CN103507954A - Air injection flying saucer - Google Patents
Air injection flying saucer Download PDFInfo
- Publication number
- CN103507954A CN103507954A CN201310043722.0A CN201310043722A CN103507954A CN 103507954 A CN103507954 A CN 103507954A CN 201310043722 A CN201310043722 A CN 201310043722A CN 103507954 A CN103507954 A CN 103507954A
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- CN
- China
- Prior art keywords
- flying saucer
- engine
- machine body
- driving engine
- aerofoils
- 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.)
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Abstract
The invention relates to a flying saucer, and particularly relates to a flying saucer taking a turbo fan air injection engine as power. The flying saucer comprises an engine, aerofoils and a machine body. The flying saucer is characterized in that the machine body is round; the engine and the aerofoils are in the machine body; a connecting plate between the engine and the machine body is also an aerofoil; the engine and the aerofoils are connected through positioning grooves and bolts; the engine is a turbo fan air injection engine, and can be a single engine or multi engines. The flying saucer has the beneficial effects that the flying saucer can lift vertically, and also can hover in air, is good in maneuvering characteristic, can brake urgently, and can rapidly change the flight direction at short distance and large angle; the flight mode is that the flying saucer flies horizontally with a jet exhaust toward the oblique rear lower part after vertical lift-off, and also can fly horizontally or flies in mode that the machine body rotates for 90 degrees, an air inlet is forward and the jet exhaust is backward; the flight direction and the posture are controlled by rudders at the rear part of the aerofoils as well as the swinging of a tail jet of the engine. The flying saucer provided by the invention is equipped with an annular parachute, improves the flight safety, can be in supersonic flight for a long time and a remote distance, and can have the functions of aerial reconnaissance, rescue, transportation, surveying and mapping and fighting after being additionally equipped with a navigation system, a radar, a weapon system and photographing equipment.
Description
(1) technical field
The present invention relates to a kind of flying saucer, especially a kind ofly take the flying saucer that turbofan is power.
(2) background technology
Existing flying saucer mainly refers to various flying disk toys in the world.Existing air injection aerial vehicle mainly comprises various erose jet airplane and disposable guided missile and carrier rocket, the technical characterstic of flying saucer in legend (UFO) is: can vertical takeoff and landing, during landing, air nozzle down, lift-off rear body be take vertical line and is horizontally rotated as axle, air nozzle along continuous straight runs is jet, high-speed flight, such flying saucer is not also really succeeded in developing, and scientists thinks that the performance-oriented flying saucer with practical value is impracticable in principle.
(3) summary of the invention
The present invention, in order to make up the deficiencies in the prior art, provides a kind of circular jet-air aircraft, and a kind of high thrust truly with practical value can be manned, the jet flying saucer of loading.
The present invention is achieved by the following technical solutions:
Its special character of the present invention is: airframe structure is annular arrangement, the position of driving engine (separate unit or many) and wing is in fuselage interior, the forming just as single engine jet fighter of a driving engine below ventral is bowed downward to an annulus by wing two ends of separate unit driving engine.The multi-engined layout that can be uniformly dispersed.This flying saucer is equipped with large-scale parachute, while breaking down, can rely on parachute safe landing, improves flight safety.
Connecting panel between driving engine of the present invention and fuselage is comprised of wale piece, perpendicular fagging and tilt prop respectively.Wale piece horizontal tail namely wherein, perpendicular fagging is equivalent to normal limb.Tilt prop is the oblique wing namely.
The jet flying saucer of the present invention has two kinds of drone version and manned versions, adopts the drone version of turbine fan jet machine because space availability ratio is high, need not consider the tolerance of aviator to supersonic flight, can realize long-time, remote supersonic flight.
The invention has the beneficial effects as follows, can vertical takeoff and landing, need not build plane track, can aloft hover; Thrust is large, and vertical lifting weight is large; Maneuvering performance is good.
(4) accompanying drawing explanation
Fig. 1 is longitudinally analysing and observe of the jet flying saucer structure of the present invention, and Fig. 2 is the jet flying saucer front elevational schematic of monomotor;
Fig. 3 and Fig. 4 are horizontal tail, normal limb and oblique wing structure front view and the longitudinal sectional views of the jet flying saucer of the present invention;
Fig. 5 is the jet flying saucer front elevation of multiple-motor;
Wherein: 1, fuselage, 2, driving engine, 3, yaw rudder, 4, horizontal tail, 5, the oblique wing, 6, normal limb.
(5) specific embodiment
Accompanying drawing is a kind of specific embodiment of the jet flying saucer of the present invention.The jet flying saucer of the present invention, comprises fuselage 1, driving engine 2, yaw rudder 3, horizontal tail 4, the oblique wing 5, normal limb 6.Adopting the turbofan technology of aviation field maturation, is by positioning groove and bolted between driving engine and wing.The present invention is equipped with annular arrangement parachute, improves flight safety.
Flying method is: can air nozzle after vertical lift-off towards the below of retreading, horizontal flight, also can body 90-degree rotation, engine inlet port forward, air nozzle high speed level cruise backwards, the control of heading and attitude is to have swung by the yaw rudder of wing back and the spray of the tail of driving engine.
Owing to having, level cruise speed is high, can be for a long time, the feature of remote supersonic flight, add that its volume is little, own wt is light, save the advantages such as available space and can effectively improve its maneuverability, by installing navigationsystem, radar, armament systems additional and taking the photograph phase photographing device, can possess aerial reconnaissance, rescue, transportation, mapping and fight function.
Claims (3)
1. a jet flying saucer.Comprise fuselage (1), wing (4), (5), (6) and driving engine (2), it is characterized in that: fuselage (1) is annular arrangement, driving engine and wing, in the inside of fuselage, connect by wing between driving engine and fuselage.Between driving engine and wing, be by positioning groove and bolted.
2. jet flying saucer according to claim 1, is characterized in that: can adopt separate unit driving engine also can adopt many driving engines.
3. jet flying saucer according to claim 1, driving engine is turbofan, flying method is: can air nozzle after vertical lift-off towards the below of retreading, horizontal flight, also can fuselage 90-degree rotation, engine inlet port forward, air nozzle high speed level cruise backwards.The control of its heading and attitude is to have swung by the yaw rudder of wing back and the spray of the tail of driving engine.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201310043722.0A CN103507954A (en) | 2013-02-05 | 2013-02-05 | Air injection flying saucer |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201310043722.0A CN103507954A (en) | 2013-02-05 | 2013-02-05 | Air injection flying saucer |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN103507954A true CN103507954A (en) | 2014-01-15 |
Family
ID=49891490
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201310043722.0A Pending CN103507954A (en) | 2013-02-05 | 2013-02-05 | Air injection flying saucer |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN103507954A (en) |
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106143907A (en) * | 2016-06-30 | 2016-11-23 | 宁波市成大机械研究所 | A kind of jet flying saucer |
| CN106494627A (en) * | 2015-09-06 | 2017-03-15 | 陈小辉 | Disc shape flight device |
| CN114435394A (en) * | 2021-12-22 | 2022-05-06 | 安徽建德基文化传媒有限公司 | Control system of unmanned automobile |
Citations (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN2528706Y (en) * | 2002-01-25 | 2003-01-01 | 王保平 | Manned craft |
| CN2923518Y (en) * | 2006-04-28 | 2007-07-18 | 李贤明 | Circular jet-air aircraft |
| CN101381001A (en) * | 2007-09-04 | 2009-03-11 | 刘新广 | Magneto-flying saucer |
| RU2471676C1 (en) * | 2011-07-06 | 2013-01-10 | Николай Борисович Болотин | Airborne vehicle of "flying saucer" type |
-
2013
- 2013-02-05 CN CN201310043722.0A patent/CN103507954A/en active Pending
Patent Citations (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN2528706Y (en) * | 2002-01-25 | 2003-01-01 | 王保平 | Manned craft |
| CN2923518Y (en) * | 2006-04-28 | 2007-07-18 | 李贤明 | Circular jet-air aircraft |
| CN101381001A (en) * | 2007-09-04 | 2009-03-11 | 刘新广 | Magneto-flying saucer |
| RU2471676C1 (en) * | 2011-07-06 | 2013-01-10 | Николай Борисович Болотин | Airborne vehicle of "flying saucer" type |
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106494627A (en) * | 2015-09-06 | 2017-03-15 | 陈小辉 | Disc shape flight device |
| CN106143907A (en) * | 2016-06-30 | 2016-11-23 | 宁波市成大机械研究所 | A kind of jet flying saucer |
| CN114435394A (en) * | 2021-12-22 | 2022-05-06 | 安徽建德基文化传媒有限公司 | Control system of unmanned automobile |
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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: 20140115 |