Electric energy out-of-control equipment for electromagnetic equipment target

Abstract

The invention relates to electric energy out-of-control equipment for an electromagnetic equipment target, and belongs to the technical field of ammunition. The device comprises a dispensing unit and a conductive fiber group, wherein the conductive fiber group is mounted on the dispensing unit; the dispensing unit comprises a dispenser and a plurality of loaders; a fourth powder cavity and multiple layers of third through holes are formed in the loader, a fourth energy body is installed in the fourth powder cavity, conductive fiber clusters are installed in the third through holes, and the conductive fiber clusters can be cast along the third through holes; the fourth medicine cavity comprises a plurality of cavity sections, and the diameter of the latter cavity section is larger than that of the former cavity section; and each cavity section is opposite to at least one layer of third through holes. According to the invention, a plurality of loaders are thrown along a plurality of directions, and the loaders throw loaded multi-layer wire fiber clusters in an echelon manner, so that fiber tows expanded by different layers of conductive fiber clusters can cover different radiuses, the distribution density of the fiber tows and the probability that the fiber tows fall on an electric power system are improved, and the reliability of the electric power system is improved. And the success rate of power failure paralysis of the power system is improved.

Description

Technical Field

[0001] The present invention relates to the technical field of ammunition, and in particular to an out-of-control electric energy device for electromagnetic equipment targets. Background Art

[0002] In order to strike electric power system targets such as high-voltage lines, power plants and substations in electromagnetic equipment, conductive fiber power-off devices are often used to power off and penetrate them, so as to power off and paralyze the electric power system. In the prior art, the conductive fiber power-off device flies over the target area through a carrier platform and throws out a conductive fiber ball. After the conductive fiber ball is unfolded, a large number of fiber bundles are thrown out. A large number of conductive fiber bundles fall on the electric power system, causing multiple short circuits in the electric power system, causing power outage and paralysis of the electric power system. However, since the conductive fiber power-off device in the prior art uses a central tube to throw the conductive fiber ball, the scattering range of the conductive fiber ball is small, thereby reducing the distribution density of the fiber bundles after the conductive fiber ball is unfolded, which leads to a low success rate of the conductive fiber power-off device in powering off and paralyzing the electric power system. Summary of the invention

[0003] In view of the above analysis, the present invention aims to provide an electric energy out-of-control equipment targeting electromagnetic equipment, so as to solve the problem that the conductive fiber balls scattered by the conductive fiber power-off device in the prior art have a small scattering range, resulting in a low distribution density of the fiber bundles after the conductive fiber balls are unfolded, thus leading to a low success rate in power outage and paralysis of the power system.

[0004] The purpose of the present invention is mainly achieved through the following technical solutions:

[0005] A power outage equipment for electromagnetic equipment targets, comprising a front connector, a rear connector, a cabin shell, a spreading unit and a conductive fiber group, wherein the conductive fiber group is installed on the spreading unit, and the spreading unit is used to spread the conductive fiber group, and the fiber bundles of the conductive fiber group after being unfolded can be dropped on the power system; the spreading unit comprises a spreader and a plurality of loaders installed on the spreader, and the loaders can be thrown in multiple directions by the spreader; the loader comprises a loading assembly; the loading assembly comprises a third seat body and a fourth energy body; the third seat body is provided with A fourth medicine cavity and multiple layers of third through holes; the third through holes extend radially along the third seat body and are connected to the fourth medicine cavity, the third through holes are used to install a conductive fiber mass, and the conductive fiber mass can be ejected along the axis of the third through hole; the fourth medicine cavity is used to install a fourth energy body; the fourth medicine cavity includes multiple cavity segments, and the diameter of the latter cavity segment in the fourth medicine cavity is greater than the diameter of the former cavity segment, so that the filling amount of the fourth energy body in the latter cavity segment is greater than the filling amount of the fourth energy body in the former cavity segment; each cavity segment in the fourth medicine cavity is opposite to at least one layer of third through holes.

[0006] Furthermore, the spreader includes a second seat body, a second plunger and a third energy body, the second plunger and the third energy body are both installed on the second seat body, the second plunger can be projected radially along the second seat body, and the third energy body is used to provide power for the second plunger to be projected radially along the second seat body.

[0007] The cam is connected to the second base body by a toothed structure, and the toothed structure is connected to the second base body by a toothed structure. The cam is connected to the second base body by a toothed structure, and the toothed structure is connected to the second base body by a toothed structure. The cam is connected to the second base body by a toothed structure, and the toothed structure is connected to the second base body by a toothed structure.

[0008] Furthermore, the driving disc is provided with a driving groove, the driving block is provided with a pin, and the pin is inserted into the driving groove and can slide in the driving groove.

[0009] Furthermore, the adjustment mechanism also includes a power member, which is installed on the second base body and can rotate on the second base body.

[0010] Furthermore, the adjustment mechanism also includes a locking spring, one end of which is fixedly connected to the second seat body, and the other end is fixedly connected to the power piece, and the locking spring is used to apply an elastic thrust to the power piece; the second seat body is provided with a plurality of locking grooves evenly arranged circumferentially; the power piece is provided with a locking protrusion, which is arranged opposite to the locking groove and can be inserted into the locking groove, and the locking spring can ensure that the locking protrusion is always inserted into the locking groove when not affected by external force, so that the power piece remains in a locked state, thereby locking the drive disk.

[0011] Furthermore, the electric energy out-of-control equipment also includes a separator, which is used to assist in separating the shell; the separator includes a first seat body, a first plunger and a second energy body, the first seat body is a cylinder, and is fixedly mounted on the front connecting body; the first plunger and the second energy body are both mounted on the first seat body, the first plunger can be radially ejected along the first seat body, and the second energy body is used to provide power for the first plunger to be radially ejected along the first seat body; one end of the first plunger is in contact with the shell, and the other end is in contact with the second energy body.

[0012] Furthermore, a first through hole and a second medicine cavity are provided on the first seat body, and the second medicine cavity is used to install the second energy body; the first through hole extends radially along the first seat body and is connected with the second medicine cavity, and the first through hole is used to install a first plunger, and the first plunger can be projected along the axis of the first through hole.

[0013] Further, the cross-sectional shape of the first plunger is adapted to the cross-sectional shape of the first through hole, and the cross-sectional area of ​​the first plunger is equal to the cross-sectional area of ​​the first through hole.

[0014] Furthermore, a plurality of the first through holes are provided, and the plurality of the first through holes are evenly arranged around a circumference.

[0015] The technical solution of the present invention can achieve at least one of the following effects:

[0016] (1) The present invention provides an electric energy out-of-control device for electromagnetic equipment, comprising a front connector, a rear connector, a cabin shell, a spreading unit and a conductive fiber group, wherein the conductive fiber group is installed on the spreading unit, and the spreading unit is used to spread the conductive fiber group, and the fiber bundles of the conductive fiber group after being unfolded can be dropped on the power system; the spreading unit comprises a spreader and a plurality of loaders installed on the spreader, and the loaders can be thrown in multiple directions by the spreader; the loader comprises a loading assembly; the loading assembly comprises a third seat body and a fourth energy body; the third seat body is provided with a fourth medicine cavity and a plurality of third through holes; the third through holes extend along the radial direction of the third seat body and are connected to the fourth medicine cavity, and the third through holes are used to install the conductive fiber group, and the conductive fiber group can be thrown along the third The fourth medicine cavity is used for installing a fourth energy body; the fourth medicine cavity includes a plurality of cavity segments, and the diameter of a rear cavity segment in the fourth medicine cavity is larger than the diameter of a front cavity segment, so that the filling amount of the fourth energy body in the rear cavity segment is larger than the filling amount of the fourth energy body in the front cavity segment; each cavity segment in the fourth medicine cavity is opposite to at least one layer of the third through hole; compared with the prior art, the present invention realizes that a spreader scatters a plurality of loaders in a plurality of directions, and the loaders throw out the multi-layer conductor fiber groups loaded therein in a cascade, so that the fiber bundles of different layers of conductive fiber groups are unfolded and form different coverage radii, thereby increasing the distribution density of the fiber bundles, and further increasing the probability of the fiber bundles falling on the power system, and increasing the success rate of power outage and paralysis of the power system in the target area.

[0017] (2) The spreading unit of the present invention further comprises an adjusting mechanism, which comprises a driving disk, a driving block, a tightening plunger and a tightening spring, wherein the driving disk is rotatably connected to the second seat body; the driving block and the tightening plunger are both slidably connected to the second seat body, and the driving block can slide along the radial direction of the second seat body, and the tightening plunger can slide along the axial direction of the second seat body; the driving disk is connected to the driving block, one end of the tightening plunger contacts the driving block, and the other end can contact the second plunger; one end of the tightening spring is connected to the spreader, and the other end is fixed to the tightening plunger The fixing connection is that the tightening spring is used to apply elastic thrust to the tightening plunger so that the tightening plunger always keeps in contact with the driving block; rotating the driving disk can control the driving block to slide radially along the second seat body, and synchronously drive the tightening plunger to slide axially along the second seat body, thereby adjusting the clamping force applied by the tightening plunger on the second plunger, and then adjusting the spreading power of the spreader, so as to adjust the ejection range of the loader according to the specific coverage requirements of the target area, accurately control the radial distribution of the loader, and then realize accurate control of the coverage range and coverage density of the conductive fiber group in the target area.

[0018] (3) The cabin shell of the present invention includes a shell and a kinetic energy cutting mechanism, and the kinetic energy cutting mechanism includes a cover shell, a first energy body and a kinetic energy cutting rope. The cover shell is buckled on the shell and together with the shell form a first charge chamber; the first energy body and the kinetic energy cutting rope are both installed in the first charge chamber; the first energy body can be detonated in the first charge chamber, and the high-temperature and high-pressure gas generated will eject the kinetic energy cutting rope along the radial direction of the shell, so that the kinetic energy cutting rope can quickly cut the shell, so that the shell is quickly dismembered into multiple shell pieces, and the shell pieces are separated under the action of aerodynamic force, thereby ensuring that the dismembered shell can be quickly and completely separated under the action of aerodynamic force, so that the dispersing unit is completely exposed, thereby improving the reliability of the shell separation.

[0019] (4) The electric energy out-of-control equipment described in the present invention also includes a separator, which is used to assist in separating the shell; the separator includes a first seat body, a first plunger and a second energy body, the first seat body is a cylinder, and is fixedly mounted on the front connecting body; the first plunger and the second energy body are both mounted on the first seat body, the first plunger can be ejected along the radial direction of the first seat body, and the second energy body is used to provide power for the first plunger to be ejected along the radial direction of the first seat body; one end of the first plunger is in contact with the shell, and the other end is in contact with the second energy body; when the shell is cut and dismembered, the second energy body is detonated, and the high-temperature and high-pressure gas generated ejects the first plunger along the radial direction of the first seat body, so that the end of the cut and dismembered shell close to the front connecting body quickly moves along the radial direction of the front connecting body and quickly separates from the front connecting body, thereby ensuring that the cut and dismembered shell can be quickly and completely separated under the action of aerodynamics, so that the spreading unit is completely exposed, thereby improving the reliability of the shell separation.

[0020] In the present invention, the above-mentioned technical solutions can also be combined with each other to achieve more preferred combination solutions. Other features and advantages of the present invention will be described in the subsequent description, and some advantages can become obvious from the description, or can be understood by practicing the present invention. The purpose and other advantages of the present invention can be realized and obtained through the contents particularly pointed out in the description and the drawings. BRIEF DESCRIPTION OF THE DRAWINGS

[0021] The drawings are only for the purpose of illustrating particular embodiments and are not to be considered limiting of the present invention. Like reference symbols denote like components throughout the drawings.

[0022] Figure 1 It is a structural explosion diagram of the power out-of-control equipment in Example 1 of the present invention;

[0023] Figure 2 This is a schematic diagram of the structure of the hull in Embodiment 1 of the present invention;

[0024] Figure 3 for Figure 2 One of the partial enlarged images in center A;

[0025] Figure 4 for Figure 2 The second partial enlarged picture of middle A;

[0026] Figure 5 It is a full cross-sectional view of the structure of the separator in Example 1 of the present invention;

[0027] Figure 6 It is a full cross-sectional view of the structure of the first seat body in Example 1 of the present invention;

[0028] Figure 7 Schematic diagram of the structure of the spreading unit in Example 1 of the present invention;

[0029] Figure 8 A half-section view of the structure of the dispenser in Example 1 of the present invention;

[0030] Fig. 9 It is a half-section view of the structure of the second seat body in Embodiment 1 of the present invention;

[0031] Fig.10 It is a structural exploded diagram of the loader in Embodiment 1 of the present invention;

[0032] Fig.11 It is a full cross-sectional view of the structure of the loading assembly in Example 1 of the present invention;

[0033] Fig.12 It is a half-section view of the structure of the second seat body in Embodiment 1 of the present invention;

[0034] Fig.13 for Fig.11 Middle B is a partial enlarged view;

[0035] Fig.14 for Figure 8 Middle C is a partial enlarged view;

[0036] Fig.15 It is a full cross-sectional view of the structure of the drive disk in Embodiment 2 of the present invention;

[0037] Fig.16 Schematic diagram of the structure of the driving block in Embodiment 2 of the present invention;

[0038] Fig.17 for Fig. 9 Middle D is a partial enlarged view;

[0039] Fig.18 for Figure 8 Middle E is a partial enlarged view;

[0040] Fig.19 This is a distribution diagram of fiber bundles after the conductive fiber group of the present invention is unfolded.

[0041] Reference numerals:

[0042] 1. Anterior connector;

[0043] 2. Postconnector;

[0044] 3. Hull;

[0045] 31. Shell; 311. Cutting groove; 32. Kinetic energy cutting mechanism; 321. Cover; 322. First energy body; 323. Kinetic energy cutting rope; 324. First fuze;

[0046] 4. Separator;

[0047] 41. first seat body; 411. first through hole; 412. second medicine cavity; 42. first plunger; 43. second energy body; 44. second fuse; 45. first cover;

[0048] 5. Spreader;

[0049] 51, second seat body; 511, third medicine cavity; 512, second through hole; 513, mounting groove; 514, fourth through hole; 515, slide groove; 516, fifth through hole; 517, locking groove; 52, second plunger; 53, third energy body; 54, third fuse; 55, second cover;

[0050] 6. Loader;

[0051] 61, loading assembly; 611, third seat body; 6111, fourth medicine chamber; 6112, third through hole; 6113, ignition tube; 612, fourth energy body; 613, fourth fuze; 614, stabilizer; 615, guard plate; 616, third cover; 62, protective shell;

[0052] 7. Restraint;

[0053] 8. Adjustment mechanism;

[0054] 81. driving disk; 811. driving groove; 812. gear; 82. driving block; 821. pin; 83. tightening plunger; 84. tightening spring; 85. power part; 86. locking spring. DETAILED DESCRIPTION

[0055] The preferred embodiments of the present invention will be described in detail below in conjunction with the accompanying drawings, wherein the accompanying drawings constitute a part of the present invention and are used together with the embodiments of the present invention to illustrate the principles of the present invention, but are not used to limit the scope of the present invention.

[0056] Example 1

[0057] A specific embodiment of the present invention discloses a power outage control device for electromagnetic equipment targets, such as Figure 1 As shown, it includes a front connector 1, a rear connector 2, a cabin shell 3, a spreading unit and a conductive fiber group, wherein the front connector 1 and the rear connector 2 are respectively mounted at the two ends of the cabin shell 3, and together with the cabin shell 3, form a storage cabin; a plurality of conductive fiber groups are provided, and the plurality of conductive fiber groups are mounted on the spreading unit; the spreading unit is mounted in the storage cabin, and the two ends of the spreading unit are respectively fixedly connected to the front connector 1 and the rear connector 2, the front connector 1 is used to connect with other front-end devices, the rear connector 2 is used to connect with other rear-end devices, and the spreading unit is used to scatter the conductive fiber group to the target area and expand the conductive fiber group; when in use, the power outage equipment is dropped over the target area, the cabin shell 3 is separated at a predetermined height, the conductive fiber group is thrown out by the spreading unit, and the conductive fiber group is expanded, and the expanded conductive fiber group falls on the power system, and the power system in the target area is powered off and paralyzed through the short-circuit arcing effect.

[0058] Preferably, the conductive fiber group includes a fiber bundle, a wire shaft and a resistance blade, the fiber bundle is wound on the wire shaft, one end of the fiber bundle is connected to the resistance blade, and the conductive fiber group is thrown out, and the fiber bundle wound on the wire shaft can be quickly unfolded under the synergistic effect of the inertia of the wire shaft and the air resistance of the resistance blade, and the fiber bundle falls on the power system, thereby paralyzing the power system in the target area through the short-circuit arcing effect.

[0059] Preferably, if Figure 2 and Figure 3 As shown, the cabin shell 3 includes a shell 31 and a kinetic energy cutting mechanism 32, and the shell 31 is a cylindrical structure; the kinetic energy cutting mechanism 32 is provided in plurality, and the plurality of kinetic energy cutting mechanisms 32 are provided on the inner wall of the shell 31, and the kinetic energy cutting mechanism 32 is used to quickly cut and dismember the shell 31 into a plurality of shell pieces, and the cut and dismembered shell 31 can be quickly separated under the action of aerodynamic force, thereby realizing rapid radial cabin opening, exposing the spreading unit, and facilitating the spreading unit to scatter the conductive fiber group.

[0060] Preferably, a plurality of the kinetic energy cutting mechanisms 32 are evenly arranged circumferentially on the inner wall of the shell 31, so that the shell 31 can be cut and dismembered into a plurality of identical shell pieces, and the identical shell pieces will be subjected to the same aerodynamic force, thereby enabling the electrical energy out-of-control equipment targeting electromagnetic equipment to maintain stable flight during the separation process of the shell 31.

[0061] Preferably, if Figure 4As shown, a cutting groove 311 is provided on the inner wall of the shell 31, and the cutting groove 311 extends along the axis of the shell 31; the kinetic energy cutting mechanism 32 is installed in the cutting groove 311. When the kinetic energy cutting mechanism 32 performs a cutting action, the shell 31 can be quickly dismembered into multiple shell pieces along the cutting groove 311, thereby further improving the efficiency of cutting, dismembering and separating the shell 31, and at the same time can also ensure that the shell 31 is completely cut and dismembered, and then ensure that the shell 31 can be completely separated, thereby improving the reliability of the separation of the shell 31 and allowing the spreading unit to be fully exposed.

[0062] Preferably, a plurality of cutting grooves 311 are provided, and the number of the cutting grooves 311 is the same as the number of the kinetic energy cutting mechanisms 32 .

[0063] Preferably, the kinetic energy cutting mechanism 32 includes a cover shell 321, a first energy body 322 and a kinetic energy cutting rope 323. The cover shell 321 is snapped into the cutting groove 311 and together with the cutting groove 311, forms a first charge cavity; the first energy body 322 and the kinetic energy cutting rope 323 are both installed in the first charge cavity; when the electrical energy out-of-control equipment flies to a predetermined height, the first energy body 322 is detonated in the first charge cavity, and the high-temperature and high-pressure gas generated will eject the kinetic energy cutting rope 323 radially along the shell 31, so that the kinetic energy cutting rope 323 quickly cuts the shell 31 along the cutting groove 311, so that the shell 31 is quickly dismembered into multiple shell fragments.

[0064] Preferably, the kinetic energy cutting mechanism 32 further comprises a first fuse 324, which is mounted on the cover 321 and in contact with the first energy body 322, and the first fuse 324 is used to detonate the first energy body 322 when the out-of-control electrical equipment flies to a predetermined height.

[0065] Preferably, a cutting blade is provided on the kinetic energy cutting rope 323, and the cutting blade is opposite to the bottom wall of the cutting groove 311. When the kinetic energy cutting rope 323 is projected along the radial direction of the shell 31, the cutting blade can quickly cut and dismember the shell 31 along the cutting groove 311, thereby further improving the efficiency of the kinetic energy cutting mechanism 32 in cutting and dismembering the shell 31, realizing rapid cabin opening, and ensuring complete cabin opening.

[0066] Preferably, the electric energy out-of-control equipment also includes a separator 4, which is used to assist in separating the shell 31 to ensure that the shell 31 can be quickly separated from the front connector 1 after being cut and dismembered, thereby preventing the shell 31 from being unable to separate under the action of aerodynamic force after being cut and dismembered, thereby improving the reliability of the separation of the shell 31, and ensuring that the electric energy out-of-control equipment can complete the radial cabin opening after flying to a predetermined height and fully expose the spreading unit.

[0067] Preferably, if Figure 5As shown, the separator 4 includes a first seat body 41, a first plunger 42 and a second energy body 43. The first seat body 41 is a cylinder and is fixedly mounted on the front connecting body 1; the first plunger 42 and the second energy body 43 are both mounted on the first seat body 41, the first plunger 42 can be radially ejected along the first seat body 41, and the second energy body 43 is used to provide power for the first plunger 42 to be radially ejected along the first seat body 41; one end of the first plunger 42 is in contact with the shell 31, and the other end is in contact with the second energy body 43; when the shell 31 is cut and dismembered, the second energy body 43 is detonated, and the high-temperature and high-pressure gas generated ejects the first plunger 42 radially along the first seat body 41, so that the end of the cut and dismembered shell 31 close to the front connecting body 1 quickly moves along the radial direction of the front connecting body 1, and quickly separates from the front connecting body 1, thereby ensuring that the cut and dismembered shell 31 can be quickly and completely separated under the action of aerodynamics, so that the spreading unit is completely exposed, thereby improving the reliability of the separation of the shell 31.

[0068] Preferably, the separator 4 also includes a second fuse 44, which is installed on the first seat 41 and contacts the second energy body 43. The second fuse 44 is used to monitor whether the shell 31 is cut and dismembered, and detonate the second energy body 43 according to a preset time.

[0069] Preferably, if Figure 6 As shown, a first through hole 411 and a second medicine cavity 412 are provided on the first seat body 41, one end of the second medicine cavity 412 is a closed end, and the other end is an open end, and the second medicine cavity 412 is used to install a second energy body 43, and the second energy body 43 can be detonated in the second medicine cavity 412; the first through hole 411 extends radially along the first seat body 41 and is connected to the second medicine cavity 412, and the first through hole 411 is used to install a first plunger 42, and the first plunger 42 can be ejected along the axis of the first through hole 411.

[0070] Preferably, a plurality of the first through holes 411 are provided, and the plurality of the first through holes 411 are evenly arranged around the circumference; the cross-sectional shape of the first plunger 42 is adapted to the cross-sectional shape of the first through hole 411, and the cross-sectional area of ​​the first plunger 42 is equal to the cross-sectional area of ​​the first through hole 411; when the second energy body 43 is detonated, the high-temperature and high-pressure gas generated enters the first through hole 411, thereby ejecting the first plunger 42 installed in the first through hole 411, thereby preventing the energy generated after the second energy body 43 is detonated from leaking from the gap between the first plunger 42 and the first through hole 411, thereby improving the utilization efficiency of the energy after the second energy body 43 is detonated, and improving the reliability of the first plunger 42 ejecting from the first through hole 411, thereby ensuring the reliability of the separation of the shell 31.

[0071] Preferably, a plurality of first plungers 42 are provided, and each shell piece after being cut and dismembered is arranged opposite to at least one first plunger 42, thereby ensuring that each shell piece after being cut and dismembered can be quickly separated from the front connector 1, further ensuring the reliability of the separation of the shell 31.

[0072] Preferably, the second medicine cavity 412 is a cylindrical cavity, and the axis of the second medicine cavity 412 coincides with the axis of the first seat body 41, so that the length of each first through hole 411 is equal, and then multiple first plungers 42 can be ejected simultaneously, so that the multiple shell fragments after being cut and dismembered can be synchronously and quickly separated from the front connecting body 1, and then the multiple shell fragments can be simultaneously affected by air resistance, so that the multiple shell fragments can be synchronously separated, and the flight stability of the electric energy out-of-control equipment during the separation of the shell 31 is further improved.

[0073] Preferably, the separator 4 further comprises a first sealing cover 45 , which is installed at the open end of the second medicine cavity 412 and is used to seal the second medicine cavity 412 , so that the second medicine cavity 412 forms a sealed space; the second fuse 44 is installed on the first sealing cover 45 .

[0074] Preferably, a plurality of the spreading units are provided, and the plurality of the spreading units are fixedly connected in sequence, and the conductive fiber groups are scattered in sequence by timing control, so as to realize step-by-step scattering of the conductive fiber groups, thereby increasing the coverage density of the conductive fiber groups on the target area, thereby increasing the distribution density of the fiber bundles after the conductive fiber groups are unfolded, and further increasing the success rate of the electric energy outage equipment in paralyzing the power system in the target area.

[0075] Preferably, if Figure 7 As shown, the spreading unit includes a spreader 5 and a loader 6, the loader 6 is mounted on the spreader 5, and the conductive fiber mass is mounted on the loader 6; the spreader 5 is used to scatter the loader 6, and the loader 6 is used to load and scatter the conductive fiber mass.

[0076] Preferably, a plurality of loaders 6 are provided, and the plurality of loaders 6 are evenly arranged around the circumference. The loaders 6 can be thrown to multiple directions by the spreader 5. The loaders 6 throw out the conductive fiber balls and spread the conductive fiber balls, thereby increasing the coverage density of the conductive fiber balls on the target area, thereby increasing the success rate of the power outage equipment in paralyzing the power system in the target area.

[0077] Preferably, if Figure 8As shown, the spreader 5 includes a second seat body 51, a second plunger 52 and a third energy body 53. The second seat body 51 is a cylinder and is fixedly connected to the adjacent second seat body 51 or the first seat body 41 or the rear connecting body 2; the second plunger 52 and the third energy body 53 are both installed on the second seat body 51, the second plunger 52 can be ejected along the radial direction of the second seat body 51, and the third energy body 53 is used to provide power for the second plunger 52 to be ejected along the radial direction of the second seat body 51; one end of the second plunger 52 is in contact with the loader 6, and the other end is in contact with the third energy body 53; when the shell 31 is separated, the third energy body 53 is detonated, generating high-temperature and high-pressure gas to eject the second plunger 52 along the radial direction of the second seat body 51, thereby ejecting the loader 6.

[0078] Preferably, the spreader 5 also includes a third fuse 54, which is installed on the second base body 51 and contacts the third energy body 53. The third fuse 54 is used to monitor whether the shell 31 is separated. After the shell 31 is separated, the third fuse 54 can detonate the third energy body 53 according to a preset time; in addition, by setting the third fuse 54 in each spreading unit, the spreading timing of multiple spreaders 5 can be controlled, thereby realizing a step-by-step spreading loader 6, increasing the spreading density of the loader 6 in the target area, and then increasing the coverage density of the conductive fiber group on the target area, thereby increasing the success rate of the power outage equipment in paralyzing the power system in the target area.

[0079] Preferably, if Fig. 9 As shown, a third medicine cavity 511 and a second through hole 512 are provided on the second seat body 51, one end of the third medicine cavity 511 is a closed end, and the other end is an open end, the third medicine cavity 511 is used to install a third energy body 53, and the third energy body 53 can be detonated in the third medicine cavity 511; the second through hole 512 extends along the radial direction of the second seat body 51 and is connected to the third medicine cavity 511, the second through hole 512 is used to install a second plunger 52, and the second plunger 52 can be ejected along the axis of the second through hole 512.

[0080] Preferably, a plurality of the second through holes 512 are provided, and the plurality of second through holes 512 are evenly arranged around the circumference; the cross-sectional shape of the second plunger 52 is adapted to the cross-sectional shape of the second through hole 512, and the cross-sectional area of ​​the second plunger 52 is equal to the cross-sectional area of ​​the second through hole 512; when the third energy body 53 is detonated, the high-temperature and high-pressure gas generated thereby enters the second through hole 512, thereby ejecting the second plunger 52 installed in the second through hole 512, thereby preventing the energy generated after the third energy body 53 is detonated from leaking from the gap between the second plunger 52 and the second through hole 512, thereby improving the utilization efficiency of the energy after the third energy body 53 is detonated.

[0081] Preferably, a plurality of the second plungers 52 are provided, and the number of the second plungers 52 is equal to the number of the loaders 6 .

[0082] Preferably, the third medicine cavity 511 is a cylindrical cavity, and the axis of the third medicine cavity 511 coincides with the axis of the second seat body 51, thereby ensuring that the length of each second through hole 512 is equal, and then multiple second plungers 52 can be ejected simultaneously, so that multiple loaders 6 in the same spreading unit can obtain the same kinetic energy, thereby controlling the scattering speed and scattering angle of the loader 6, and then controlling the scattering density of the loader 6.

[0083] Preferably, the second seat body 51 is also provided with a mounting groove 513, and the mounting groove 513 is connected to the second through hole 512, and is used for mounting the loader 6, so as to prevent the loader 6 from rotating along the circumference of the second seat body 51; a plurality of the mounting grooves 513 are provided, and the plurality of the mounting grooves 513 are evenly arranged around the circumference, and the number of the mounting grooves 513 is equal to the number of the second through holes 512.

[0084] Preferably, the dispenser 5 further comprises a second sealing cover 55 , which is installed at the open end of the third medicine cavity 511 and is used to seal the third medicine cavity 511 , so that the third medicine cavity 511 forms a sealed space; the third fuse 54 is installed on the second sealing cover 55 .

[0085] Preferably, if Fig.10 and Fig.11 As shown, the loader 6 includes a loading component 61, and the conductive fiber group is installed on the loading component 61, and the loading component 61 can throw out the conductive fiber group and make the conductive fiber group unfold; the loading component 61 includes a third seat body 611 and a fourth energy body 612, and the third seat body 611 is a cylinder; the conductive fiber group and the fourth energy body 612 are both installed on the third seat body 611, and the conductive fiber group can be ejected along the radial direction of the third seat body 611, and the third energy body 53 is used to provide power for the second plunger 52 to be ejected along the radial direction of the second seat body 51; when the loader 6 is thrown out of the storage cabin, the fourth energy body 612 is detonated to generate high-temperature and high-pressure gas to eject the conductive fiber group along the radial direction of the third seat body 611, and the ejected conductive fiber group can be rapidly unfolded under the action of aerodynamic force and fall on the power system in the target area to paralyze the power system.

[0086] Preferably, the loading assembly 61 also includes a fourth fuse 613, which is installed on the third base body 611 and connected to the fourth energy body 612. The fourth fuse 613 is used to monitor whether the loader 6 is thrown out and detonate the fourth energy body 612 according to a preset time to provide power for ejecting the conductive fiber group.

[0087] Preferably, if Fig.12 As shown, the third seat body 611 is provided with a fourth medicine cavity 6111 and a third through hole 6112, and the fourth medicine cavity 6111 is used to install a fourth energy body 612, and the fourth energy body 612 can be detonated in the fourth medicine cavity 6111; the third through hole 6112 extends radially along the third seat body 611 and is connected to the fourth medicine cavity 6111, and the third through hole 6112 is used to install a conductive fiber group, and the conductive fiber group can be ejected along the axis of the third through hole 6112.

[0088] Preferably, the third through holes 6112 are provided in multiple layers, each layer including multiple third through holes 6112; the third through holes 6112 in each layer are uniformly arranged around the circumference, and the axes of the third through holes 6112 in adjacent layers are not parallel (i.e., the third through holes 6112 in adjacent layers are staggered), thereby achieving multi-directional scattering of conductive fiber clusters and improving the distribution density of conductive fiber clusters.

[0089] Preferably, the fourth medicine cavity 6111 includes a plurality of cavity segments. When viewed from the front connector 1 to the rear connector 2, the diameter of the rear cavity segment in the fourth medicine cavity 6111 is larger than the diameter of the front cavity segment, so that the filling amount of the fourth energy body 612 in the rear cavity segment is larger than the filling amount of the fourth energy body 612 in the front cavity segment; each cavity segment in the fourth medicine cavity 6111 is opposite to at least one layer of the third through hole 6112, and when the fourth energy body 612 is detonated, due to the different cavity segments in the fourth medicine cavity 6111, The filling amounts of the fourth energy body 612 are different, and therefore the energies generated after the explosion of the fourth energy bodies 612 in different cavity sections of the fourth medicine cavity 6111 are also different, so that the third through holes 6112 corresponding to each cavity of the fourth medicine cavity 6111 obtain different scattering energies, and then the conductive fiber groups arranged in different third through holes 6112 obtain different scattering kinetic energies, thereby realizing the step-by-step scattering of the conductive fiber groups, and then realizing the control of the distribution density of the conductive fiber groups in the target area, thereby improving the coverage effect.

[0090] Compared with the prior art, multiple loaders 6 are scattered in multiple directions by a spreader 5, and the loaders 6 throw out the multi-layer conductor fiber balls loaded therein in stages. The fiber bundles of different layers of conductive fiber balls are unfolded to form different coverage radii, thereby increasing the distribution density of the fiber bundles, and further increasing the probability of the fiber bundles falling on power facilities such as power grids, thereby increasing the success rate of the power outage equipment in power outages and paralysis of the power system in the target area.

[0091] Preferably, a fire transmission tube 6113 is also provided on the third seat body 611, and the fire transmission tube 6113 is used to connect the multiple cavity segments in the fourth medicine cavity 6111 to connect the fourth energy body 612 and the fourth fuse 613. When the fourth fuse 613 is detonated, the fourth energy body 612 in the multiple cavity segments arranged in the fourth medicine cavity 6111 is detonated in sequence through the fire transmission tube 6113.

[0092] Preferably, the loading assembly 61 further includes a stabilizer 614 for stabilizing the loading assembly 61 after scattering, so that the loading assembly 61 can maintain a certain speed and posture.

[0093] The stabilizer 614 is a parachute.

[0094] Preferably, if Fig.13 As shown, the loading assembly 61 also includes a protective plate 615, which is arranged in the third through hole 6112 and located between the conductive fiber group and the fourth medicine cavity 6111, and is used to protect the conductive fiber group from high temperature burning after the fourth energy body 612 is detonated to prevent damage to the conductive fiber group.

[0095] Preferably, the loading assembly 61 also includes a third cover 616, and the third cover 616 is arranged in the third through hole 6112 to close the third through hole 6112 to prevent external foreign matter from entering the third through hole 6112 and causing damage to the conductive fiber group; in addition, when the conductive fiber group is thrown out, it can break through the third cover 616.

[0096] Preferably, the loader 6 also includes a protective shell 62, which is mounted on the loading assembly 61 to protect the conductive fiber clusters installed in the loading assembly 61 when the loader 6 is scattered, thereby preventing the conductive fiber clusters from being damaged; the protective shell 62 is provided with multiple pieces, and can automatically separate from the loading assembly 61 when the loader 6 is scattered.

[0097] Preferably, the spreading unit further comprises a restrainer 7, which is used to fix the loader 6 in the mounting groove 513 of the second seat body 51, so that the loader 6 can break free from the restraint of the restrainer 7 and detach from the second seat body 51 only when it is subjected to the kinetic energy transmitted by the second plunger 52.

[0098] Preferably, the restraint 7 can be a belt.

[0099] Preferably, the first energy body 322, the second energy body 43, the third energy body 53 and the fourth energy body 4222 can all be made of materials that can be instantly ignited and release a large amount of energy, such as explosives; the first fuse 324, the second fuse 44, the third fuse 54 and the fourth fuse 613 all adopt fuses in the prior art.

[0100] Preferably, the loaders 6 in adjacent spreading units are staggered, so that the density of the conductive fiber clusters spread by the loaders 6 can be further improved.

[0101] Example 2

[0102] The out-of-control electric energy equipment in Example 1 realizes the step-by-step scattering of the scattering units by performing timing control on the multiple scattering units (i.e., by controlling the detonation time of the fuse); after the out-of-control electric energy equipment of this type is assembled, it is impossible to perform targeted adjustment on the scatterer 5 according to the specific coverage requirements of the target area, thereby making it impossible for the scatterer 5 of the out-of-control electric energy equipment in Example 1 to adjust the scattering density of the loader 6 according to the specific coverage requirements of the target area, thereby affecting the coverage density of the conductive fiber group on the target area; in order to overcome the above-mentioned defects, Example 2 is further improved on the basis of Example 1, such as Figure 7 As shown, the spreading unit also includes an adjusting mechanism 8, and the adjusting mechanism 8 is installed on the spreader 5. The adjusting mechanism 8 is used to adjust the throwing range of the loader 6 thrown by the spreader 5, so as to achieve individual adjustment of the throwing range of the loader 6 for each spreading unit, thereby achieving precise control of the throwing range of the loader 6 according to the specific coverage requirements of the target area, and further improving the coverage range and coverage density of the conductor fiber group thrown by the loader 6 in the target area.

[0103] Preferably, if Fig. 9 As shown, the second seat body 51 is also provided with a fourth through hole 514 and a slide groove 515, the fourth through hole 514 extends along the axis of the second seat body 51 and is connected to the second through hole 512; the number of the fourth through holes 514 is equal to the number of the second through holes 512, and the fourth through holes 514 are evenly arranged around the circumference; the number of the slide grooves 515 is equal to the number of the second through holes 512, and the slide grooves 515 are evenly arranged around the circumference.

[0104] Preferably, if Fig.14As shown, the adjusting mechanism 8 includes a driving disk 81, a driving block 82, a tightening plunger 83 and a tightening spring 84. The driving disk 81 is installed on the end surface of the second seat body 51 and is rotatably connected to the second seat body 51. The driving disk 81 is connected to the driving block 82; the driving block 82 is arranged in the slide groove 515 and can slide in the slide groove 515 along the radial direction of the second seat body 51; the tightening plunger 83 is arranged in the fourth through hole 514 and can slide in the fourth through hole 514 along the axial direction of the second seat body 51; one end of the tightening plunger 83 can contact the second plunger 52, and the other end contacts the driving block 82; the tightening spring 84 is arranged in the fourth through hole 514, one end is fixedly connected to the fourth through hole 514, and the other end is fixedly connected to the tightening plunger 83, and the tightening spring 84 is used to tighten the top The tightening plunger 83 applies an elastic thrust so that the tightening plunger 83 always maintains contact with the driving block 82; when in use, the driving disk 81 is rotated to control the driving block 82 to slide radially along the second seat body 51, and the driving block 82 drives the tightening plunger 83 to slide axially along the second seat body 51, thereby adjusting the clamping force applied by the tightening plunger 83 to the second plunger 52, so that the thrust acting on the second plunger 52 after the third energy body 53 deflagrates or explodes will further overcome the clamping force applied by the tightening plunger 83 to the second plunger 52, thereby adjusting the ejection kinetic energy of the second plunger 52, and then adjusting the ejection speed of the loader 6, so as to adjust the ejection range of the loader 6 according to the specific coverage requirements of the target area, accurately control the radial distribution of the loader 6, and then accurately control the coverage range and coverage density of the conductive fiber group in the target area.

[0105] Preferably, if Fig.15 and Fig.16 As shown, the driving disk 81 is provided with a driving groove 811, and the driving groove 811 is a vortex groove; the driving block 82 is provided with a pin 821, and the pin 821 is inserted into the driving groove 811 and can slide in the driving groove 811; when the driving disk 81 is rotated, the position of the pin 821 in the driving groove 811 is controlled by the driving groove 811 to realize the radial sliding of the driving block 82 in the slide groove 515 along the second seat body 51, and then realize the control of the tightening plunger 83 in the fourth through hole 514 along the axial sliding of the second seat body 51, so as to adjust the clamping force applied by the tightening plunger 83 on the second plunger 52, and then realize the adjustment of the kinetic energy of the second plunger 52.

[0106] Preferably, the driving block 82, the tightening plunger 83 and the tightening spring 84 are provided in plurality, and the number of the driving block 82, the tightening plunger 83 and the tightening spring 84 is the same; the number of the tightening plunger 83 is equal to the number of the second plunger 52; when the driving disk 81 is rotated, the plurality of driving blocks 82 can be synchronously controlled to slide radially along the second seat body 51 in the slide groove 515, thereby synchronously controlling the tightening plunger 83 to slide axially along the second seat body 51 in the fourth through hole 514, and then synchronously adjusting the clamping force applied to the plurality of second plungers 52, so that the plurality of second plungers 52 are subjected to the same clamping force, and then synchronously adjusting the ejection kinetic energy of the plurality of second plungers 52, so as to synchronously adjust the ejection speed of the plurality of loaders 6, so that the plurality of loaders 6 obtain the same ejection speed, thereby controlling the radial ejection range of the plurality of loaders 6, and then accurately controlling the radial distribution of the loaders 6, so as to accurately control the coverage range and coverage density of the conductive fiber group in the target area.

[0107] Preferably, if Fig.17 As shown, the second base body 51 is further provided with a fifth through hole 516 , and the fifth through hole 516 extends along the radial direction of the second base body 51 .

[0108] Preferably, a gear 812 is also provided on the driving disc 81 .

[0109] Preferably, if Fig.18 As shown, the adjustment mechanism 8 also includes a power piece 85, which is installed in the fifth through hole 516 and can rotate in the fifth through hole 516; one end of the power piece 85 is a driving button, and the other end is a gear end, and the gear end is engaged with the gear 812 on the driving disk 81. By rotating the driving button, the driving disk 81 can be driven to rotate, thereby realizing convenient and quick adjustment of the clamping force applied by the clamping plunger 83 on the second plunger 52.

[0110] Preferably, a locking groove 517 is further provided on the second seat body 51, and the locking groove 517 is opposite to the driving button; a plurality of locking grooves 517 are provided, and the plurality of locking grooves 517 are evenly arranged around the axis of the fifth through hole 516; a locking protrusion is provided on the driving button, and the locking protrusion is arranged opposite to the locking groove 517 and can be inserted into the locking groove 517; the adjustment mechanism 8 also includes a locking spring 86, and the locking spring 86 is arranged in the fifth through hole 516, and one end of the locking spring 86 is fixed to the inner wall of the fifth through hole 516 The locking protrusion, the locking groove 517 and the locking spring 86 constitute a locking structure, and the locking protrusion is always inserted into the locking groove 517 when not subjected to external force through the locking spring 86, so that the power piece 85 remains in a locked state, thereby locking the driving disk 81 to prevent the driving disk 81 from rotating into place and freely rotating when not subjected to external force, thereby avoiding fluctuations in the clamping force applied by the clamping plunger 83 on the second plunger 52.

[0111] When implementing, Fig.19 As shown, according to the specific coverage requirements of the target area, the adjustment mechanism 8 in each spreading unit is adjusted respectively to adjust the ejection range of the corresponding spreader 5 and the loader 6, thereby controlling the radial distribution density of the loader 6 after the ejection; the power out-of-control equipment is dropped above the target area, the cabin shell 3 is separated at a predetermined height, each spreading unit throws out the loader 6 according to the control sequence, and the loader 6 throws out the conductive fiber group, and the fiber bundle wound on the wire shaft can be quickly unfolded under the synergistic effect of the inertia of the wire shaft and the air resistance of the resistance blade. The unfolded fiber bundle forms a wire mesh, thereby increasing the spreading density of the fiber bundle, thereby increasing the probability of the fiber bundle falling on power facilities such as the power grid, and improving the efficiency of the power outage equipment in paralyzing the power system in the target area.

[0112] The above description is only a preferred specific implementation manner of the present invention, but the protection scope of the present invention is not limited thereto. Any changes or substitutions that can be easily conceived by any technician familiar with the technical field within the technical scope disclosed by the present invention should be covered within the protection scope of the present invention.

Claims

1. An electric energy out-of-control device for electromagnetic equipment targets, characterized in that: The invention comprises a front connector (1), a rear connector (2), a cabin shell (3), a spreading unit and a conductive fiber mass, wherein the conductive fiber mass is mounted on the spreading unit and the spreading unit is used for spreading the conductive fiber mass. The fiber bundles of the conductive fiber mass after being unfolded can be dropped on the power system.

2. The power out-of-control equipment for electromagnetic equipment according to claim 1, characterized in that: The spreading unit comprises a spreader (5) and a plurality of loaders (6) mounted on the spreader (5), and the loaders (6) can be thrown in multiple directions through the spreader (5).

3. The power out-of-control equipment for electromagnetic equipment according to claim 2, characterized in that: The loader (6) comprises a loading assembly (61); the loading assembly (61) comprises a third seat body (611) and a fourth energy body (612).

4. The power out-of-control equipment for electromagnetic equipment according to claim 3, characterized in that: The third base body (611) is provided with a fourth medicine cavity (6111) and a multi-layer third through hole (6112); the third through hole (6112) extends radially along the third base body (611) and is connected to the fourth medicine cavity (6111); the third through hole (6112) is used to install a conductive fiber group, and the conductive fiber group can be ejected along the axis of the third through hole (6112).

5. The power out-of-control equipment for electromagnetic equipment according to claim 4, characterized in that: The fourth medicine cavity (6111) includes a plurality of cavity segments.

6. The power out-of-control equipment for electromagnetic equipment according to claim 5, characterized in that: Furthermore, the diameter of the rear cavity section in the fourth medicine cavity (6111) is greater than the diameter of the front cavity section, so that the filling amount of the fourth energy body (612) in the rear cavity section is greater than the filling amount of the fourth energy body (612) in the front cavity section.

7. The power out-of-control equipment for electromagnetic equipment according to claim 6, characterized in that: Each cavity segment in the fourth medicine cavity (6111) is opposite to at least one layer of third through holes (6112).

8. The power out-of-control equipment for electromagnetic equipment according to claim 7, characterized in that: It also includes a separator (4), which is used to assist in separating the shell (31).

9. The power out-of-control equipment for electromagnetic equipment according to claim 8, characterized in that: The separator (4) comprises a first seat body (41), a first plunger (42) and a second energy body (43); the first plunger (42) and the second energy body (43) are both mounted on the first seat body (41); the first plunger (42) can be ejected in the radial direction of the first seat body (41); and the second energy body (43) is used to provide power for the first plunger (42) to eject in the radial direction of the first seat body (41).

10. The power out-of-control equipment for electromagnetic equipment according to claim 9, characterized in that: One end of the first plunger (42) contacts the housing (31), and the other end contacts the second energy body (43).

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