TWM543985U - Attack system of missile combined with quality-strengthened net - Google Patents

Description

Flying missile combined with strong network attack system

This creation is about an attack system, especially an attack system that combines a strong mesh with a missile with a missile and a strong mesh technology to defend or intercept the target of foreign invasion.

National defense is also a very important part for all countries. At present, national defense in the face of foreign invading targets, such as sea, land and air weapons and personnel, although defensive weapons, such as flying missiles, turrets, etc., to defend or attack, however, the defense methods of each country All use one-to-one interception methods to defend or attack.

As mentioned above, the creators of this creation think about and design an attack system combining flight missiles with strong quality nets, in order to improve the lack of conventional technology, and thus enhance the implementation and utilization of the industry.

In view of the above-mentioned problems of the prior art, the purpose of the present invention is to provide an attack system combining a flying missile with a strong mesh, and to replace the point-like attack with a planar mesh attack to solve the lack of the prior art.

According to the purpose of the present invention, an attack system of a flying missile combined with a strong mesh is proposed, which comprises at least one primary flying missile device, which can be located in a transmitting channel, and at least one primary flying missile device can include a flying missile body, a mesh component and A plurality of auxiliary warhead assemblies. The main body of the flying missile has a space for accommodation. The mesh component is located in the accommodating space. A plurality of auxiliary warhead assemblies are respectively disposed on the corner sides of the mesh assembly. Wherein, when at least one primary flying missile device is fired toward at least one target and the flying missile body is separated, the plurality of auxiliary warhead assemblies are disengaged from the main body of the flying missile and approach the position of at least one target or the oncoming route, and in part When the auxiliary warhead assembly receives at least one control signal, the partial auxiliary warhead assemblies are away from each other to cause the mesh assembly to be in an unfolded state, thereby intercepting at least one target by the mesh assembly.

Preferably, the attack system of the flying missile combined with the strong mesh may further comprise at least one transmitting device and the control device. At least one of the transmitting devices has a transmitting channel. The control device is electrically connected to the at least one transmitting device, and the communication link portion assists the warhead assembly. When the control device receives the execution signal, the control device drives the at least one transmitting device to fire at least one main flying missile toward the position of the at least one target or the oncoming route. Device.

Preferably, the attack system of the flying missile combined with the strong mesh may further comprise a detecting device electrically connected to the control device, and the detecting device senses at least one target in the range of the region to generate at least one detecting signal.

Preferably, the control device can drive the at least one transmitting device to fire at least one primary flying missile device toward the position of the at least one target or the oncoming route according to the execution signal and the at least one detecting signal.

Preferably, the detecting device generates at least one control signal according to the path or position of the at least one target.

Preferably, the attack system of the flying missile combined with the strong mesh may further comprise an operating device electrically connected to the control device, and when the operating device is touched to generate an execution signal, the operating device transmits the execution signal to the control device.

Preferably, the mesh fabric of the mesh component can have a heterogeneous layer.

Preferably, when the mesh component intercepts at least one target, the heterogeneous layer is adhered to at least one target.

Preferably, the mesh fabric of the mesh component can have a plurality of bursts.

Preferably, when the mesh component intercepts at least one target and at least one target touches at least one burst, the burst generates a burst.

As described above, the proposed flying missile combined with the strong mesh attack system can be provided with a plurality of warheads combined with the intercepting net design, and a plurality of auxiliary warhead assemblies and mesh components are disposed in the main missile of the main flight missile device. When a flying missile is used as a strong mesh vehicle, when several foreign invading targets enter the range of the launching device, after predicting the oncoming route or position, the flying missile can be combined with the attack system of the strong mesh to fire the main flying missile device. After the main body of the flying missile is separated, a plurality of auxiliary warhead assemblies can drive the mesh component to approach the oncoming route or position of the invading target, and intercept multiple external invading targets with a single mesh component, thereby improving the defense. The benefits can be reduced and the cost of wear and tear can be reduced. At the same time, a large number of foreign invasive objects can be destroyed in a short time.

In order to understand the technical characteristics, content and advantages of the creation and the effects that can be achieved by the examiner, the author will use the drawings in detail and explain the following in the form of the examples, and the drawings used therein The subject matter is only for the purpose of illustration and supplementary manual. It is not necessarily the true proportion and precise configuration after the implementation of the original creation. Therefore, the proportion and configuration relationship of the attached drawings should not be limited to the scope of patents created in actual implementation. Narration.

The embodiments of the attack system of the flying missile combined with the strong mesh according to the present invention will be described below with reference to the related drawings. For ease of understanding, the same components in the following embodiments are denoted by the same reference numerals.

Please refer to FIG. 1 to FIG. 4 , which are respectively a system schematic diagram, a first implementation schematic diagram, a second implementation schematic diagram and a system block diagram of a first embodiment of an attack system for a flying missile combined with a strong quality network. As shown, the attack system 1 of the flying missile combined with the strong mesh includes at least one primary flying missile device 11 that can be located in the transmitting channel 100. The at least one primary flying missile device 11 can include the flying missile body 110 and the mesh assembly 111. And a plurality of auxiliary warhead assemblies 112. The flying missile body 110 has an accommodation space 110A. The mesh member 111 is located in the accommodating space 110A. A plurality of auxiliary warhead assemblies 112 are respectively disposed on the sides of the mesh assembly 111. Wherein, when at least one primary flight missile device 11 is fired toward at least one target 2 and the flying missile body 110 is disengaged, the plurality of auxiliary warhead assemblies 112 are disengaged from the flying missile body 110 and directed toward at least one target 2 or an oncoming route. As the partial auxiliary warhead assembly 112 receives the at least one control signal 131, the partial auxiliary warhead assemblies 112 are away from each other, so that the mesh assembly 111 is in an unfolded state, and at least one target 2 is intercepted by the mesh assembly 111. .

Specifically, the inventive flying missile combined with the strong mesh attack system 1 includes at least one primary flying missile device 11, and the primary flying missile device 11 may be a flying missile or missile equipped with a plurality of auxiliary warheads, wherein, in this implementation In the example, the number of the main flight missile devices 11 is taken as an example, but not limited thereto. In actual implementation, the number may be determined by the user. The primary flight missile device 11 can be disposed in the launch channel 100 of the launch device of any sea, land, and air vehicle. The primary flight missile device 11 includes a flight missile body 110, a mesh assembly 111, and a plurality of auxiliary warhead assemblies 112, the flight missile body 110. The accommodating space 110A is used for accommodating the mesh component 111 and the plurality of auxiliary warhead assemblies 112. The mesh component 111 can be any metal alloy material, such as a wire mesh, but not limited thereto. The plurality of auxiliary warhead assemblies 112 are respectively disposed on the side of the mesh assembly 111, such as four corners of the mesh assembly 111, but not limited thereto, wherein the plurality of auxiliary warhead assemblies 112 can be meshed according to the creation The assembly 111 can be circular or polygonal with different set positions.

Therefore, when the operator finds that a plurality of objects 2 are approaching, as shown in (A), (B), and (C) of FIG. 2, the object 2 may be an air vehicle, a marine vehicle, or land. For the vehicle or the personnel, the operator can first estimate the oncoming route or position of the target 2, and then fire the main flight missile device 11 toward the target 2 via the launching device 10. After the primary flight missile device 11 is fired from the launch channel 100, the primary flight missile device 11 approaches the target 2, and during a certain flight, or the primary flight missile device 11 detects proximity to the target 2 At this time, the flying missile body 110 will be separated, and the plurality of auxiliary warhead assemblies 112 will be disengaged from the flying missile body 110. Then, after the main flying missile device 11 releases the plurality of auxiliary warhead assemblies 112, the partial auxiliary warhead assembly 112 can receive the regulating signal 131 transmitted by the control end of the satellite, the drone, the ground radar or the reconnaissance plane, and drive the mesh. The component 111 approaches the position of the target 2 or the oncoming route. At the same time, the partial auxiliary warhead assemblies 112 can be separated from each other according to the adjustment signal 131, so that the mesh assembly 111 is in an unfolded state, and the plurality of mesh components 111 are used to intercept the plurality of mesh components 111. Target 2, causing the enemy's incoming weapon to be out of balance or sluggish.

As shown in Fig. 3, when the target 2 is an aircraft carrier, the inventive flying missile combined with the strong mesh attack system 1 can also use the mesh component 111 to cover the take-off runway on the aircraft carrier, or sprinkle the obstruction, and make the aircraft carrier The aircraft on board cannot take off, and thus the ability to suppress the air combat capability of the aircraft carrier is achieved.

Further, the inventive flying missile combined with the strong mesh attack system 1 preferably further includes at least one transmitting device 10 and the control device 12. At least one launching device 10 has a launch channel 100 that can accommodate at least one primary missile device 11. The control device 12 is electrically connected to the at least one transmitting device 10 and communicates with the connecting portion of the auxiliary warhead assembly 112. When the control device 12 receives the execution signal 120, the control device 12 drives the at least one transmitting device 10 toward the position of at least one target 2 or The oncoming route fires at least one primary flight missile device 11.

Specifically, the inventive flying missile combined with the strong mesh attack system 1 may further comprise at least one transmitting device 10 and a control device 12, which may be a conventional flying missile launching device, such as a turret or a flight fighter. The barrel, but not limited to this, the launching device 10 can be placed on a land, warship, submarine, or fighter aircraft in different shapes. The control device 12 can be a control device on a control center or a land, sea and air vehicle. In the present embodiment, the number of the transmitting device 10 and the main flying missile device 11 is taken as an example, and the control device 12 takes the control device of the control center as an example, but not limited thereto. In actual implementation, the transmitting device 10 The number of main flight missile devices 11 can be determined by the user. The control device 12 can be electrically connected to at least one of the transmitting devices 10 and communicate with the connecting portion of the auxiliary warhead assembly 112.

Therefore, when the operator finds that a plurality of objects 2 are approaching, the oncoming route or position is estimated, and as shown in (A), (B), and (C) in FIG. 2, the operator can give the control device 12 The signal 120 is executed such that the control device 12 drives the transmitting device 10 to fire the primary flying missile device 11 toward the target 2 in accordance with the execution signal 120. While the main flight missile device 11 is in a certain flight, or when the primary flight missile device 11 detects proximity to the target 2, the flying missile body 110 is separated, causing the plurality of auxiliary warhead assemblies 112 to be disengaged from the flying missile body 110. Then, the auxiliary auxiliary warhead assembly 112 can receive the control signal 131 transmitted by the control end of the satellite, the drone, the ground radar or the reconnaissance plane, and drive the mesh assembly 111 toward the target 2, and at the same time, the auxiliary auxiliary warhead assembly 112. The mesh components 111 can be deployed in an unfolded state according to the control signal 131, and the plurality of objects 2 can be intercepted by the single mesh component 111, resulting in an imbalance of the enemy's incoming weapon or a delay in action.

Thereby, the inventive flying missile combined with the strong mesh attack system 1 utilizes the design of the multiple warhead combined with the intercepting net to fire the main flying missile device 11 when several foreign intruding objects 2 enter the range of the launching device 10, and After the flying missile body 110 is properly separated, the plurality of auxiliary warhead assemblies 112 are used to drive the mesh component 111 toward the foreign invading target 2 and the mesh component 111 is deployed, thereby intercepting a large number of aliens with a single mesh component 111. Invade the target 2 to improve the effectiveness of the defense and reduce the cost of wear and tear. At the same time, it can also destroy a large number of foreign invading targets in a short time.

In addition, the primary flight missile device 11 can also be replaced by high and low speed aircraft (such as fighter aircraft) that can be used in the air network.

Please refer to FIG. 5 and FIG. 6 , which are respectively a system schematic diagram and a system block diagram of a second embodiment of the proposed attack system of a flying missile combined with a strong quality net, and please refer to FIG. 1 to FIG. 3 together. . As shown in the figure, the attacking system of the flying missile combined with the strong mesh in the present embodiment is similar to the operation of the same component described in the attacking system of the flying missile combined with the strong mesh of the first embodiment, and therefore will not be described herein. However, it is worth mentioning that in the present embodiment, the attack system 1 of the flying missile combined with the strong mesh preferably further includes a detecting device 13 electrically connected to the control device 12, and the detecting device 13 senses the area of the area. At least one target 2 in a to generate at least one detection signal 130. Moreover, the control device 12 can drive the at least one transmitting device 10 to fire at least one primary flying missile device 11 toward the position of the at least one target 2 or the oncoming route according to the execution signal 120 and the at least one detection signal 130.

For example, the inventive flying missile combined with the strong mesh attack system 1 can further be provided with a detecting device 13, such as any air ground radar detecting device, which is electrically connected to the control device 12. Therefore, when the plurality of objects 2 are in the area a of the defense system of the attack system 1 combined with the strong mesh, the detecting device 13 generates the equal detection signal according to the detected number of the target 2 130, and transmits the detection signal 130 to the control device 12 to estimate the target 2's oncoming route or location. Then, the operator can give the control device 12 a signal 120 according to the information of the detection signal 130. At this time, the control device 12 generates the detection signal 130 generated according to the execution signal 120 and the estimated enemy oncoming route or position. The launching device 10 is driven to fire the main flight missile device 11 toward the target 2 to intercept the target 2.

It is worth mentioning that the proposed flying missile combined with the strong mesh attack system 1 can also be provided with a display device (not shown), such as a screen display, to display information of the detection signal 130, such as a conventional radar. Display information.

Further, the detecting device 13 generates at least one control signal 131 according to the path or position of the at least one object 2 . That is to say, the detecting device 13 can predict the enemy target 2 travel route (such as flight path, walking path, etc.), and generate at least one control signal 131. Then, the detecting device 13 can transmit the control signal 131 to the partial auxiliary warhead assembly 112. After receiving the control signal 131, the auxiliary auxiliary warhead assembly 112 can approach the target 2 according to the control signal 131 while being away from each other. The mesh member 111 is brought into an unfolded state, and the target 2 is intercepted by a single mesh member 111.

Further, the attack system 1 of the flying missile combined with the strong mesh preferably further includes an operating device 14 electrically connected to the control device 12, and when the operating device 14 is touched to generate the execution signal 120, the operating device 14 transmits The signal is sent to the control device 120. That is to say, the inventive flying missile combined with the strong mesh attack system 1 can further be provided with an operating device 14, such as an input device such as voice control or touch, which is electrically connected to the control device 12. Accordingly, the operator can generate the execution signal 120 via the operating device 14 and transmit it to the control device 120 to drive the launch device 10 to fire the primary flight missile device 11 via the control device 120. Among them, the operation device of the operation device 14 in different forms can be determined according to the sea, land and air vehicle or the control center installed.

Please refer to FIG. 7 , which is a schematic diagram of the mesh component of the third embodiment of the attack system of the proposed flying missile combined with the strong mesh, and please refer to FIG. 1 to FIG. 5 together. As shown in the figure, the attacking system of the flying missile combined with the strong mesh in the present embodiment is similar to the action of the same component described in the attack system of the flying missile combined with the strong mesh of the above embodiments, and therefore will not be described herein. However, it is worth mentioning that in the present embodiment, the mesh fabric 1100 of the mesh member 111 preferably has a heterogeneous layer 1101. Moreover, when the mesh component 111 intercepts at least one target 2, the heterogeneous layer 1101 is adhered to at least one target 2.

For example, the inventive flying missile combined with the strong mesh attack system 1 can further apply at least one heterogeneous layer 1101 to the metal alloy mesh fabric 1100 of the mesh component 111, as shown in FIG. 6(A). It is shown that the heterogeneous layer 1101 can be an adhesive or a chemically harmful liquid. Therefore, when the target 2 is a living species, the present flying missile combined with the strong mesh attack system 1 can intercept the target 2 by using the mesh component 111, and use the heterogeneous layer 1101 on the mesh fabric 1100 to adhere to the target. Object 2 to limit the ability of the target 2 to move or reduce the vitality of the target 2.

Further, the mesh fabric 1100 of the mesh component 111 preferably has a plurality of bursts 1102. Moreover, when the mesh component 111 intercepts at least one target 2 and at least one target 2 touches at least one bursting member 1102, the bursting member 1102 bursts.

That is to say, the inventive flying missile combined with the strong mesh attack system 1 can also be provided with a plurality of bursting members 1102 on the metal alloy mesh fabric 1100 of the mesh component 111, as shown in (B) of FIG. The burst 1102 can be a bomb. Therefore, when the target 2 is a living species or a land, sea and air offensive weapon, the present flying missile combined with the strong mesh attack system 1 can intercept the target 2 by the mesh component 111 and touch the burst 1102 at the target 2 At this time, the bursting member 1102 is caused to burst, thereby reducing the mobility, vitality or attacking power of the target 2. Or, the bursting member 1102 can contain a sharp object. When the bursting member 1102 bursts, the sharp object can be sprinkled on the warplane of the ship to prevent the aircraft from taking off.

It is worth mentioning that the attacking missile system 1 of the present invention can also provide a damage component such as a spike or a blade on the metal mesh fabric 1100 of the mesh component 111 for the mesh component 111. When the target 2 is intercepted, the action, vitality or attack power of the target 2 can be immediately reduced.

The above is intended to be illustrative only and not limiting. Any equivalent modifications or alterations to the spirit and scope of this creation shall be included in the scope of the appended patent application.

1‧‧‧Attack system of flying missile combined with strong mesh
10‧‧‧ Launcher
100‧‧‧ Launch channel
11‧‧‧Main flight missile device
110‧‧‧ Flying missile body
110A‧‧‧ accommodating space
111‧‧‧ mesh components
1100‧‧‧ mesh fabric
1101‧‧‧Heterogeneous layer
1102‧‧‧Burst pieces
112‧‧‧Auxiliary warhead assembly
12‧‧‧Control device
120‧‧‧Execution signal
131‧‧‧Regulatory signals
13‧‧‧Detection device
130‧‧‧Detection signal
14‧‧‧Operator
2‧‧‧ Targets
a‧‧‧Regional range

The first figure is a schematic diagram of the system of the first embodiment of the attack system of the proposed flying missile combined with the strong mesh. Figure 2 is a first embodiment of the first embodiment of the attack system of the proposed flying missile combined with the strong mesh. Fig. 3 is a second embodiment of the first embodiment of the attack system of the proposed flying missile combined with the strong mesh. Figure 4 is a system block diagram of a first embodiment of the attack system of the proposed flying missile combined with a strong quality net. Figure 5 is a schematic diagram of a second embodiment of the attack system of the proposed flying missile combined with a strong mesh. Figure 6 is a system block diagram of a second embodiment of the attack system of the proposed flying missile combined with a strong mesh. Fig. 7 is a schematic view showing the mesh assembly of the third embodiment of the attack system of the proposed flying missile combined with the strong mesh.

1‧‧‧Attack system of flying missile combined with strong mesh

10‧‧‧ Launcher

100‧‧‧ Launch channel

11‧‧‧Main flight missile device

110‧‧‧ Flying missile body

110A‧‧‧ accommodating space

111‧‧‧ mesh components

112‧‧‧Auxiliary warhead assembly

12‧‧‧Control device

Claims (10)

An attack system of a flying missile combined with a strong mesh, comprising at least one main missile device, which can be located in a launching channel, the at least one main missile device comprising: a flying missile body having an accommodation space; a plurality of auxiliary warhead assemblies respectively disposed on a side of the mesh assembly; wherein the at least one primary flight missile device is fired toward the at least one target and the flying missile When the main body is separated, the plurality of auxiliary warhead assemblies are separated from the main body of the flying missile and approach the position of the at least one target or the oncoming route, and when the auxiliary warhead assembly receives at least one control signal, part of the auxiliary warhead assembly Then moving away from each other, so that the mesh component is in an unfolded state, and the at least one target is intercepted by the mesh component. The attack system of the flying missile combined with the strong mesh according to claim 1, further comprising: at least one transmitting device having the transmitting channel; and a control device electrically connected to the at least one transmitting device, And the communication link portion of the auxiliary warhead assembly, when the control device receives an execution signal, the control device drives the at least one launching device to fire the at least one primary flight missile device toward the position of the at least one target or the oncoming route. The attack system of the flying missile combined with the strong mesh as described in claim 2, further comprising a detecting device electrically connected to the control device, the detecting device sensing the at least one of a range of regions Target to generate at least one detection signal. The attack system of the flying missile combined with the strong mesh according to claim 3, wherein the control device drives the position of the at least one transmitting device toward the at least one target according to the execution signal and the at least one detecting signal. Or the oncoming route fires the at least one primary flight missile device. The attack system of the flying missile combined with the strong mesh according to claim 3, wherein the detecting device generates the at least one control signal according to the path or position of the at least one target. The attack system of the flying missile combined with the strong mesh as described in claim 2, further comprising an operating device electrically connected to the control device, when the operating device is touched to generate the execution signal, The operating device transmits the execution signal to the control device. The attack system of the flying missile combined with the strong mesh according to claim 1, wherein the mesh fabric of the mesh component has a heterogeneous layer. The attack system of the flying missile combined with the strong mesh according to claim 7, wherein the heterogeneous layer is adhered to the at least one target when the mesh component intercepts the at least one target. The attack system of the flying missile combined with the strong mesh according to claim 1, wherein the mesh fabric of the mesh component has a plurality of bursting members. The attack system of the flying missile combined with the strong mesh according to claim 9, wherein the bursting member is when the mesh component intercepts the at least one target and the at least one target touches at least one of the bursting members Burst.