promote the power (F among Fig. 3 that aircraft rises
2), by angle and the size that changes vector propeller thrust, and the time of taking place, position realize aircraft is carried out the control of running state.At the self-rotating stable type aircraft center metastable part is set, can flies synchronously with aircraft, and not spin, can realize manned and control.
Claims (8)
1. self-rotating stable type aircraft principle of design, it is characterized in that: according to object spin stabilization principle, utilize vector propeller that the power of aircraft around its axle center spin stabilization both can be provided, the power that makes himself rising, decline and change of flight direction can be provided again, reach purpose in the earth, space, extraterrestrial controllable flight.
2, self-rotating stable type aircraft mentality of designing, it is characterized in that: make according to object spin stabilization principle, can realize both can relying on air also can not rely on air and can be from ground up to space, even extraterrestrially can take off whenever and wherever possible, fly, hover, land, a kind of aircraft that is different from existing all kinds of offline mode.
3. the self-rotating stable type aircraft control principle is characterized in that: rely on the direction and size of regulating the thrust vectoring that vector propeller produced, and the control of all running statees is carried out in the time, the position that take place to aircraft.
4. all purposes of self-rotating stable type aircraft is characterized in that: utilize the characteristic of self-rotating stable type aircraft and drill living practical use with the general character of present all kinds of artificial aircraft.
5, the relatively stable part at self-rotating stable type aircraft center is characterized in that: at the self-rotating stable type aircraft center metastable part is set, can flies synchronously with aircraft, and not spin.
6, contacting and the noncontact connection mode between self-rotating stable type aircraft stator and rotor is characterized in that: realizing the connection mode that the relatively stable part at aircraft center does not spin with aircraft flight synchronously, can be that contact also can be contactless.
7, self-rotating stable type aircraft rotation and relatively stable part bonded assembly magnetic suspension design, it is characterized in that: for realizing carrying people to fly, metastable part must be set, i.e. " stator ", the connection mode of itself and rotating part (being rotor) can be a contact, also can be contactless, and contactless with electromagnetic levitation type efficient, best results, also can select other modes as required.
8, the information transmitting methods between self-rotating stable type aircraft stator and rotor is characterized in that: realize that with variety of ways such as digital optical signals both transmit the method for information mutually.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN 200610012613 CN1830724A (en) | 2006-04-20 | 2006-04-20 | Self-rotating stable type aircraft |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN 200610012613 CN1830724A (en) | 2006-04-20 | 2006-04-20 | Self-rotating stable type aircraft |
Publications (1)
Publication Number | Publication Date |
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CN1830724A true CN1830724A (en) | 2006-09-13 |
Family
ID=36993260
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
CN 200610012613 Pending CN1830724A (en) | 2006-04-20 | 2006-04-20 | Self-rotating stable type aircraft |
Country Status (1)
Country | Link |
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CN (1) | CN1830724A (en) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
WO2013004070A1 (en) * | 2011-07-04 | 2013-01-10 | Liu Gang | Spherical saucer-shaped aviation aircraft |
-
2006
- 2006-04-20 CN CN 200610012613 patent/CN1830724A/en active Pending
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
WO2013004070A1 (en) * | 2011-07-04 | 2013-01-10 | Liu Gang | Spherical saucer-shaped aviation aircraft |
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C06 | Publication | ||
PB01 | Publication | ||
C10 | Entry into substantive examination | ||
SE01 | Entry into force of request for substantive examination | ||
C02 | Deemed withdrawal of patent application after publication (patent law 2001) | ||
WD01 | Invention patent application deemed withdrawn after publication |