CN102167161A - Three-dimensional flying aircraft - Google Patents
Three-dimensional flying aircraft Download PDFInfo
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- CN102167161A CN102167161A CN2010105600475A CN201010560047A CN102167161A CN 102167161 A CN102167161 A CN 102167161A CN 2010105600475 A CN2010105600475 A CN 2010105600475A CN 201010560047 A CN201010560047 A CN 201010560047A CN 102167161 A CN102167161 A CN 102167161A
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- aircraft
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Abstract
The invention provides a three-dimensional flying aircraft which is characterized in that engines with rotatable tails are mounted under an aircraft tail and two wings respectively, wherein the three-dimensional flying aircraft can vertically take off and land, ensure an aircraft head against an enemy not to change when avoiding missiles in the high-speed flying process, and rapidly go up and down or drift left and right to fly in a three-dimensional manner, so as to prevent a large area from being exposed to the front enemy during the rapid going-up/down process, and meanwhile master the opportunities of attacks to the enemy when avoiding missiles. The three-dimensional flying aircraft provided by the invention comprises a high intelligence information system, the engines with the rotatable tails, a universal missile firing system, general missiles, general shells, network missiles and other aircraft systems.
Description
One, field under the present invention:
The present invention is a kind of three-dimensional flight flying machine.
Two, background technology:
At present, all aircrafts all are linear aircraft, the F-35 of the U.S. also can only be when landing vertical takeoff and landing, the same with other aircrafts when in high-speed flight, hiding guided missile, when altitude dash and decline, large-area top and belly are exposed to the place ahead enemy unavoidably, its hidden function just is forced to reduce before attack, also can lose the inning that the enemy is attacked simultaneously.
Three, content of the present invention:
The present invention can solve above technology and use defective.Three-dimensional flight flying machine of the present invention installs a rotatable engine of afterbody respectively under tail and both wings, can vertical takeoff and landing, in the time of can also in high-speed flight, hiding guided missile, it is constant to enemy's posture to remain the body head, but can raise rapidly and sink, or left and right sides drift, carry out solid flight, avoid when altitude dash and decline, large tracts of land being exposed to the place ahead enemy, when hiding, control the opportunity that the enemy is attacked.
Three-dimensional flight flying machine machine of the present invention is made of high intelligent information system, the rotatable engine of afterbody, universal missile release system, conventional missile, conventional artillery, network guided missile and other aircraft systems.As shown in drawings.
1, high intelligent information system is made of computer system, remote sensing forewarn system, position fixing system.
2, aircraft can allow the rotatable engine mouth of afterbody engine afterbody make tail to the liter of appearing on the stage downwards awing, and wing adjustment simultaneously makes the synchronous platform liter of forebody, and the both wings engine continues to push ahead, and can make the constant attitude of aircraft, the middle machine body horizontal stand liter that advances; Or the oblique forward below of both wings engine afterbody mouth, halting, standard of fuselage platform liter is exposed to the place ahead enemy's defective with large tracts of land when avoiding linear flight.
3, afterbody engine mouth upwards makes tail to sinking in-flight, left and right sides both wings engine afterbody mouth also turns to left respectively and tiltedly goes up, right tiltedly on, forebody is sunk, engine stops then, the wing adjustment is slowed down aircraft, complete machine keeps head that the enemy is sunk.
4, left engine afterbody and afterbody engine afterbody simultaneously left, right engine speed governing can make aircraft drift to the right, on the contrary then drift left.
5, when enemy's guided missile was close, the transmit network guided missile set a net to catch enemy missile, and engine stops, reduce flying speed, allow aircraft sink, make enemy missile lose infrared ray and follow the trail of the objective, make the aircraft of oneself avoid being caught again, still keep simultaneously the attitude of launching an attack the enemy by the network guided missile of oneself.
6, need the anxious stopping time can be with engine afterbody mouth to oblique front lower place, then gradually downwards, make the aircraft weak point from anxious hover in the air.
7, needing original place rotation can one of them engine afterbody to adjust direction and speed, to make aircraft be axle with a bit, and two engines rotate caudal directions and build up speed in addition, and making the aircraft original place serves as spool to rotate rapidly with fuselage center or set point.
8, the enemy from about up and down near or when attacking from behind, availablely be positioned at fuselage universal missile release system up and down to the left and right up and down or front and back transmit network guided missile, conventional artillery and guided missile, catch enemy's shell, guided missile and aircraft; Or smash its aircraft.
9, arrive enemy's terrain object is attacked the position, can keep the fuselage attitude of needs, ground and aerial target are dropped a bomb and launch precision guidance missile with universal missile release system.
Four, description of drawings:
Accompanying drawing is the constructional drawing of three-dimensional flying machine.
Claims (9)
1. three-dimensional flight flying machine.
2. three-dimensional flight flying machine installs a rotatable engine of afterbody respectively under tail and both wings, can vertical takeoff and landing, in the time of can also in high-speed flight, hiding guided missile, it is constant to enemy's posture to remain the body head, but can raise rapidly and sink, or left and right sides drift, carry out solid flight, avoid when altitude dash and decline, large tracts of land being exposed to the place ahead enemy, when hiding, control the opportunity that the enemy is attacked;
Three-dimensional flight flying machine is made of high intelligent information system, the rotatable engine of afterbody, universal missile release system, conventional missile, conventional artillery, network guided missile and other aircraft systems.
3. high intelligent information system is made of computer system, remote sensing forewarn system, position fixing system.
4. aircraft can allow the rotatable engine mouth of afterbody engine afterbody make tail to the liter of appearing on the stage downwards awing, and wing adjustment simultaneously makes the synchronous platform liter of forebody, and the both wings engine continues to push ahead, and can make the constant attitude of aircraft, the middle machine body horizontal stand liter that advances; Or the oblique forward below of both wings engine afterbody mouth, halting, standard of fuselage platform liter is exposed to the place ahead enemy's defective with large tracts of land when avoiding linear flight.
Afterbody engine mouth upwards makes tail to sinking in-flight, left and right sides both wings engine afterbody mouth also turns to left respectively and tiltedly goes up, right tiltedly on, forebody is sunk, engine stops then, the wing adjustment is slowed down aircraft, complete machine keeps head that the enemy is sunk;
Left side engine afterbody and afterbody engine afterbody while, right engine speed governing can make aircraft drift to the right left, on the contrary then drift left;
5. when enemy's guided missile was close, the transmit network guided missile set a net to catch enemy missile, and engine stops, reduce flying speed, allow aircraft sink, make enemy missile lose infrared ray and follow the trail of the objective, make the aircraft of oneself avoid being caught again, still keep simultaneously the attitude of launching an attack the enemy by the network guided missile of oneself.
6. need the anxious stopping time can be with engine afterbody mouth to oblique front lower place, then gradually downwards, make the aircraft weak point from anxious hover in the air.
7. needing original place rotation can one of them engine afterbody to adjust direction and speed, to make aircraft be axle with a bit, and two engines rotate caudal directions and build up speed in addition, and making the aircraft original place serves as spool to rotate rapidly with fuselage center or set point.
The enemy from about up and down near or when attacking from behind, availablely be positioned at fuselage universal missile release system up and down to the left and right up and down or front and back transmit network guided missile, conventional artillery and guided missile, catch enemy's shell, guided missile and aircraft; Or smash its aircraft.
9. arrive enemy's terrain object is attacked the position, can keep the fuselage attitude of needs, ground and aerial target are dropped a bomb and launch precision guidance missile with universal missile release system.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN2010105600475A CN102167161A (en) | 2010-11-26 | 2010-11-26 | Three-dimensional flying aircraft |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN2010105600475A CN102167161A (en) | 2010-11-26 | 2010-11-26 | Three-dimensional flying aircraft |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN102167161A true CN102167161A (en) | 2011-08-31 |
Family
ID=44488529
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN2010105600475A Pending CN102167161A (en) | 2010-11-26 | 2010-11-26 | Three-dimensional flying aircraft |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN102167161A (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN107943075A (en) * | 2017-11-22 | 2018-04-20 | 何振平 | It is a kind of that the method that yawing breaks away from attack is penetrated using big gun |
| CN108089594A (en) * | 2017-12-13 | 2018-05-29 | 王俊梅 | A kind of unmanned plane visual dead angles turn to escape flight method |
-
2010
- 2010-11-26 CN CN2010105600475A patent/CN102167161A/en active Pending
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN107943075A (en) * | 2017-11-22 | 2018-04-20 | 何振平 | It is a kind of that the method that yawing breaks away from attack is penetrated using big gun |
| CN108089594A (en) * | 2017-12-13 | 2018-05-29 | 王俊梅 | A kind of unmanned plane visual dead angles turn to escape flight method |
| CN108089594B (en) * | 2017-12-13 | 2020-11-27 | 王俊梅 | Unmanned aerial vehicle sight dead angle steering escape flight method |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C06 | Publication | ||
| PB01 | Publication | ||
| C02 | Deemed withdrawal of patent application after publication (patent law 2001) | ||
| WD01 | Invention patent application deemed withdrawn after publication |
Application publication date: 20110831 |