CN203127146U - Ring-shaped aircraft with power - Google Patents
Ring-shaped aircraft with power Download PDFInfo
- Publication number
- CN203127146U CN203127146U CN2012206888376U CN201220688837U CN203127146U CN 203127146 U CN203127146 U CN 203127146U CN 2012206888376 U CN2012206888376 U CN 2012206888376U CN 201220688837 U CN201220688837 U CN 201220688837U CN 203127146 U CN203127146 U CN 203127146U
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- Prior art keywords
- ring
- main engine
- aircraft
- annulus
- groove
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Abstract
The utility model aims at providing a ring-shaped aircraft with power. The ring-shaped aircraft comprises a main engine, an oval bracket, a supporting rod, a ring, a groove, auxiliary engines and a cross-shaped control plane, wherein the main engine is arranged on the oval bracket; the oval bracket is connected with three supporting rods which are connected with the ring; an included angle between the two adjacent supporting rods is 60 degrees; the groove is formed in the bottom of the ring; the two auxiliary engines are arranged on the ring; and the cross-shaped control plane is arranged on the main engine. The ring-shaped aircraft has the advantages that the continuous autonomous flying can be achieved, all the directions can be controlled, the flying with the power is achieved, a wetted area is small, the frictional resistance and the viscous resistance are small, the stability is good and the flying distance is far.
Description
Technical field
The utility model relates to a kind of aircraft, is specifically related to a kind of annular aircraft of drive.
Background technology
Modern aviation knowledge is told us: it is that wing is a fairing or an approximate fairing that aircraft can fly up its groundwork, can produce lift under the condition that the angle of attack and high velocity air are arranged.The version of aircraft comprises fixed wing aircraft and rotary wing aircraft.And the action principle of flying barrel aircraft is slightly different with it, and aloft flying barrel is by advancing and rotation produces relative motion with air, thereby produces lift, and the moment of momentum by rotation guarantees stable.Existing invention or utility model about flying barrel now all is to be that the master can not carry out the drive autonomous flight or carry out reality control in real time effectively with the toy.China's publication publication number: CN1439444A discloses a kind of aerodynamic flight ring open day on September 3rd, 2003, and its weak point is to be a kind of toy, does not have power system can not carry out autonomous flight and each is to control.
The utility model content
For overcoming above-mentioned the deficiencies in the prior art, the purpose of this utility model provides a kind of annular aircraft of drive.
The utility model is achieved in that a kind of annular aircraft of drive, comprise sustainer, main engine, ellipse support, pole, annulus, groove, auxiliary motivation and cross rudder face, sustainer, main engine is installed on the ellipse support, ellipse support is connected with three poles, pole is connected with annulus, and the angle between the adjacent pole is 60 °, and the bottom of annulus is provided with groove, two auxiliary engines are installed on the annulus, and sustainer, main engine is provided with the cross rudder face.
The utility model is a kind of aircraft that can continue autonomous flight, can be to each to controlling, and be drive flight, wetted area is little, and friction drag and viscosity drag are little, good stability, flying distance is far away.
Description of drawings
Fig. 1 is structural representation of the present utility model;
Fig. 2 is cross rudder face scheme drawing described in the utility model;
Fig. 3 is groove scheme drawing described in the utility model.
The specific embodiment
The utility model is described in further detail below in conjunction with accompanying drawing:
As Fig. 1, Fig. 2 and shown in Figure 3, a kind of annular aircraft of drive, comprise sustainer, main engine 1, ellipse support 8, pole 3, annulus 4, groove 5, auxiliary motivation 6 and cross rudder face 7, sustainer, main engine 1 is installed on the ellipse support 2, and ellipse support 2 is connected with three poles 3, and pole 3 is connected with annulus 4, angle between the adjacent pole 3 is 60 °, the bottom of annulus 4 is provided with groove 5, and two auxiliary engines 6 are installed on the annulus 4, and sustainer, main engine 1 is provided with cross rudder face 7.
The utility model is by the longitudinal movement of sustainer, main engine realization flying barrel, and two auxiliary engines are realized the circular movement of flying barrels, produces lift.Sustainer, main engine trailing edge configuration cross rudder face is realized pitching and the course control of flying barrel.Annulus section of the present utility model adopts Airfoil Design can further increase lift and reduces resistance, realizes the long distance flight of aircraft.
The utility model is a kind of aircraft that can continue autonomous flight, can be to each to controlling, and be drive flight, wetted area is little, and friction drag and viscosity drag are little, good stability, flying distance is far away.
Claims (1)
1. the annular aircraft of a drive, comprise sustainer, main engine (1), ellipse support (2), pole (3), annulus (4), groove (5), auxiliary motivation (6) and cross rudder face (7), it is characterized in that: sustainer, main engine (1) is installed on the ellipse support (2), ellipse support (2) is connected with three poles (3), pole (3) is connected with annulus (4), angle between the adjacent pole (3) is 60 °, the bottom of annulus (4) is provided with groove (5), two auxiliary engines (6) are installed on the annulus (4), and sustainer, main engine (1) is provided with cross rudder face (7).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN2012206888376U CN203127146U (en) | 2012-12-14 | 2012-12-14 | Ring-shaped aircraft with power |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN2012206888376U CN203127146U (en) | 2012-12-14 | 2012-12-14 | Ring-shaped aircraft with power |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN203127146U true CN203127146U (en) | 2013-08-14 |
Family
ID=48935149
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN2012206888376U Expired - Fee Related CN203127146U (en) | 2012-12-14 | 2012-12-14 | Ring-shaped aircraft with power |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN203127146U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN103010464A (en) * | 2012-12-14 | 2013-04-03 | 中国航空工业空气动力研究院 | Annular aircraft with power |
-
2012
- 2012-12-14 CN CN2012206888376U patent/CN203127146U/en not_active Expired - Fee Related
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN103010464A (en) * | 2012-12-14 | 2013-04-03 | 中国航空工业空气动力研究院 | Annular aircraft with power |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| C17 | Cessation of patent right | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20130814 Termination date: 20131214 |