TW200412418A - Projectile for radially deploying sub-projectiles - Google Patents

Abstract

A projectile (10) for firing from a barrel, said projectile including a multiplicity of barrel assemblies (12, 13, 14) radially disposed from the centre of mass of the projectile, wherein each of said multiplicity of barrel assemblies includes a plurality of sub-projectiles (16) axially disposed within a barrel; each of said sub-projectiles associated with a discrete propellent charge (17) for propelling a respective sub-projectile from the barrel, wherein said projectile is capable of selectively firing sub-projectiles (16), suitably with the aid of primers (18) each coupled to an electronic controller (15), to provide a predetermined pattern of deployed sub-projectiles. A defence system employing projectiles of the type described is also disclosed, together with a method for disguising the launch location of a projectile utilising divert propulsion.

Description

200412418 (Explanation of the invention (the description of the invention should state the technical field of w, the prior art, the content, and the implementation of the eighth description) [Technical Field of the Invention] The present invention relates to the dispersal of objects with the essence of a projectile. In particular, 5 but not limited to the method of forming a predetermined type of diffused cut-off projectile by using the main projectile projectile and a projectile projectile for hiding the launching position of the projectile projectile. ι C prior art] BACKGROUND OF THE INVENTION 10 & By using a projectile containing explosives as a splitting device to disperse a plurality of lobes, in a simple form, the shell of this projectile shard is fragmented when the explosive is detonated, making the shell Individual lobes of radioactive radiation spread out to form a splitting pattern that is slightly spherical. In other groups, you can also change the shape of the medicament and the configuration of the shell to control the 15-type split type, but this split projectile produces a thin shell-like split shell type ’so it needs to be able to increase or control the split depth. These projectiles may be particularly suitable for defending a designated area, to prevent this area from becoming dangerous after the threat situation is lifted (such as in the case of a conventional minefield). Existing defenses against external attacks include systems for acquiring and monitoring the trajectory of objects including flying objects such as missiles and rockets. Examples of trajectory acquisition and monitoring systems are described in the United States by Boeck et al. Patent No. 4,622,458 and U.S. Patent No. 5,960,009, No. 412418 of Pfeiffer et al., Description of Invention Recently, for bullets that include throwing or throwing targets at higher firing angles (such as the characteristics of mortars) The threat precision defense device can be obtained from the projectile's track-the position of the projectile launcher can be used to calculate the source of the attack. 0 [^^ 明明] SUMMARY OF THE INVENTION The projectile of the present invention is suitable for the first type. Shot from a barrel to intercept and destroy invading missiles, especially high-altitude ballistic missiles. In a second form, the present invention provides a method for intercepting a missile, which method comprises the following steps: the path of a gas bomb; the path of a projectile of the type described herein is injected into the missile; And firing the selected secondary projectile to form a predetermined type of secondary projectile in and near the determined missile path. The projectile of the present invention can be used to defend the vehicle itself. A vehicle that has been attacked by a particularly private attack may shoot a projectile of the type described here at 15 attackers and spread the secondary ejection in a predetermined pattern among the attackers. body. In the third type, the present invention provides a method for self-defense of a vehicle against attack force. The method includes the following steps: determining the position of the attack force; and projecting a projectile of the type described here toward a predetermined position of the attack force; and The selected human projectile is fired to form a secondary projectile of a predetermined type in and adjacent to the predetermined position of the attack force. The projectile of the present invention can be used to drive the infantry forward. In the fourth form, the present invention provides a method of driving back infantry. The method includes the following steps to determine the position of the father eight, and at least one of the types described here will be ejected. The projectile is fired at the determined infantry position, and the selected secondary projectile is fired to form a predetermined type of secondary projectile in and near the determined 200412418, invention description. The projectile of the present invention can be used to form an air transport image, such as a firework. In a fifth form, the present invention provides a method for forming an air transport image. The method includes the following steps: project a projectile of the type described herein into 5 air; and projecting a selected sub-projectile including the image forming object to form a predetermined type of image forming object in the air. The projectile of the present invention can be used for firefighting in the sixth form. The present invention provides a method of firefighting, which includes the following steps: determining the location of the fire field; shooting at least the projectile of the type described here to the determined Fire field position 10; fire selected secondary projectiles to form a predetermined type of secondary projectiles in and near the predetermined position of the fire field; and disperse a fire extinguishing agent from the projectile. The projectile of the present invention can be used to generate a fuel_air explosion. In the seventh type, the present invention provides a method of generating a fuel_air explosion. This method includes the following steps: · Selecting the required fuel_air explosion position, -Shooting at least one projectile of the type described here towards a fuel-air explosion location; firing a selected secondary projectile including a fuel to form a predetermined type of secondary projectile; dispersing fuel from the projected secondary projectile; The ejection includes detonating a secondary projectile selected to form a predetermined type of secondary projectile; 20 detonating the detonators to generate a fuel-air explosion. The projectiles of the present invention can be used to spread a variety of different payloads. In the eighth 3L, the present invention provides a method of spreading payloads. This method includes the following steps: selection-the ideal transport position of the payloads; will be described here Type at least-projectiles are projected adjacent to the payload; projecting the projectile including the payload sill, the selected secondary projectiles of the invention to form a predetermined type of secondary projectiles; and dispersing the projectiles from the projectile Payload. The projectile of the present invention can be used to prevent purple-designated areas. The ninth form / the present invention broadly relates to a defense system for preventing purple-designated areas. The defense system includes: at least-a monitor for monitoring Designate an area to detect any areas where new objects appear; anti-π devices that are sufficient to attenuate personnel appearing anywhere in a specified area far away, where the purple-proof device includes a weapon capable of projecting projectiles, of which A bobbin assembly including an array of reduced bombardment radioactive arrangements, each bobbin assembly has a plurality of secondary or secondary projectiles arranged axially in the bobbin, the secondary ejection system and a mechanism for advancing the tube from the bobbin. The secondary propulsion agents of the secondary projectiles are coupled together, wherein the tube assembly of the array is capable of selectively ejecting the secondary projectiles from the selected tube, whereby the projectiles can disperse a predetermined type of secondary projectiles; and, A communication device that provides communication between the monitor and the anti-violet device to trigger selective activation of the defense mechanism to deliver the weakening attack to the monitored monitor system, including deployment in a designated area One or more of the local sensors or remote sensors are located away from the shirt area, or the monitoring device may include both the local sensors and the remote sensors. The monitoring device can also provide a visual display of one of the designated areas to be monitored, so that the manual compulsory control device can be actuated as needed to control the fixed defense device manually. τ σχ shows 12418 玖, description of the invention can be shot from a plurality of bobbins at the same time or from a single bobbin to quickly and continuously shot individuals, and or-people? Early shots' These configurations make it possible to carry the signal to the outside of the bobbin Or carry it through the superimposed secondary projectiles, the superimposed secondary projectile systems are clamped on top of each other to continue through the circuit of the bobbin, or produce electrical contact against each other 5. The secondary projectile may carry a control circuit or may form a circuit with the bobbin. The array of bobbin assemblies can be configured adjacent to the leading or trailing end of the projectile, so as to change the attitude of the projectile, or cause the projectile to move laterally in the middle. Alternatively, the 'direction control system may include a bobbin assembly in an array adjacent to both the leading end and the trailing end of the projectile. The array or the bobbin assembly of each array can shoot a projectile once in a direction with a longitudinal component to increase the kinetic energy of the projectile, or once in a direction that has a component that is tangent to the longitudinal axis of the missile The projectile thus transfers or changes the rotation of the projectile about its longitudinal axis. The bobbin assembly 15 can shoot a secondary projectile (such as a wing) across the flying surface to trigger a step-by-step manoeuvre effect on the projectile. Alternatively, the tube assembly can extend through the airfoil surface to project in both directions, which may add structural strength to the aerodynamic design. If necessary, a separate or opposite array tube assembly is provided to control the rotation of the projectile around the longitudinal axis of the projectile. The configuration of the array may include relatively paired bobbin assemblies which are shot simultaneously to change only the rotation about the longitudinal axis of the projectile. The secondary projectile can be selectively actuated before and / or after the directional control system ejects the secondary projectile, thereby canceling or using these projectiles to rotate about their longitudinal axis. Effect on the projectile 10 200412418 发明, invention description should be 0 In certain embodiments of the present invention, the energy required to change the attitude and / or flight direction of the main projectile may be provided by firing secondary projectiles from one or more selected barrel official assemblies. 5 According to a second form of the present invention, a method for concealing the launching position of a projectile launcher is provided. The method includes the steps of discharging at least one projectile from a barrel official assembly, the tube assembly having A bobbin, a plurality of projectiles arranged axially in the bobbin to operatively seal the bore diameter of the bobbin, and separate propellants for sequentially pushing the respective projectiles through the nozzle 10 of the bobbin, and The at least one projectile is in a flying state, and at least one projectile is fired from a steering propulsion assembly of an included array, and each steering propulsion assembly has a plurality of secondary projectiles axially disposed in a steering propulsion tube. The secondary ejection system is connected with a secondary separation propulsion agent used to sequentially advance the secondary projectiles such as σH from the steering propulsion tube. The 15-array steering propulsion tube assembly can propel the tube from the selected steering propulsion tube. The secondary projectile is selectively fired, whereby the reaction force generated by the firing action of the secondary projectile is used to accelerate the projectile. Because the secondary ejection system is a mass that can be resisted by the secondary propellant and exerts a reaction force on the rear barrel of the steering propulsion tube, the overall shape of the secondary ejection body is not important. In the current form of the present invention, the tail bore can be formed by sealing the subsequent secondary projectiles remaining in the bobbin to the bore of the steering propulsion tube, and the reaction force is transferred from the secondary or steering swelling of the protuberance tube. To the projectile and cause it to accelerate.

20 The barrel assembly of this array can present a radioactive configuration from the center of mass of the projectile. 11 200412418 发明, description of the invention ‘This mi system of the barrel assembly is suitable for objects that do not include the propulsion system in flight’, that is, rockets and missiles. When ejecting a secondary projectile, it is only necessary to make the ejection position similar to the ejection system. The part other than ㈣1 is the apparent trajectory. The present invention is particularly applicable to area rejection systems where the area is bombarded by projectiles fired from, for example, mortar bases. It will be understood that the present invention can also be applied to camouflage the launching position of other projectile launching or ejection systems. For a preferred implementation, it may be selected to transfer the firepower from the launcher 10 to other empty mine locations. The projectiles of the present invention preferably use bobbin assemblies of the type described in international patent applications PCT / AU94 / 00124 and PCT / AU96 / 00459. These bobbin assemblies include a bobbin; a plurality of secondary projectiles , Which is arranged axially in the bobbin to operatively seal the bore diameter of the bobbin, and uses 15 in order to propel the separate projectiles through the mouth of the bobbin to separate the propellant. -Human projectiles may be round, traditionally shaped or dart-shaped and their fins may be offset to produce a suspected C 疋 carrying secondary projectile when the dart is advanced from a bobbin that may be a smooth bore tube The projectile may be approximately 20 cylindrical, oval, or spherical, if desired.

The propulsion agent may be formed as a solid block for the secondary projectile in the operational isolation tube, or the propulsion agent may be enclosed in a metal or other rigid shell, which may include an embedded detonator having The external contact device is adapted to contact a pre-inserted electrical connection 12 玖, invention description contact 4 connected to the bobbin. For example, the detonator can be provided with a spring contact, which can be retracted to insert the loaded medicament into the bobbin and pop-up into the opening of the bobbin to operatively contact its docking when aligned with the opening. Tube contact. 5 Peripheral kits can be incineration of expendable or chemically assisted propellants, as required. , And can provide an assembly of medicaments and sub-projectiles that are stacked and combined or dispensed to refill a tube. Each secondary projectile may include a head and an extension device for at least partially delimiting a propellant space. The extension device may include a spacer assembly that extends backward from the head and abuts an adjacent The secondary projectile assembly 10. " The spacer assembly can extend through the propellant space and the head to transfer compressive load directly through the adjacent adjacent spacer assembly. In these configurations, the spacer assembly can be used for thin cylinders that may be the head One extension at the rear of the shape adds support. Also, the extension device may make an operational sealing contact with the bobbin aperture to prevent incineration from leaking through the secondary projectile. The spacer assembly may include a rigid collar that extends outward to engage a thin cylindrical rear portion of a malleable head and that non-operatively sealed contact with the bobbin aperture is provided for axial compression The load is transferred directly between the spacer assemblies to avoid ductile head deformation. 20 Complementary wedge surfaces can be placed on the spacer assembly and the head, respectively, and in response to the relative axial compression between the spacer and the head, the head is driven into engagement with the bobbin bore. In this configuration, the head and the spacer assembly can be installed in the barrel f and ensure a good seal between the secondary projectile and the barrel after causing an axial displacement. It is also suitable for driving the extension device into the joint effect with the bobbin aperture 13 200412418 发明, description of the invention. The head may define a push-shaped opening at its rear end, and a complementary push-type socket located at the leading end of the spacer assembly is accommodated in the opening, where the head and the complementary push-type socket are Relative axial movement will cause a 5-direction expansion force to be applied to the secondary projectile. The bobbin may be non-metallic and the bore diameter of the bobbin may include a recess that can be used to contain the ignition device in a rude or sullen manner. In this configuration, the bobbin system accommodates the electrical conduction control device and the ignition device. Electrical conductor, this configuration can be used in a disposable bobbin assembly with limited injection life, so 10 ignition devices and one or more control lines can be made integrally with the bobbin. A bobbin assembly may additionally include an ignition opening in the bobbin, and the ignition device is arranged outside the bobbin and adjacent to the opening.

A printed circuit stack for an ignition device.

After the actual loading work, the load located in the barrel is applied, or the negative cut swells for 20 months. It may be fixed on the cylindrical part where the secondary projectile and the propellant are installed. 14 200412418 发明, description of the invention May come from an external secondary projectile. Carcass special-the rear end of the projectile of the adjacent outer projectile may include a skirt located in a recessed area Zhouyuan 5 such as a conical recess or a part of a spherical recess The projectile's propellant extends into this recess and the backward movement of the secondary projectile around this recess will cause the radial expansion of the secondary projectile. This backward movement may be due to the secondary projectile moving along the leading part of the propellant One of the occurrences of the shrinkage of ❹ 10 15 20 Π may also occur because the metal flows from the relatively «large-differential part of the subprojectile to its smaller ㈣. Alternatively, a one-person projectile may be provided with a peripheral sealing protrusion that diverges backwards or the shaft is flexed outward to engage with the aperture / push-sealed type when the secondary projectile moves backwards. Also, it is possible to insert the secondary projectiles into a heated cylinder and this Yasuo contractor seals in the rows of the secondary projectiles. The secondary projectile can scoop people, 1: 1 dagger 3 is a harder mandrel part, the mandrel part is positioned by the propellant and formed with a deformable annular p-port that may be molded around the mandrel— Early ejection sub-projectiles, this time the projectile ㈣㈣ ““ __ metal flow expands outward relative to the mandrel to produce a tight joint with the bobbin bore. The human projectile assembly may include—the drill surface that bulges later And a sealing collar is supported around and around 'This sealing collar is suitable for controlling the direction expansion when the secondary projectile moves through the bobbin to cause a sealed state with the bore diameter.' Leading part. "A round ejection system with a flat end face of 4㈣, may be suitable for seating and / or positioning in a circumferential groove or 15 200412418 玖, invention description through the annular rib in the hole ^ or the fracture in the hole The groove is positioned, and a metal sheath covering at least the outer end of the secondary projectile is mouthed. The secondary projectile can sigh with a retractable peripheral positioning ring. The retractable peripheral positioning ring extends into the annular groove in the bobbin and retracts into the reading body when it is fired to freely. Through the bobbin. 10 actuated. It is suitable to insure all propulsion agents in a loaded bobbin end point by inserting separate insulation leads located between normally closed electrical contacts. Μ The electrical ignition used to sequentially ignite the propulsion agent of the barrel assembly may preferably include the following steps: transmitting an ignition signal through the stacked secondary projectiles to ignite the leading propulsion agent and ignite the leading propellant By opening the insurance order, the next propellant can be applied by the next ignition signal, and the propellant can be ignited electrically, or it can be ignited by a conventional firing pin method, such as using a central ejection detonator to charge the outermost 15 projectiles. Ignition and controlled ignition will cause sequential ignition of the propellant in subsequent rounds. This can be achieved by controlled backward leakage of the combustion gas or by controlled incineration of a fuze post extending through the secondary projectile. In other embodiments, the ignition is controlled electrically, wherein each of the pushing agents is connected to a detonator triggered by a different ignition signal. For example, the detonators in the stacked propulsion agent can be sequenced to increase the pulse width ignition condition, whereby the electronic controller can selectively transmit the ignition pulse with increased pulse width to sequentially ignite the propulsion agent at a remote timing. However, preferably, the propulsion agent is ignited by a set pulse width signal, and the leading propellant 16 200412418 玖, the incineration of the invention illustrative agent will cause the next propulsion agent to open the insurance of the insurance room for the pulse issued To actuate. In these embodiments, it is suitable to insert a separate insulated fuze between the normally closed electrical contacts to insure that all the propulsion agent in the loaded bobbin end point is insured. The incinerator is sufficient to close the contact when transmitting an appropriate trigger signal, and to cause the m-edge fuze to open for a respective lead propulsion agent for ignition. In a specific embodiment, the bobbin assembly may belong to a low-pressure type used to eject a grenade-like secondary projectile. Each of the bobbin assemblies may be loaded with different secondary projectiles and the bobbin assemblies may have different sizes of apertures. To accommodate different sizes of secondary projectiles. Each secondary projectile is suitable to include a-tail collar, which is trappedly mounted to the secondary projectile body and extends backwards when stored in the bobbin to wedge against a rear secondary projectile body The head of the nose. A shallow wedge is suitable for providing this wedging effect, so when in use, the tail end of the collar expands to produce an operationally sealed joint with the bobbin. The tail end collar can be installed to have limited axial movement relative to the body of the secondary projectile, and the leading end of the collar is provided with an annular sealing surface that can be joined to the body of the secondary projectile A complementary surface is formed, so the 20 backward movement of the projectile body due to the reaction force of the propulsion gas on it will force its complementary surface to seal tightly with the annular sealing surface at the leading end of the collar .

10

The complementary surface and the annular sealing surface may extend substantially radially and have complementary sealing characteristics formed thereon. But these surfaces are preferably complementary part conical 17 200412418 玖, description of the invention The sealing surfaces are wedged to each other to form a tight sealing joint, and the leading end part can also expand to produce an operational sealing joint with the bobbin. However, the wedging effect between some conical surfaces is suitable for steeper hills, so the clamping effect does not expand the leading end of the collar and operatively engage the bobbin. 5 纟 For low-pressure applications, it is preferred that each projectile can be connected to a high-pressure propellant chamber. This high-pressure propellant chamber is exhausted to a low-pressure propellant chamber formed between adjacent subprojectiles to produce an efficient Low nozzle speed operation. The high-pressure propellant chamber may be integrally formed with the body of the secondary projectile or the tail end collar, or may be provided outside the bobbin to conduct conduction through a port passing through the bobbin wall. 10. The space configuration and propellant properties that can propel the propellant propagating into it are suitable for use with only low bobbin pressures, such as pressures around 20 Torr to 5000 pS1. In general, the collar in its relaxed position will not prevent the projectile from moving freely through the barrel for filling purposes or during ejection. 15 A pressure pad is mounted on the housing inside the open tail end. The collar is repositioned from the engaged state when the propellant is ignited and held in the released state by the pressure pad to pass through the tube and leave the tube orifice. The projectile can be of a conventional type and can be ejected in a conventional manner, and preferably can be ejected from a cymbal assembly. This bobbin assembly includes a plurality of projectiles arranged axially in a bobbin 20, each of which The ejection system is coupled to a propellant used to separate one of the projectiles from the bobbin. In a preferred form, the projectile may be approximately spherical and have a plurality of barrel assemblies having a self-spherical mass center in a radioactive configuration. The bobbin assembly can be the same or different. For example, a large-diameter bobbin can be configured from the center of a ball projectile 18 200412418 玖, description of the invention: =, the diameter of the bobbin can be ^ located in the larger projectile_max The density of ㈣㈣ is based on the largest tube filling density in the net supply, so two === body lifts are provided on the projectile to provide a variety of different μ projectiles with the same card diameter. The body hole can be made into a soft shell projectile with a variety of non-ejective bodies in order to facilitate dispersal. Γ is made into a more convenient shape in a soft shell way to be set out from, for example, the conventional arsenal. Or, it is necessary to provide an increased nozzle velocity. Its projectile can accommodate an increased propulsion agent without requiring an excessively long sheet opening length. By using a tube assembly that is radioactively arranged from the projectile's center of mass, it is possible to allow the projectile to spread out the secondary projectiles in a regular and easily controlled manner. The tube assembly of the self-ejecting f's center of mass is radioactively configured to keep the projectile in its posture. By arranging the secondary projectile 15 with zero reaction force on the projectile, the projectile can maintain the required track. Multiple shots can be shot at the same time or in rapid succession. In these configurations, the electrical signal can be carried to the outside of the bobbin or with a secondary shot system that is overlaid by overlapping secondary shots. Continue through the circuit of the bobbin, or make electrical contact against each other. The secondary projectile can carry 20 control circuits or form a circuit with the bobbin. The projectile of the present invention can disperse the secondary projectiles according to a predetermined type selected for a specific application. For example, in order to intercept and destroy invading missiles, it is necessary to increase the possibility of the missiles colliding with one or more secondary projectiles. To spread out the secondary projectiles. A split system has been used in the path of an invading missile. 19 200412418 玖, the description of the invention W-scattering projectiles, but systems such as exploding the projectiles-generally produce a series of scattered formations-expansion ball shells-a series of lobes, The projectile may diffuse the sub-dancing projectile of the present invention in a more homogeneous manner in the overall space occupied by the predetermined pattern. By controlling the firing timing of the secondary projectiles, it is possible to establish three-dimensional "flags," which have a substantially homogeneous distribution of secondary projectiles. Or, 'the secondary projectiles can be set in areas where they are more likely to intercept missiles, The effectiveness of secondary projectiles scattered by Zengnan. Secondary projectiles may include materials used to form airborne images. Image-forming materials may include, for example, external explosives, combustibles, incandescent or luminescent materials or 10 other materials used to provide Substances that are highly visible temporary images. Alternatively, image formations may include such materials as fumes, gases, particles or flakes or strips that have the nature of metallic maggots, or other materials that can spread to form an image. Therefore, the present invention may be advantageously used The projectile fires countermeasures from military aircraft, and the image formation can also include devices such as parachutes and the like for slowing down the speed of the self-dispersing position. The secondary projectile can be configured in the tube assembly so once it is fired After the image formations are dispersed, the required temporary air transport image is formed. Different image formations (with different Color or form) the secondary projectiles are sequentially loaded into each barrel assembly. For example, the image formation can be diffused by the external explosion device, stored energy or the separable A-piece of the secondary projectile to expose the image The formation, or using any other suitable dispersing device. The image formation may be contained within a housing, which may have any suitable configuration to enclose the image formation and be properly configured to engage a previous ejection 20 200412418玖, the tail end of the expandable collar of the invention description body. This casing has a lower shape than the type used by the dislocation rod system as a grenade-like projectile, but it also has a long casing. Projectile. The housing may be adapted to be formed from a biodegradable material and / or a flammable material, which may be based on a natural product such as wood chips or a synthetic material such as a biodegradable polymer 1520. . The projectile of the present invention is preferably capable of spreading out the selected secondary projectiles to control the distance of the projectiles. This spreading effect is known to possibly be a steering propulsion system and can be used to implement limited correction of the position of the projectiles to spread out in the required form The remaining secondary projectiles. The projectile of the present invention can be suitably used in an anti-violet system of one of the types described in the applicant's international patent application PCT / AU00 / 0 i 3 51. Brief Description of the Drawings In order to better understand and actually implement the present invention, reference is now made to the accompanying drawings showing preferred embodiments of this month, wherein, Figure 1 is a preferred embodiment according to the present invention- A cross-sectional view of a projectile; $ 图 2 is a view of a soft shell projectile used in a barrel official assembly with a plurality of axially arranged soft shell projectiles; FIG. 3 is a view shown in FIG. 2 Sectional view of the firing mode of the soft shell projectile; Figure 4 I a ^. I _ Figure; Figure 4 is a side view of the m system according to another embodiment of the present invention Figure 5 is a defense system of another embodiment Perspective view 21 200412418 玖, description of the invention

[Implementation of the preferred embodiment I] FIG. 1 shows a projectile 10 including six large-bore bobbins 12 with convenient clamping diameters, but only four large-bore bobbins are shown in this cross-sectional view, and the remaining 5 two Each large-bore bobbin (extending perpendicularly to the paper surface) is labeled n, and the cross-sectional view also shows four medium-bore bobbin 13 having a medium card diameter, and 48 small-bore bobbin 14 having a small card diameter. As shown in the figure, each of the large-diameter 12, medium-diameter 13 and small-diameter 14 bobbins includes a plurality of axially disposed secondary projectiles 16. The secondary projectile is connected with the propulsion agent 17 and the ignition device 18, and the ignition device 10 can be sequentially fired under the control of an electronic controller 15. In some embodiments, the projectile 10 may also include an explosive for terminal detonation. In this embodiment, the electronic controller 15 disposed at the center of the projectile 10 at the rear of the tube U, 12 may include a sensor for tracking an invading missile during flight. Alternatively, the electronic controller 15 may pass A communication link receives an ejection instruction from a 15 backtracking station, thereby coordinating the sequential ejection of several projectiles to improve the possibility of collision with a target's invading missile or similar threat. Fig. 2 shows a projectile having a soft shell 20 and belonging to the type shown in Fig. 1, with the secondary projectile omitted for clarity. The projectile body 10 is held in a bobbin within a soft 20 shell 20, and the soft shell system includes a front soft shell part 2 丨, a rear soft shell part 22, and a rear chamfer disposed at the rear soft shell part. One of the expansion sleeves 2 3 'around the surface 24 is located in front of the front soft shell portion 21 and the detonation and ejection of the propellant will force the rear soft shell portion 22 against the expandable sleeve 23 and cause the expandable sleeve to seal the joint. The aperture of a main bobbin. 22 200412418 发明. Description of the invention Fig. 3 shows a series of projectiles 10 ejected from a main bobbin assembly 30. The main bobbin assembly 30 has a plurality of main bobbins 31, 32 and 33. The projectile 10A has been ejected from the bobbin 33 and its soft shell (not shown) has been ejected, the ejection body 108 has been ejected from the 4 tube 32 and the soft shell 20 has been discarded in the figure. The expandable sleeve 5 23 has been The rear soft shell 22 and the rear soft shell 22 have also been detached from the projectile 10B, the front soft shell 21 has been similarly detached from the projectile 10B, and the projectile 10c has been ejected from the bobbin 31 and softened later. The shell 20 has begun to disengage from the projectile 10c. Referring to Figures 4 and 5, it has been seen that a field sensor 41 that is receiving defense is monitored by a field sensor 41 distributed in an array of the entire specified area. These 10 sensors may be pressure type, sound type, or vibration Type sensor and any suitable type. The weapon used in the defense system 42 shown is in the form of a pair of grenade boxes 43. Each of the right bomb boxes 43 uses a bobbin assembly 30 and is transferred to a remote sensing device 44 and a connection to the field sensor 41 The receiver unit 49 selects the type of the secondary projectile required according to the nature of the invader. Intruders entering the designated area 40 may be one of any of several forms and may include military personnel in the form of a plurality of invaders, such as soldiers. Alternatively, the intruder may be a manned or unmanned vehicle such as an armored vehicle or an L.K vehicle, and the intruder may have a sophisticated anti-violet system that can track the trajectory of 20 guns and calculate the position of the launching device to attack the previously hidden Launching device. The anti-purple system of this embodiment can turn the projectile's trajectory during the flight by transmitting the secondary projectile, so it can only track-view the trajectory and hide the true position of the launching device. If circumstances permit,

The invader may be an infantry or an invader, and may choose to direct enemy fire against the defense system 42 to other enemy positions. 23 200412418 Although the above-mentioned defense system is based on land, another form of the present invention relates to projectiles that may be referred to as mines. These mines can be launched from ships and kept floating in the water, and remotely controlled by ancient orders + & m & Way or start by spontaneous operation including radar, sonar or infrared sensor system, configurable-track to contain mines defense lines such as suspension weight code, etc. to provide-a way to activate or deactivate as required Water with perimeter defense. In another layout mode, the projectile of the present invention can be dropped from an aircraft such as a helicopter, and a stabilizing or stinging device such as a spear can be provided to fix the position where the 105 early projectile is held on the ground. The secondary projectile may include a sensor system for launching to detect the presence of enemy forces or vehicles, and may be used to engage enemy forces or to rely on subsequent layers of puppets in the respective barrels of the projectile. The vehicle can provide other sensors in other layers to investigate the engagement results. 15 20 The projectile of the present invention can be carried into space as needed and sent to a planet: in the guideway around the satellite, it actually contains an artificial satellite . Because the tube and tube assembly can be radioactively dispersed in a generally spherical body, it can be reported to effectively deploy another mold; cut, provide-a projectile with a size of convenient material reduction, similar to the conventional hand division. However, if a secondary projectile is included in the barrel of the by-pass projectile, the system will use money-a preset time delay or a remote control device to be used in repeat mode, which can save money in areas such as street battle or cave terrain. Provides specific advantages in the event of an engagement. The secondary projectile can contain non-lethal ammunition and a warning audio system. Perhaps in a confrontation situation, if the gangster does not surrender immediately, additional ammunition can be issued. 24 200412418 The invention explains how to correct the position of satellites in orbit, protect an area around a precious satellite from space debris, meteorite and the like, or connect with an enemy space vehicle or satellite war. Because of the energy liberated from the gas burst of a solid subprojectile instead of a traditional artificial satellite, 5 position changes can be made much faster in low-gravity environments. Appropriately constructed satellite catapults can be consumed by burning when the channel re-enters the atmosphere. In a specific form, the artificial satellite may include a super projectile, and the super projectile may disperse the 10 projectiles of the present invention from the tube assembly in which it is radioactively arranged, and these diffuse projectiles may themselves be equipped with secondary projectiles In order to provide a first-order defense system, this second-order defense system can of course be used in other applications with appropriate scale. Of course, it is understood that the above is only an illustrative example of the present invention, and all such modifications and 15 variations deemed to be within the broad scope and spirit of the present invention by those skilled in the art are defined by the scope of patent application. [Schematic diagram * simple and clear] FIG. 1 is a cross-sectional view of a projectile according to a preferred embodiment of the present invention; FIG. 2 is a tube 20 in a soft shell projectile having a plurality of axial arrangements; A cross-sectional view of a soft-shell projectile used in the assembly; FIG. 3 is a cross-sectional view of the firing mode of the soft-shell projectile shown in FIG. 2; and FIG. 4 is a view of a defense system according to another embodiment of the present invention. Side view; FIG. 5 is a perspective view of a defense system according to another embodiment. 25 200412418 发明, description of the invention [representative table of the main elements of the drawing] 10, 10, 8, 106, 10 (: ... projectile 23 ... expandable sleeve large-bore bobbin 24 ... angled rear surface 13 ... medium-bore bobbin 30 ... main bobbin assembly 14 ... small-bore bobbin 31,32,33 ... main bobbin 15 ... electronic controller 40 ... specified area 16 ... second ejection Body 41 ... Field sensor 17 ... Propellant 42 ... Defense system 18 ... Ignition device 43 ... Grenade case 20 ... Soft case 44 ... Remote sensing device 21 ... Front soft case portion 49 ... Receiver unit 22 ... rear soft shell portion 26

Claims (1)

200412418 The scope of application and patent application 1 ·-a kind of bullet for the target launch ^ ^ 4 projectiles include: a number of tube assembly, which is radioactive configuration from the center of mass / sweat body's The multiple ejection bodies in a tube of the majority of the tube assembly are connected to each of the ejection systems and are connected to a propulsion agent used to advance from the tube-one of the separate ejection bodies. Sister, tu… wherein the projectile energy »k Selectively ejects the secondary projectile to raise the primary projectile. ~ 型 的 散发 的 ίο 15 2. If the projectile of item * of the scope of patent application is applied, the projectile is suitable to be ejected from a barrel. 3. For the projectile of item 2 of the scope of patent application, the plurality of times are axially arranged in the bobbin to operatively seal the bore diameter of the bobbin. The projectile of any one of them is roughly as in the case of the patent application scope of items 1 to 3, and has a plurality of bobbin assemblies that are spherical and have a main projection configuration from the center of the ball. & ^ The projectile in the scope of patent application No. 4 has a plurality of different barrels S, thereby utilizing secondary projectiles having a variety of different card diameters. 6. For the projectiles in the scope of patent application No. 4 or 5, the middle and larger diameter tube is arranged from the center of the spherical projectile and the smaller diameter tube is positioned in the larger diameter tube. In order to increase the density of the secondary projectiles in the projectile as much as possible. 7. The projectile of any one of the scope of application for a patent, wherein the projectile comprises a soft shell. 27. Scope of patent application 8. The projectile according to any one of item ⑴ of the scope of patent application, further including an electronic controller for controlling ignition of the material. 9. If the projectile in the scope of patent application No. 8 is used, the projectile can be fired at the same time or several consecutive projectiles can be fired in rapid succession. 10. The projectile of item 8 or 9 of the scope of patent application, wherein most of the T bobbin assemblies are configured so that the projectile has minimal reaction. The method of Q force is used to spread out these ejection slugs. As a result, the projectile can maintain a desired trajectory. U. The projectile of item 8 of the scope of patent application, further including sensors for tracking ~ threats or intruders. 12. If the projectile of item 8 of the patent is requested, the electronic controller receives an ejection instruction from a remote tracking station via a communication link. For example, the projectiles of any one of the items 1 to 12 in the scope of the patent application in which the projectiles are dispersed to change or control the trajectory of the projectiles. 4 ... A method for intercepting a missile, the method comprising the following steps: determining the path of the missile; projecting a projectile according to any one of claims 丨 to the path of the missile; and projecting The secondary projectile II is selected to form a predetermined type of secondary projectile in and near the predetermined path # of the Yanhai missile. 15 · —A method for-vehicle self-defense-attack force, including the following steps: determining the position of the attack force; shooting a vicinity of the determined position of the attack force in accordance with U13 of the scope of the patent application Item of projectiles; and projected selected secondary projectiles to form a predetermined type of secondary projectiles in the attack force, in and near the decision 28 200412418 fe, patent perimeter projectile. 16 · A method for driving back Qiu Yi //, including the following steps: determine the position of this step, shoot at least one root in the vicinity of the determined position of the infantry " Please refer to items 1 to 13 of the patent scope Projectiles of any item; and project selected secondary projectiles at and near the infantry's determined position order to form a predetermined type of secondary projectile. 17. A method for forming an airborne image, comprising the steps of: firing a projectile according to any of the m-th item of the patent scope of the patent to "two middles" and projecting a selected secondary projectile including an image forming object to Form in the air-a predetermined type of image formation. 18 · — A method for fire fighting, which includes the following steps: determining the location of the fire field; shooting at least one of the positions in the vicinity of the determined location of the fire field in accordance with items 15 to 13 The projectile of item _; ejects the selected secondary projectile to form a predetermined material in and near the determined position of the fire field: undercarcass; the projectile ejected from the material disperses a fire extinguishing agent. 19_ A method for generating a fuel _ gas, including the following steps: selecting the required position of the fuel-gas explosion; shooting at least a range 1 to 13 adjacent to the required position of the fuel-gas explosion The bullet of any one of the items X Xiang Shen patent patent projectiles' shot selected secondary projectiles containing-fuel to form a predetermined type of secondary projectiles of the type ^ ,,; from the two-person projectiles ejected from these ejected The fuel; ejects the secondary projectiles of the bag to form a -predetermined type: two projectiles of under-projectiles to produce a fuel-air explosion. Li, 忒, etc. 29 20 200412418 Pick up and apply for a patent scope 20 ·-a method for spreading a payload, including the v town · choose one of the required locations for the transport of a payload; in the payload Project at least one projectile according to any one of claims 丨 to 丨] in the vicinity of the required position; project a selected secondary projectile containing the payload to form a predetermined type of secondary projectile; and from The number of shots = the projectile disperses the payload. 21.-A violet protection system for preventing a designated area, the defence system includes: at least one monitor for monitoring the designated area to detect any area in which a new object appears; a defense device, which Capable of weakening intruders appearing anywhere in a distant designated area, wherein the defensive device includes a weapon capable of ejecting projectiles, wherein the projectiles include:-a cylinder in an array of radioactive arrangements from the center of mass of the projectiles Tube assembly, each tube assembly has a plurality of secondary or secondary projectiles arranged axially in a tube, the secondary ejection system and the secondary projectiles used for propulsion from the tube shell The separated propulsion agents are connected, and a-the array's bobbin assembly is capable of selectively ejecting the sub-projectiles from the selected bobbin, whereby the projectile can disperse a predetermined type of sub-projectiles; and communication A device that provides communication between the monitor and the defensive device to trigger selective activation of the defensive device to send a weakened attack round to the detected area. 30 200412418 Patent application scope 22. If the defense system of item 21 of the patent application scope, the monitors include one or more of the current sensors or sensors located in the designated area or located away from the designated area. Remote sensing device. 23. If the defense system of the scope of patent application No. 21 or 22, wherein these monitoring devices provide a visual display of one of the designated areas monitored, so that the manual mandatory control device can be activated as needed to control the weapon manually 24 · For example, the defensive system according to any one of claims 21 to 23, wherein a plurality of bobbins can be fired simultaneously or a plurality of projectiles can be fired in rapid succession from a single bobbin. 25. The defense system according to item 24 of the patent application, wherein an electrical emission signal is carried through a circuit outside the bobbin. 26. If the defense system of item 24 of the patent application is applied, # will carry an electrical emission signal through the overlaid secondary projectile. 15 27. The defense system according to item 26 of the application, wherein the secondary ejection systems are clipped on top of each other to continue a circuit through the tube. 28. The defense system according to item 26 of the patent application, wherein the secondary projectiles abut against each other to make electrical contact. 20 29. The defense system according to item 24 of the patent application, wherein the secondary projectiles each carry a control circuit. 30. If the defense system according to any one of claims 21 to 29 of the scope of patent application, the bobbin assembly of the array includes a bobbin arranged near one end of the projectile to implement the attitude change of the projectile . 31. If the defense system of any one of the scope of patent applications Nos. 21 to 30, 31 200412418 The bobbin assembly of the array in the scope of patent applications includes a bobbin arranged in the middle to cause the projectile to laterally displace. . 32. The defense system according to any one of claims 21 to 31 in which the bobbin assembly of each array can project a projectile once in a direction having a longitudinal component to thereby increase the kinetic energy of the projectile. 33. The defense system of any one of items 21 to 31 of the scope of application for a patent, wherein the bobbin assembly of each array can eject a shot in a direction having a component in a direction with the longitudinal axis of the projectile Body, by which the rotation of the projectile about its longitudinal axis is transmitted or changed. 3 (If the anti-piping system of any of _ items in the scope of application for patents 21 to 33, at least part of these tube assemblies can shoot secondary projectiles such as -wings across the flying surface to The projectile triggers the steering effect of the step. 15 20 A. ~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~ At least part of the bobbin assembly extends through the airfoil surface and shoots in both directions. & As in any of the 21st to 33rd patent scope of the M patent, the violet-preventing system provides a separate array or a relative array n of total ㈣㈣5 body rotation about the longitudinal axis of the projectile. For example, please refer to the anti-violet system and system of item 36 of the patent scope, and its arrays, H # 'contains a pair of bobbins for changing the rotation around the sleeve of the projectile. Assembly. 3 8 · If the defense system of any one of the patent application scope No. 2 ▲ to 7 is provided, t may provide j by projecting a secondary projectile from a selected knot 32 200412418 The scope of the patent application and the energy required to change the attitude and track of these projectiles. 39. —A method for concealing the launching position of a projectile launching device The method includes the following steps: 5 10 ⑽-the same official assembly discharges at least one projectile, the cylinder _ has a tube, a plurality of projectiles Axially disposed in the bobbin to operatively seal the bore diameter of the bobbin, and separate propulsion agents for sequentially propelling individual projectiles through the mouth of the bobbin; (b) when the at least one When the projectile is in flight, at least one projectile is ejected from the included steering propulsion assembly of the array, and each steering propulsion assembly has a plurality of ^ projectiles axially disposed in the steering propulsion tube, such ejections The system is associated with a secondary separation propulsion agent for sequentially propelling the cut bodies from the steering propulsion cylinder; where The 15 ^ steerable propulsion bobbin assembly can selectively eject these projectiles from the selected rotor r into the barrel S, thereby using the -projectiles to shoot the difficult side forces to relied on the projectiles. . 33