CN211373368U - Target drone is put in to dexterous type interference bullet - Google Patents
Target drone is put in to dexterous type interference bullet Download PDFInfo
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- CN211373368U CN211373368U CN201922281488.0U CN201922281488U CN211373368U CN 211373368 U CN211373368 U CN 211373368U CN 201922281488 U CN201922281488 U CN 201922281488U CN 211373368 U CN211373368 U CN 211373368U
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Abstract
The utility model discloses a smart interference projectile throwing target drone, which comprises a target drone body, wherein the target drone body comprises a body, wings, empennages and a vertical tail, the body and the vertical tail are integrally connected, two sides of the body are detachably connected with the two wings, and one end of the body is detachably connected with the two empennages; the device also comprises an infrared interference bomb throwing device arranged in the machine body; the aircraft further comprises two traction light pipe fixing devices arranged on the two wings. The utility model discloses target drone can hide and load infrared foil strip interference bullet, and simple structure, light in weight, and the load is big, does not influence the flight performance of aircraft, and the mainly used army combat confrontation training improves army's operational capability, also can carry out the verification to the infrared performance of looking for of novel weaponry.
Description
Technical Field
The utility model belongs to the technical field of the target drone, especially, relate to a target drone is put in to dexterous type interference bomb.
Background
The infrared interference bomb is also called infrared decoy bomb or infrared glowing bomb, it is a kind of pyrotechnical decoy, its pyrotechnical is mostly made up by mixing magnesium powder, nitrocotton, polytetrafluoroethylene. The infrared guided weapon is generally used for luring enemy infrared guided weapons to be separated from real targets, has higher temperature, and is widely applied to self-defense of airplanes and ships. When a missile is discovered to attack, the infrared bait projectile can be projected into the air from an airplane or a ship, the pyrotechnic agent is ignited and quickly burns to form a false target, and the attacking missile completely abandons the target to track the infrared bait projectile, so that the aims of luring the enemy and improving the survival ability of the own are fulfilled.
At present, the number of the high-altitude unmanned drone aircraft is less, the number of the drone aircraft with the altitude of more than 8000km is less, the size of the existing unmanned drone aircraft is larger, the weight is larger, the task load is smaller, the structure for loading the infrared/foil strip interference bomb is complex, the weight is large, the outer surface of the airplane is protruded, and the flight performance of the airplane is influenced.
SUMMERY OF THE UTILITY MODEL
The utility model aims to overcome the not enough of above-mentioned prior art, provide a target drone is put in to dexterous type jamming bomb.
In order to solve the technical problem, the technical scheme of the utility model is that: a smart interference projectile throwing target drone comprises a target drone body, wherein the target drone body comprises a drone body, and an infrared interference projectile throwing device is arranged in the drone body; the infrared interference bomb throwing device comprises an upper supporting plate, a lower supporting plate, an infrared interference bomb, a fixing plate and a protective plate;
an aircraft separation frame is arranged in the fuselage, the upper supporting plate and the lower supporting plate are both vertically arranged on the aircraft separation frame, and the upper supporting plate and the lower supporting plate are parallel to each other;
one end of the infrared interference bomb penetrates through the lower supporting plate and is installed on the upper supporting plate, the middle of the infrared interference bomb is tightly pressed through a fixing plate installed on the lower supporting plate, the protection plate is connected with the fixing plate, and the protection plate is parallel to the aircraft bulkhead.
Preferably, the aircraft further comprises two wings, and the two wings are detachably arranged on two sides of the middle of the fuselage.
Preferably, the device also comprises two traction light pipe fixing devices respectively arranged on the two wings,
the flare fixing device comprises a flare, a hoop, a base, a first connecting plate, a second connecting plate and a fairing;
the towing pipe is arranged on the base through two hoops, and the base is arranged on the wing through a first connecting plate and a second connecting plate;
the fairing is sleeved outside the first connecting plate, the second connecting plate and the base.
Preferably, the airplane further comprises a vertical fin and two tail wings, wherein the two tail wings are detachably arranged on two sides of the tail end of the airplane body, and the vertical fin is integrally connected with the tail end of the airplane body.
Preferably, the wings and the vertical tails are both provided with night navigation indicating lamps.
Preferably, the bottom end of the machine body is provided with two air bag cavities at intervals along the longitudinal axis direction of the machine body, and the top end of the machine body is provided with an umbrella cavity and an airspeed head.
Preferably, a head cover is arranged at one end of the machine body far away from the vertical tail.
Preferably, one end of the infrared interference bomb is clamped on the upper supporting plate.
Compared with the prior art, the utility model has the advantages of:
(1) the infrared interference bomb is arranged in the target drone, the flight performance of the target drone is not influenced, the horizontal flight speed is as high as 180m/s, and the horizontal flight height can reach more than 9000 km;
(2) the body of the utility model is respectively connected with the wings and the empennage in a detachable way, which is convenient for packaging and transportation;
(3) the utility model adopts the design of double air bag cabins, which can reduce the damage of landing impact to the target drone to the utmost extent;
(4) the utility model discloses target drone is put in to dexterous type jamming bomb simple structure, workable, but greatly reduced processing cost, so light in weight because of target drone simple structure simultaneously, never brought big load capacity and better flight performance, can use in a large number in army's actual combat training.
Drawings
Fig. 1 is a schematic structural view of a smart interference projectile launching drone of the present invention;
fig. 2 is a schematic structural diagram of an infrared jamming bomb device in a smart jamming bomb throwing target drone of the present invention;
fig. 3 is a schematic view of an external structure of a collimator tube fixing device of a smart interfering projectile shooting target drone of the present invention;
fig. 4 is a schematic structural view of a traction tube fixing device of a smart interference projectile launching target drone, which is not provided with a fairing;
description of reference numerals:
1. the device comprises a nose cover, 2, an airspeed head, 3, an umbrella cabin, 4, an air bag cabin, 5 and a night navigation indicator light;
6. the device comprises a light dragging pipe fixing device, 6-01, a light dragging pipe, 6-02, a hoop, 6-03, a base, 6-04, a first connecting plate, 6-05, a second connecting plate, 6-06 and a fairing;
7. wing, 8, tail wing, 9, fuselage, 10, vertical fin;
11. the device comprises an infrared interference bomb throwing device 11-01, an upper supporting plate 11-02, a lower supporting plate 11-03, a fixing plate 11-04, a guard plate 11-05, an infrared interference bomb 11-06 and an airplane bulkhead.
Detailed Description
The following description of the embodiments of the present invention is provided in connection with the following embodiments:
it should be noted that the structures, ratios, sizes, etc. illustrated in the present specification are only used to cooperate with the contents disclosed in the specification for the understanding and reading of the people skilled in the art, and are not used to limit the limit conditions that the present invention can be implemented, and any modifications of the structures, changes of the ratio relationships or adjustments of the sizes should still fall within the scope that the technical contents disclosed in the present invention can cover without affecting the functions and the achievable purposes of the present invention.
Meanwhile, the terms such as "upper", "lower", "left", "right", "middle" and "one" used in the present specification are for convenience of description, and are not intended to limit the scope of the present invention, and changes or adjustments of the relative relationship thereof may be made without substantial technical changes, and the present invention is also regarded as the scope of the present invention.
As shown in fig. 1, a smart interfering bomb launching drone comprises a drone body, wherein the drone body comprises a drone body 9, and an infrared interfering bomb launching device 11 is installed inside the drone body 9. The infrared interference bomb throwing device 11 is completely arranged inside the machine body 9 and is hidden in the machine body 9. The infrared interference bomb throwing device 11 comprises an upper supporting plate 11-01, a lower supporting plate 11-02, an infrared interference bomb 11-05, a fixing plate 11-03 and a protection plate 11-04. The interior of the fuselage is provided with aircraft bulkheads 11-06. The upper supporting plate 11-01 and the lower supporting plate 11-02 are both vertically arranged on the aircraft bulkhead 11-06, and the upper supporting plate 11-01 and the lower supporting plate 11-02 are parallel to each other. One end of the infrared interference bomb 11-05 penetrates through the lower supporting plate 11-02 and is clamped on the upper supporting plate 11-01, the middle part of the infrared interference bomb 11-05 is tightly pressed through a fixing plate 11-03 arranged on the lower supporting plate 11-02, the protection plate 11-04 is connected with the fixing plate 11-03, and the protection plate 11-04 is parallel to the airplane bulkhead 11-06. All components are formed by bending steel plates, and the steel plate bending machine is simple in structure, easy to process and low in cost.
When a missile is discovered to attack, the infrared bait projectile can be projected into the air from an airplane or a ship, the pyrotechnic agent is ignited and quickly burns to form a false target, and the attacking missile completely abandons the target to track the infrared bait projectile, so that the aims of luring the enemy and improving the survival ability of the own are fulfilled.
As shown in fig. 2, specifically: the aircraft further comprises two wings 7, and the two wings 7 are detachably arranged on two sides of the middle of the aircraft body 9. The detachable installation mode is convenient for dismouting and transportation.
As shown in fig. 3 and 4, two traction tube fixing devices 6 respectively mounted on two wings 7 are further included,
the flare fixing device 6 comprises a flare 6-01, a hoop 6-02, a base 6-03, a first connecting plate 6-04, a second connecting plate 6-05 and a fairing 6-06;
the dragging light pipe 6-01 is arranged on a base 6-03 through two hoops 6-02, and the base 6-03 is arranged on the wing 7 through a first connecting plate 6-04 and a second connecting plate 6-05;
the fairing 6-06 is sleeved outside the first connecting plate 6-04, the second connecting plate 6-05 and the base 6-03.
The fairing 6-06 is used for protecting the first connecting plate 6-04 and the second connecting plate 6-05 from being damaged when the target drone flies at a high speed, and can reduce wind resistance and ensure the flight performance of the target drone.
Specifically, the multifunctional airplane further comprises a vertical fin 10 and two tail wings 8, wherein the two tail wings 8 are detachably arranged on two sides of the tail end of the airplane body 9, and the vertical fin 10 is integrally connected with the tail end of the airplane body 9. The detachable installation mode is convenient for dismouting and transportation, and the vertical fin is convenient for produce with fuselage integrated into one piece.
Specifically, the night navigation indicator lamps 5 are mounted on the wings 8 and the vertical tails 10, and the purpose of the night navigation indicator lamps is to avoid air traffic accidents.
The bottom of fuselage 9 is provided with two gasbag chambeies 4 along its axis of ordinates direction interval, and 9 tops of fuselage are equipped with umbrella chamber 3 and airspeed tube 2.
The end of the body 9 far away from the vertical tail 10 is provided with a head cover 1.
The design of the two air bag cabins 4 can reduce the damage of landing impact on the target drone to the maximum extent, the parachute cabin 3 releases the parachute when the target drone lands, and reduces the damage of the landing impact on the target drone, and the airspeed tube 2 is also called a pitot tube, a total pressure tube and a total-static pressure tube, and is a device for sensing the total pressure (also called total pressure) and static pressure of airflow and transmitting the measured pressure data to an atmospheric data computer and a flight instrument.
To sum up, this kind of drone is light in weight, and load is big, and the speed of flat flight is up to 180m/s, and the height of flat flight can reach 9000km, and the time of endurance is long, possesses the ability of navigating at night, can put in infrared jamming bullet automatically when discovering the guided missile and attacking, and the infrared searching performance of mainly used army combat confrontation training also can be to novel weaponry verifies.
Although the preferred embodiments of the present invention have been described in detail, the present invention is not limited to the above embodiments, and various changes can be made without departing from the spirit of the present invention within the knowledge of those skilled in the art.
Many other changes and modifications can be made without departing from the spirit and scope of the invention. It is to be understood that the invention is not to be limited to the specific embodiments, and that the scope of the invention is defined by the appended claims.
Claims (8)
1. The utility model provides a target drone is put in to dexterous type jamming bomb, includes the target drone body, its characterized in that: the target drone body comprises a drone body, an infrared interference bomb throwing device is arranged in the drone body, and the infrared interference bomb throwing device comprises an upper supporting plate, a lower supporting plate, an infrared interference bomb, a fixing plate and a protective plate;
an aircraft separation frame is arranged in the fuselage, the upper supporting plate and the lower supporting plate are both vertically arranged on the aircraft separation frame, and the upper supporting plate and the lower supporting plate are parallel to each other;
one end of the infrared interference bomb penetrates through the lower supporting plate and is installed on the upper supporting plate, the middle of the infrared interference bomb is tightly pressed through a fixing plate installed on the lower supporting plate, the protection plate is connected with the fixing plate, and the protection plate is parallel to the aircraft bulkhead.
2. The smart chaff delivery drone of claim 1, wherein: the aircraft further comprises two wings, and the two wings are detachably arranged on two sides of the middle of the aircraft body.
3. The smart chaff delivery drone of claim 2, wherein: also comprises two dragging light pipe fixing devices which are respectively arranged on the two wings,
the flare fixing device comprises a flare, a hoop, a base, a first connecting plate, a second connecting plate and a fairing;
the towing pipe is arranged on the base through two hoops, and the base is arranged on the wing through a first connecting plate and a second connecting plate;
the fairing is sleeved outside the first connecting plate, the second connecting plate and the base.
4. The smart chaff delivery drone of claim 1, wherein: the novel airplane tail structure is characterized by further comprising a vertical fin and two tail wings, wherein the two tail wings are detachably arranged on two sides of the tail end of the airplane body, and the vertical fin is integrally connected with the tail end of the airplane body.
5. The smart chaff delivery drone of claim 4, wherein: and night navigation indicator lamps are arranged on the wings and the vertical tails.
6. The smart chaff delivery drone of any one of claims 1 to 5, wherein: the fuselage bottom is provided with two gasbag chambeies along its axis of ordinates direction interval, and the fuselage top is equipped with umbrella chamber and airspeed head.
7. The smart chaff delivery drone of any one of claims 1 to 5, wherein: a head cover is arranged at one end of the body far away from the vertical tail.
8. The smart chaff delivery drone of claim 1, wherein: one end of the infrared interference bomb is clamped on the upper supporting plate.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201922281488.0U CN211373368U (en) | 2019-12-18 | 2019-12-18 | Target drone is put in to dexterous type interference bullet |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201922281488.0U CN211373368U (en) | 2019-12-18 | 2019-12-18 | Target drone is put in to dexterous type interference bullet |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN211373368U true CN211373368U (en) | 2020-08-28 |
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Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201922281488.0U Active CN211373368U (en) | 2019-12-18 | 2019-12-18 | Target drone is put in to dexterous type interference bullet |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN211373368U (en) |
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2019
- 2019-12-18 CN CN201922281488.0U patent/CN211373368U/en active Active
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| GR01 | Patent grant | ||
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Effective date of registration: 20201015 Address after: Room 11402, unit 1, building 1, Xinhui building, No. 33, Gaoxin Road, high tech Zone, Xi'an City, Shaanxi Province Patentee after: Xi'an Pangang electromechanical technology service partnership (limited partnership) Address before: No.11606, 16 / F, unit 1, building 1, CICI, No.10, No.1, Jinye Road, Zhangba street, hi tech Zone, Xi'an City, Shaanxi Province Patentee before: XI'AN LONG TECHNOLOGY & DEVELOPMENT Co.,Ltd. |
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Effective date of registration: 20220323 Address after: 710300 Building 9, second zone of science and technology enterprise accelerator, No. 6 West Qinling Avenue, Caotang science and technology industry base, high tech Zone, Xi'an, Shaanxi Province Patentee after: XI'AN LONG TECHNOLOGY & DEVELOPMENT Co.,Ltd. Address before: 710075 room 11402, unit 1, building 1, Xinhui building, No. 33, Gaoxin Road, high tech Zone, Xi'an, Shaanxi Province Patentee before: Xi'an Pangang electromechanical technology service partnership (limited partnership) |
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