CN204021246U - A kind of partition air injection aerial vehicle - Google Patents
A kind of partition air injection aerial vehicle Download PDFInfo
- Publication number
- CN204021246U CN204021246U CN201420376728.XU CN201420376728U CN204021246U CN 204021246 U CN204021246 U CN 204021246U CN 201420376728 U CN201420376728 U CN 201420376728U CN 204021246 U CN204021246 U CN 204021246U
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- aircraft
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Abstract
The utility model relates to a kind of partition air injection aerial vehicle, comprises outer wall, inwall, engine installation, controller and air nozzle, passes through stent support between inner and outer wall.Inner and outer wall forms partition space, and inwall inner space is working space.Air nozzle is positioned at the bottom of outer wall, and 4 ~ 50 air nozzles are uniformly distributed around outer wall.Engine installation is arranged on the inner side of inwall, engine installation outlet and partition spatial joins.Controller is arranged on working space, and controller is connected to the by-pass valve control of air nozzle.Controlled the heading of aircraft during work by the jet amount of the controller control outer wall air nozzle in aircraft and jet velocity, aircraft can be moved to any direction.The utility model partition air injection aerial vehicle flight and handling good, fly under adapting to various climatic conditions, for scientific exploration, building and bridge inspection, travelling among the people and military use.
Description
Technical field
The utility model belongs to aircraft devices technical field, relates to a kind of aircraft, is specifically related to a kind of partition air injection aerial vehicle.
Background technology
Existing aircraft kind is a lot, be widely used, utilizing atm difference to produce power is modal application, existing air injection aerial vehicle comprises aircraft and guided missile and the carrier rocket etc. of various shape, aircraft jet power resources are in various automotive gas turbine, and rocket-powered missile power resources are generally various solid fueled engines.Existing aircraft is mostly physical construction, bulky, not only wastes power, and not easily manipulates, high to environmental requirement.
Publication number is that the patent application of CN1405527A discloses a kind of jet propelling aircraft, and " by main jet propeller, keystone configuration is made up of the detachable propellant tank group of the longitudinal tandem multi-stage of main jet propeller aircraft primary structure.In flight course, the propellant tank used will be separated with aircraft body, and this structure is applicable to space vehicle carrier rocket, the jet propelling aircrafts such as various military seekers ".But this patent can not solve the problems of the technologies described above.
Utility model content
The utility model provides a kind of partition air injection aerial vehicle, and improve the performance of aircraft, fly under adapting to various condition, flexible operation is swift in response.
The utility model partition air injection aerial vehicle, comprises outer wall, inwall, engine installation, controller and air nozzle, passes through stent support between inner and outer wall.Inner and outer wall forms partition space, and inwall inner space is working space.Air nozzle is positioned at the bottom of outer wall, and 4 ~ 50 air nozzles are uniformly distributed around outer wall.Engine installation is arranged on the inner side of inwall, engine installation outlet and partition spatial joins.Controller is arranged on working space, and controller is connected to the by-pass valve control of air nozzle.
Engine installation is automotive gas turbine or solid fuel power engine.Aircraft is circular or oval, does not get rid of other shape.The material of outer wall and inwall is high-strength alloy.Described aircraft is provided with external jet engine, and described external jet engine is arranged on the top of outer wall.
Controlled the heading of aircraft during work by the jet amount of the controller control outer wall air nozzle in aircraft and jet velocity, aircraft can be moved to any direction.The function of heat insulation to aircraft cabin is also played in high pressure gas motion in aircraft partition.Time under attack, high pressure gas, from by the ejection at a high speed of attack position, make aircraft to flee from fast.At the outer wall of aircraft, external jet engine is installed, the power of aircraft can be increased, improve vehicle flight speeds and carrying capacity further.The not only airflight of partition air injection aerial vehicle, and the high pressure in seabed can be born, in seabed, navigation performs seabed task.
The utility model partition air injection aerial vehicle flight and handling good, fly under adapting to various climatic conditions, flexible operation is swift in response, for scientific exploration, building and bridge inspection, travelling among the people and military use.
Accompanying drawing explanation
Fig. 1 is the structural representation of the utility model partition air injection aerial vehicle;
Fig. 2 is the birds-eye view of Fig. 1.
Wherein,
1-outer wall, 2-inwall, 3-engine installation, 4-air nozzle.5-outer wall bracket, 6-partition space, 7-working space.
Detailed description of the invention
By reference to the accompanying drawings the utility model is described in detail.
The utility model partition air injection aerial vehicle as shown in Figure 1, Figure 2 described in, aircraft is that circle comprises outer wall 1, inwall 2, engine installation 3, controller and air nozzle 4, is supported between inner and outer wall by outer wall bracket 5.Inner and outer wall forms partition space 6, and inwall inner space is working space 7.Partition space is enclosed high pressure chamber, is full of the tail gas that engine installation is discharged, and partition space mesohigh gas is ejection at a high speed, produces powered aircraft flight.Air nozzle is positioned at the bottom of outer wall, and 20 air nozzles are uniformly distributed around outer wall.Engine installation is arranged on the inner side of inwall.Engine installation is automotive gas turbine, automotive gas turbine outlet and partition spatial joins.Controller is arranged on working space, and controller is connected to the by-pass valve control of air nozzle.The material of aircraft outer wall 1 and inwall 2 is high-strength alloy.
Start engine installation during aircraft flight, ejection gas is the punching press of partition space, and the jet amount of controller control outer wall air nozzle and jet velocity control the heading of aircraft, and aircraft can be moved to any direction.Needs more strong impetus time can also in the external jet engine of aircraft outer wall, improve aircraft movements speed further.Owing to being full of high pressure gas in partition, the high pressure that partition aircraft can bear seabed can navigate by water in seabed.
Adopt the aircraft of dividing wall structure can fly to any direction by regulating the air nozzle be arranged on outer wall at aircraft outer layer covers one deck high pressure gas; Partition mesohigh gas can play function of heat insulation to aircraft interior; Partition mesohigh gas sprays at a high speed when receiving attack and aircraft can be made to flee the scene rapidly.
Claims (5)
1. a partition air injection aerial vehicle, it is characterized in that: described aircraft comprises outer wall (1), inwall (2), engine installation (3), controller and air nozzle (4), supported by outer wall bracket (5) between inner and outer wall, inner and outer wall forms partition space (6), and inwall inner space is working space (7); Described air nozzle is positioned at the bottom of outer wall, and 4 ~ 50 air nozzles are uniformly distributed around outer wall; Engine installation is arranged on the inner side of inwall, engine installation outlet and partition spatial joins; Described controller is arranged on working space, and controller is connected to the by-pass valve control of air nozzle.
2. partition air injection aerial vehicle according to claim 1, is characterized in that: described engine installation (3) is automotive gas turbine or solid fuel power engine.
3. partition air injection aerial vehicle according to claim 1, is characterized in that: described aircraft is for circular or oval.
4. partition air injection aerial vehicle according to claim 1, is characterized in that: the material of described outer wall (1) and inwall (2) is high-strength alloy.
5. partition air injection aerial vehicle according to claim 1, it is characterized in that: described aircraft is provided with external jet engine, described external jet engine is arranged on the top of outer wall (1).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201420376728.XU CN204021246U (en) | 2014-07-09 | 2014-07-09 | A kind of partition air injection aerial vehicle |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201420376728.XU CN204021246U (en) | 2014-07-09 | 2014-07-09 | A kind of partition air injection aerial vehicle |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN204021246U true CN204021246U (en) | 2014-12-17 |
Family
ID=52061144
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201420376728.XU Active CN204021246U (en) | 2014-07-09 | 2014-07-09 | A kind of partition air injection aerial vehicle |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN204021246U (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108945484A (en) * | 2018-07-02 | 2018-12-07 | 山东理工大学 | A kind of two-way air injection aerial vehicle |
| CN112298609A (en) * | 2019-07-29 | 2021-02-02 | 之江实验室 | Jet-propelled mars detection unmanned aerial vehicle |
-
2014
- 2014-07-09 CN CN201420376728.XU patent/CN204021246U/en active Active
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108945484A (en) * | 2018-07-02 | 2018-12-07 | 山东理工大学 | A kind of two-way air injection aerial vehicle |
| CN112298609A (en) * | 2019-07-29 | 2021-02-02 | 之江实验室 | Jet-propelled mars detection unmanned aerial vehicle |
| CN112298609B (en) * | 2019-07-29 | 2022-06-28 | 之江实验室 | Jet-propelled mars detection unmanned aerial vehicle |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant |