CN112027050A - Novel invisible fighter - Google Patents
Novel invisible fighter Download PDFInfo
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- CN112027050A CN112027050A CN202010935753.7A CN202010935753A CN112027050A CN 112027050 A CN112027050 A CN 112027050A CN 202010935753 A CN202010935753 A CN 202010935753A CN 112027050 A CN112027050 A CN 112027050A
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- 239000011248 coating agent Substances 0.000 claims abstract description 22
- 238000000576 coating method Methods 0.000 claims abstract description 22
- 210000001015 abdomen Anatomy 0.000 claims description 28
- 241000272525 Anas platyrhynchos Species 0.000 claims description 7
- 238000010586 diagram Methods 0.000 description 7
- 230000000694 effects Effects 0.000 description 6
- 238000001514 detection method Methods 0.000 description 3
- 238000012986 modification Methods 0.000 description 3
- 230000004048 modification Effects 0.000 description 3
- 238000012827 research and development Methods 0.000 description 2
- 230000009286 beneficial effect Effects 0.000 description 1
- 230000007547 defect Effects 0.000 description 1
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C1/00—Fuselages; Constructional features common to fuselages, wings, stabilising surfaces or the like
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C3/00—Wings
- B64C3/28—Leading or trailing edges attached to primary structures, e.g. forming fixed slots
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- 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
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C5/00—Stabilising surfaces
- B64C5/06—Fins
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- 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
- B64D33/00—Arrangements in aircraft of power plant parts or auxiliaries not otherwise provided for
- B64D33/02—Arrangements in aircraft of power plant parts or auxiliaries not otherwise provided for of combustion air intakes
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- 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
- B64D33/00—Arrangements in aircraft of power plant parts or auxiliaries not otherwise provided for
- B64D33/04—Arrangements in aircraft of power plant parts or auxiliaries not otherwise provided for of exhaust outlets or jet pipes
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- 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
- B64D43/00—Arrangements or adaptations of instruments
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U20/00—Constructional aspects of UAVs
- B64U20/10—Constructional aspects of UAVs for stealth, e.g. reduction of cross-section detectable by radars
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- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Mechanical Engineering (AREA)
- Remote Sensing (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Radar, Positioning & Navigation (AREA)
- Toys (AREA)
Abstract
The invention provides a novel invisible fighter, which belongs to the technical field of military equipment and comprises a fighter body, wherein the fighter body is provided with a invisible coating, an air inlet, a tail nozzle and a cockpit; the design of the invention has the advantages of stealth, supersonic cruise, high voyage and super maneuver; the front two and the back one are laser or energy beam weapon systems, which provide the capabilities of bundling high energy attack take-off section ballistic missiles, beam splitting attack air-air missiles, ground-air missiles, unmanned planes and the like, the back one can resist the air combat capabilities of infrared air-air missiles, tail chasing and the like during short-distance attack, and the front two can attack targets during attack chasing.
Description
Technical Field
The invention relates to the technical field of military equipment, in particular to a novel invisible fighter.
Background
The existing invisible fighter is poor in comprehensive combat capability and performance.
Disclosure of Invention
Aiming at the technical defects, the invention aims to provide a novel invisible fighter, which has the advantages of invisibility, supersonic cruise, high range and super maneuverability. The first to third aircrafts and the second and forth laser or energy beam weapon systems provide the capabilities of bundling high-energy attack take-off section ballistic missiles, beam-splitting attack air-air missiles, ground-air missiles, unmanned planes and the like, the first aircraft can resist the air combat capabilities of infrared air-air missiles, tail chasing and the like when the aircraft is in close range, and the second aircraft can attack targets when the aircraft is in attack chasing; the engine of upper and lower staggered arrangement can have multiple engine to arrange the combination and be used for different usage states, but single-shot cruise, two-shot super patrol, super motor-driven, reduce the novel engine of research and development to the restriction, reduced the restriction to the engine model, increased the journey.
In order to solve the technical problems, the invention adopts the following technical scheme:
a novel invisible fighter comprises a fighter body, wherein the fighter body is provided with a invisible coating, an air inlet, a tail nozzle and a cockpit, and is characterized in that the fighter body is provided with a double engine, a sawtooth guide plate, an inward-inclined vertical tail, a front edge maneuvering wing front fly, a rear edge maneuvering wing front fly and a high maneuvering front duck wing; the middle part of the air inlet is embedded in the fighter body in the front; the tail nozzle is invisible and can deflect; the cockpit is in a middle-mounted upper horizontal type; the warplane body is smooth in belly and designed as an integral buoyancy body; the fighter plane body is provided with a forward-exploring weapon unit, and the tail part of the fighter plane body is provided with a single laser energy beam cannon; the body of the fighter plane body is provided with a distributed radar and sensor, and the comprehensive information system in the cockpit can penetrate through the display helmet.
A novel invisible fighter comprises a fighter body, wherein the fighter body is provided with a invisible coating, an air inlet, a tail nozzle and a cockpit, and is characterized in that the fighter body is provided with a double engine, a sawtooth guide plate, a large-angle outward-tilting vertical tail, a front edge moving wing front fly, a rear edge moving wing front fly and a large sweepback angle full-fuselage main wing; the middle part of the air inlet is embedded in the fighter body in the front; the tail nozzle is invisible and can deflect; the cockpit is in a middle-mounted upper horizontal type; the warplane body is smooth in belly and designed as an integral buoyancy body; the fighter plane body is provided with a forward-exploring weapon unit, and the tail part of the fighter plane body is provided with a single laser energy beam cannon; the body of the fighter plane body is provided with a distributed radar and sensor, and the comprehensive information system in the cockpit can penetrate through the display helmet.
A novel invisible fighter comprises a fighter body, wherein the fighter body is provided with a invisible coating, an air inlet, a tail nozzle and a cockpit, and is characterized in that the fighter body is provided with a double engine, a sawtooth guide plate, an inward-inclined vertical tail, a front edge maneuvering wing front fly, a rear edge maneuvering wing front fly and a high maneuvering tail wing; the middle part of the air inlet is embedded in the fighter body in the front; the tail nozzle is invisible and can deflect; the cockpit is in a middle-mounted upper horizontal type; the warplane body is smooth in belly and designed as an integral buoyancy body; the fighter plane body is provided with a forward-exploring weapon unit, and the tail part of the fighter plane body is provided with a single laser energy beam cannon; the body of the fighter plane body is provided with a distributed radar and sensor, and the comprehensive information system in the cockpit can penetrate through the display helmet.
A novel invisible fighter comprises a fighter body, wherein the fighter body is provided with a invisible coating, an air inlet, a tail nozzle and a cockpit, and is characterized in that the fighter body is provided with a double engine, a sawtooth guide plate, an inward-inclined vertical tail, a front edge maneuvering wing front, a rear edge maneuvering wing front, an integral fuselage main wing and an forward-inclined guide opening; the middle part of the air inlet is embedded in the fighter body in the front; the tail nozzle is invisible and can deflect; the cockpit is in a middle-mounted upper horizontal type; the warplane body is smooth in belly and designed as an integral buoyancy body; the body of the fighter plane body is provided with a distributed radar and sensor, and the comprehensive information system in the cockpit can penetrate through the display helmet.
A novel invisible fighter comprises a fighter body, wherein the fighter body is provided with a invisible coating, an air inlet, a tail nozzle and a cockpit, and is characterized in that the fighter body is provided with a double engine, a sawtooth guide plate, an inward-inclined vertical tail, a front edge maneuvering wing front, a rear edge maneuvering wing front, an integral fuselage main wing, a high maneuvering front duck wing and an invisible inclination angle; the stealth dip angle is half buried between the inward-inclining vertical tails; the middle part of the air inlet is arranged on the fighter body; the tail nozzle is invisible and can deflect; the cockpit is in a middle-mounted upper horizontal type; the warplane body is smooth in belly and designed as an integral buoyancy body; the body of the fighter plane body is provided with a distributed radar and sensor, and the comprehensive information system in the cockpit can penetrate through the display helmet.
A novel invisible fighter comprises a fighter body, wherein the fighter body is provided with a invisible coating, an air inlet, a tail nozzle and a cockpit; the stealth dip angle is fully buried between the inward-inclined vertical tails; the tail nozzles are vertically arranged and staggered from front to back; the middle part of the air inlet is arranged on the fighter body; the tail nozzle is invisible and can deflect; the cockpit is buried in the rear part; the warplane body is smooth in belly and designed as an integral buoyancy body; the body of the fighter plane body is provided with a distributed radar and sensor, and the comprehensive information system in the cockpit can penetrate through the display helmet.
A novel invisible fighter comprises a fighter body, wherein the fighter body is provided with a invisible coating, an air inlet, a tail nozzle and a cockpit; the stealth dip angle is fully buried between the inward-inclined vertical tails; the tail spout is vertically arranged; the middle part of the air inlet is buried on the fighter body; the tail nozzle is invisible and can deflect; the warplane body is smooth in belly and designed as an integral buoyancy body; the body of the fighter plane body is provided with a distributed radar and sensor, and the comprehensive information system in the cockpit can penetrate through the display helmet.
Preferably, the weapon unit is any one of a double laser gun or an energy beam gun.
The invention has the beneficial effects that: the design of the invention has the advantages of stealth, supersonic cruise, high range and super maneuver. The first to third aircrafts and the second and forth laser or energy beam weapon systems provide the capabilities of bundling high-energy attack take-off section ballistic missiles, beam-splitting attack air-air missiles, ground-air missiles, unmanned planes and the like, the first aircraft can resist the air combat capabilities of infrared air-air missiles, tail chasing and the like when the aircraft is in close range, and the second aircraft can attack targets when the aircraft is in attack chasing; the engines are arranged in a vertically staggered manner, so that various engines can be arranged and combined to be used in different use states, single-engine cruising, double-engine super cruising and super-maneuvering are realized, restriction on the research and development of novel engines is reduced, restriction on the models of the engines is reduced, and the voyage is increased.
Drawings
In order to more clearly illustrate the embodiments of the present invention or the technical solutions in the prior art, the drawings used in the description of the embodiments or the prior art will be briefly described below, it is obvious that the drawings in the following description are only some embodiments of the present invention, and for those skilled in the art, other drawings can be obtained according to the drawings without creative efforts.
Fig. 1 is a schematic structural diagram of a novel invisible fighter according to embodiment 1 of the invention;
fig. 2 is a schematic structural diagram of a novel invisible fighter according to embodiment 2 of the invention;
fig. 3 is a schematic structural diagram of a novel invisible fighter according to embodiment 3 of the invention;
fig. 4 is a schematic structural diagram of a novel invisible fighter according to embodiment 4 of the invention;
fig. 5 is a schematic structural diagram of a novel invisible fighter according to embodiment 5 of the invention;
fig. 6 is a schematic structural diagram of a novel invisible fighter according to embodiment 6 of the invention;
fig. 7 is a schematic structural diagram of a novel invisible fighter according to embodiment 7 of the invention.
Description of reference numerals:
the front edge engine moving wing fly 1, the rear edge engine moving wing fly 2, the inward-inclined vertical tail 3, the tail nozzle 4, the cockpit 5, the air inlet 6, the forward-exploring weapon unit 7, the high-maneuvering front duck wing 8, the large-angle outward-inclined vertical tail 9, the large-sweepback-angle full-fuselage main wing 10, the high-maneuvering tail wing 11, the forward-inclined diversion port 12 and the whole fuselage main wing 13.
Detailed Description
The technical solutions in the embodiments of the present invention will be clearly and completely described below with reference to the drawings in the embodiments of the present invention, and it is obvious that the described embodiments are only a part of the embodiments of the present invention, and not all of the embodiments. All other embodiments, which can be derived by a person skilled in the art from the embodiments given herein without making any creative effort, shall fall within the protection scope of the present invention.
It should be noted that in the description of the present invention, the terms "in", "upper", "lower", "lateral", "inner", etc. indicate directions or positional relationships based on those shown in the drawings, which are merely for convenience of description, and do not indicate or imply that the device or element must have a specific orientation, be constructed and operated in a specific orientation, and thus, should not be construed as limiting the present invention.
Furthermore, it should be noted that, in the description of the present invention, unless otherwise explicitly specified or limited, the terms "disposed," "mounted," "connected," and "connected" are to be construed broadly and may be, for example, fixedly connected, detachably connected, or integrally connected; may be a mechanical connection; they may be connected directly or indirectly through intervening media, or they may be interconnected between two elements. The specific meanings of the above terms in the present invention can be understood by those skilled in the art according to specific situations.
Example 1
As shown in fig. 1, a novel invisible fighter comprises a fighter body, wherein the fighter body is provided with a invisible coating, an air inlet 6, a tail nozzle 4 and a cockpit 5, and the fighter body is provided with a double engine, a sawtooth guide plate, an inward-inclined vertical tail 3, a front edge dynamic wing fly 1, a rear edge dynamic wing fly 2 and a high dynamic front duck wing 8; the vertical fin is inclined inwards and hidden; the parcel type stealth has good effect of avoiding radar; the middle part of the air inlet 6 is embedded in the fighter body; the tail nozzle 4 is invisible and can deflect, so that the invisibility and the maneuverability are improved; the cockpit 5 is in a middle-mounted horizontal type, and the scanning shielding angle of the ground radar is good at each angle; the fighter plane body has smooth belly, integral buoyancy body design, large width and length of internal storage space, large oil-carrying and bullet-carrying capacity, high flexibility and strong adaptability; the fighter body is provided with a forward-detection double-laser or energy beam cannon, and the tail part of the fighter body is provided with a single-laser energy beam cannon; the belly has large length and width and can accommodate weapons and equipment with various dimensions. The body of the fighter plane body is provided with a distributed radar and sensor, and the cockpit of the cockpit 5 is provided with a comprehensive information system which can penetrate through the display helmet.
Example 2
As shown in fig. 2, a novel invisible fighter comprises a fighter body, wherein the fighter body is provided with a invisible coating, an air inlet 6, a tail nozzle 4 and a cockpit 5, and the fighter body is provided with a double engine, a sawtooth guide plate, a large-angle outward-inclined vertical tail 9, a hidden front-edge moving wing fly 1, a rear-edge moving wing fly 2 and a large-sweepback-angle full-fuselage main wing 10; the vertical fin is inclined inwards and hidden; the parcel type stealth has good effect of avoiding radar; the middle part of the air inlet 6 is embedded in the fighter body; the tail nozzle 4 is invisible and can deflect, so that the invisibility and the maneuverability are improved; the cockpit 5 is in a middle-mounted horizontal type, and the scanning shielding angle of the ground radar is good at each angle; the fighter plane body has smooth belly, integral buoyancy body design, large width and length of internal storage space, large oil-carrying and bullet-carrying capacity, high flexibility and strong adaptability; the fighter body is provided with a forward-detection double-laser or energy beam cannon, and the tail part of the fighter body is provided with a single-laser energy beam cannon; the belly has large length and width and can accommodate weapons and equipment with various dimensions. The body of the fighter plane body is provided with a distributed radar and sensor, and the cockpit of the cockpit 5 is provided with a comprehensive information system which can penetrate through the display helmet.
Example 3
As shown in fig. 3, a novel invisible fighter comprises a fighter body, wherein the fighter body is provided with a invisible coating, an air inlet 6, a tail nozzle 4 and a cockpit 5, and the fighter body is provided with a double engine, a sawtooth guide plate, an inward-inclined vertical tail 3, a front edge maneuvering wing fly 1, a rear edge maneuvering wing fly 2 and a high maneuvering tail 11; the parcel type stealth has good effect of avoiding radar; the middle part of the air inlet 6 is embedded in the fighter body; the tail nozzle 4 is invisible and can deflect, so that the invisibility and the maneuverability are improved; the cockpit 5 is in a middle-mounted horizontal type, and the scanning shielding angle of the ground radar is good at each angle; the fighter plane body has smooth belly, integral buoyancy body design, large width and length of internal storage space, large oil-carrying and bullet-carrying capacity, high flexibility and strong adaptability; the fighter body is provided with a forward-detection double-laser or energy beam cannon, and the tail part of the fighter body is provided with a single-laser energy beam cannon; the belly has large length and width and can accommodate weapons and equipment with various dimensions. The body of the fighter plane body is provided with a distributed radar and sensor, and the cockpit of the cockpit 5 is provided with a comprehensive information system which can penetrate through the display helmet.
Example 4
As shown in fig. 4, a novel invisible fighter comprises a fighter body, wherein the fighter body is provided with a invisible coating, an air inlet 6, a tail nozzle 4 and a cockpit 5, and the fighter body is provided with a double engine, a sawtooth guide plate, an inward-inclined vertical tail 3, a front edge dynamic wing fly 1, a rear edge dynamic wing fly 2, an integral fuselage main wing 13 and a forward-inclined guide opening 12; the parcel type stealth has good effect of avoiding radar; the middle part of the air inlet 6 is embedded in the fighter body; the tail nozzle 4 is invisible and can deflect, so that the invisibility and the maneuverability are improved; the cockpit 5 is in a middle-mounted horizontal type, and the scanning shielding angle of the ground radar is good at each angle; the fighter plane body has smooth belly, integral buoyancy body design, large width and length of internal storage space, large oil-carrying and bullet-carrying capacity, high flexibility and strong adaptability; the belly has large length and width and can accommodate weapons and equipment with various dimensions. The body of the fighter plane body is provided with a distributed radar and sensor, and the cockpit of the cockpit 5 is provided with a comprehensive information system which can penetrate through the display helmet.
Example 5
As shown in fig. 5, a novel invisible fighter comprises a fighter body, wherein the fighter body is provided with a invisible coating, an air inlet 6, a tail nozzle 4 and a cockpit 5, and the fighter body is provided with a double engine, a sawtooth guide plate, an inward-inclined vertical tail 3, a front edge dynamic wing fly 1, a rear edge dynamic wing fly 2, an integral fuselage main wing 13, a high maneuvering front duck wing 8 and an invisible inclination angle; the parcel type stealth has good effect of avoiding radar; the stealth dip angle is half buried between the inward-inclining vertical tails 3; the middle part of the air inlet 6 is arranged on the fighter body; the tail nozzle 4 is invisible and can deflect, so that the invisibility and the maneuverability are improved; the cockpit 5 is in a middle-mounted horizontal type, and the scanning shielding angle of the ground radar is good at each angle; the fighter plane body has smooth belly, integral buoyancy body design, large width and length of internal storage space, large oil-carrying and bullet-carrying capacity, high flexibility and strong adaptability; the belly has large length and width and can accommodate weapons and equipment with various dimensions. The body of the fighter plane body is provided with a distributed radar and sensor, and the cockpit of the cockpit 5 is provided with a comprehensive information system which can penetrate through the display helmet.
Example 6
As shown in fig. 6, a novel invisible fighter comprises a fighter body, wherein the fighter body is provided with a invisible coating, an air inlet 6, a tail nozzle 4 and a cockpit 5, and the fighter body is provided with a double engine, a invisible inclination angle and an inward-inclined vertical tail 3; the parcel type stealth has good effect of avoiding radar; the stealth dip angle is fully buried between the inward-inclining vertical tails 3; the tail nozzles 4 are vertically arranged and staggered from front to back; the middle part of the air inlet 6 is arranged on the fighter body; the tail nozzle 4 is invisible and can deflect, so that the invisibility and the maneuverability are improved; the cockpit 5 is buried in the rear part, and the scanning and shielding angles of the ground radar at all angles are good; the fighter plane body has smooth belly, integral buoyancy body design, large width and length of internal storage space, large oil-carrying and bullet-carrying capacity, high flexibility and strong adaptability; the belly has large length and width and can accommodate weapons and equipment with various dimensions. The body of the fighter plane body is provided with a distributed radar and sensor, and the cockpit of the cockpit 5 is provided with a comprehensive information system which can penetrate through the display helmet.
The vertical arrangement engine:
1. the engine can be arranged in different models, sizes and power engines, can be switched between single-engine and double-engine opening and closing, can be used for cruising and fighting, and can be flexibly applied to supersonic speed and subsonic speed. And the range and supersonic cruise selection are improved.
2. The front engine and the rear engine which are staggered are opened and closed in a single-double-engine mode, different torques are formed by different powers, and super-power is provided.
Example 7
As shown in fig. 7, a novel invisible fighter comprises a fighter body, wherein the fighter body is provided with a invisible coating, an air inlet 6, a tail nozzle 4 and a cockpit 5, and the fighter body is provided with a double engine, a invisible inclination angle and an inward-inclined vertical tail 3; the stealth dip angle is fully buried between the inward-inclining vertical tails 3; the tail nozzle 4 is vertically arranged; the middle part of the air inlet 6 is buried on the fighter body; the tail nozzle 4 is invisible and can deflect; the belly of the fighter plane body is smooth, and the whole buoyancy body is designed; the belly has large length and width and can accommodate weapons and equipment with various dimensions. The body of the fighter plane body is provided with a distributed radar and sensor, and the cockpit of the cockpit 5 is provided with a comprehensive information system which can penetrate through the display helmet.
The vertical arrangement engine:
1. the engine can be arranged in different models, sizes and power engines, can be switched between single-engine and double-engine opening and closing, can be used for cruising and fighting, and can be flexibly applied to supersonic speed and subsonic speed. And the range and supersonic cruise selection are improved.
2. The single-engine and double-engine opening and closing are arranged up and down, different torques are formed by different powers, and super-power is provided.
The design of the invention has the advantages of stealth, supersonic cruise, high range and super maneuver.
It will be apparent to those skilled in the art that various changes and modifications may be made in the present invention without departing from the spirit and scope of the invention. Thus, if such modifications and variations of the present invention fall within the scope of the claims of the present invention and their equivalents, the present invention is also intended to include such modifications and variations.
Claims (8)
1. A novel invisible fighter comprises a fighter body, wherein the fighter body is provided with a invisible coating, an air inlet, a tail nozzle and a cockpit, and is characterized in that the fighter body is provided with a double engine, a sawtooth guide plate, an inward-inclined vertical tail, a front edge maneuvering wing front fly, a rear edge maneuvering wing front fly and a high maneuvering front duck wing; the middle part of the air inlet is embedded in the fighter body in the front; the tail nozzle is invisible and can deflect; the cockpit is in a middle-mounted upper horizontal type; the warplane body is smooth in belly and designed as an integral buoyancy body; the fighter plane body is provided with a forward-exploring weapon unit, and the tail part of the fighter plane body is provided with a single laser energy beam cannon; the body of the fighter plane body is provided with a distributed radar and sensor, and the comprehensive information system in the cockpit can penetrate through the display helmet.
2. A novel invisible fighter comprises a fighter body, wherein the fighter body is provided with a invisible coating, an air inlet, a tail nozzle and a cockpit, and is characterized in that the fighter body is provided with a double engine, a sawtooth guide plate, a large-angle outward-tilting vertical tail, a front edge moving wing front fly, a rear edge moving wing front fly and a large sweepback angle full-fuselage main wing; the middle part of the air inlet is embedded in the fighter body in the front; the tail nozzle is invisible and can deflect; the cockpit is in a middle-mounted upper horizontal type; the warplane body is smooth in belly and designed as an integral buoyancy body; the fighter plane body is provided with a forward-exploring weapon unit, and the tail part of the fighter plane body is provided with a single laser energy beam cannon; the body of the fighter plane body is provided with a distributed radar and sensor, and the comprehensive information system in the cockpit can penetrate through the display helmet.
3. A novel invisible fighter comprises a fighter body, wherein the fighter body is provided with a invisible coating, an air inlet, a tail nozzle and a cockpit, and is characterized in that the fighter body is provided with a double engine, a sawtooth guide plate, an inward-inclined vertical tail, a front edge maneuvering wing front fly, a rear edge maneuvering wing front fly and a high maneuvering tail wing; the middle part of the air inlet is embedded in the fighter body in the front; the tail nozzle is invisible and can deflect; the cockpit is in a middle-mounted upper horizontal type; the warplane body is smooth in belly and designed as an integral buoyancy body; the fighter plane body is provided with a forward-exploring weapon unit, and the tail part of the fighter plane body is provided with a single laser energy beam cannon; the body of the fighter plane body is provided with a distributed radar and sensor, and the comprehensive information system in the cockpit can penetrate through the display helmet.
4. A novel invisible fighter comprises a fighter body, wherein the fighter body is provided with a invisible coating, an air inlet, a tail nozzle and a cockpit, and is characterized in that the fighter body is provided with a double engine, a sawtooth guide plate, an inward-inclined vertical tail, a front edge maneuvering wing front, a rear edge maneuvering wing front, an integral fuselage main wing and an forward-inclined guide opening; the middle part of the air inlet is embedded in the fighter body in the front; the tail nozzle is invisible and can deflect; the cockpit is in a middle-mounted upper horizontal type; the warplane body is smooth in belly and designed as an integral buoyancy body; the body of the fighter plane body is provided with a distributed radar and sensor, and the comprehensive information system in the cockpit can penetrate through the display helmet.
5. A novel invisible fighter comprises a fighter body, wherein the fighter body is provided with a invisible coating, an air inlet, a tail nozzle and a cockpit, and is characterized in that the fighter body is provided with a double engine, a sawtooth guide plate, an inward-inclined vertical tail, a front edge maneuvering wing front, a rear edge maneuvering wing front, an integral fuselage main wing, a high maneuvering front duck wing and an invisible inclination angle; the stealth dip angle is half buried between the inward-inclining vertical tails; the middle part of the air inlet is arranged on the fighter body; the tail nozzle is invisible and can deflect; the cockpit is in a middle-mounted upper horizontal type; the warplane body is smooth in belly and designed as an integral buoyancy body; the body of the fighter plane body is provided with a distributed radar and sensor, and the comprehensive information system in the cockpit can penetrate through the display helmet.
6. A novel invisible fighter comprises a fighter body, wherein the fighter body is provided with a invisible coating, an air inlet, a tail nozzle and a cockpit; the stealth dip angle is fully buried between the inward-inclined vertical tails; the tail nozzles are vertically arranged and staggered from front to back; the middle part of the air inlet is arranged on the fighter body; the tail nozzle is invisible and can deflect; the cockpit is buried in the rear part; the warplane body is smooth in belly and designed as an integral buoyancy body; the body of the fighter plane body is provided with a distributed radar and sensor, and the comprehensive information system in the cockpit can penetrate through the display helmet.
7. A novel invisible fighter comprises a fighter body, wherein the fighter body is provided with a invisible coating, an air inlet, a tail nozzle and a cockpit; the stealth dip angle is fully buried between the inward-inclined vertical tails; the tail spout is vertically arranged; the middle part of the air inlet is buried on the fighter body; the tail nozzle is invisible and can deflect; the warplane body is smooth in belly and designed as an integral buoyancy body; the body of the fighter plane body is provided with a distributed radar and sensor, and the comprehensive information system in the cockpit can penetrate through the display helmet.
8. The stealth fighter machine of any one of claims 1-3, wherein the weapon unit is any one of a twin laser gun or an energy beam gun.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202010935753.7A CN112027050A (en) | 2020-09-08 | 2020-09-08 | Novel invisible fighter |
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| Application Number | Priority Date | Filing Date | Title |
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| CN202010935753.7A CN112027050A (en) | 2020-09-08 | 2020-09-08 | Novel invisible fighter |
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| CN112027050A true CN112027050A (en) | 2020-12-04 |
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| CN202010935753.7A Pending CN112027050A (en) | 2020-09-08 | 2020-09-08 | Novel invisible fighter |
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Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN113148105A (en) * | 2021-05-17 | 2021-07-23 | 西北工业大学 | Double-head wing body fusion low-detectable layout |
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2020
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| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN113148105A (en) * | 2021-05-17 | 2021-07-23 | 西北工业大学 | Double-head wing body fusion low-detectable layout |
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Application publication date: 20201204 |