CN201362361Y - Forward and rearward attacking type fighter - Google Patents
Forward and rearward attacking type fighter Download PDFInfo
- Publication number
- CN201362361Y CN201362361Y CNU2008201707560U CN200820170756U CN201362361Y CN 201362361 Y CN201362361 Y CN 201362361Y CN U2008201707560 U CNU2008201707560 U CN U2008201707560U CN 200820170756 U CN200820170756 U CN 200820170756U CN 201362361 Y CN201362361 Y CN 201362361Y
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- CN
- China
- Prior art keywords
- fuselage
- missiles
- fighter
- radar
- rearward
- 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
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Abstract
The utility model relates to a forward and rearward attacking type fighter, which is used in the military aerial warfare. The fighter comprises a fuselage, a cockpit, a front radar, wings, missiles and a driver; wherein, the cockpit is arranged on the fuselage; the front radar is arranged in the fuselage; and the missiles are arranged under the wings. The fighter is characterized in that a rear radar is also arranged in the rear part of the fuselage; back-to-back seats for front and rear pilots are arranged in the cockpit; and the wings can carry forward-fired missiles as well as rearward-fired missiles. The utility model can effectively avoid the situation of passively receiving attack; while one of the pilots looks ahead, the other pilot can receive the information coming from the rear, consequently, distant targets in all directions can be discovered in time, and the missiles are fired to destroy the enemy fighters in all directions.
Description
Technical field
The utility model relates to the aircraft technology field, especially relates to a kind of fighter plane.
Background technology
Fighter plane is that the military equipment to research is competed in countries in the world, and the speed of technological improvement is exceedingly fast, and the U.S. has succeeded in developing the F22 stealth fighter of excellent performance; But present fighter plane mostly is the one-man operation, and radar is to receive the place ahead information; When entering the fistfight state, can only forwards launch a guided missile, the rear of aircraft can be in situation passive and vulnerable to attack.
Summary of the invention
The purpose of this utility model is in order to overcome above-mentioned defective, provide a kind of front and back attack fighter plane, when an aviator concentrates the place ahead on, another aviator can receive the information from the rear, the target in each orientation before and after in time finding at a distance, the enemy plane of each target direction is launched a guided missile and is smashed forwards, backwards.
For achieving the above object, the technical solution of the utility model is such: the attack fighter plane in a kind of front and back comprises fuselage, the preposition radar in the operator's compartment on the fuselage, fuselage, the guided missile under the wing, wing, actuating device; It is characterized in that, in the rear portion of fuselage, also be provided with rearmounted radar; Aviator's seat dorsad before and after in said operator's compartment, establishing; Guided missile under the said wing except that launching forward, also carries retro-launched missile.
Owing to adopted technique scheme, the attack fighter plane in a kind of front and back of the present utility model, can effectively avoid the appearance of situation passive and vulnerable to attack, when an aviator concentrates the place ahead on, another aviator can receive the information from the rear, in time find the target in each orientation at a distance, launch a guided missile to the enemy plane of each target direction and smashed.
Description of drawings
The present invention is further illustrated below in conjunction with accompanying drawing.
Fig. 1 is a structural representation of the present utility model.
Among the figure: 1, preposition guided missile, 2, operator's compartment, 3, fuselage, 4, rearmounted radar, 5, wing, 6, guided missile, 7, guided missile.
The specific embodiment
By shown in Figure 1, the attack fighter plane in a kind of front and back of the present utility model comprises fuselage 3, the preposition radar 1 in the operator's compartment 2 on the fuselage, fuselage, the guided missile under the wing 5, wing, actuating device; It is characterized in that, in the rear portion of fuselage, also be provided with rearmounted radar 4; Aviator's seat dorsad before and after in said operator's compartment 2, establishing; Guided missile under the said wing 5 has guided missile 6 and the retro-launched missile 7 launched forward;
Be arranged with the sleeve of the stream line pattern outer wall that can reduce air resistance at the afterbody of said retro-launched missile 7.
Claims (2)
1, the attack fighter plane in a kind of front and back comprises fuselage (3), the preposition radar (1) in the operator's compartment on the fuselage (2), fuselage, wing (5), the guided missile under the wing, actuating device; It is characterized in that: in the rear portion of fuselage (3), also be provided with rearmounted radar (4); Aviator's seat dorsad before and after in said operator's compartment (2), establishing; Guided missile under the said wing (5) has the guided missile (6) of emission forward, and retro-launched missile (7).
2, said at the attack fighter plane in said a kind of front and back according to claim 1, it is characterized in that: the afterbody of said retro-launched missile (7) is arranged with the sleeve of the stream line pattern outer wall that can reduce air resistance.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CNU2008201707560U CN201362361Y (en) | 2008-12-25 | 2008-12-25 | Forward and rearward attacking type fighter |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CNU2008201707560U CN201362361Y (en) | 2008-12-25 | 2008-12-25 | Forward and rearward attacking type fighter |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN201362361Y true CN201362361Y (en) | 2009-12-16 |
Family
ID=41473020
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CNU2008201707560U Expired - Fee Related CN201362361Y (en) | 2008-12-25 | 2008-12-25 | Forward and rearward attacking type fighter |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN201362361Y (en) |
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN103209892A (en) * | 2010-07-28 | 2013-07-17 | 航空集团联合控股公司 | Aircraft with an integral aerodynamic configuration |
| CN104667539A (en) * | 2015-02-21 | 2015-06-03 | 佛山市三水区希望火炬教育科技有限公司 | Special aircraft capable of lunching aluminum paper to replace jamming bomb for teenager national defense scientific literacy education and training |
| CN105318792A (en) * | 2014-08-01 | 2016-02-10 | 王正铉 | Device for launching guided missile reversed with flight path of aircraft to conduct offence and defense |
| CN106828925A (en) * | 2017-01-21 | 2017-06-13 | 佛山市三水区希望火炬教育科技有限公司 | A kind of teenager's defence education it is special plunder extra large ground effect vehicle |
-
2008
- 2008-12-25 CN CNU2008201707560U patent/CN201362361Y/en not_active Expired - Fee Related
Cited By (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN103209892A (en) * | 2010-07-28 | 2013-07-17 | 航空集团联合控股公司 | Aircraft with an integral aerodynamic configuration |
| CN103209892B (en) * | 2010-07-28 | 2015-09-16 | 航空集团联合控股公司 | There is the aircraft of integrated aerodynamic force configuration |
| CN105318792A (en) * | 2014-08-01 | 2016-02-10 | 王正铉 | Device for launching guided missile reversed with flight path of aircraft to conduct offence and defense |
| CN104667539A (en) * | 2015-02-21 | 2015-06-03 | 佛山市三水区希望火炬教育科技有限公司 | Special aircraft capable of lunching aluminum paper to replace jamming bomb for teenager national defense scientific literacy education and training |
| CN106828925A (en) * | 2017-01-21 | 2017-06-13 | 佛山市三水区希望火炬教育科技有限公司 | A kind of teenager's defence education it is special plunder extra large ground effect vehicle |
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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: 20091216 Termination date: 20101225 |