CN203094448U - Airplane with front and rear rudders and multiple power wings - Google Patents
Airplane with front and rear rudders and multiple power wings Download PDFInfo
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- CN203094448U CN203094448U CN 201320072111 CN201320072111U CN203094448U CN 203094448 U CN203094448 U CN 203094448U CN 201320072111 CN201320072111 CN 201320072111 CN 201320072111 U CN201320072111 U CN 201320072111U CN 203094448 U CN203094448 U CN 203094448U
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Abstract
The utility model relates to an airplane with front and rear rudders and multiple power wings. The airplane is characterized in that a front wing (A) and a rear wing (B) are symmetrically arranged on two sides of an airplane body; the rear side of the front wing (A) is provided with a wing flap (A5) and an aileron (A2), the lower side of the wing is provided with a group of engines (A1), the upper side of the wing is provided with a directional wing (A3), and a rudder (A4) is arranged on the directional wing; and the rear side of the rear wing (B) is provided with a wing flap (B5) and an aileron (B2), the lower side of the wing is provided with a group of engines (B1), the upper side of the wing is provided with a directional wing (B3), and a rudder (B4) is arranged on the directional wing. By virtue of the technical scheme, the airplane has the advantages of high takeoff weight, good flight balance, small turning radius, fast direction change, short takeoff and landing sliding distance and the like.
Description
Technical field:
The utility model relates to a kind of aircraft, particularly a kind of many power wings of fore-and-aft direction rudder aircraft.
Background technology:
The take-off weight of aircraft and the size of wing and power have direct relation, owing to be subjected to material and technology limitation, wing can not unconfinedly strengthen; The design of big-block engine and processing all have a very high technology content, and manufacturing cost and service expenditure height and weight, size, noise are all bigger.Because now large aircraft adopts an assembly that the wing of big-block engine is arranged, so maximum take-off weight just is subjected to certain restriction; Aircraft now has only afterbody to be provided with yaw rudder, and turning to of aircraft and balance are also had certain restriction, and again because the gross area of aileron on the wing and wing flap is less, and the takeoff speed and the landing speed of aircraft are higher, it is longer with the landing and sliding distance to take off.
The utility model content:
The purpose of this utility model is exactly in order to solve the deficiency of existing aircraft, design a kind of many power wing, multi-aspect rudder, many wing flaps aircraft, be exactly front and rear at fuselage specifically and be provided with wing more than two groups or two groups, wing is provided with wing flap, aileron, yaw rudder and organizes put-put more, to overcome the above-mentioned shortcoming of large aircraft now.
To achieve these goals, the utility model has adopted following technical scheme:
Many power wings of fore-and-aft direction rudder aircraft, it comprises the fuselage of aircraft, it is characterized in that: the front and rear bilateral symmetry of fuselage is provided with preceding wing, back wing; Preceding wing rear side is provided with wing flap, aileron, and the downside of preceding wing is provided with one group of driving engine, and the upside of preceding wing is provided with the direction wing, and the direction wing is provided with yaw rudder; Back wing rear side is provided with wing flap, aileron, and the downside of back wing is provided with one group of driving engine, and the upside of back wing is provided with the direction wing, and the direction wing is provided with yaw rudder.The quantity N of driving engine can determine according to the aircraft size more than or equal to 1 on the forward and backward wing.
On the basis of technique scheme, also have following further technical scheme:
Secondary wing before being arranged with on the fuselage of preceding wing below, preceding secondary wing rear side is provided with wing flap, aileron, and the downside of preceding secondary wing is provided with one group of driving engine; The quantity N of driving engine can determine according to the aircraft size more than or equal to 1 on the preceding secondary wing;
Be arranged with the secondary wing in back on the fuselage of back wing below, the secondary wing rear side in back is provided with wing flap, aileron, and the downside of the secondary wing in back is provided with one group of driving engine, and the quantity N of driving engine can determine according to the aircraft size more than or equal to 1 on the secondary wing in back.
Owing to adopted technique scheme, made to the utlity model has following advantage:
(1), increase power wing quantity, can improve the load carrying ability of aircraft;
(2), increase the quantity of aileron, wing flap, promptly increase their gross area, can improve rising or falling speed and decelerating power at any time;
(3), increase the quantity of yaw rudder, promptly increase their gross area, thereby improve turning velocity.
For more detailed explanation the utility model, following accompanying drawing provides three most preferred embodiments.
Description of drawings:
Fig. 1 is a double dynamical wing aircraft block diagram of the present utility model;
Fig. 2 is three engine wing aircraft block diagrams of the present utility model:
Fig. 3 is four engine wing aircraft block diagrams of the present utility model.
The specific embodiment:
Embodiment one,
Fig. 1 is a kind of many power wings of fore-and-aft direction rudder aircraft that the utility model provides, it comprises: forebody is provided with preceding wing A, preceding wing A rear side is provided with wing flap A5, aileron A2, the downside of preceding wing is provided with one group of driving engine A1, the upside of preceding wing is provided with direction wing A3, and the direction wing is provided with yaw rudder A4; Fuselage afterbody is provided with back wing B, and back wing B rear side is provided with wing flap B5, aileron B2, and the downside of back wing is provided with one group of driving engine B1, and the upside of back wing is provided with direction wing B3, and the direction wing is provided with yaw rudder B4.
EmbodimentTwo,
Fig. 2 is another many power wings of fore-and-aft direction rudder aircraft that the utility model provides, it comprises: forebody is provided with preceding wing A, preceding wing A rear side is provided with wing flap A5, aileron A2, the downside of preceding wing is provided with one group of driving engine A1, the upside of preceding wing is provided with direction wing A3, and the direction wing is provided with yaw rudder A4; Fuselage afterbody is provided with back wing B, and back wing B rear side is provided with wing flap B5, aileron B2, and the downside of back wing is provided with one group of driving engine B1, and the upside of back wing is provided with direction wing B3, and the direction wing is provided with yaw rudder B4; Secondary wing C before being arranged with on the fuselage of preceding wing A below, preceding secondary wing C rear side is provided with wing flap C5, aileron C2, and the downside of preceding secondary wing is provided with one group of driving engine C1.
EmbodimentThree,
Fig. 3 is another many power wings of fore-and-aft direction rudder aircraft that the utility model provides, it comprises: forebody is provided with preceding wing A, preceding wing A rear side is provided with wing flap A5, aileron A2, the downside of wing is provided with one group of driving engine A1, the upside of preceding wing is provided with direction wing A3, and the direction wing is provided with yaw rudder A4; Fuselage afterbody is provided with back wing B, and back wing B rear side is provided with wing flap B5, aileron B2, and the downside of back wing is provided with one group of driving engine B1, and the upside of back wing is provided with direction wing B3, and the direction wing is provided with yaw rudder B4; Secondary wing C before being arranged with on the fuselage of preceding wing A below, preceding secondary wing C rear side is provided with wing flap C5, aileron C2, and the downside of preceding secondary wing is provided with one group of driving engine C1; Be arranged with the secondary wing D in back on the fuselage of back wing B below, the secondary wing D rear side in back is provided with wing flap D5, aileron D2, and the downside of the secondary wing in back is provided with one group of driving engine D1.
Owing to adopted technique scheme, many power wings of the fore-and-aft direction rudder aircraft that makes the utility model relate to has that take-off weight is big, flight balance good, turn radius is little, change the orientation fast, take off and landing and sliding apart from advantage such as short.
Claims (3)
1. many power wings of fore-and-aft direction rudder aircraft comprises the fuselage of aircraft it is characterized in that it comprises:
The front and rear bilateral symmetry of a, fuselage is provided with preceding wing (A), back wing (B);
B, preceding wing (A) rear side are provided with wing flap (A5), aileron (A2), and the downside of preceding wing is provided with one group of driving engine (A1), and the upside of preceding wing is provided with the direction wing (A3), and the direction wing is provided with yaw rudder (A4);
C, back wing (B) rear side are provided with wing flap (B5), aileron (B2), and the downside of back wing is provided with one group of driving engine (B1), and the upside of back wing is provided with the direction wing (B3), and the direction wing is provided with yaw rudder (B4).
2. another many power wings of fore-and-aft direction rudder aircraft according to claim 1, it is characterized in that: secondary wing (C) before being arranged with on the fuselage of preceding wing (A) below, preceding secondary wing (C) rear side is provided with wing flap (C5), aileron (C2), and the downside of preceding secondary wing is provided with one group of driving engine (C1).
3. another many power wings of fore-and-aft direction rudder aircraft according to claim 2, it is characterized in that: be arranged with back secondary wing (D) on the fuselage of back wing (B) below, back secondary wing (D) rear side is provided with wing flap (D5), aileron (D2), and the downside of the secondary wing in back is provided with one group of driving engine (D1).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN 201320072111 CN203094448U (en) | 2013-02-08 | 2013-02-08 | Airplane with front and rear rudders and multiple power wings |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN 201320072111 CN203094448U (en) | 2013-02-08 | 2013-02-08 | Airplane with front and rear rudders and multiple power wings |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN203094448U true CN203094448U (en) | 2013-07-31 |
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Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN 201320072111 Expired - Fee Related CN203094448U (en) | 2013-02-08 | 2013-02-08 | Airplane with front and rear rudders and multiple power wings |
Country Status (1)
| Country | Link |
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| CN (1) | CN203094448U (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN103072691A (en) * | 2013-02-08 | 2013-05-01 | 郭建中 | Front-rear-rudder multiple-power-wing airplane |
| CN107914863A (en) * | 2017-12-09 | 2018-04-17 | 佛山市神风航空科技有限公司 | One kind deformation biplane |
-
2013
- 2013-02-08 CN CN 201320072111 patent/CN203094448U/en not_active Expired - Fee Related
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN103072691A (en) * | 2013-02-08 | 2013-05-01 | 郭建中 | Front-rear-rudder multiple-power-wing airplane |
| CN107914863A (en) * | 2017-12-09 | 2018-04-17 | 佛山市神风航空科技有限公司 | One kind deformation biplane |
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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: 20130731 Termination date: 20160208 |
|
| CF01 | Termination of patent right due to non-payment of annual fee |