CN107054647A - A kind of sky penetrates bait machine - Google Patents
A kind of sky penetrates bait machine Download PDFInfo
- Publication number
- CN107054647A CN107054647A CN201710156435.9A CN201710156435A CN107054647A CN 107054647 A CN107054647 A CN 107054647A CN 201710156435 A CN201710156435 A CN 201710156435A CN 107054647 A CN107054647 A CN 107054647A
- Authority
- CN
- China
- Prior art keywords
- sky
- engine
- fuselage
- decoy
- bait machine
- 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.)
- Pending
Links
- 230000000149 penetrating effect Effects 0.000 claims abstract description 6
- 238000000034 method Methods 0.000 claims description 5
- 241000700199 Cavia porcellus Species 0.000 claims description 4
- 238000004088 simulation Methods 0.000 claims description 2
- 230000000087 stabilizing effect Effects 0.000 claims description 2
- 230000006641 stabilisation Effects 0.000 abstract 1
- 238000011105 stabilization Methods 0.000 abstract 1
- 230000007547 defect Effects 0.000 description 1
- 230000007812 deficiency Effects 0.000 description 1
- 238000010586 diagram Methods 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 239000000203 mixture Substances 0.000 description 1
- 230000001737 promoting effect Effects 0.000 description 1
- 230000005855 radiation Effects 0.000 description 1
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C39/00—Aircraft not otherwise provided for
- B64C39/02—Aircraft not otherwise provided for characterised by special use
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D1/00—Dropping, ejecting, releasing, or receiving articles, liquids, or the like, in flight
- B64D1/02—Dropping, ejecting, or releasing articles
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Catching Or Destruction (AREA)
Abstract
The present invention disclose a kind of sky penetrate bait machine include fuselage（1）, wing（2）, empennage（3）, engine and electronic decoy（5）, it is characterised in that wing（2）, positioned at fuselage（1）Middle part, lift is provided when penetrating bait machine flight for sky；Empennage（3）, it is fixed on fuselage（1）Afterbody；Electronic decoy（5）, installed in fuselage（1）Inside, launches radio signal after the power-up；Engine is arranged on fuselage（1）Afterbody；Wing（2）With the upper counterangle, upper counterangle scope is 0o~15o.The high-temperature plume that engine is produced（9）For infrared decoy.The principle of the invention is simple, and realizability is strong.Do not need control system to complete the stabilization of aircraft, it is easy to reduce cost, radar decoy and infrared trick can be taken into account simultaneously, be adapted as bait high-volume and use.
Description
Technical field
The invention belongs to Flight Vehicle Design specialty, it is related to the design and decoy method of a kind of aircraft.
Background technology
Current aircraft is self-contained electronic jamming device to the trick mode of radio or infrared acquisition or released to outside machine
Put jamming bomb.The defect that aforesaid way is present be can not while carry out radar decoy and infrared trick, therefore do not adapt to first
Enter the confrontation of anti-ECM technique.
The content of the invention
It is an object of the invention to overcome deficiency of the prior art, a kind of thinking is proposed effectively, it is with low cost and have
The sky that can be engineered penetrates bait machine.The need for taking into account radar decoy and infrared trick.
The present invention realizes that the technical scheme of above-mentioned purpose is：
A kind of sky penetrates bait machine, including fuselage, wing, empennage, engine and electronic decoy, and wing 2, positioned at waist, is
Sky provides lift when penetrating bait machine flight；Empennage is fixed on afterbody；Electronic decoy is arranged on fuselage interior, sends out after the power-up
Penetrate radio signal；Engine is arranged on afterbody；Wing has the 0o~15o upper counterangle.
The engine is rocket engine, and the high-temperature plume that rocket engine is produced is infrared decoy.
The empennage is V-shaped on fuselage, X-type or Y-type layout, and stabilizing moment is provided for fuselage.
The radio signal of the electronic decoy transmitting is guinea pig target signature signal.
The temperature of the wake flame is the infrared signature temperature of simulation aircraft engine.
A kind of decoy method of radar and infrared acquisition, step is：
Bait machine is penetrated by carrier aircraft carrying sky to fly to setting position, is delivered sky and is penetrated bait machine；
Sky penetrates bait machine and starts engine after dispensing, and engine driving sky penetrates bait machine flight forward；
The high-temperature plume that engine is produced is infrared decoy, simulates the infrared signature temperature of aircraft engine；
Sky penetrates bait machine and starts electronic decoy after dispensing, launches radio signal, guinea pig target signature signal.
The flight of bait machine is penetrated when carrier aircraft carries sky, when running into radar or infrared acquisition threat, sky is delivered and penetrates bait machine, it is right
Radar or infrared acquisition carry out trick interference.Sky penetrates bait machine with energy source device, installed in fuselage interior, can be touched by fuse
Hair, electric energy is provided for electronic decoy.The decoy method that sky penetrates bait machine includes radar decoy and infrared trick.
It is an advantage of the invention that：Dynamic radar and infrared spoofed signal, and the wavelength of infrared spoofed signal can be produced
It is similar to actual airplane infrared signature, have to existing radar and infrared acquisition and preferably inveigle effect.
The principle of the invention is simple, and realizability is strong.It is appropriate for promoting the use of.
Brief description of the drawings
Fig. 1 is the empty example schematic for penetrating bait machine
Fig. 2 is that sky penetrates bait machine and radar decoy, infrared trick, the relation schematic diagram of wake flame.
Embodiment
With reference to an example of the present invention and accompanying drawing, the present invention is further described.
Referring to Fig. 1, Fig. 2, it is fuselage 1, the machine of 2 sweepback by 1 body of revolution shape that sky of the present invention, which penetrates bait machine,
The wing 2,3 be located at the afterbody of fuselage 1 Y-shaped distribution empennage 3,1 loaded on the afterbody of fuselage 1 engine 4,1 be loaded on fuselage 1 before
The compositions such as the electronic decoy 5 in portion, 1 energy source device 6 loaded on the middle part of fuselage 1.
Sky is penetrated after bait machine is launched, and the lift that wing 2 is produced and the empty gravitational equilibrium for penetrating bait machine maintain sky to penetrate bait
Machine is flat to fly；The upper counterangle of wing 2 penetrates bait machine for sky for 15o and provides enough roll stabilities, and empennage 3 is penetrated bait machine for sky and carried
For enough shipping-direction stability and pitching stability；The thrust that engine 4 is produced overcomes the empty aerodynamic drag for penetrating bait machine, and sky is penetrated
Bait machine, which maintains to put down forward, to fly.
Sky is penetrated after bait machine is launched, and electronic decoy 5 starts, and electronic decoy 5, can mould to the default electronic signal of external radiation
Intend corresponding mockup target signature；The temperature of wake flame 9 is controlled, the infrared signature of corresponding aircraft engine can be simulated；Electronics is lured
There is no mutually exclusive property between bait 5 and wake flame 9, therefore can ensure that radar decoy 7 has feature simultaneously with infrared trick 8.
Claims (6)
1. a kind of sky penetrates bait machine, including fuselage（1）, wing（2）, empennage（3）, engine and electronic decoy（5）, its feature exists
In wing（2）, positioned at fuselage（1）Middle part, lift is provided when penetrating bait machine flight for sky；Empennage（3）, it is fixed on fuselage（1）Tail
Portion；Electronic decoy（5）, installed in fuselage（1）Inside, launches radio signal after the power-up；Engine is arranged on fuselage（1）Tail
Portion；Wing（2）With the upper counterangle, upper counterangle scope is 0o~15o.
2. according to claim（1）A kind of described sky penetrates bait machine, it is characterised in that the engine is rocket engine
（4）, rocket engine（4）The high-temperature plume of generation（9）For infrared decoy.
3. according to claim（1）A kind of described sky penetrates bait machine, it is characterised in that the empennage（3）In fuselage（1）On be in
V-type, X-type or Y-type layout, are fuselage（1）Stabilizing moment is provided.
4. a kind of sky according to claim 1 penetrates bait machine, it is characterised in that the electronic decoy（5）That launches is wireless
Electric signal is guinea pig target signature signal.
5. a kind of sky according to claim 2 penetrates bait machine, it is characterised in that the wake flame（9）Temperature for simulation fly
The infrared signature temperature of machine engine.
6. the decoy method of a kind of radar and infrared acquisition, it is characterised in that step is：
Bait machine is penetrated by carrier aircraft carrying sky to fly to setting position, is delivered sky and is penetrated bait machine；
Sky penetrates bait machine and starts engine after dispensing, and engine driving sky penetrates bait machine flight forward；
The high-temperature plume that engine is produced（9）For infrared decoy, the infrared signature temperature of aircraft engine is simulated；
Sky penetrates bait machine and starts electronic decoy after dispensing（5）, launch radio signal, guinea pig target signature signal.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201710156435.9A CN107054647A (en) | 2017-03-16 | 2017-03-16 | A kind of sky penetrates bait machine |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201710156435.9A CN107054647A (en) | 2017-03-16 | 2017-03-16 | A kind of sky penetrates bait machine |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN107054647A true CN107054647A (en) | 2017-08-18 |
Family
ID=59620950
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201710156435.9A Pending CN107054647A (en) | 2017-03-16 | 2017-03-16 | A kind of sky penetrates bait machine |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN107054647A (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN107554790A (en) * | 2017-08-31 | 2018-01-09 | 中国航空工业集团公司沈阳飞机设计研究所 | A kind of wind-force damping unit |
Citations (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN2706401Y (en) * | 2003-12-27 | 2005-06-29 | 陈绍勇 | Metal cloth aerated imitation aeroplane of antiradar infrared proof guidance missile |
| CN1634748A (en) * | 2003-12-27 | 2005-07-06 | 陈绍勇 | Radar preventing and infrared preventing bomb type inflated simulated airplane for protecting airplane |
| CN200967562Y (en) * | 2006-11-20 | 2007-10-31 | 大连三科航空科技有限公司 | High subsonic speed unmanned plane |
| CN204184576U (en) * | 2014-10-16 | 2015-03-04 | 刘得华 | Emulation military secret bait bullet system |
| 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 |
| CN104875885A (en) * | 2015-06-17 | 2015-09-02 | 沈阳飞机工业（集团）有限公司 | Composite aircraft |
-
2017
- 2017-03-16 CN CN201710156435.9A patent/CN107054647A/en active Pending
Patent Citations (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN2706401Y (en) * | 2003-12-27 | 2005-06-29 | 陈绍勇 | Metal cloth aerated imitation aeroplane of antiradar infrared proof guidance missile |
| CN1634748A (en) * | 2003-12-27 | 2005-07-06 | 陈绍勇 | Radar preventing and infrared preventing bomb type inflated simulated airplane for protecting airplane |
| CN200967562Y (en) * | 2006-11-20 | 2007-10-31 | 大连三科航空科技有限公司 | High subsonic speed unmanned plane |
| CN204184576U (en) * | 2014-10-16 | 2015-03-04 | 刘得华 | Emulation military secret bait bullet system |
| 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 |
| CN104875885A (en) * | 2015-06-17 | 2015-09-02 | 沈阳飞机工业（集团）有限公司 | Composite aircraft |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN107554790A (en) * | 2017-08-31 | 2018-01-09 | 中国航空工业集团公司沈阳飞机设计研究所 | A kind of wind-force damping unit |
| CN107554790B (en) * | 2017-08-31 | 2020-04-21 | 中国航空工业集团公司沈阳飞机设计研究所 | Wind power damping device applied to aviation towing system |
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| Date | Code | Title | Description |
|---|---|---|---|
| PB01 | Publication | ||
| PB01 | Publication | ||
| SE01 | Entry into force of request for substantive examination | ||
| SE01 | Entry into force of request for substantive examination | ||
| WD01 | Invention patent application deemed withdrawn after publication | ||
| WD01 | Invention patent application deemed withdrawn after publication |
Application publication date: 20170818 |