CN101913428A - Flying disk - Google Patents
Flying disk Download PDFInfo
- Publication number
- CN101913428A CN101913428A CN 201010238201 CN201010238201A CN101913428A CN 101913428 A CN101913428 A CN 101913428A CN 201010238201 CN201010238201 CN 201010238201 CN 201010238201 A CN201010238201 A CN 201010238201A CN 101913428 A CN101913428 A CN 101913428A
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- CN
- China
- Prior art keywords
- main body
- flying saucer
- pusher
- flying disk
- hole
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- 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.)
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Abstract
The invention discloses a flying disk comprising a flying disk main body, the center of the flying disk main body is provided with an axial through hole; the through hole is provided with a fan blade assembly; a connecting rod of the fan blade assembly is provided with a power device driving the connecting rod to rotate; and the bottom of the main body of the flying disk is provided with a pusher so that the flying disk flies stably and reliably. The installation structure of a fan is characterized in that both ends of the through hole are provided with brackets; the inner sides of the brackets are provided with shaft sleeves; the tail ends of the shaft sleeves and both ends of a shaft center provided with the fan blade assembly are all provided with hemispherical recesses; a space formed by recessing the shaft sleeves and the shaft center is internally provided with roll balls; the roll balls can both axially and radially support and position the shaft center of the fan blade assembly; the pusher is arranged on the main body of the flying disk through a regulating device, and direction change and the like can be realized by changing the direction of the pusher. The invention adopts double power of the fan blade assembly and the pusher on power, power energy sources can be obtained by burning gases, i.e. hydrogen and the like, and nuclear energy sources and the like can also be used.
Description
Technical field
The present invention relates to a kind of high-altitude vehicle.
Background technology
UFO, the unidentified flying object Chinese meaning is a UFO, is commonly called as flying saucer.The report of witnessing that 20th century were in the past more complete has more than 300.Report according to witnesses, UFO profile (dish shape) how in the form of annular discs, spherical and cigar shape.Late 1940s rises, and UFO is witnessed incident and sharply increased, and has caused the arguement of scientific circles.The scientist who holds a negating attitude thinks that much to witness report insincere, and UFO does not exist, and only people's illusion or eyewitness twist a kind of of natural phenomenon.The yea-sayer thinks that UFO is a kind of real phenomena, by increasing true the confirmation.Till the eighties, total the witnessing in the whole world reported about 100,000.About kind surplus the monograph of UFO about 350, nearly hundred kinds in various periodicals.Countries in the world have a collection of expert to participate in this work.China has also set up the academic research among the people group based on the scientific worker---Chinese UFO research association.China starts publication in 1981 about the science popularization publication " flying saucer exploration " of UFO.Though up to the present, the human mysterious veil that still can't open flying saucer, its concrete structure has no way of learning especially, but only according to the imagination of borrowing people, still can find numerous patent documentations that fly the aspect about flying saucer in the patent database of countries in the world, therefore, the applicant also designs a kind of flying saucer structure, and hope can be contributed share for the mankind's space travel cause.
Summary of the invention
In order to overcome the deficiencies in the prior art, the invention provides a kind of flying saucer simple in structure.
The technical solution adopted for the present invention to solve the technical problems is:
A kind of flying saucer comprises the flying saucer main body, and the center of described flying saucer main body is provided with axial through hole, and the flabellum assembly is installed in the described through hole, and flabellum assembly pipe link has the engine installation that drives its rotation, and the bottom of described flying saucer main body is provided with pusher.
The two ends of described through hole are equipped with support, and described support installed inside has axle sleeve, and the two ends, axle center terminal and installation flabellum assembly of described axle sleeve are provided with the semisphere indent, in the space that described axle sleeve and axle center indent form ball are installed.
Described pusher is installed on the flying saucer main body by control apparatus.
The surface of described flying saucer main body is provided with solar panel.
The invention has the beneficial effects as follows: the center of flying saucer main body of the present invention is provided with axial through hole, and the flabellum assembly is installed in the through hole, and the bottom of flying saucer main body is provided with pusher, has a smooth flight, reliably.The mounting structure of fan is at the two ends of through hole support to be installed, the support installed inside has axle sleeve, the two ends, axle center terminal and installation flabellum assembly of axle sleeve are provided with the semisphere indent, in the space that axle sleeve and axle center indent form ball is installed, ball is in the axle center that axially upwards all can support, locate the flabellum assembly with the footpath, pusher is installed on the flying saucer main body by control apparatus, changes the direction of pusher, can realize break-in etc.The present invention adopts the double dynamical of flabellum assembly and pusher on power, power source can also can adopt nuclear power source etc. from gases such as burning hydrogens.
Description of drawings
The present invention is further described below in conjunction with drawings and Examples.
Fig. 1 is a birds-eye view of the present invention;
Fig. 2 is a upward view of the present invention;
Fig. 3 is that axle of the present invention cuts open figure.
The specific embodiment
With reference to Fig. 1, Fig. 2, Fig. 3, a kind of flying saucer comprises flying saucer main body 1, is provided with working space 7 in the flying saucer main body 1.Be provided with axial through hole 3 in the center of described flying saucer main body 1, in the described through hole 3 flabellum assembly 4 be installed, flabellum assembly pipe link has the engine installation that drives its rotation.Specifically, the two ends of described through hole 3 are equipped with support 5, described support 5 installed inside have axle sleeve 9,10 two ends, axle center terminal and installation flabellum assembly 4 of described axle sleeve 9 are provided with the semisphere indent, in the space that described axle sleeve and axle center 10 indents form ball 8 is installed, ball is in the axle center that axially upwards all can support, locate the flabellum assembly with the footpath.
The bottom of described flying saucer main body 1 is provided with pusher 6, and described pusher 6 is installed on the flying saucer main body 1 by control apparatus, changes the direction of pusher, can realize break-in etc.
The surface of described flying saucer main body 1 is provided with solar panel 2, too can cell panel 2 electric energy that produce can be used as electric energy compensation, cleaning, energy-conservation.
The present invention adopts the double dynamical of flabellum assembly and pusher on power, power source can also can adopt nuclear power source etc. from gases such as burning hydrogens.
Claims (4)
1. flying saucer, comprise flying saucer main body (1), the center that it is characterized in that described flying saucer main body (1) is provided with axial through hole (3), flabellum assembly (4) is installed in the described through hole (3), flabellum assembly (4) pipe link has the engine installation that drives its rotation, and the bottom of described flying saucer main body (1) is provided with pusher (6).
2. flying saucer according to claim 1, the two ends that it is characterized in that described through hole (3) are equipped with support (5), described support (5) installed inside has axle sleeve (9), the two ends, axle center (10) terminal and installation flabellum assembly (4) of described axle sleeve (9) are provided with the semisphere indent, in the space that described axle sleeve and axle center (10) indent forms ball (8) are installed.
3. flying saucer according to claim 1 is characterized in that described pusher (6) is installed on the flying saucer main body (1) by control apparatus.
4. flying saucer according to claim 1 is characterized in that the surface of described flying saucer main body (1) is provided with solar panel (2).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN 201010238201 CN101913428A (en) | 2010-07-26 | 2010-07-26 | Flying disk |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN 201010238201 CN101913428A (en) | 2010-07-26 | 2010-07-26 | Flying disk |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN101913428A true CN101913428A (en) | 2010-12-15 |
Family
ID=43321124
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN 201010238201 Pending CN101913428A (en) | 2010-07-26 | 2010-07-26 | Flying disk |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN101913428A (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN102582834A (en) * | 2012-03-09 | 2012-07-18 | 北京工业大学 | Saucer-shaped aircraft |
| CN105015785A (en) * | 2015-07-08 | 2015-11-04 | 上海理工大学 | Micro solar reconnaissance flight vehicle incorporated with Coanda effect |
Citations (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| DE4112585A1 (en) * | 1991-04-17 | 1991-08-29 | Hans Geschka | Aircraft with annular wing - generates laminar air flow radially from centre line to provide lift |
| CN1081984A (en) * | 1992-08-13 | 1994-02-16 | 迟宇光 | Flying saucer |
| RU2151717C1 (en) * | 1998-03-02 | 2000-06-27 | Безруков Юрий Иванович | Flying saucer |
| CN1322658A (en) * | 2000-05-17 | 2001-11-21 | 高恒伟 | Helicopter with ring wing |
| CN2528706Y (en) * | 2002-01-25 | 2003-01-01 | 王保平 | Manned craft |
| CN2799401Y (en) * | 2005-05-13 | 2006-07-26 | 沙庆军 | Dish shaped aircraft |
-
2010
- 2010-07-26 CN CN 201010238201 patent/CN101913428A/en active Pending
Patent Citations (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| DE4112585A1 (en) * | 1991-04-17 | 1991-08-29 | Hans Geschka | Aircraft with annular wing - generates laminar air flow radially from centre line to provide lift |
| CN1081984A (en) * | 1992-08-13 | 1994-02-16 | 迟宇光 | Flying saucer |
| RU2151717C1 (en) * | 1998-03-02 | 2000-06-27 | Безруков Юрий Иванович | Flying saucer |
| CN1322658A (en) * | 2000-05-17 | 2001-11-21 | 高恒伟 | Helicopter with ring wing |
| CN2528706Y (en) * | 2002-01-25 | 2003-01-01 | 王保平 | Manned craft |
| CN2799401Y (en) * | 2005-05-13 | 2006-07-26 | 沙庆军 | Dish shaped aircraft |
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN102582834A (en) * | 2012-03-09 | 2012-07-18 | 北京工业大学 | Saucer-shaped aircraft |
| CN105015785A (en) * | 2015-07-08 | 2015-11-04 | 上海理工大学 | Micro solar reconnaissance flight vehicle incorporated with Coanda effect |
| CN105015785B (en) * | 2015-07-08 | 2017-03-22 | 上海理工大学 | Micro solar reconnaissance flight vehicle incorporated with Coanda effect |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| 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 |
Application publication date: 20101215 |