JP2004108738A - Dropping type laying artillery shell - Google Patents

Abstract

<P>PROBLEM TO BE SOLVED: To provide a dropping type laying artillery shell releasing a child shell in air and provided with an inexpensive child shell release device capable of increasing attack precision for a target. <P>SOLUTION: Reflected light of laser beam 35 emitted for the target 36 is received by a detection mechanism part 11 provided in the child shell release device 2 which is released from a flying cargo shell 1 and is descending by obtaining spin movement not by a spin drive engine. A child shell is released from the child shell release device 2 during descent in accordance with a signal level of the received signal. <P>COPYRIGHT: (C)2004,JPO

Description

[0001]
TECHNICAL FIELD OF THE INVENTION
BACKGROUND OF THE INVENTION 1. Field of the Invention The present invention relates to a drop-type aiming shell equipped with a grandchild bullet discharge device used to discharge a grandchild bullet in the air.
[0002]
[Prior art]
Conventionally, as a discharge type ammunition equipped with a submunition as a grandchildren discharging device used to discharge a grandchild in the air, as shown in FIG. There is known a parent-child bullet that emits submunitions 41 in a preset order in a direction orthogonal to the flight direction of the parent-submunitions 40, and releases a grandchild bullet 42 while each submunition 41 is descending (see Patent Document 1). ).
[0003]
Also, as shown in FIG. 14, a large number of secondary emitters 46 are emitted from the flying object 45 in flight in a direction orthogonal to the flight direction, and each secondary emitter 46 is provided to each secondary emitter 46 while the secondary emitter 46 is descending. By rotating the secondary ejector 46 about an axis passing through the center of gravity by a spin motor (not shown), a plurality of submunitions 47 mounted on the secondary ejector 46 are centrifuged by the centrifugal force of the rotational motion. 2. Description of the Related Art There is known an on-board discharge device that discharges in a radial direction by force (see Patent Document 2).
[0004]
Further, as shown in FIG. 15, a system for discharging a weapon 51 for destroying a target 50 from a discharge platform 52 in flight toward the target 50, and guiding the weapon 51 to the target 50, comprising: By emitting a synthetic aperture radar single pulse 53 from the inside emission platform 52 to the target 50, a synthetic aperture laser single pulse map of an area surrounding the target 50 is created, and the target indicated on the map is generated. An additional monopulse map is formed to track the target and remove target position errors due to navigation errors. Thereafter, the weapon 51 is released from the release platform 52, and the guidance command transmitted from the release platform 52 and the reflection of the single pulse 53 released to the target 50 are received by the weapon 51 to control the attitude of the weapon 51. Thus, a synthetic aperture radar single-pulse and inverse single-pulse weapon guidance system has been proposed that flies in an optimal trajectory with respect to the target 50 (see Patent Document 3).
[0005]
However, in the parent and child bullets shown in FIG. 13, in order to destroy the target by the grandchild bullet 42, it is necessary to discharge a large number of the sub bullets 41 to the target. In order to disperse the submunitions 41 in a wide range, the order in which the submunitions 41 are released is controlled in accordance with the flight speed of the parent bullets 40. Only by releasing 42 was it possible to disperse the grandchild bomb 42 over a wide area and destroy the target.
[0006]
Further, in the on-load discharge device as shown in FIG. 14, it is necessary to provide a spin motor in each of the secondary dischargers 46 in order to discharge the submunitions 47 in a radial direction with a predetermined or higher centrifugal force.
For this reason, these devices would cause ammunition to be scattered over a wide area, and were suitable for controlling large areas using large-scale firepower. It has to be done. It destroys things that do not need to be destroyed or dissipates the destructive power of the target. Therefore, a large-scale thermal power was required to destroy the target.
[0007]
In particular, in the case of a widespread decentralized battle in a small-scale inhabited area expected in the future, the dissemination of shells over a wide area will involve the general public. In such a battle, it is necessary to have a child who eliminates variations in the state of impact of the shells and performs a precision attack with high accuracy, and prevention of damage to inhabitants' districts has become an important issue.
[0008]
The arrangement shown in FIG. 15 allows the weapon 51 to be accurately landed on the target 50 by radar guidance, but always controls the trajectory of the weapon 51 with respect to the target 50 by means of the release platform 52. It is necessary to capture the position of an object. In order to emit a guidance signal to the weapon 51 or cause the weapon 51 to receive a reflected single pulse from the target 50, it was necessary to always emit a single pulse from the release platform 52 to the target 50. Thus, the release platform 52 was at risk of being attacked by the opponent during the flight.
[0009]
In addition, such a weapon for guidance requires a wing control device for controlling the trajectory of a target, a seeker for terminal guidance for performing terminal guidance, and the like, and these devices are expensive, and these devices are expensive. It is difficult to deploy large quantities of weapons equipped with such equipment over a wide area. Therefore, the range of use of such a weapon for guidance is limited to a specific target, and the range of use is limited.
[0010]
[Patent Document 1]
JP-A-8-261595 (paragraph [0009] ~
[0012]
FIGS. 1 to 19)
[Patent Document 2]
JP-A-2002-62099 (paragraph,
[0024]
[0034]
[0059]
(FIGS. 1 to 20)
[Patent Document 3]
JP-A-8-210798 (paragraph [0004]-
[0007]
[0010]
FIGS. 1 to 5)
[0011]
[Problems to be solved by the invention]
The present invention has been made in view of the above-described conventional situation, and an object of the present invention is to provide a drop-type aiming ammunition that is inexpensive and has improved landing accuracy.
[0012]
[Means for Solving the Problems]
The above object is effectively achieved by the invention according to each claim of the present application having the following matters.
In other words, the invention according to claim 1 is a grandchild bullet discharging device for discharging a grandchild bullet that is released from a flying cargo bullet and obtains a turning motion not depending on the rotary drive engine and is mounted during the rotation descent. The discharge device has an adjusting means for adjusting a descending trajectory of the descendant bomb discharge device, a control device and a detection mechanism portion, wherein the detection mechanism portion detects a reflected light from a target irradiated with laser. Means for controlling the discharge timing of the grandchild bullet based on a detection value from the detection mechanism unit.
[0013]
According to the present invention, the grandchild bullet discharge device released from the flying cargo bullet is caused to descend in a rotating state while descending after the discharge. The turning motion given to the grandchildren discharge device obtains the turning motion without using a turning drive engine that generates a rotary driving force such as a motor. As a method of obtaining the turning motion, the cargo bullets are caused to perform a turning motion and fly, and the grandchildren ejection device is released behind the cargo bullet in the flight direction, so that the turning kinetic energy of the cargo bullet is transferred to the grandchild bullet ejection device. It can be given as a rolling motion.
[0014]
In addition, when the cargo bullet flies without performing a swiveling motion, the swirling wing or the like is deployed from the grandchild bomb ejection device after discharging from the cargo bullet, and the swirling motion is applied to the grandchild bomb ejection device by the swirling wing or the like. For example, a method of giving a swinging motion to the grandchildren discharging device by a guide member formed in a spiral shape when discharging from a cargo bullet can be used.
In addition, by rotating the grandchildren discharge device by these methods, it is not necessary to mount a rotary drive engine such as a motor for giving a rotary motion to the grandchildren discharge device, and the rotational energy of the cargo bullet can be used. The weight of the grandchild bomb discharge device can be reduced.
[0015]
The detection mechanism unit may be provided on the outer wall of the grandchild bullet discharging device, or may be stored in the grandchild bullet discharging device when the grandchild bullet discharging device is mounted on the cargo bullet, and the grandchild bullet discharging device is released from the cargo bullet. It can also be configured to be deployed outward from the grandchild bomb discharge device later.
[0016]
The timing at which the grandchildren are released from the grandchildren discharge device during the turning descent is detected by the laser detecting means detecting the reflected light of the laser light irradiated on the target from another place such as the ground and detecting by the control device. When it is determined that the value exceeds a predetermined level value, that is, based on the magnitude of the detected value, the grandchild bomb is ignited by explosive charge or discharge medicine for releasing the grandchild bomb. The target can be released from the grandchild bomb release device.
[0017]
The area that can be detected by the laser detecting means is a narrow range around the central axis of the grandchild bomb ejection device, and when the laser reflected light is received within the narrow range, the grandchild bullet is linearly directed toward the target like a bullet. Can also be released. Also in this case, it is necessary to discharge the grandchild when it is determined that the value of the detection value detected by the laser detection means exceeds a predetermined level value.
The discharged grandchild bullets are released according to the type of the grandchild bullet, for example, by a known release method corresponding to, for example, an EFP bullet, a DP-ICM bullet, a grenade, and the like, thereby destroying the target.
[0018]
Also, an altimeter is installed in the detection mechanism, and the release timing is set so that the grandchild bullet is released from the grandchild bullet discharge device only when the altitude of the grandchild bullet discharge device when the reflected light is detected is equal to or less than the predetermined altitude. You can also judge. In this case, if the altitude at the time of detecting the reflected light is high, the reflected light from the next target is detected by continuously rotating the descendant discharge device without discharging the grandchild bullet. When the reflected light from the target cannot be detected, the grandchild discharge device is landed on the ground without discharging the grandchild.
By irradiating each of the plurality of targets with laser light, it is possible to easily detect the reflected light from the targets by the laser detection means provided in the grandchild bullet discharging device that is rotating and descending.
The timing of releasing these grandchildren can be determined by setting the determination conditions in the control device in advance. In addition, tactically possible grandchildren release timing can be set as appropriate.
[0019]
As the adjusting means for adjusting the descending trajectory of the grandchild bomb discharge device, a parachute, a wing, or the like capable of adjusting a predetermined descending speed or maintaining the descending state in a turning state can be used. If necessary, the attitude of the wings can be controlled to adjust the descending trajectory of the grandchild bomb ejection device, or to adjust the number of rotations of the grandchild bomb ejection device.
[0020]
These parachutes, wings, and the like are stored in a closed state inside the grandchildren discharge device or in the outer periphery when the grandchildren discharge device is mounted in the cargo ammunition. It can be configured to deploy after being released from a bullet. A plurality of grandchildren discharging devices are mounted on a cargo bullet, and the plurality of grandchildren discharging devices can be discharged backward in the flight direction at the time of discharge. The number of grandchildren discharging devices mounted on the cargo ammunition can be set to a required number from the relationship of the weight of the cargo ammunition and the like.
As the attitude of the grandchild bullet discharging device during the descent, for example, the grandchild bullet can be rotated downward in the direction of gravity while maintaining the state in which the rotation axis of rotation of the grandchild is inclined at a predetermined angle with respect to the direction of gravity.
[0021]
According to a second aspect of the present invention, in addition to the first aspect, the detecting mechanism further includes an altimeter, and the control device is configured to control the detected value of the altimeter and the detected value of the reflected light received by the laser detecting means. In this case, there is a drop-type aiming shell that restricts the items that control the timing of the release of grandchildren.
[0022]
According to the present invention, when the altitude position of the grandchild bomb ejection device at which the reflected light from the target is detected by the laser detecting means is higher than or equal to a predetermined altitude, even if the grandchild bomb is released from the same position, destruction to the target is possible The power is weakened, and in some cases, it is impossible to break away from the target. In order to avoid such a situation, when it is determined that the altitude detected by the altimeter is within the predetermined altitude and the altitude position corresponding to the type of the grandchild to be released, the grandchild is released and the predetermined altitude is released. In the above case, the grandchild bullet is not emitted, and the reflected light from the next target is detected. As a result, the grandchild can be reliably attacked against the target.
[0023]
The invention according to claim 3 is, in addition to the features of claim 1, a drop-type aiming ammunition in which the adjusting means is provided with a posture control mechanism that deploys outward from the grandchild bullet discharging device.
In the present invention, the adjusting means for adjusting the descending trajectory of the grandchild bomb discharge device is constituted by the attitude control mechanism that extends outward from the grandchild bomb discharge device. The attitude control mechanism includes a wing that is stored in the grandchildren discharge device when the grandchildren discharge device is mounted on the cargo ammunition, and can be deployed from the grandchildren discharge device after the grandchildren discharge device is released from the cargo bullet. , A parachute or the like can be used. The descending posture of the grandchild bomb discharge device can be controlled by adjusting the angle of the wing or the like, and it is possible to adjust a predetermined descending speed, adjust the number of revolutions, and adjust the descending trajectory.
[0024]
According to a fourth aspect of the present invention, in addition to the features of the first aspect, an EFP warhead, a DP-ICM bullet or an EFP warhead that can be selectively mounted in a grandchild bullet storage unit and a grandchild bullet storage unit formed in the grandchild bullet discharge device. This is a drop-type aiming ammunition that limits the items to be formed by unitizing the explosives that discharge the grenade and the like.
[0025]
According to the present invention, an EFP warhead, a DP-ICM bullet, a grenade, or the like can be used as a grandchild bullet to be stored in the grandchild discharge device. The medicine is unitized, and various grandchild bullets can be selectively stored in the common grandchild bullet storage unit. Regarding the release medicine that releases the grandchild bomb, in the EFP warhead, the explosive charge and the facsimile correspond to the release medicine, and in the DP-ICM bomb and grenade, etc., the release medicine is the release medicine that releases the grandbomb here. Equivalent to.
Thereby, the manufacturing cost of the drop-type aiming shell can be reduced by sharing the grandchild bullet storage space in the grandchild bullet discharge device.
[0026]
According to a fifth aspect of the present invention, in addition to the first aspect, the detecting mechanism further includes a detecting unit for detecting an electromagnetic wave generated from a heat source of the target, and the detecting unit detects the detected value input to the control device. The present invention is directed to a drop-type aiming ammunition in which items provided with a switching means for switching between a detection value detected by a means and a detection value detected by the laser detection means are limited.
[0027]
According to the present invention, the detection mechanism is provided with the detection means for detecting the electromagnetic wave generated from the heat source of the target, so that the detection means for detecting the light generated from the heat source of the target when the target cannot be irradiated with the laser beam. Can be used to determine the timing of the release of the grandchild bullet, and when the target can be irradiated with laser light, the timing of the release of the grandchild is determined using the detection value detected by the laser detection means For example, the detection method for the target can be switched according to the situation of the battle scene, and a battle attack can be performed.
[0028]
In addition, two types of shells, such as a shell that detects and attacks an electromagnetic wave generated from a heat source of a target object as a drop-type aiming shell and a shell that detects and attacks reflected light of a laser beam, do not have two types of shells. The attack method for the target can be easily changed only by switching.
Switching means for switching between the laser detecting means and the detecting means for detecting electromagnetic waves generated from the heat source is provided on an outer shell of the cargo ammunition.
[0029]
DETAILED DESCRIPTION OF THE INVENTION
Hereinafter, preferred embodiments of the present invention will be specifically described with reference to the accompanying drawings.
1 to 12 are explanatory diagrams of an embodiment of the present invention. FIG. 1 is a schematic explanatory diagram of a drop-type aiming shell. FIG. 2 is a cross-sectional view showing a schematic configuration inside a cargo ammunition as a parent ammunition. FIGS. 3 to 5 and FIG. 6 show a child when an EFP warhead, a DP-ICM ammunition or a grenade is used as a grandchild ammunition. FIG. 6 shows an arrangement relationship between a grandchild bullet discharge device as a bullet and a grandchild bullet, and FIG. 6 shows an enlarged view of a DP-ICM bullet.
[0030]
In FIG. 1, two grandchildren discharging devices 2 and 2 are released from a cargo bullet 1 discharged from a cargo bullet discharging device (not shown), and a grandchild bullet that is descending after being discharged rearward is shown. The state of the devices 2 and 2 is shown. The cargo ammunition 1 flies while rotating, and ejects the grandchildren discharging devices 2 and 2 from the rear of the cargo bullets 1 at the discharge positions of the grandchildren discharging devices 2 and 2 set in advance.
[0031]
At this time, the grandchild bullet discharge devices 2 and 2 are given a turning motion by the turning motion energy of the cargo bullet 1 and are discharged.
In addition, as a method of giving a swirling motion to the grandchild bomb discharge devices 2 and 2, a swirling wing or the like is developed from the grandchild bomb discharge device after discharging from the cargo ammunition to obtain a turning motion, or when discharging from the cargo bullet. For example, a method of giving a turning motion to the grandchild bomb discharge device by a spiral guide groove or the like can be used. In the method of imparting a turning motion to the grand-bomb-dispensing device, another method may be used as long as the method is such that the rotating motion is imparted to the grand-bomb-dispensing device without mounting a rotating drive engine such as a motor.
[0032]
As shown in FIG. 2, inside the cargo bullet 1, a release agent 5 such as a gas generating agent used to release the grandchild bullet discharge devices 2 and 2 and a bottom plug 3 from the rear, and the release agent An ignition device 4 for igniting 5 is provided. In the igniter 4, the flight time of the cargo ammunition 1 up to the target object and the flight altitude at which the grandchild bomb ejection devices 2 and 2 are ejected before being ejected from the cargo ammunition ejection device are set, and these set values are set. Is satisfied, the ignition device 4 is activated.
[0033]
The grandchild bullet discharge devices 2 and 2 are mounted in rooms partitioned by the pressure plate 6 as partitions. At the rear of the cargo bullet 1, a bullet plug 3 is provided. Inside the grandchild bullet discharge device 2, the shape of the grandchild bullet storage unit 10 that stores the grandchild bullets such as the EFP warhead 20, the DP-ICM 25 bullet, or the grenade 30 and the grandchild bullets and the grandchild bullets that are stored in the storage unit are released. By unitizing the discharged medicine, these grandchild bullets can be commonly stored in the grandchild bullet storage section regardless of the type of the grandchild bullet. Various grandchild bullets can be appropriately and selectively stored in the grandchild bullet storage unit 10 as needed.
[0034]
Inside the grandchild bomb discharge device 2, in addition to the grandchild bomb storage unit 10, a storage mechanism 11 that can be stored and deployed, an attitude control mechanism 12 when the grandchild bomb discharge device 2 is descending, and a signal detected by the detection mechanism unit 11. The control unit 13 that performs arithmetic processing, controls the timing of discharge of the grandchild bullet, and controls the ignition of the discharged medicine for discharging the grandchild bullet from the grandchild discharge device 2, the power supply unit 14, and the grandchild bullet storage unit 10 is covered. It has a grandchild presser 8 and the like.
The grandchild bomb retainer 8 is released together with the grandchild from the grandchild discharge device by a detonating force of a release medicine for releasing the grandchild or a frill.
The grandchild bullet is provided with an explosive 21, an explosive 22, discharged drugs 26 and 31, a pressure plate 27 and the like according to the type of the grandchild bullet stored in the grandchild bullet discharge device 2.
[0035]
As shown in FIG. 3, for example, in the EFP warhead 20, the liner 23, which is a thick disk-shaped metal plate in a normal state, is deformed into a piercing bullet shape by the explosive force of the filing agent 22 and destroys the target. It is a configuration that can be done.
Further, as shown in FIG. 3C, the EFP warhead 20 as the grandchild bullet is configured to have an outer diameter shape that can be stored in the grandchild bullet storage unit 10 together with the explosive charge 21 for detonating the fender 22.
[0036]
As shown in FIGS. 4 and 6, the DP-ICM bullet 25 as a grandchild bullet is released by an explosive 26 for discharging an anti-personnel bomb 28 and the detonating force of the explosive 26 to release the anti-human bomb 28. It comprises a pressure plate 27 and an anti-personnel bomb 28 (see FIG. 6).
The DP-ICM bullet 25 is stored in the grandchild bullet storage unit 10 as shown in FIG.
[0037]
The anti-personnel bomb 28 is discharged through the pressure plate 27 by the gas pressure generated by the combustion of the discharge medicine 26. The released anti-personnel bomb 28 is designed to stabilize its flight at the time of dropping by expanding the ribbon 29, and to explode the filing medicine at the time of impact to scatter metal fragments.
[0038]
As shown in FIG. 5, when the grenade 30 is used as the grandchild bullet, the discharged medicine 31 and the grenade are stored in the grandchild bullet storage unit 10.
As the grandchild bullet, in addition to the above-described grandchild bullet, various grandchild bullets having a conventionally known configuration such as an EFP warhead, a DP-ICM bullet, and a grenade can be used.
[0039]
In the cargo bullet 1, when the igniting device 4 is activated and ignites the discharged medicine 5, gas is generated by the discharged medicine 5, and the pressure plate 6 is pressed by the gas pressure, and the grandchild munition discharge device arranged behind the pressure plate 6 2, 2 and other pressure plates 6 and bottom plugs 3 used as partitions are discharged to the rear of the cargo bullets 1. The discharge timing is performed by the operation of the ignition device 4 in which the discharge timing is set in advance.
[0040]
The projectiles 2 and 2 ejected from the cargo ammunition 1 can adjust the rotation speed and the discharge speed by giving resistance to the rotation speed and the backward discharge speed. 7 is projected (see FIG. 1). It is not always necessary to provide these projections 7 when the speed, the number of revolutions, and the like after the release of the grandchildren release devices 2 and 2 can be adjusted in advance by adjusting the amount of the release medicine 5. Further, after the grandchildren discharging devices 2 and 2 are released from the cargo bullet 1, after the backward speed and the number of revolutions of the grandchildren discharging devices 2 and 2 are adjusted, these projections 7 are removed. By separating from the discharge devices 2, 2, it is possible to prevent reverse resistance from occurring while the grandchild discharge devices 2, 2 are descending.
In the above-described embodiment, two grandchildren discharging devices 2 mounted on the cargo bullets 1 are shown. However, the number of mounted grandchildren discharging devices 2 is not limited to two. A required number can be mounted depending on the size and the like.
[0041]
As shown in FIG. 1, the detection mechanism 11 expands outward while the grandchildren discharging devices 2 and 2 descend, and the wings 15 as the attitude control mechanism 12 expand outward from the left and right. While the grandchild bomb discharge device 2 is descending, the descending posture of the grandchild bomb discharge device 2 can be controlled while giving a turning motion by the wing 15. By providing a mechanism for adjusting the angle of the wing 15, the descending trajectory of the grandchild bomb discharge device 2 can be controlled. Further, as the attitude control mechanism 12, a parachute 16 can be used as shown in FIG.
As the attitude of the grandchild bullet discharging device during the descent, for example, the grandchild bullet can be rotated downward in the direction of gravity while maintaining the state in which the rotation axis of rotation of the grandchild is inclined at a predetermined angle with respect to the direction of gravity.
[0042]
As shown in FIG. 8, the detection mechanism 11 includes an altimeter 17 (a transmission 17a for transmitting a signal to the ground and a reception 17b for receiving a reflected signal from the ground) and a laser. Laser detecting means 18 for detecting reflected light and detecting means 19 for detecting an electromagnetic wave from a heat source of a target are provided. As the altimeter 17, an existing altimeter such as an altimeter that measures altitude by radio waves can be used.
[0043]
The switching means 9 for switching between the laser detecting means 18 and the detecting means 19 is provided in the cargo shell outer shell shown in FIG. The switching signal from the switching means 9 is input to the control device 13 in each of the grandchild bullet discharging devices 2 and 2. Switching from the switching means 9 may be performed mechanically without performing electrical control.
The laser detecting means 18 is for detecting the reflected light of the laser light 35 emitted by the means (not shown) to the target 36 as shown in FIG. 10, and is detected by the laser detecting means 18 as shown in FIG. When it is determined by the control device 13 that the signal level of the reflected laser exceeds the threshold value for the discharge of the grandchild bomb, the explosive 21 and the explosives 26 and 31 in FIGS. By detonating the medicine, the grandchild bullet can be released from above the target object 36.
[0044]
A threshold value is similarly set for the detection value from the detection unit 19 that detects the electromagnetic wave generated from the heat source of the target 36, and the timing of discharging the grandchild bullet can be determined based on the comparison with the threshold value.
Also, according to the value detected by the altimeter 17, the grandchild bullet can be discharged from the grandchild bullet discharging device only when the grandchild bullet discharging device is at or below a predetermined altitude. When the grandchild bullet discharge device is at a predetermined altitude or higher, the grandchild bullet can be released when the next target is detected without discharging the grandchild bullet. In order to detect the laser reflected light and perform such emission control of grandchildren, it is necessary to irradiate a plurality of targets with laser light to generate reflected light.
[0045]
As shown in FIG. 12, the area that can be detected by the laser detecting means 18 and the detecting means 19 for detecting the electromagnetic wave generated from the heat source of the target 36 is a narrow range 37 centered on the center axis of the grandchild bomb discharge device. Can be. At this time, as shown in FIG. 11, since the center axis of the grandchild bomb discharge device is oscillating and rotating by the rotation rotation of the grandchild bomb discharge device, a narrow range on the ground surface is caused by the rotation descent of the grandchild bomb discharge device. The search trajectory 37 searches for a target while narrowing in a spiral shape.
[0046]
When each of the detection means receives a detection value equal to or higher than a predetermined level within a narrow range while searching along this search trajectory, a grandchild bullet is straightened from a grandchild discharge device toward a target like a bullet. It can also be released in a targeted manner.
[Brief description of the drawings]
FIG. 1 is an overall configuration diagram of the present invention.
FIG. 2 is an arrangement configuration diagram in a cargo ammunition. FIG. 3 is an explanatory diagram in a grandchild bullet discharge device when an EFP warhead is a grandchild bullet.
FIG. 4 is an explanatory diagram of the inside of a grandchild bullet discharge device when a DP-ICM bullet is a grandchild bullet.
FIG. 5 is an explanatory diagram of the inside of a grandchild bullet discharge device when a grenade is a grandchild bullet.
FIG. 6 is an enlarged sectional view of a DP-ICM bullet as a grandchild bullet.
FIG. 7 is a diagram showing a modification of the attitude control mechanism.
FIG. 8 is a front view of the grandchild bullet discharging device.
FIG. 9 is a conceptual diagram of an acquisition signal in a detection mechanism unit. FIG. 10 is a conceptual diagram of a laser aiming shell.
FIG. 11 is a view showing the relationship between the rotation axis of rotation of the grandchild bullet launching device and the central axis of the grandchild bullet discharging device.
FIG. 12 is a diagram illustrating a search trajectory in a narrow range.
FIG. 13 is an overall view showing a conventional example.
FIG. 14 is an overall view showing another conventional example.
FIG. 15 is an explanatory diagram of a laser-guided missile.
[Explanation of symbols]
DESCRIPTION OF SYMBOLS 1 Cargo ammunition 2 Grandchild bomb discharge device 3 Bullet plug 4 Ignition device 5 Discharge medicine 6 Pressure plate 7 Protrusion part 8 Grandchild bomb presser 9 Switching means 10 Storage unit 11 Detection mechanism unit 12 Attitude control mechanism 13 Control device 14 Power supply unit 15 Wing 16 Parachute 17 Altimeter 18 Laser detecting means 19 Detecting means 20 EFP warhead 21 Explosive 22 Explosive 23 Liner 25 DP-ICM ammunition 26 Ejector 27 Pressure plate 28 Anti-personnel bomb 29 Ribbon 30 Grenade 31 Ejector 32 Shell 35 Laser Light 36 target 40 parent-submunition 41 submunition 42 grandchildren 45 projectile 46 secondary ejector 47 submunition 50 target 51 weapon 52 emission platform 53 synthetic aperture radar single pulse

Claims (5)

In a grandchild bullet release device that emits a grandchild bullet that is released from a flying cargo bullet and obtains a turning motion that is not dependent on the rotary drive engine, and is mounted during the rotation descent,
The grandchild bullet discharging device has an adjusting means for adjusting a descending trajectory of the grandchild bullet discharging device, a control device and a detection mechanism,
The detection mechanism unit includes a laser detection unit that detects reflected light from a target irradiated with the laser,
The above-mentioned control device controls the discharge timing of the grandchild bullet based on a detection value from the above-mentioned detection mechanism part, The drop type aiming ammunition characterized by the above-mentioned. The detection mechanism further includes an altimeter,
2. The drop-type aiming shell according to claim 1, wherein the control device controls the timing of discharge of the grandchild bullet based on the detection value by the altimeter and the detection value of the reflected light received by the laser detection unit. 3. 2. A drop-type aiming shell according to claim 1, wherein said adjusting means includes an attitude control mechanism for deploying outward from said grandchild bullet discharging device. A unit for discharging a grandchild and a grandchild such as an EFP warhead, a DP-ICM bullet or a grenade that can be selectively loaded into the grandchild bullet storage unit and the grandchild bullet storage unit formed in the grandchild bullet discharge device. The drop-type aiming shell according to claim 1, characterized in that it is formed. The detection mechanism further includes a detection unit that detects an electromagnetic wave generated from a heat source of the target, and a detection value input to the control device is a detection value detected by the detection unit and a detection value detected by the laser detection unit. 2. A drop-type aiming ammunition according to claim 1, further comprising switching means for switching between (a) and (b).

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