CN1275514A - Jet-propelled fly-star, fly-disc and fly-rocket series - Google Patents
Jet-propelled fly-star, fly-disc and fly-rocket series Download PDFInfo
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- CN1275514A CN1275514A CN 00121110 CN00121110A CN1275514A CN 1275514 A CN1275514 A CN 1275514A CN 00121110 CN00121110 CN 00121110 CN 00121110 A CN00121110 A CN 00121110A CN 1275514 A CN1275514 A CN 1275514A
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- jet
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- star
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- arrow
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Abstract
The present invention relates to a series of jet flying vehicles including flying star, flying saucer and flying arrow, in which the flying star is made into normal round body, flying saucer is made into oblate body and flying arrow is made into long-circular body, and their center of gravity is being in right lower position of their centers. They adopts two groups of jet-injectors with jetting downwards or jetting backwards. Said invention also provides their working schematic diagram. As compared with aricraft and helicopter, the said invented flying vehicles have no need of runway, and can stably and freely fly.
Description
The present invention relates to the jet-propelled flyer that flies star flying saucer flying arrow series of a class.
In the present prior art, aircraft have runway take off the landing, have go straight up to take off the landing dual mode.The necessary duty runway of preceding a kind of mode gives the special runway of its making cumbersome like this, moreover in road, barrier must land for some reason, and it can not be implemented because of no runway, its weak point that Here it is.A kind of mode in back must be used piston rod formula driving engine, and it is slower than the flyer speed of using jet engine like this, its weak point that Here it is.
Any jet-propelled flyer that flies star flying saucer flying arrow series that a class formation is simple, cost is low that provides of the present invention.This series utilization be jet engine.Go straight up to the landing of taking off.Be fireballing.
The jet-propelled principle of work that flies star flying saucer flying arrow series of the present invention: the profile structure: flying star is spherial body, and flying saucer is an oblate body, and flying arrow is a long round body.The composition line of reference of their external surface shape, at will each bar line all is a camber line.The center of gravity of star dish arrow is under the center.The power of star dish arrow respectively is to utilize a jet engine.Jet is to utilize two groups of air blasts that different directions is jet, and wherein one group is jet downwards, and another group is rearward jet.The gas circuit of these two groups of air blasts is by a three-way valve switch, controls to adjust jet and jet backward opening and closing function downwards.One group of downward air blast is made up of four air blasts, the position all flyer up and down apart from bisector below, the adjacent bisector of air blast, four the air blast size is identical, equal, jet flow equates at interval, jet direction is not vertically downward, it is outwards tiltedly to go out an angle, and it is just to overlap with the air flow line that flyer flight is cut apart that the air-flow of this angle ejection requires.Another is organized backward air blast and is made up of two air blasts, the position is all at flyer longitudinal separation bisector rear, the adjacent bisector of air blast, two the air blast size is identical, equal, jet flow equates at interval, jet direction is not backward parallel, it is outwards tiltedly to go out an angle, and it is just to overlap with the air flow line that flyer flight is cut apart that the air-flow of this angle ejection requires.These two groups of jet flows of air blast equate.Two of another groups gas circuit of air blast backward are by a three-way valve switch, control to adjust two jet flows of air blast and equate and unequal effect.The inside of star dish arrow will be by adorning an automatically regulating balancing device.Here it is should the series flyer aufbauprinciple.The flight of star dish arrow, upwards flight: the three-way valve of two groups of air blasts of operation control tube, close one group of jet backward air blast, also be simultaneously open one group of jet air blast downwards.Fire an engine is jet, and open out jet going straight up to downwards takes off.To fly forward: fly to suitable height throttle and do not subtract, close downward air blast, it simultaneously also is open air blast backward, in the time of this conversion direction, the jet amount of air blast reduces gradually downwards, the jet amount of air blast increases gradually backward simultaneously, has so just no longer upwards flown, and changes into flight forward gradually.Turn about wanting: two of operation control tubes are the three-way valve of air blast backward, and a jet amount is reduced gradually, simultaneously another jet amount is corresponding increases gradually, it is unequal the jet amount in the left and right sides so just to have occurred, makes it just to spray narrow-minded there turning.Take off sideling, fly sideling: the open simultaneously two groups of air blasts of the three-way valve of two groups of air blasts of operation pipe, one group of jet downwards opening greatly, one group of jet backward opening little, fire an engine is jet, and open out just also also forwards flies to upward sideling.Also can be in atmosphere the motionless state of held stationary.Here it is should the series flyer flight theory.
Because this series star dish arrow has adopted two groups of air blasts, downward jet and jet backward method.Than one group of air blast advanced person that aircraft autogyro adopts, can reach the landing of taking off without runway, high-speed effect.
The present invention is further detailed explanation below in conjunction with the drawings and specific embodiments.
Fig. 1 is the jet-propelled upward view that flies star of the present invention.
Fig. 2 is the jet-propelled lateral plan that flies star of the present invention.
Fig. 3 is the upward view of the jet-propelled flying saucer of the present invention.
Fig. 4 is the lateral plan of the jet-propelled flying saucer of the present invention.
Fig. 5 is the upward view of the jet-propelled flying arrow of the present invention.
Fig. 6 is the lateral plan of the jet-propelled flying arrow of the present invention.
The jet-propelled flyer that flies star flying saucer flying arrow series that Fig. 1, Fig. 2, Fig. 3, Fig. 4, Fig. 5, Fig. 6 describe respectively, their common structure feature, flying body 1 and one group of downward air blast 2 are organized air blast 3 formation flyer and principle of work backward with another.
The shell of this series star dish arrow and the gas circuit of air blast and air blast must be used crisp firmly and not steel manufacturing.The aufbauprinciple of air blast, it is made up of air flow divert joint, jet chamber, air nozzle.Stealthy naked mouthful of air blast, mouth is neat equally with the profile of flying body.Backward in the air blast mouth by adorning a balancing patch, be used to take off or stop downward or upward air-flow when landing, keep balance before and after making flyer.The air nozzle of air blast is microscler downwards, and the air nozzle of air blast is long a little circle backward.
Claims (3)
1, the jet-propelled flyer that flies star flying saucer flying arrow series that constitutes by jet engine, it is spherial body that its feature flies star, and flying saucer is an oblate body, and flying arrow is a long round body, the composition line of reference of their external surface shape, at will each bar line all is a camber line.
2, the star that flies according to claim 1 is a spherial body, and flying saucer is an oblate body, and flying arrow is a long round body, and the center of gravity that it is characterized in that them is all under the center.
3, the star that flies according to claim 1 is a spherial body, and flying saucer is an oblate body, and flying arrow is a long round body, it is characterized in that they all are to have adopted two groups of air blasts, downwards jet and jet backward method.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN 00121110 CN1275514A (en) | 2000-07-26 | 2000-07-26 | Jet-propelled fly-star, fly-disc and fly-rocket series |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN 00121110 CN1275514A (en) | 2000-07-26 | 2000-07-26 | Jet-propelled fly-star, fly-disc and fly-rocket series |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN1275514A true CN1275514A (en) | 2000-12-06 |
Family
ID=4588593
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN 00121110 Pending CN1275514A (en) | 2000-07-26 | 2000-07-26 | Jet-propelled fly-star, fly-disc and fly-rocket series |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN1275514A (en) |
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN102638018A (en) * | 2012-03-25 | 2012-08-15 | 河南省电力公司安阳供电公司 | Remotely-controlled deicing device for high-tension lines |
| CN103640701A (en) * | 2013-09-21 | 2014-03-19 | 张宝海 | Basic structure and basic flying principle of flying saucer |
| CN112158325A (en) * | 2020-09-30 | 2021-01-01 | 浙江大学 | Tailstock type vertical take-off and landing unmanned aerial vehicle and control method thereof |
-
2000
- 2000-07-26 CN CN 00121110 patent/CN1275514A/en active Pending
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN102638018A (en) * | 2012-03-25 | 2012-08-15 | 河南省电力公司安阳供电公司 | Remotely-controlled deicing device for high-tension lines |
| CN102638018B (en) * | 2012-03-25 | 2015-02-04 | 河南省电力公司安阳供电公司 | Remotely-controlled deicing device for high-tension lines |
| CN103640701A (en) * | 2013-09-21 | 2014-03-19 | 张宝海 | Basic structure and basic flying principle of flying saucer |
| CN112158325A (en) * | 2020-09-30 | 2021-01-01 | 浙江大学 | Tailstock type vertical take-off and landing unmanned aerial vehicle and control method thereof |
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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 |