Non-aiming intelligent patrolling bomb

Abstract

The invention relates to the technical field of intelligent ammunition, and discloses a non-aiming intelligent patrolling ammunition which comprises an induction part and a warhead part. The inducing part comprises a first flying mechanism, a plurality of controllable connecting mechanisms evenly connected to the first flying mechanism and a flue generating mechanism detachably connected to the controllable connecting mechanisms, and the first flying mechanism is used for driving the controllable connecting mechanisms and the flue generating mechanism to move along a set track; the flue generation mechanism is used for generating a flue along a set track; the induction part is additionally arranged on the warhead, when the target hitting command is executed, the induction part is separated from the warhead and forms the covering flue on the hitting flight track of the warhead, the specific position of the warhead in the view of an enemy can be effectively shielded, and therefore the risk that the warhead is hit down can be effectively reduced; and meanwhile, the induction part can intercept the attack of the enemy for the warhead, so that the striking success rate of the warhead is further improved.

Description

Technical Field

[0001] The present invention relates to the technical field of intelligent ammunition, and more specifically, it relates to a non-aiming intelligent loitering munition. Background Art

[0002] A loitering munition is a precision ammunition that can cruise over a target area and execute combat commands. It is also a product of the organic combination of unmanned aerial vehicle technology and ammunition technology, and mainly undertakes combat tasks such as battlefield reconnaissance, target indication, precision strike, damage assessment, communication relay, electronic countermeasure, air alert, and special payload delivery.

[0003] A loitering munition is a lightweight intelligent aerospace missile between a cruise missile and an unmanned aerial vehicle. Its greatest feature is that it can fly over a target area for a period of time for reconnaissance and then launch an attack after the operator determines the target.

[0004] When existing loitering munitions execute an attack command, each propeller blade generates a pulling force in the same direction as the gravity direction; this pulling force and the gravity act on the projectile body together to generate an attack acceleration greater than 1 g (g is 9.8 m / s²), so as to achieve rapid and accurate strikes. However, during this process, there is still a possibility of crashing due to counterattacks from the target being attacked. Summary of the Invention

[0005] The purpose of the present invention is to provide a non-aiming intelligent loitering munition to solve the above problems.

[0006] The present invention provides a non-aiming intelligent loitering munition, including: An induction part, the induction part includes a flight mechanism I, a plurality of controllable connection mechanisms evenly connected to the flight mechanism I, and a flue generating mechanism detachably connected to the controllable connection mechanism. The flight mechanism I is used to drive the plurality of controllable connection mechanisms and the flue generating mechanism to move along a set track, and the flue generating mechanism is used to generate a flue along the set track; A warhead, the warhead includes a flight mechanism II and a munition striking assembly connected to the flight mechanism II. The flight mechanism II is detachably connected to the flight mechanism I. The flight mechanism II is used to drive the munition striking assembly to move along the flue, and the distance between the flight mechanism II and the flight mechanism I is adjustable.

[0007] As a further optimized solution of the present invention, the flight mechanism I includes a housing I, an integrated control part I arranged inside the housing I, a connecting rod I connected to the housing I, a slot I arranged on the connecting rod I, a plurality of slot II arranged on the inner wall of the slot I, a plurality of power motors I evenly connected to the housing I, and a propeller blade I connected to the output end of the power motor I. The plurality of controllable connection mechanisms are evenly distributed among the plurality of power motors I.

[0008] As a further optimization scheme of the present invention, the controllable connection mechanism includes a second connecting rod, a first cavity provided inside the second connecting rod, a first electromagnet fixedly connected to the inner wall of the first cavity, two first wedges slidably connected to the inner wall of the first cavity, and a first spring connected between the first wedge and the first electromagnet. The two first wedges are symmetrically distributed on both sides of the first electromagnet. When the first electromagnet is energized, the distance between the first wedge and the first electromagnet is shortened. One end of the second connecting rod is fixedly connected to the first housing, and the other end of the second connecting rod is in a convex shape. The first cavity, the first electromagnet, the first spring, and the first wedge are all located at the other end of the second connecting rod.

[0009] As a further optimization scheme of the present invention, a pulling-back assembly is provided inside the controllable connection mechanism. The pulling-back assembly is used to adjust the distance between the flue generating mechanism separated from the first flight mechanism and the first flight mechanism.

[0010] As a further optimization scheme of the present invention, the pulling-back assembly includes a second cavity provided inside the second connecting rod, an integrated motor fixedly connected to the inner wall of the second cavity, a first synchronous pulley connected to the output end of the integrated motor, a wire winding cylinder movably connected to the inner wall of the second cavity, a second synchronous pulley fixedly connected to the wire winding cylinder, a synchronous belt connected between the first synchronous pulley and the second synchronous pulley, and a reinforced connection cable wound around the wire winding cylinder. Wiring channels are provided inside both the second connecting rod and the flue generating mechanism for laying the reinforced connection cable. The reinforced connection cable is electrically connected to the first integrated control unit.

[0011] As a further optimization scheme of the present invention, the flue generating mechanism includes an arc-shaped connecting piece, an elastic pressure-sensitive connecting piece connected to the arc-shaped connecting piece, an arc-shaped protective plate connected to the elastic pressure-sensitive connecting piece, a plurality of smoke generators fixedly connected to the arc-shaped connecting piece, and a concave-shaped connecting piece fixedly connected to the arc-shaped connecting piece. The concave-shaped connecting piece is arranged in cooperation with the second connecting rod, and a first wedge groove for cooperating with the first wedge is provided on the concave-shaped connecting piece. Both the elastic pressure-sensitive connecting piece and the smoke generator are electrically connected to the first integrated control unit through the reinforced connection cable.

[0012] As a further optimization scheme of the present invention, the elastic pressure-sensitive connecting piece includes a first arc-shaped bellows, a second arc-shaped bellows, and an elastic pressure-sensitive component connected to the arc-shaped connecting piece. The other ends of the first arc-shaped bellows, the second arc-shaped bellows, and the elastic pressure-sensitive component are all fixedly connected to the arc-shaped protective plate. The elastic pressure-sensitive component is electrically connected to the first integrated control unit through the reinforced connection cable.

[0013] As a further optimization scheme of the present invention, the smoke generator includes a combustion box, smoke generating materials provided in the combustion box, and an electric igniter. The electric igniter is electrically connected to the first integrated control unit through the reinforced connection cable, and the electric igniter is used to ignite the smoke generating materials.

[0014] As a further optimization solution of the present invention, the second flight mechanism includes a second housing, an integrated control unit two connected to the second housing, a plurality of power motors two connected to the second housing, propeller blades two connected to the power motors two, a connecting rod three connected to the integrated control unit two, a wiring cavity and a plurality of cavities three provided inside the connecting rod three, an electromagnet two fixedly connected to the inner wall of the cavity three, a wedge two slidably connected to the inner wall of the cavity three, and a spring two connected between the wedge two and the electromagnet two. The wedge two is arranged in cooperation with the slot two.

[0015] As a further optimization solution of the present invention, the ammunition striking assembly includes a projectile body provided on the second housing and a seeker provided on the projectile body.

[0016] The beneficial effects of the present invention are as follows: The present invention adds an induction part to the warhead. When executing the command to strike the target, the induction part detaches from the warhead and forms a covering smoke channel on the flight trajectory of the warhead strike, which can effectively block the specific position of the warhead in the enemy's field of vision, thereby effectively reducing the risk of the warhead being shot down. At the same time, the induction part can provide interception of the enemy's attack for the warhead, further improving the hitting success rate of the warhead. Description of the Drawings

[0017] Figure 1 is the overall structural schematic diagram of the present invention; Figure 2 is the matching view of the induction part and the warhead of the present invention; Figure 3 is the partial cross-sectional view of the warhead of the present invention; Figure 4 is the partial cross-sectional view of the induction part of the present invention; Figure 5 is the Figure 2 enlarged view of the A position in the present invention; Figure 6 is the matching view of the controllable connection mechanism and the smoke channel generating mechanism of the present invention; Figure 7 is the Figure 6 enlarged view of the B position in the present invention; Figure 8 is the Figure 6 enlarged view of the C position in the present invention.

[0018] In the figure: 1. Induction part; 11. Flight mechanism I; 1101. Housing I; 1102. Connecting rod I; 1103. Slot I; 1104. Slot II; 1105. Power motor I; 1106. Propeller blade I; 12. Controllable connection mechanism; 1201. Connecting rod II; 1202. Cavity I; 1203. Electromagnet I; 1204. Spring I; 1205. Wedge block I; 1206. Cavity II; 1207. Integrated motor; 1208. Synchronous pulley I; 1209. Timing belt; 1210. Winding drum; 1211. Reinforced connection cable; 1212. Wiring channel; 13. Flue generating mechanism; 1301. Arc-shaped connecting piece; 1302. Elastic pressure-sensitive connecting piece; 1303. Arc-shaped protection plate; 1304. Smoke generator; 2. Warhead; 200. Housing II; 201. Projectile body; 202. Integrated control part II; 203. Power motor II; 204. Propeller blade II; 205. Seeker; 206. Connecting rod III; 207. Wiring cavity; 208. Cavity III; 209. Electromagnet II; 210. Spring II; 211. Wedge block II. Detailed implementation mode

[0019] Now, the subject matter described herein will be discussed with reference to exemplary implementation modes. It should be understood that discussing these implementation modes is only to enable those skilled in the art to better understand and thus implement the subject matter described herein. Additionally, features described relative to some examples can also be combined in other examples.

[0020] As Figures 1 - 8 shown, a non-aiming intelligent cruise missile includes: An induction part 1, the induction part 1 includes a flight mechanism I 11, a plurality of controllable connection mechanisms 12 uniformly connected to the flight mechanism I 11, and a flue generating mechanism 13 detachably connected to the controllable connection mechanism 12. The flight mechanism I 11 is used to drive the plurality of controllable connection mechanisms 12 and the flue generating mechanism 13 to move along a set track, and the flue generating mechanism 13 is used to generate a flue along the set track; A warhead 2, the warhead 2 includes a flight mechanism II and an ammunition striking assembly connected to the flight mechanism II. The flight mechanism II is detachably connected to the flight mechanism I 11. The flight mechanism II is used to drive the ammunition striking assembly to move along the flue, and the distance between the flight mechanism II and the flight mechanism I 11 is adjustable.

[0021] It should be noted that before the hitting task is executed, the induction part 1 and the warhead 2 are in a connected and co-flying state. When the hitting target is locked and the execution starts, the induction part 1 is disconnected from the warhead 2, and the flight mechanism 11 drives the flue generating mechanism 13 to fly preferentially on the set track. During the flight, the flue generating mechanism 13 is activated so that the flue generating mechanism 13 can generate an obstructive flue on the flight trajectory. At a set time point after the flight mechanism 11 has flown, the warhead 2 starts to fly along the set track. The flight trajectory of the warhead 2 is adjustable, mainly based on the trajectory formed by the flue. The coverage range of the flue is much larger than the volume of the warhead 2. Under the influence of external factors, such as the influence of crosswind on the flue, it will not deviate from the established flight trajectory of the hitting target and can still complete the precise hitting target. Moreover, under the cover of the flue, the warhead 2 can effectively reduce the risk of being hit and crashing by the enemy.

[0022] In an alternative embodiment of the present invention, as Figure 4 shown, the flight mechanism 11 includes a housing 1101, an integrated control unit 1 disposed inside the housing 1101, a connecting rod 1102 connected to the housing 1101, a slot 1103 disposed on the connecting rod 1102, a plurality of slots 1104 disposed on the inner wall of the slot 1103, a plurality of power motors 1105 evenly connected to the housing 1101, and a propeller blade 1106 connected to the output end of the power motor 1105. A plurality of controllable connection mechanisms 12 are evenly distributed among the plurality of power motors 1105.

[0023] It should be noted that as described above, when the flight mechanism 11 drives the controllable connection mechanism 12 and the flue generating mechanism 13 to fly along the established track, the output power of the plurality of power motors 1105 can be adjusted through the integrated control unit 1, so as to adjust the attitude of the housing 1101 and the flight path, and fly quickly towards the hitting target with a precise flight trajectory.

[0024] In an alternative embodiment of the present invention, as Figure 4 and Figure 7As shown in the figure, the controllable connection mechanism 12 includes a second connecting rod 1201, a first cavity 1202 provided inside the second connecting rod 1201, a first electromagnet 1203 fixedly connected to the inner wall of the first cavity 1202, two first wedges 1205 slidably connected to the inner wall of the first cavity 1202, and a first spring 1204 connected between the first wedge 1205 and the first electromagnet 1203. The two first wedges 1205 are symmetrically distributed on both sides of the first electromagnet 1203. When the first electromagnet 1203 is energized, the distance between the first wedge 1205 and the first electromagnet 1203 is shortened. One end of the second connecting rod 1201 is fixedly connected to the first housing 1101, and the other end of the second connecting rod 1201 is convex. The first cavity 1202, the first electromagnet 1203, the first spring 1204, and the first wedge 1205 are all located at the other end of the second connecting rod 1201.

[0025] It should be noted that, as described above, when the first flight mechanism 11 drives the controllable connection mechanism 12 and the flue generating mechanism 13 to fly along the set path, not only can the flue generating mechanism 13 generate a flue, but also the first flight mechanism 11, the controllable connection mechanism 12, and the flue generating mechanism 13 can provide shielding for the subsequent flying warhead 2. When the flue generating mechanism 13 is attacked and stressed, the first integrated control unit can quickly obtain this information and disconnect the rigid connection between the controllable connection mechanism 12 and the corresponding attacked flue generating mechanism 13 to prevent the stressed flue generating mechanism 13 from driving the first flight mechanism 11 to deviate from the established orbit. In this way, the path length and stability of flue generation can be further improved. The disconnection process is specifically as follows: The first integrated control unit energizes the first electromagnet 1203. After the first electromagnet 1203 is energized, it generates a corresponding magnetic force and applies it to the corresponding first wedge 1205. At this time, the first wedge 1205 receiving the magnetic force starts to move towards the first electromagnet 1203 and compresses the first spring 1204 between them. When the first spring 1204 is compressed to the set length, the first wedge 1205 is disconnected from the flue generating mechanism 13, so that the flue generating mechanism 13 can be disconnected from the rigid connection with the second connecting rod 1201, enabling the flue generating mechanism 13 to freely release the influence of the external force it receives. This force is offset by air resistance, and the moving distance is determined by the magnitude of the force.

[0026] In an optional embodiment of the present invention, as Figure 7 and Figure 8 shown, a pulling-back assembly is provided inside the controllable connection mechanism 12. The pulling-back assembly is used to adjust the distance between the flue generating mechanism 13 separated from the first flight mechanism 11 and the first flight mechanism 11.

[0027] The pulling-back assembly includes a second cavity 1206 provided inside the second connecting rod 1201, an integrated motor 1207 fixedly connected to the inner wall of the second cavity 1206, a first synchronous pulley 1208 connected to the output end of the integrated motor 1207, a wire winding cylinder 1210 movably connected to the inner wall of the second cavity 1206, a second synchronous pulley fixedly connected to the wire winding cylinder 1210, a synchronous belt 1209 connected between the first synchronous pulley 1208 and the second synchronous pulley, and a reinforced connection cable 1211 wound around the wire winding cylinder 1210. Both the second connecting rod 1201 and the flue generating mechanism 13 are provided with wiring channels 1212 for laying the reinforced connection cable 1211, and the reinforced connection cable 1211 is electrically connected to the first integrated control unit.

[0028] It should be noted that as described above, when the flue generating mechanism 13 is separated from the second connecting rod 1201, in order to prevent the excessive separation of the flue generating mechanism 13, which may affect the formation of the flue, a pulling-back mechanism is provided inside the controllable connection mechanism 12. The pulling-back mechanism is soft-connected to the flue generating mechanism 13 and is not affected by the movement of the flue generating mechanism 13. That is, during the movement of the flue generating mechanism 13 after it is separated from the second connecting rod 1201, it will not affect the first flight mechanism 11 through the pulling-back mechanism. When the energy release of the flue generating mechanism 13 is completed, the corresponding flue generating mechanism 13 can be pulled back to the position of the second connecting rod 1201 through the pulling-back mechanism, so that the flue generating mechanism 13 can continue to provide the smoke volume for the flue, ensuring that the flue is complete and the coverage range remains unchanged. Specifically: After the flue generating mechanism 13 is separated from the second connecting rod 1201, during its free movement, the reinforced connection cable 1211 connected to it can be continuously pulled out from the wire winding cylinder 1210. During this pulling-out process, the pulling force on the wire winding cylinder 1210 is extremely small and basically does not affect the first flight mechanism 11. When the energy release of the flue generating mechanism 13 is completed, the integrated motor 1207 is driven to rotate the first synchronous pulley 1208. After the first synchronous pulley 1208 rotates, it drives the synchronous belt 1209 and the second synchronous pulley to rotate, thereby driving the wire winding cylinder 1210 fixedly connected to the second synchronous pulley to rotate, so that the wire winding cylinder 1210 pulls back the reinforced connection cable 1211 again, and the flue generating mechanism 13 connected to the reinforced connection cable 1211 is pulled back to the position of the second connecting rod 1201. The method for judging the end of the energy release of the flue generating mechanism 13 can be to arrange an angle sensor on the integrated motor 1207. When the angle sensor detects that the change speed of the rotation angle of the first synchronous pulley 1208 decreases to the set value, it can be judged that the energy release of the flue generating mechanism 13 is completed.

[0029] In an optional embodiment of the present invention, as Figure 4As shown, the flue generating mechanism 13 includes an arc-shaped connecting piece 1301, an elastic pressure-sensitive connecting piece 1302 connected to the arc-shaped connecting piece 1301, an arc-shaped protective plate 1303 connected to the elastic pressure-sensitive connecting piece 1302, a plurality of smoke generators 1304 fixedly connected to the arc-shaped connecting piece 1301, and a concave-shaped connecting piece fixedly connected to the arc-shaped connecting piece 1301. The concave-shaped connecting piece is arranged in cooperation with the second connecting rod 1201, and a first wedge groove matched with the first wedge block 1205 is provided on the concave-shaped connecting piece. Both the elastic pressure-sensitive connecting piece 1302 and the smoke generator 1304 are electrically connected to the first integrated control unit through a reinforced connecting cable 1211.

[0030] The elastic pressure-sensitive connecting piece 1302 includes a first arc-shaped corrugated pipe, a second arc-shaped corrugated pipe and an elastic pressure-sensitive component connected to the arc-shaped connecting piece 1301. The other ends of the first arc-shaped corrugated pipe, the second arc-shaped corrugated pipe and the elastic pressure-sensitive component are fixedly connected to the arc-shaped protective plate 1303. The elastic pressure-sensitive component is electrically connected to the first integrated control unit through a reinforced connecting cable 1211.

[0031] The smoke generator 1304 includes a combustion chamber, a smoke generating material arranged in the combustion chamber, and an electric igniter. The electric igniter is electrically connected to the first integrated control unit through a reinforced connecting cable 1211, and the electric igniter is used to ignite the smoke generating material.

[0032] It should be noted that as described above, when the flue generating mechanism 13 generates a flue through the first integrated control unit, specifically, the first integrated control unit supplies power to the electric igniter through the reinforced connecting cable 1211, so that the electric igniter ignites the smoke generating material, so that the smoke generating material burns in the combustion chamber and generates a large amount of smoke. The smoke spreads from the combustion chamber and forms a flue on the moving track. When the arc-shaped protective plate 1303 is stressed by an external impact, the force it receives is transmitted to the elastic pressure-sensitive component. The elastic pressure-sensitive component transmits a signal to the reinforced connecting cable 1211, and the reinforced connecting cable 1211 transmits it to the first integrated control unit. When the first integrated control unit receives the signal and determines that the external force received by the arc-shaped protective plate 1303 exceeds the set threshold, it starts to control the first electromagnet 1203 to work, so that the arc-shaped connecting piece 1301 is disconnected from the second connecting rod 1201.

[0033] In an optional embodiment of the present invention, as Figure 3 and Figure 5As shown in the figure, the second flight mechanism includes a second housing 200, an integrated control unit two 202 connected to the second housing 200, a plurality of power motors two 203 connected to the second housing 200, propeller blades two 204 connected to the power motors two 203, a connecting rod three 206 connected to the integrated control unit two 202, a wiring cavity 207 and a plurality of cavities three 208 provided inside the connecting rod three 206, an electromagnet two 209 fixedly connected to the inner wall of the cavity three 208, a wedge two 211 slidably connected to the inner wall of the cavity three 208, and a spring two 210 connected between the wedge two 211 and the electromagnet two 209. The wedge two 211 is arranged in cooperation with the slot two 1104.

[0034] It should be noted that after the second flight mechanism is disconnected from the first flight mechanism 11 and flies along the established track, the output power of multiple power motors two 203 can be adjusted through the integrated control unit two 202, so as to adjust the attitude of the second housing 200 and the flight path, and fly quickly towards the strike target with a precise flight trajectory. When the second flight mechanism is disconnected from the first flight mechanism 11, the integrated control unit two 202 powers the electromagnet two 209. After the electromagnet two 209 is powered, it can generate a magnetic force and apply it to the corresponding wedge two 211. The wedge two 211 is forced to compress the spring two 210 until the wedge two 211 disengages from the slot two 1104. At this time, the connecting rod three 206 is disconnected from the connecting rod one 1102, so that the first housing 1101 and the second housing 200 can be separated.

[0035] In an optional embodiment of the present invention, the ammunition striking assembly includes a projectile 201 provided on the second housing 200 and a seeker 205 provided on the projectile 201.

[0036] It should be noted that the projectile 201 can be various types of projectiles 201, and different types of seekers 205 are configured, such as any type of seeker 205 including a platform seeker, a strapdown seeker, a visible light seeker, a laser seeker, and a radar seeker. By configuring different seekers 205, the locking and tracking tasks of different target types in different meteorological environments can be achieved.

[0037] The above describes this embodiment, but this embodiment is not limited to the above specific implementation manners. The above specific implementation manners are only illustrative and not restrictive. Under the inspiration of this embodiment, those of ordinary skill in the art can also make many forms, all of which fall within the protection scope of this embodiment.

Claims

1. A non-aiming intelligent cruise missile, characterized in that: include: An induction section (1), the induction section (1) comprising a flying mechanism (11), a plurality of controllable connecting mechanisms (12) uniformly connected to the flying mechanism (11), and a smoke duct generating mechanism (13) detachably connected to the controllable connecting mechanism (12), the flying mechanism (11) being used to drive the plurality of controllable connecting mechanisms (12) and the smoke duct generating mechanism (13) to move along a set track, and the smoke duct generating mechanism (13) being used to generate a smoke duct along the set track; A warhead (2), the warhead (2) comprising a second flying mechanism and an ammunition striking assembly connected to the second flying mechanism, the second flying mechanism being detachably connected to the first flying mechanism (11), the second flying mechanism being used to drive the ammunition striking assembly to move along the flue, and the distance between the second flying mechanism and the first flying mechanism (11) being adjustable.

2. The non-aiming intelligent cruise missile according to claim 1, characterized in that: The flight mechanism (11) comprises a shell (1101), an integrated control unit (1) arranged inside the shell (1101), a connecting rod (1102) connected to the shell (1101), a slot (1103) arranged on the connecting rod (1102), a plurality of slots (1104) arranged on the inner wall of the slot (1103), a plurality of power motors (1105) evenly connected to the shell (1101), and a propeller blade (1106) connected to the output end of the power motor (1105), and a plurality of controllable connection mechanisms (12) are evenly distributed between the plurality of power motors (1105).

3. The non-aiming intelligent cruise missile according to claim 2, characterized in that: The controllable connection mechanism (12) comprises a second connecting rod (1201), a cavity (1202) disposed inside the second connecting rod (1201), an electromagnet (1203) fixedly connected to the inner wall of the cavity (1202), two wedges (1205) slidably connected to the inner wall of the cavity (1202), and a spring (1204) connected between the wedges (1205) and the electromagnet (1203), wherein the two wedges (1205) are symmetrically distributed on the electromagnet. On both sides of (1203), when the electromagnet one (1203) is energized, the distance between the wedge block one (1205) and the electromagnet one (1203) is shortened, one end of the connecting rod two (1201) is fixedly connected to the shell one (1101), and the other end of the connecting rod two (1201) is convex-shaped, and the cavity one (1202), the electromagnet one (1203), the spring one (1204) and the wedge block one (1205) are all located at the other end of the connecting rod two (1201).

4. The non-aiming intelligent cruise missile according to claim 3, characterized in that: The controllable connection mechanism (12) is provided with a pull-back component, which is used to adjust the distance between the smoke duct generating mechanism (13) separated from the flying mechanism one (11) and the flying mechanism one (11).

5. The non-aiming intelligent cruise missile according to claim 4, characterized in that: The pullback assembly comprises a second cavity (1206) arranged inside the second connecting rod (1201), an integrated motor (1207) fixedly connected to the inner wall of the second cavity (1206), a synchronous wheel (1208) connected to the output end of the integrated motor (1207), a winding drum (1210) movably connected to the inner wall of the second cavity (1206), a second synchronous wheel fixedly connected to the winding drum (1210), a synchronous belt (1209) connected between the first synchronous wheel (1208) and the second synchronous wheel, and a reinforced connection cable (1211) wound around the winding drum (1210), and a wiring cavity (1212) is provided inside the second connecting rod (1201) and the smoke duct generating mechanism (13), and the wiring cavity (1212) is used to lay the reinforced connection cable (1211), and the reinforced connection cable (1211) is electrically connected to the first integrated control unit.

6. The non-aiming intelligent cruise missile according to claim 5, characterized in that: The flue gas generating mechanism (13) comprises an arc-shaped connecting member (1301), an elastic pressure-sensitive connecting member (1302) connected to the arc-shaped connecting member (1301), an arc-shaped protective plate (1303) connected to the elastic pressure-sensitive connecting member (1302), a plurality of smoke generators (1304) fixedly connected to the arc-shaped connecting member (1301), and a concave-shaped connecting member fixedly connected to the arc-shaped connecting member (1301), wherein the concave-shaped connecting member is arranged in coordination with a second connecting rod (1201), and a wedge groove 1 is provided on the concave-shaped connecting member, which is coordinated with a first wedge block (1205), and the elastic pressure-sensitive connecting member (1302) and the smoke generator (1304) are both electrically connected to an integrated control unit 1 via a reinforced connecting cable (1211).

7. The non-aiming intelligent cruise missile according to claim 6, characterized in that: The elastic pressure-sensitive connector (1302) comprises an arc-shaped bellows 1, an arc-shaped bellows 2 and an elastic pressure-sensitive component connected to the arc-shaped connector (1301); the other ends of the arc-shaped bellows 1, the arc-shaped bellows 2 and the elastic pressure-sensitive component are fixedly connected to the arc-shaped protective plate (1303); and the elastic pressure-sensitive component is electrically connected to the integrated control unit 1 via a reinforced connecting cable (1211).

8. The non-aiming intelligent cruise missile according to claim 7, characterized in that: The smoke generator (1304) comprises a combustion box, smoke generating material arranged in the combustion box, and an electric igniter. The electric igniter is electrically connected to an integrated control unit via a reinforced connection cable (1211). The electric igniter is used to ignite the smoke generating material.

9. The non-aiming intelligent cruise missile according to claim 8, characterized in that: The second flight mechanism comprises a second shell (200), a second integrated control unit (202) connected to the second shell (200), a plurality of second power motors (203) connected to the second shell (200), a second propeller blade (204) connected to the second power motor (203), a third connecting rod (206) connected to the second integrated control unit (202), a wiring cavity (207) and a plurality of third cavities (208) arranged inside the third connecting rod (206), a second electromagnet (209) fixedly connected to the inner wall of the third cavity (208), a second wedge (211) slidably connected to the inner wall of the third cavity (208), and a second spring (210) connected between the second wedge (211) and the second electromagnet (209), wherein the second wedge (211) is arranged in cooperation with the second slot (1104).

10. The non-aiming intelligent cruise missile according to claim 9, characterized in that: The ammunition striking assembly comprises a projectile body (201) arranged on the second shell (200) and a guidance head (205) arranged on the projectile body (201).

Images