CN205396519U - Warhead shape aircraft - Google Patents
Warhead shape aircraft Download PDFInfo
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- CN205396519U CN205396519U CN201620166468.2U CN201620166468U CN205396519U CN 205396519 U CN205396519 U CN 205396519U CN 201620166468 U CN201620166468 U CN 201620166468U CN 205396519 U CN205396519 U CN 205396519U
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Abstract
The utility model discloses a warhead shape aircraft possesses traditional jet airplane and helicopter's advantage simultaneously, and fast, the loading capacity is big, and vertical take -off or dash way take off to can the land, sea, air three way, the cabin wing is integrative, and simple structure is firm, balancing capability is strong, can fly in the weather environment of complicacy, and the security performance is high.
Description
Technical field
This utility model relates to a kind of bullet-shaped aircraft, the advantage being provided simultaneously with conventional jet aircraft and helicopter, and speed is fast, and loading capacity is big, takes off vertically or short field take-off.
Background technology
Conventional jet air speed is fast, and loading capacity is big.Conventional helicopter is without takeoff runway.Bullet-shaped aircraft is that both advantages are combined, and can use land, sea, air three.
Utility model content
In order to be that the advantage of conventional jet aircraft, conventional helicopter is combined, and can land, sea, air three use, invented bullet-shaped aircraft.
This utility model solves its technical problem and be the technical scheme is that, fuselage is designed to bullet-shaped (seeing it is bullet-shaped up and down, left and right sees it is half bullet-shaped), cabin wing is integrated, and is flank above cabin；Cabin is pushed up air above by pipeline under additional power drive and is sent under fuselage by lifting propeller, and the lift of aircraft, except the counteracting force pushing away gas from propeller, also obtains lift because air pressure decline above is pushed up in cabin；Pipeline seals water-tight with the bilge, and aircraft can travel on the water；Three lifting propeller combined effect decapacitation make aircraft vertical take off, climb, dive outside, also enhance the balanced capacity of aircraft, make aircraft can flight in complicated weather environment, security performance is high；Two, left and right propellant-actuated device makes aircraft obtain onward impulse, and simultaneously under the combined effect of flank, top, cabin air above is by ura-rate, and air pressure decline aircraft obtains lift, and therefore the lift of aircraft is huge；The jet-driven thrust in regulation and control left and right, can be achieved with aircraft and turns to；Retractable wheel makes aircraft can land, travel on land.
The beneficial effects of the utility model are the advantages being provided simultaneously with conventional jet aircraft and helicopter, and speed is fast, and loading capacity is big, takes off vertically or short field take-off, and can use land, sea, air three；Cabin wing one, simple in construction is firm；Balanced capacity is strong, can fly in complicated weather environment, and security performance is high.
Accompanying drawing explanation
In order to this utility model embodiment or of the prior art technical scheme are better described, accompanying drawing required in embodiment or description of the prior art will be briefly described below, apparently, accompanying drawing in the following describes is only an embodiment of the present utility model, for those of ordinary skill in the art, under the premise not paying creative work, it is also possible to obtain other accompanying drawings according to these accompanying drawings.
Fig. 1 is bullet-shaped aircraft schematic diagram.In figure, the parts of mark are, 1: bullet-shaped aircraft top view；2: bullet-shaped aircraft side view；3: bullet-shaped aircraft rearview；A: cabin；B: flank；C1: lifting propeller, power set and pipeline 1；C2: lifting propeller, power set and pipeline 2；C3: lifting propeller, power set and pipeline 3；D1: left propellant-actuated device, D2；Right propellant-actuated device.
Detailed description of the invention
Below in conjunction with the accompanying drawing in this utility model embodiment, the technical scheme in this utility model embodiment is clearly and completely described, it is clear that described embodiment is only a part of embodiment of this utility model, rather than whole embodiments.Based on the embodiment in this utility model, the every other embodiment that those of ordinary skill in the art obtain under not paying creative work premise, broadly fall into the scope of this utility model protection.
Fig. 1 is bullet-shaped aircraft schematic diagram.
Fuselage is designed to bullet-shaped (seeing it is bullet-shaped up and down, left and right sees it is half bullet-shaped), cabin wing is integrated, and is flank above cabin；Lifting propeller is arranged on top, cabin, by pipeline, cabin is pushed up air above and send under fuselage under additional power drive, and the lift of aircraft, except the counteracting force pushing away gas from propeller, also obtains lift because air pressure decline above is pushed up in cabin；Pipeline seals water-tight with the bilge, and aircraft can travel on the water；Three lifting propeller combined effect decapacitation make aircraft vertical take off, climb, dive outside, also enhance the balanced capacity of aircraft, make aircraft can flight in complicated weather environment, security performance is high；Two, left and right propellant-actuated device is arranged on cabin and pushes up upper, rear, makes aircraft obtain onward impulse, and simultaneously under the combined effect of flank, top, cabin air above is by ura-rate, and air pressure decline aircraft acquisition lift, therefore the lift of aircraft is huge；The jet-driven thrust in regulation and control left and right, can be achieved with aircraft and turns to.The bilge installs retractable wheel, makes aircraft can land, travel on land.
Driving device can be used instead and push away gas propeller or other type of drive.
Accompanying drawing is without auxiliary device such as retractable wheel.
The power set of lifting propeller are closed when water travels.
The profile of fuselage meets stealthy principle, uses stealth material manufacture, and stealthy ability is higher.
One of ordinary skill in the art will appreciate that: accompanying drawing is the schematic diagram of an embodiment, module or flow process in accompanying drawing are not necessarily implemented necessary to this utility model.
Last it is noted that above example is only in order to illustrate the technical solution of the utility model, it is not intended to limit；Although this utility model being described in detail with reference to previous embodiment, it will be understood by those within the art that: the technical scheme described in previous embodiment still can be modified by it, or wherein portion of techniques feature is carried out equivalent replacement；And these amendments or replacement, do not make the essence of appropriate technical solution depart from the spirit and scope of this utility model embodiment technical scheme.
Claims (1)
1. bullet-shaped aircraft, is characterized in that: the advantage being provided simultaneously with conventional jet aircraft and helicopter, and can use land, sea, air three；Fuselage being designed to bullet-shaped, cabin wing is integrated, and is flank above cabin；Lifting propeller is arranged on top, cabin, by pipeline, cabin is pushed up air above and send under fuselage under additional power drive, and the lift of aircraft, except the counteracting force pushing away gas from propeller, also obtains lift because air pressure decline above is pushed up in cabin；Pipeline seals water-tight with the bilge, and aircraft can travel on the water；Three lifting propeller combined effect decapacitation make aircraft vertical take off, climb, dive outside, also enhance the balanced capacity of aircraft, make aircraft can flight in complicated weather environment, security performance is high；Two, left and right propellant-actuated device is arranged on cabin and pushes up upper, rear, makes aircraft obtain onward impulse, and simultaneously under the combined effect of flank, top, cabin air above is by ura-rate, and air pressure decline aircraft acquisition lift, therefore the lift of aircraft is huge；The jet-driven thrust in regulation and control left and right, can be achieved with aircraft and turns to；The bilge installs retractable wheel, makes aircraft can land, travel on land.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201620166468.2U CN205396519U (en) | 2016-03-06 | 2016-03-06 | Warhead shape aircraft |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201620166468.2U CN205396519U (en) | 2016-03-06 | 2016-03-06 | Warhead shape aircraft |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN205396519U true CN205396519U (en) | 2016-07-27 |
Family
ID=56444710
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201620166468.2U Active CN205396519U (en) | 2016-03-06 | 2016-03-06 | Warhead shape aircraft |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN205396519U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN105564631A (en) * | 2016-03-06 | 2016-05-11 | 陈俞任 | Bullet shaped plane |
-
2016
- 2016-03-06 CN CN201620166468.2U patent/CN205396519U/en active Active
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN105564631A (en) * | 2016-03-06 | 2016-05-11 | 陈俞任 | Bullet shaped plane |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant |