CN204196620U - A kind of novel Aeroamphibious triphibian aircraft - Google Patents
A kind of novel Aeroamphibious triphibian aircraft Download PDFInfo
- Publication number
- CN204196620U CN204196620U CN201420677367.2U CN201420677367U CN204196620U CN 204196620 U CN204196620 U CN 204196620U CN 201420677367 U CN201420677367 U CN 201420677367U CN 204196620 U CN204196620 U CN 204196620U
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- fuselage
- pyramid shape
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Abstract
The utility model discloses a kind of novel Aeroamphibious triphibian aircraft, comprise fuselage, be positioned at the wing of fuselage both sides and be positioned at the empennage of afterbody, the front portion of fuselage is provided with cabin, ventral is provided with below the middle part of fuselage, the rectangular pyramid shape of to be front end be in the front portion of the fuselage vertex of a cone, the top in cabin is provided with hatchcover, the epirelief rectangular pyramid shape of the upper surface of hatchcover to be postmedian the be vertex of a cone, the lower surface of forebody is provided with the conical plate that front end is a cone angle, the lower convex rectangular pyramid shape of the lower surface of conical plate to be middle front part the be vertex of a cone, the lower convex pentagonal pyramid shape of the lower surface of ventral to be middle front part the be vertex of a cone.The utility model is by being all designed to the polygonal pyramid shape of evagination by the lower surface of the conical plate of forebody, hatchcover upper surface, forebody lower surface and ventral lower surface, resistance can be reduced, line speed before improving, is convenient to again manufacture, also has good anti-radar effect; The lower convex rectangular pyramid shape structure of forebody lower surface can also play a point water effect, increases buoyancy, balance fuselage.
Description
Technical field
The utility model relates to a kind of aircraft, particularly relate to a kind of can in land-based area, marine site, spatial domain navigation and there is the novel Aeroamphibious triphibian aircraft of better anti-radar effect.
Background technology
Along with development and the growth in the living standard of science and technology, the part vehicle start to possess function of dwelling more, as can the automobile of amph air cushion vehicle or band water boat function, in recent years also start to occur the automobile that can fly.These two purpose vehicles have been applied or have been prepared to start application at present, but land, sea and air three-purpose vehicle not yet appears in market.
Publication number is " CN 101513934A ", name is called the patent of invention of " Aeroamphibious triphibian aircraft ", disclose a kind of air-sea-land aircraft, comprise drive system assembly, aircraft body is made up of head fuselage two parts, head is provided with elevating rudder: the air flow inlet bottom head is provided with the air inlet valve controlling suction quantity size, be made up of two valve blocks be hinged on axle, left and right side has air stream outlet to head; Fuselage afterbody top board is provided with the leg-of-mutton vertical wing; Afterbody is provided with fixed type horizontal tail and telescopic movable horizontal tail; Left and right wing is hinged on two waists of the isosceles trapezoid of base plate, and two wing flaps are hinged on two waists of the equicrural triangle of base plate; Base plate is provided with four wheels.Lift control when this patent solves flight from many aspects, when solving land locomotion and surface navigation time reverse buoyancy problem, be applicable to actual traffic tool making or toy makes.
But, in above-mentioned patent, the section components of this aircraft is globoidal structure, be not easy to processing, manufacture difficulty is comparatively large, and the effect in anti-radar is also poor, and head and ventral resistance is comparatively large, empennage controlling party to ability poor, cause the reason of these defects to be: fuselage middle front part has one section of cylindrical body, the bullet length of its front end is very little; Nacelle top is plane, and cabin door is in side; Forebody lower surface and ventral lower surface are plane; Empennage is two horizontal empennages, and back is provided with a vertical wing.These shortcomings cause this aircraft to there is applied defect, and the utility model proposes new solution based on these problems just.
Utility model content
The purpose of this utility model is just to provide to solve the problem a kind of and has better anti-radar effect and the little novel Aeroamphibious triphibian aircraft of running resistance.
The utility model is achieved through the following technical solutions above-mentioned purpose:
A kind of novel Aeroamphibious triphibian aircraft, comprise fuselage, be positioned at the wing of described fuselage both sides and be positioned at the empennage of described afterbody, the front portion of described fuselage is provided with cabin, ventral is provided with below the middle part of described fuselage, the rectangular pyramid shape of to be front end be in the front portion of the described fuselage vertex of a cone, the top in described cabin is provided with hatchcover, the epirelief rectangular pyramid shape of the upper surface of described hatchcover to be postmedian the be vertex of a cone, the lower surface of described forebody is provided with the conical plate that front end is a cone angle, the lower convex rectangular pyramid shape of the lower surface of described conical plate to be middle front part the be vertex of a cone, the lower convex pentagonal pyramid shape of the lower surface of described ventral to be middle front part the be vertex of a cone.
In said structure, the structural development of forebody, hatchcover upper surface, forebody lower surface and ventral lower surface is all presented as a core concept, forms the outer male conical of outside face exactly, and the quantity of its seamed edge is identical with the base angle quantity of corresponding component.
In order to make aircraft keep better balance in flight course, two sides of the transparent front panel of described hatchcover are inner concave.
Described empennage comprises the balance wing of a vertical vertical wing and two transverse directions, and two described balance wing are symmetrically set in the arranged on left and right sides of the described vertical wing, and the described vertical wing and described balance wing are triangle empennage.
The beneficial effects of the utility model are:
The utility model is by being all designed to the rectangular pyramid shape of evagination by the lower surface of the conical plate of forebody, hatchcover upper surface and forebody lower surface, ventral lower surface is designed to lower convex pentagonal pyramid shape, windage and water resistance can be reduced, line speed before improving, reduce energy consumption, be convenient to again processing, productive costs is low, and has good anti-radar effect; The lower convex rectangular pyramid shape structure of forebody lower surface, also helps when this aircraft moves ahead in water and plays a point water effect, and increase buoyancy, fuselage is balanced more; By the vertical wing and two balance wing are located at afterbody as empennage, controlling party to ability grow, be convenient to the direction controlling whole aircraft better.
Accompanying drawing explanation
Fig. 1 is the block diagram of novel Aeroamphibious triphibian aircraft described in the utility model;
Fig. 2 is the block diagram of fuselage described in the utility model;
Fig. 3 is the block diagram of hatchcover described in the utility model;
Fig. 4 is the birds-eye view of hatchcover described in the utility model;
Fig. 5 is the upward view of the conical plate of forebody lower surface described in the utility model;
Fig. 6 is the block diagram of the conical plate of forebody lower surface described in the utility model;
Fig. 7 is the block diagram of ventral described in the utility model;
Fig. 8 is the upward view of ventral described in the utility model;
Fig. 9 is the block diagram of the vertical wing described in the utility model;
Figure 10 is the block diagram of balance wing described in the utility model.
Detailed description of the invention
Below in conjunction with accompanying drawing, the utility model is described in further detail:
As shown in Fig. 1-Figure 10, novel Aeroamphibious triphibian aircraft described in the utility model comprises fuselage 1, be positioned at the wing 2 of fuselage 1 both sides and be positioned at the empennage of fuselage 1 afterbody, the front portion of fuselage 1 is provided with cabin 11, ventral 5 is provided with below the middle part of fuselage 1, the rectangular pyramid shape of to be front end be in the front portion of fuselage 1 vertex of a cone, the top in cabin 11 is provided with hatchcover 3, the epirelief rectangular pyramid shape of the upper surface of hatchcover 3 to be postmedian the be vertex of a cone, two sides 31 of the transparent front panel of hatchcover 3 are inner concave, the lower surface of fuselage 1 front portion is provided with the conical plate 4 that front end is a cone angle, the lower convex rectangular pyramid shape of the lower surface of conical plate 4 to be middle front part the be vertex of a cone, the lower convex pentagonal pyramid shape of the lower surface of ventral 5 to be middle front part the be vertex of a cone, the upper surface middle part of ventral 5 is provided with the groove 52 for being connected with fuselage 1, two inclined-planes that two sidepieces 51 of groove 52 both sides have middle high two ends low are formed, balance wing 7, two balance wing 7 that described empennage comprises a vertical vertical wing 6 and two transverse directions are symmetrically set in the arranged on left and right sides of the vertical wing 6, and the vertical wing 6 and balance wing 7 are triangle empennage.
From Fig. 1 and Fig. 7, the outer end of two sidepieces 51 of ventral 5 is connected with two wings 2 respectively, and two sidepieces 51 of ventral 5 also serve the effect of part wing simultaneously.
Also show the screw propeller 8 being positioned at fuselage 1 tail end in Fig. 1, rotate under the drive of motor, drive this aircraft to advance.The bottom of fuselage 1 is also provided with roller, not shown.
This aircraft as carrying the true aircraft of passenger, also can be used as the toy aircraft of amusement or experiment, also can be used as military aircraft, and dwell performance and anti-radar performance of its land, sea and air three has extremely strong practicality.
Above-described embodiment is preferred embodiment of the present utility model; it is not the restriction to technical solutions of the utility model; as long as without the technical scheme that creative work can realize on the basis of above-described embodiment, all should be considered as falling within the scope of the rights protection of the utility model patent.
Claims (3)
1. a novel Aeroamphibious triphibian aircraft, comprise fuselage, be positioned at the wing of described fuselage both sides and be positioned at the empennage of described afterbody, the front portion of described fuselage is provided with cabin, ventral is provided with below the middle part of described fuselage, it is characterized in that: the rectangular pyramid shape of to be front end be in the front portion of the described fuselage vertex of a cone, the top in described cabin is provided with hatchcover, the epirelief rectangular pyramid shape of the upper surface of described hatchcover to be postmedian the be vertex of a cone, the lower surface of described forebody is provided with the conical plate that front end is a cone angle, the lower convex rectangular pyramid shape of the lower surface of described conical plate to be middle front part the be vertex of a cone, the lower convex pentagonal pyramid shape of the lower surface of described ventral to be middle front part the be vertex of a cone.
2. novel Aeroamphibious triphibian aircraft according to claim 1, is characterized in that: two sides of the transparent front panel of described hatchcover are inner concave.
3. novel Aeroamphibious triphibian aircraft according to claim 1 and 2, it is characterized in that: described empennage comprises the balance wing of a vertical vertical wing and two transverse directions, two described balance wing are symmetrically set in the arranged on left and right sides of the described vertical wing, and the described vertical wing and described balance wing are triangle empennage.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201420677367.2U CN204196620U (en) | 2014-11-13 | 2014-11-13 | A kind of novel Aeroamphibious triphibian aircraft |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201420677367.2U CN204196620U (en) | 2014-11-13 | 2014-11-13 | A kind of novel Aeroamphibious triphibian aircraft |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN204196620U true CN204196620U (en) | 2015-03-11 |
Family
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Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201420677367.2U Expired - Fee Related CN204196620U (en) | 2014-11-13 | 2014-11-13 | A kind of novel Aeroamphibious triphibian aircraft |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN204196620U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN114578449A (en) * | 2022-03-04 | 2022-06-03 | 重庆交通大学 | Underground river hydrogeology detection ball |
-
2014
- 2014-11-13 CN CN201420677367.2U patent/CN204196620U/en not_active Expired - Fee Related
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN114578449A (en) * | 2022-03-04 | 2022-06-03 | 重庆交通大学 | Underground river hydrogeology detection ball |
| CN114578449B (en) * | 2022-03-04 | 2024-04-26 | 重庆交通大学 | Underground river hydrogeology condition detection ball |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20150311 Termination date: 20171113 |
|
| CF01 | Termination of patent right due to non-payment of annual fee |