CN206107556U - High -speed type dish -shaped aircraft - Google Patents
High -speed type dish -shaped aircraft Download PDFInfo
- Publication number
- CN206107556U CN206107556U CN201621006526.1U CN201621006526U CN206107556U CN 206107556 U CN206107556 U CN 206107556U CN 201621006526 U CN201621006526 U CN 201621006526U CN 206107556 U CN206107556 U CN 206107556U
- Authority
- CN
- China
- Prior art keywords
- air inlet
- annular
- dish cover
- high speed
- aircraft
- 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
Links
- 239000002828 fuel tank Substances 0.000 claims description 7
- 238000004080 punching Methods 0.000 claims description 5
- 230000008450 motivation Effects 0.000 claims 1
- 230000000694 effects Effects 0.000 description 3
- 230000004888 barrier function Effects 0.000 description 2
- 240000002836 Ipomoea tricolor Species 0.000 description 1
- 206010044565 Tremor Diseases 0.000 description 1
- 230000009286 beneficial effect Effects 0.000 description 1
- 230000001914 calming effect Effects 0.000 description 1
- 238000000034 method Methods 0.000 description 1
- 238000009987 spinning Methods 0.000 description 1
- 239000007921 spray Substances 0.000 description 1
Classifications
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T50/00—Aeronautics or air transport
- Y02T50/60—Efficient propulsion technologies, e.g. for aircraft
Landscapes
- Toys (AREA)
Abstract
The utility model discloses a high -speed type dish -shaped aircraft, including dish cover (1) and storehouse (7), dish cover (1) the outside is equipped with air inlet (2), dish cover (1) bottom edge is equipped with evenly distributed exhaust hole (3) and little ramjet engine (14), dish cover (1) links to each other with annular motor (5) through axle sleeve (13), storehouse (7) link to each other with annular motor (5) through annular air exit (4) interior skeleton (11), big ramjet engine (12) that annular air exit (4) hung evenly distributed, be equipped with on the annular motor (5) driver's cabin (6). This aircraft has than traditional aircraft and more has more the screw, and lift is big and stable, and evenly distributed has ramjet engine to provide drive power. Multiple uses such as unmanned aerial vehicle, cargo airplane can be made, for the hybrid mode, the high -speed flight is fit for.
Description
Technical field
The utility model is related to single rotor culvert type aircraft, specially a kind of high speed class disc-shaped flying craft.
Background technology
Current Flight Vehicle Structure is complicated, and screw is less, is only applicable to single power flight, and lift is less and shakiness
It is fixed.This aircraft has more propellers than conventional aircraft, and lift is big and stable.The multiple uses such as unmanned plane, transporter can be made,
For hybrid mode, it is adapted to high-speed flight.
The content of the invention
The purpose of this utility model is, for the problems referred to above, to overcome prior art not enough, there is provided a kind of new single rotor
Culvert type aircraft.
For achieving the above object, the utility model is employed the following technical solutions：
A kind of high speed class disc-shaped flying craft described in the utility model, including dish cover and freight house, the dish cover outside
Air inlet is provided with, the dish-shaped cover bottom margin is provided with equally distributed steam vent and little ramjet, the dish
Cover is connected by axle sleeve with annular generator, and the freight house is connected by the skeleton in annular exhaust outlet with annular generator, the ring
Shape exhaust outlet has hung equally distributed big ramjet, and the annular generator is provided with driver's cabin.
Further, the air inlet is zigzag, and the air inlet is connected by dividing plate with axle sleeve, and the dividing plate is by air inlet
Mouth is divided into enterprising gas port and lower air inlet, and enterprising gas port and lower air inlet length ratio are 4.5: 2.5, the dividing plate correspondence ring
It is skeleton structure at shape exhaust outlet.
Further, the freight house outside is provided with equally distributed spin-ended.
Further, the axle sleeve outside is provided with annular fuel tank.
Further, the freight house bottom is provided with undercarriage.
Further, the dish cover top hypotenuse angle radian is 70 ° to 90 °, and the dish cover bottom hypotenuse angle radian is
35 ° to 45 °.
The beneficial effects of the utility model are：This aircraft has more propellers than conventional aircraft, and lift is big and stable,
It is provided with ramjet and driving force is provided.The multiple uses such as unmanned plane, transporter can be made, be hybrid mode, be adapted to
High-speed flight.
Description of the drawings
Fig. 1 is the utility model structure chart；
Fig. 2 is the utility model cut-away view；
Fig. 3 is the utility model top view；
Fig. 4 is the utility model upward view；
Fig. 5 is the big ramjet structure chart of the utility model.
In figure：1st, outer dish；2nd, air inlet；3rd, steam vent；4th, annular exhaust outlet；5th, annular generator；6th, driver's cabin；7th, goods
Storehouse；8th, spin-ended；9th, dividing plate；10th, undercarriage；11st, skeleton；12nd, big ramjet；13rd, axle sleeve；14th, little punching press spray
Gas engine；15th, annular fuel tank；16th, arc air inlet；17th, spout.
Specific embodiment
The utility model is further described below in conjunction with the accompanying drawings.
As shown in Figure 1, Figure 2, a kind of high speed class disc-shaped flying craft shown in Fig. 3, Fig. 4 and Fig. 5, it is characterised in that including dish
Cover 1 and freight house 7, the outside of dish cover 1 is provided with air inlet 2, and 1 bottom margin of the dish cover is provided with equally distributed steam vent
3 and little ramjet 14, the dish cover 1 is connected by axle sleeve 13 with annular generator 5, and the freight house 7 passes through annular
Skeleton 11 in exhaust outlet 4 is connected with annular generator 5, and the annular exhaust outlet 4 has hung equally distributed big punching jetting and started
Machine 12, the annular generator 5 is provided with driver's cabin 6.Driver's cabin 6 is located at top, is easy to observe external environment condition, and freight house 7 is located at winged
In the middle of row device, to a greater extent utilization space, improves carrying capacity.
Further, the air inlet 2 is zigzag, and the air inlet 2 is connected by dividing plate 9 with axle sleeve 13, the dividing plate 9
Air inlet 2 is divided into into enterprising gas port and lower air inlet, and enterprising gas port and lower air inlet length ratio are 4.5: 2.5, it is described every
It is skeleton structure at the correspondence annular exhaust outlet 4 of plate 9.When aircraft is run at high speed, more than velocity of sound, sound barrier can be produced, air inlet 2 sets
Counting into zigzag can reduce sound barrier impact, and in addition dividing plate 9 is divided into two parts by the air blast in dish 1 passage of cover is entered, and realizes
Flight effect.
Further, the outside of the freight house 7 is provided with equally distributed spin-ended 8, plays reaction torque effect.
Further, the outside of the axle sleeve 13 is provided with annular fuel tank 15, used as the fuel tank of little ramjet 14.
Further, the bottom of the freight house 7 is provided with undercarriage 10, is easy to the safe falling of aircraft.
Further, 1 top hypotenuse angle radian of the dish cover is 70 ° to 90 °, 1 bottom hypotenuse angle radian of the dish cover
For 35 ° to 45 °, the convex lower flat structure of aircraft is adapted to, for aircraft lift slow down air resistance simultaneously is provided.
The aircraft is belonging to single rotor culvert type aircraft, and the convex lower flat similar flying saucer of profile, the aircraft is mixing
Power, can be used for high-speed flight.The dish cover 1 of the aircraft, equivalent to the rotor of helicopter, is umbrella formula.The aircraft power
It is annular generator 5, in whole process, middle air flow continues to provide air-flow by the rotatable interface being connected with axle sleeve 13, it is ensured that
The normal work of annular generator 5.The start-up course annular generator 5, as motor, is then generator in flight course, is aircraft
The radar airborne video recorder at top provides the energy.
During work, air inlet 2 is initially closed mode, starts annular generator 5, is connected with annular generator 5 by axle sleeve 13
Dish cover 1 start to begin spinning up, when dish 1 edge linear velocity of cover reaches 2 Mach, rise is hidden in dish cover 1
Four little ramjets 14, the annular fuel tank 15 located at the outside of axle sleeve 13 is four little ramjets 14
Fuel tank, after the operating of little ramjet 14 is stable, opens air inlet 2, and now annular generator 5 is converted to by startup motor
Generator.Air inlet 2 is provided with dividing plate 9, and the outside air-flow for entering is divided into into edge airflow and middle air flow, and edge airflow passes through goods
Rotatable spin-ended 8 of the outer wall of storehouse 7, plays reaction torque effect, and middle air flow is entered located at annular row by internal wheel of calming the anger
Three big ramjets 12 in air port 4.When the wind speed for entering annular exhaust outlet 4 reaches 2 Mach, startup is hung in ring
The big ramjet 12 of three of shape exhaust outlet 4, big ramjet 12 can left and right 360 ° and it is upper and lower 90 ° rotation,
Now adjust the steering horizontal direction of spout 17 of ramjet 12.There are two strands of gas around big ramjet 12
Stream, one is the air-flow from the top of annular exhaust outlet 4, and another stock carrys out wind, carrys out wind when heading on and reach 2 for heading on for horizontal direction
During Mach, the arc air inlet 16 of big ramjet 12 is opened.After aircraft is stable, carry-on air inlet is closed
Mouth 2, hides little ramjet 14, opens arc air inlet 16, and air-flow is sprayed by arc air inlet 16 into big punching press
Gas engine 12, now annular generator 5 drive dish cover 1 rotate.
This aircraft has more propellers than conventional aircraft, and lift is big and stable, and rotor rotates at a high speed, bottom even point
It is furnished with ramjet and forward drive power is provided.The aircraft can make the multiple uses such as unmanned plane, transporter, be that mixing is dynamic
Force mode, is adapted to high-speed flight.
Claims (6)
1. a kind of high speed class disc-shaped flying craft, it is characterised in that including dish cover (1) and freight house (7), the dish covers (1) outward
Side is provided with air inlet (2), and described dish cover (1) bottom margin is provided with equally distributed steam vent (3) and little punching jetting starts
Machine (14), dish cover (1) is connected by axle sleeve (13) with annular generator (5), and the freight house (7) is by annular exhaust outlet
(4) skeleton (11) in is connected with annular generator (5), and the annular exhaust outlet (4) has been hung equally distributed big punching jetting and sent out
Motivation (12), the annular generator (5) is provided with driver's cabin (6).
2. a kind of high speed class disc-shaped flying craft according to claim 1, it is characterised in that the air inlet (2) is sawtooth
Shape, the air inlet (2) is connected by dividing plate (9) with axle sleeve (13), and air inlet (2) is divided into enterprising gas port by the dividing plate (9)
And lower air inlet, and enterprising gas port and lower air inlet length ratio are 4.5: 2.5, the dividing plate (9) correspondence annular exhaust outlet (4)
Locate as skeleton structure.
3. a kind of high speed class disc-shaped flying craft according to claim 1, it is characterised in that freight house (7) outside is provided with
Equally distributed spin-ended (8).
4. a kind of high speed class disc-shaped flying craft according to claim 1, it is characterised in that axle sleeve (13) outside is provided with
Annular fuel tank (15).
5. a kind of high speed class disc-shaped flying craft according to claim 1, it is characterised in that freight house (7) bottom is provided with
Undercarriage (10).
6. a kind of high speed class disc-shaped flying craft according to claim 1, it is characterised in that described dish cover (1) top is oblique
Corner radian is 70 ° to 90 °, and dish cover (1) bottom hypotenuse angle radian is 35 ° to 45 °.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201621006526.1U CN206107556U (en) | 2016-08-29 | 2016-08-29 | High -speed type dish -shaped aircraft |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201621006526.1U CN206107556U (en) | 2016-08-29 | 2016-08-29 | High -speed type dish -shaped aircraft |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN206107556U true CN206107556U (en) | 2017-04-19 |
Family
ID=58516266
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201621006526.1U Expired - Fee Related CN206107556U (en) | 2016-08-29 | 2016-08-29 | High -speed type dish -shaped aircraft |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN206107556U (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN107323668A (en) * | 2017-07-21 | 2017-11-07 | 常州工学院 | One kind is without rotor remotely-piloted vehicle |
| CN109305360A (en) * | 2018-09-30 | 2019-02-05 | 杨清太 | Umbellate form jet type helicopters constructive method |
-
2016
- 2016-08-29 CN CN201621006526.1U patent/CN206107556U/en not_active Expired - Fee Related
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN107323668A (en) * | 2017-07-21 | 2017-11-07 | 常州工学院 | One kind is without rotor remotely-piloted vehicle |
| CN107323668B (en) * | 2017-07-21 | 2019-11-01 | 常州工学院 | A kind of no rotor remotely-piloted vehicle |
| CN109305360A (en) * | 2018-09-30 | 2019-02-05 | 杨清太 | Umbellate form jet type helicopters constructive method |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CN207417149U (en) | A kind of double lift culvert vertical take-off and landing aircrafts based on tilting duct | |
| CN101229822B (en) | Moving device | |
| CN106892102A (en) | A kind of VUAV and its control method | |
| CN108382579A (en) | A kind of new and effective tilting rotor unmanned vehicle | |
| CN103935517B (en) | Aircraft | |
| CN202783780U (en) | Annular blown flap ducted aerial vehicle | |
| CN105416572A (en) | Vectored thrust ducted propeller | |
| CN106864744A (en) | A kind of co-axial rotor variant vertically taking off and landing flyer | |
| CN206141828U (en) | Unmanned rotation rotor helicopter | |
| CN206107556U (en) | High -speed type dish -shaped aircraft | |
| CN102145744B (en) | High-speed energy-saving warplane | |
| CN206327567U (en) | A kind of compound unmanned vehicle | |
| CN101284570A (en) | Centrifugal fan type lift/propulsion device and aerocraft with the device | |
| CN102745329A (en) | Vortex rotary wing type flight vehicle | |
| CN107021208A (en) | The tail sitting posture VUAV and control method of a kind of utilization duct | |
| CN103407444B (en) | Based on the Fixed Wing AirVehicle of the landing technology that hovers | |
| CN107662703A (en) | Electronic double coaxial homonymy reversion tiltrotor aircrafts | |
| CN101121441A (en) | Aircraft with multi-wing and multi-thruster | |
| CN106945826A (en) | A kind of aircraft | |
| CN207417148U (en) | A kind of single lift culvert vertical take-off and landing aircraft based on tilting duct | |
| CN206598982U (en) | A kind of VUAV | |
| CN205819564U (en) | Modified model level of approximation rotates propeller wing flap lift-rising and connects wing aircraft | |
| WO2017121116A1 (en) | Engine for vertically taking off or landing with airfoil lift | |
| CN208291467U (en) | A kind of double ducted fan vector power short take-off and landing devices of fixed-wing | |
| CN209535458U (en) | A kind of unmanned plane based on multi-composite type dynamical system |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20170419 |