CN2318410Y - Jet vortexing flight vehicle - Google Patents
Jet vortexing flight vehicle Download PDFInfo
- Publication number
- CN2318410Y CN2318410Y CN 97205608 CN97205608U CN2318410Y CN 2318410 Y CN2318410 Y CN 2318410Y CN 97205608 CN97205608 CN 97205608 CN 97205608 U CN97205608 U CN 97205608U CN 2318410 Y CN2318410 Y CN 2318410Y
- Authority
- CN
- China
- Prior art keywords
- jet
- utility
- model
- air
- vortex chamber
- 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.)
- Expired - Fee Related
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Abstract
The utility model discloses a jet vortexing flight vehicle, which is composed of air compressors, jet tubes, reflection shells, jet plates, vortexing chambers, flow guiding rings, and annular reflection plates. Because wings and propellers of traditional flight vehicles are abandoned by the utility model, the utility model has the advantages of small size and simple structure. When the utility model is used, high pressure air current is reflected onto the jet plates by the reflection shells through the jet tubes, the jet plates spray the high speed air current to the flow guiding rings, which causes pressure difference to be generated from the flow guiding rings, lifting force is also generated from the annular reflection plates, and the pressure difference is generated from that vortex flow is formed by that the air current which is positioned on the outer part of walls of the flow guiding rings flows into the vortexing chambers. Because the upward pressure difference is simultaneously acted, the utility model can fly in the sky.
Description
The utility model relates to a kind of aircraft.
Present aircraft of the prior art generally all adopts will have fairshaped wing or propeller is installed on the body, make aircraft when motion, because flowing of air producing lift on the wing or on the propeller, thereby make the aircraft lift-off.The shortcoming of these aircraft is: complex structure, volume are big.
The purpose of this utility model is: a kind of wing and propeller and aircraft simple in structure, that volume is less of not adopting is provided.
The utility model is to constitute like this: it is by air compressor (1), air jet pipe (2), refecting cover (3), jet plate (4), vortex chamber (5), baffle liner (6), annular anode reflector (7) is formed, the air outlet of air compressor (1) is connected with air jet pipe (2), vortex chamber (5) is spill circle basin shape, air jet pipe (2) passes at the bottom of the basin of vortex chamber (5) and with it and is fixed together, refecting cover (3) is fixed on the top of air jet pipe (2) by pole (8), jet plate (4) is contained on the air jet pipe (2), baffle liner (6) is the horn mouth shape, baffle liner (6) links together with vortex chamber (5) by pole (9), and between the inwall of the outer wall of duct ring (6) and vortex chamber (5) gapped (10), annular anode reflector (7) is housed in the top of baffle liner (6).
The utility model is compared with existing aircraft, because it has abandoned the wing and the propeller of conventional aircraft, thereby has little, the advantage of simple structure of volume.And owing to adopted technique scheme, the utility model is when work, the high pressure draught that comes out from air compressor (1) reflexes on the jet plate (4) by air jet pipe (2) cover (3) that is reflected, jet plate (4) is sprayed onto high velocity air on the inwall of baffle liner (6), make the inside and outside wall of baffle liner (6) produce upwards draught head, and make annular anode reflector (7) produce lift upwards, simultaneously crossing gap (10) in the air communication of baffle liner outer wall enters in the vortex chamber (5) and forms eddy current, also form draught head upwards inside and outside making the vortex chamber like this, these draught heads act on simultaneously just can make its lift-off flight on the utility model.
Accompanying drawing 1 is a structural representation of the present utility model.
Embodiment of the present utility model: air compressor (1) can adopt common air compressor, but preferably adopt aluminum alloy material to make, air jet pipe (2), refecting cover (3), jet plate (4), vortex chamber (5), baffle liner (6), annular anode reflector (7) waits other all to adopt the Light Aluminum Alloy material by part, the air outlet of air compressor (1) is connected with air jet pipe (2), vortex chamber (5) is made as spill circle basin shape, and air jet pipe (2) is passed at the bottom of the basin of vortex chamber (5) and and be fixed together with it, refecting cover (3) is fixed on the top of air jet pipe (2) by three poles (8), and jet plate (4) is contained on the air jet pipe (2), baffle liner (6) is made into the horn mouth shape, baffle liner (6) is linked together with vortex chamber (5) with 4～8 poles (9), and make between the inwall of the outer wall of duct ring (6) and vortex chamber (5) and form certain clearance (10), load onto annular anode reflector in the top of baffle liner (6) and (7).
Claims (1)
1, a kind of air-jet eddy-current formula aircraft, it is characterized in that: it is by air compressor (1), air jet pipe (2), refecting cover (3), jet plate (4), vortex chamber (5), baffle liner (6), annular anode reflector (7) is formed, the air outlet of air compressor (1) is connected with air jet pipe (2), vortex chamber (5) is spill circle basin shape, air jet pipe (2) passes at the bottom of the basin of vortex chamber (5) and with it and is fixed together, refecting cover (3) is fixed on the top of air jet pipe (2) by pole (8), jet plate (4) is contained on the air jet pipe (2), baffle liner (6) is the horn mouth shape, baffle liner (5) links together with vortex chamber (5) by pole (9), and between the inwall of the outer wall of duct ring (6) and vortex chamber (5) gapped (10), annular anode reflector (7) is housed in the top of baffle liner (6).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN 97205608 CN2318410Y (en) | 1997-12-12 | 1997-12-12 | Jet vortexing flight vehicle |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN 97205608 CN2318410Y (en) | 1997-12-12 | 1997-12-12 | Jet vortexing flight vehicle |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN2318410Y true CN2318410Y (en) | 1999-05-12 |
Family
ID=33925802
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN 97205608 Expired - Fee Related CN2318410Y (en) | 1997-12-12 | 1997-12-12 | Jet vortexing flight vehicle |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN2318410Y (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN103629012A (en) * | 2013-11-28 | 2014-03-12 | 陕西飞机工业（集团）有限公司 | Propeller |
-
1997
- 1997-12-12 CN CN 97205608 patent/CN2318410Y/en not_active Expired - Fee Related
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN103629012A (en) * | 2013-11-28 | 2014-03-12 | 陕西飞机工业（集团）有限公司 | Propeller |
| CN103629012B (en) * | 2013-11-28 | 2016-02-24 | 陕西飞机工业（集团）有限公司 | A kind of propulsion device |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| C19 | Lapse of patent right due to non-payment of the annual fee | ||
| CF01 | Termination of patent right due to non-payment of annual fee |