CN202429350U - Aerial vehicle - Google Patents
Aerial vehicle Download PDFInfo
- Publication number
- CN202429350U CN202429350U CN2011205346826U CN201120534682U CN202429350U CN 202429350 U CN202429350 U CN 202429350U CN 2011205346826 U CN2011205346826 U CN 2011205346826U CN 201120534682 U CN201120534682 U CN 201120534682U CN 202429350 U CN202429350 U CN 202429350U
- Authority
- CN
- China
- Prior art keywords
- aerial vehicle
- aircraft
- cabin
- cylindrical
- utility
- 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
Images
Abstract
The utility model relates to an aircraft appliance and particularly relates to an aerial vehicle. The aerial vehicle comprises a conical roof and a cylindrical cabin which are inosculated and fixedly connected. The aerial vehicle is characterized in that the top end of the conical roof is provided with a small propeller connected through a hollow supporting frame; the upper part of the cylindrical cabin is provided with two layers of main propellers rotating inversely; the two sides of the lower part of the cylindrical cabin are respectively provided with a semi-cylindrical side wing; and the bottom part of the cylindrical cabin is provided with an undercarriage. The aerial vehicle has the beneficial effects of simple structure, light body, small occupied area, big bearing capacity and high stability.
Description
(1) technical field
The utility model relates to a kind of airflight apparatus, particularly a kind of aircraft.
(2) background technology
The helicopter aspects such as military affairs, agricultural or industry of society in modern times all is widely used, but existing helicopter is mostly because own wt is too heavy, thereby load carrying ability is too little and really powerless during constantly with some must handling heavy article in danger and disaster.
(3) summary of the invention
The utility model provides the aircraft that a kind of load carrying ability is big, stability is high in order to remedy the shortcoming of prior art.
The utility model is realized through following technical scheme:
A kind of aircraft; It is characterized in that: the taper machine top and the cylindricality cabin that comprise identical each other and captive joint; Top, said taper machine top is provided with through hollow support frame bonded assembly minor spiral oar, and main screw, both sides, bottom that top, cylindricality cabin is provided with two-layer opposite spin respectively are provided with semicircle column type flank, a bottom and are provided with alighting gear.
Therefore, the beneficial effect of the utility model is: this aircraft, and simple in structure, fuselage is light, and floor area is little, and bearing capacity is big, and stability is high.
(4) description of drawings
Below in conjunction with accompanying drawing the utility model is further described.
Accompanying drawing 1 is the structural representation of the utility model.Among the figure, 1 taper machine top, 2 cylindricality cabins, 3 bracing frames, 4 minor spiral oars, 5 main screws, 6 flanks, 7 alighting gears.
(5) specific embodiment
Accompanying drawing is a kind of specific embodiment of the utility model.This embodiment comprises the taper machine top 1 and cylindricality cabin 2 of identical each other and captive joint; It is characterized in that: said taper machine pushes up 1 top and is provided with through hollow support frame 3 bonded assembly minor spiral oars 4, and main screw 5, both sides, bottom that 2 tops, cylindricality cabin are provided with two-layer opposite spin respectively are provided with semicircle column type flank 6, a bottom and are provided with alighting gear 7.
Adopt the aircraft of the utility model, but minor spiral oar 4 Be Controlled plane of rotations, the power that provides lift or horizontal direction to go for aircraft; Dynamic dwang provides the power of minor spiral oar 4 in the hollow support frame 3, and main screw 5 is two-layer, respectively along converse direction rotation; Can both can be aircraft main lift was provided; Can reduce the power of aircraft self rotation again, powerful air-flow is arranged during owing to aircraft flight, the semicircle column type flank 6 of fuselage both sides can produce the power that contends with hull rotation according to aerodynamic principle; Thereby prevent that fuselage from spinning, keeping the fuselage balance, alighting gear 7 can support aircraft and be supported on the ground.Therefore, the beneficial effect of the utility model is: this aircraft, and simple in structure, fuselage is light, and floor area is little, and bearing capacity is big, and stability is high.
Claims (1)
1. aircraft; It is characterized in that: the taper machine top (1) and cylindricality cabin (2) that comprises identical each other and captive joint; (1) top, said taper machine top is provided with through hollow support frame (3) bonded assembly minor spiral oar (4), and main screw (5), the both sides, bottom that top, cylindricality cabin (2) is provided with two-layer opposite spin respectively are provided with a semicircle column type flank (6), the bottom is provided with alighting gear (7).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN2011205346826U CN202429350U (en) | 2011-12-20 | 2011-12-20 | Aerial vehicle |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN2011205346826U CN202429350U (en) | 2011-12-20 | 2011-12-20 | Aerial vehicle |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN202429350U true CN202429350U (en) | 2012-09-12 |
Family
ID=46778817
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN2011205346826U Expired - Fee Related CN202429350U (en) | 2011-12-20 | 2011-12-20 | Aerial vehicle |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN202429350U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN107416196A (en) * | 2017-07-05 | 2017-12-01 | 南宁学院 | A kind of aileron short distance logistics unmanned plane of a main wing four |
-
2011
- 2011-12-20 CN CN2011205346826U patent/CN202429350U/en not_active Expired - Fee Related
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN107416196A (en) * | 2017-07-05 | 2017-12-01 | 南宁学院 | A kind of aileron short distance logistics unmanned plane of a main wing four |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CN104085530B (en) | The coaxial multi-rotor aerocraft of duct | |
| CN104925253A (en) | Triphibious coaxial four-rotor aircraft | |
| CN103935510A (en) | Tilted four-rotor aircraft | |
| CN103552686B (en) | A kind of compound type duct aerial reconnaissance machine people | |
| CN206590103U (en) | A kind of collapsible arm fuselage based on integral type multi-rotor unmanned aerial vehicle central frame | |
| CN104787327A (en) | Axle distance-variable multi-rotor aircraft | |
| CN204197290U (en) | A kind of novel tiltrotor aircraft | |
| CN104590535A (en) | Propelling device for airship power device | |
| CN202429350U (en) | Aerial vehicle | |
| CN201175582Y (en) | Model aircraft | |
| CN106114842A (en) | A kind of oil electricity mixing coaxial dual-rotor helicopter and using method thereof | |
| CN204802084U (en) | Many rotors plant protection unmanned aerial vehicle | |
| CN108609164B (en) | Utilize aircraft undercarriage of spring buckle | |
| CN208775012U (en) | A kind of VTOL flying platform high efficiency lift unit | |
| CN209889098U (en) | Unmanned aerial vehicle with buffer function undercarriage | |
| CN206358351U (en) | A kind of wing and the double two axle aircraft verted of engine | |
| CN104476993A (en) | Extensible tail wing structure | |
| CN103466496B (en) | A kind of aircraft jack-up device | |
| CN201045076Y (en) | 360 degree steering helicopter | |
| CN207523920U (en) | Landing gear assembly and unmanned plane | |
| CN204124358U (en) | A kind of dirigible alighting gear | |
| CN105435466A (en) | Toy plane | |
| CN206511118U (en) | A kind of multi-rotor unmanned aerial vehicle housing construction design | |
| CN215663984U (en) | Aircraft | |
| CN220518611U (en) | Lightweight unmanned aerial vehicle flight platform |
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: 20120912 Termination date: 20131220 |