CN112484583A

CN112484583A - Shell filled with ten-ton-grade solid-liquid phase mixed fuel and having differential pressure stirring function

Info

Publication number: CN112484583A
Application number: CN202011209736.1A
Authority: CN
Inventors: 许志峰; 袁宝慧; 郭双锋
Original assignee: Xian Modern Chemistry Research Institute
Current assignee: Xian Modern Chemistry Research Institute
Priority date: 2020-11-03
Filing date: 2020-11-03
Publication date: 2021-03-12
Anticipated expiration: 2040-11-03
Also published as: CN112484583B

Abstract

The invention discloses a shell filled with ten-ton-grade solid-liquid phase mixed fuel and having a differential pressure stirring function, wherein the axis of a revolving body of a mixing chamber is superposed with the axis of a revolving body of an upper end cover, the mixing chamber is positioned at the upper end of the upper end cover, a certain gap is formed between a seventh lower end circular plane of the mixing chamber and a second upper end circular plane of the upper end cover, and one of a seventh lower end circular through hole axis of the mixing chamber is superposed with one of twelve second peripheral circular hole axes; the fuel is sucked into the mixing chamber by utilizing the pressure difference, and the layered solid-phase fuel and the layered liquid-phase fuel are re-mixed until the components are uniformly mixed, so that the concentration ratio of each component reaches the design value. The fuel can participate in detonation in a better concentration ratio when the warhead is detonated, and the power of the warhead can be ensured. The impact of the center of mass deviation of the warhead on the trajectory is avoided, and the target hitting precision is guaranteed.

Description

Shell filled with ten-ton-grade solid-liquid phase mixed fuel and having differential pressure stirring function

Technical Field

The invention belongs to the technical field of fuel filling shells, relates to a shell for filling ten-ton-grade solid-liquid phase mixed fuel, and particularly relates to a shell for filling ten-ton-grade solid-liquid phase mixed fuel and having a differential pressure stirring function.

Background

The high-energy liquid-phase fuel is thrown into the air through the explosive explosion throwing driving action, the high-energy liquid-phase fuel is atomized and mixed with the air to form a large-range active cloud cluster, and the active cloud cluster generates body detonation through secondary explosive initiation to release strong shock waves, so that the high-energy liquid-phase fuel weapon is one of the most powerful weapons.

The improvement of the explosive power of the body detonation warhead mainly depends on the improvement of the energy of the internally filled fuel, and the improvement is reported in the literature "high power FAE liquid fuel optimization selection" (fire and explosive bulletin 2016, page 14 of 3 rd year): the metal powder is added into the liquid fuel, the liquid fuel and the metal powder are mixed to form the solid-liquid mixed fuel, and the energy of the fuel in the body detonation warhead can be greatly improved due to the high heat value of the metal powder.

With competitive development of weapon technologies at home and abroad, the power demand on the weapon is further improved, and the most direct method for improving the power of the warhead is to increase the size of the warhead. Along with the gradual increase of the bearing capacity of the weapon platform, the carrying size is gradually increased, the large size of processing equipment is improved, the size of the warhead can be designed to be larger and larger, and at present, the weight of fuel loaded on the body detonation warhead can reach ten tons at most.

Because the solid-liquid phase mixed fuel can not be mutually dissolved and the densities of all components are different, the fuel with higher density in the solid-liquid phase mixed fuel can be settled to the lower part and the fuel with lower density can be lifted to the upper part under the action of gravity. The solid-liquid phase mixed fuel which is uniformly mixed can only be maintained for about one week, and the layering of the solid-phase fuel and the liquid-phase fuel is very obvious after more than one week through practical observation. When the body detonation warhead is actually applied, solid-phase fuel and liquid-phase fuel are inevitably layered after the charging is finished and the actual use is carried out for a plurality of years.

The proportion of each component given by the solid-liquid phase mixed fuel in the process of developing the formula is the proportion of the maximum power. Once the solid-liquid phase mixed fuel is layered, the fuel at each part cannot participate in the explosion reaction in the maximum power proportion during subsequent scattering and secondary detonation. The Wang ocean et al reported in the literature "Experimental study of cloud detonation characteristics of gas-liquid-solid three-phase system" (high pressure Physics, 12 months 2014, volume 28, pp 6, 671): when the proportions of the components of the solid-liquid mixture are different, the detonation pressure, the detonation velocity and the critical detonation energy of the body detonation are different greatly, and the power of the body detonation warhead is greatly reduced due to the change of the proportions of the components of the solid-liquid mixture.

After the solid-liquid phase mixed fuel is layered, the mass center of the body detonation warhead is changed along with the solid-liquid phase mixed fuel. The lie et al report in the document "trend toward centroid measurement and calibration technology" (measurement technology, 2016, vol 36, page 2, 1): in the field of national defense, the position of a mass center is related to the flight attitude, the flight speed and the flight direction of a warhead, and finally the trajectory of the warhead is influenced, the flight track of the warhead depends on the mass center, a guidance system and other factors, when the mass center of the warhead deviates from a flight plane, an additional moment is given to the warhead to change the motion track of the warhead, the radial mass center deviation of the warhead can cause the warhead to generate a yawing moment, the axial mass center deviation can cause the pitching moment of the warhead, and the serious mass center deviation can cause the warhead to lose balance or deviate from the track, so that the warhead cannot hit a target area, and therefore, the mass center deviation can cause the hit precision of the warhead on the target to be reduced.

For the small-volume and light-weight body detonation warhead, the internal layered solid-liquid phase fuel can be remixed by rolling back and forth before use, and the weight of the shell filled with ten tons of solid-liquid phase mixed fuel is too large to remix the internal fuel in a rolling mode.

Disclosure of Invention

In order to overcome the defects and defects of the prior art, the invention provides the shell which is filled with ten-ton-grade solid-liquid phase mixed fuel and has the function of differential pressure stirring, the fuel is sucked into the mixing chamber by utilizing the pressure difference, the layered solid phase fuel and the layered liquid phase fuel are mixed again until the mixture is uniform, and the concentration ratio of each component reaches the design value. The fuel can participate in detonation in a better concentration ratio when the warhead is detonated, and the power of the warhead can be ensured. The impact of the center of mass deviation of the warhead on the trajectory is avoided, and the target hitting precision is guaranteed.

The invention provides a shell filled with ten-ton-grade solid-liquid phase mixed fuel and having a differential pressure stirring function. The device comprises a shell 1, an upper end cover 2, a lower end cover 3, a scattering device 4 and a solid-liquid phase mixed fuel 6, and is characterized by also comprising a baffle 5, a mixing chamber 7 and a conduit 8;

the shape of the shell 1 is a first cylinder, the first cylinder of the shell 1 is a revolving body, the inner side surface of the first cylinder of the shell 1 is a first inner cylindrical surface, the upper end surface of the first cylinder of the shell 1 is a first upper end concentric torus, and the lower end surface of the first cylinder of the shell 1 is a first lower end concentric torus;

the axis of the revolution body of the shell 1 is vertical to the ground, and the shell 1 is an outer shell filled with ten-ton solid-liquid mixed materials;

the upper end cover 2 is in a second circular plate shape, the second circular plate of the upper end cover 2 is a revolving body, the upper end surface of the second circular plate of the upper end cover 2 is a second upper end circular plane, the lower end surface of the second circular plate of the upper end cover 2 is a second lower end circular plane, the center of the upper end cover 2 is provided with a second central circular hole, and the periphery of the upper end cover 2 is provided with twelve second peripheral circular holes which are uniformly distributed in the circumferential direction;

the axis of the revolving body of the upper end cover 2 coincides with the axis of the revolving body of the shell 1, the upper end cover 2 is positioned at the upper end of the shell 1, the diameter of a second circular plate of the upper end cover 2 is the same as the outer diameter of a first cylinder of the shell 1, and the edge of a second lower end circular plane of the upper end cover 2 is hermetically connected with a first upper end concentric circular ring surface of the shell 1;

the lower end cover 3 is in the shape of a third circular plate, the third circular plate of the lower end cover 3 is a revolving body, and the upper end surface of the third circular plate of the lower end cover 3 is a third upper end circular plane;

the axis of a revolving body of the lower end cover 3 is superposed with the axis of a revolving body of the shell 1, the lower end cover 3 is positioned at the lower end of the shell 1, the diameter of a third circular plate of the lower end cover 3 is the same as the outer diameter of a first cylinder of the shell 1, and the edge of a third upper end circular plane of the lower end cover 3 is hermetically connected with a first lower end concentric circular ring surface of the shell 1;

the shape of the scattering device 4 is a fourth cylinder, the fourth cylinder of the scattering device 4 is a revolving body, the upper end surface of the fourth cylinder of the scattering device 4 is a fourth upper end circular plane, the side surface of the fourth cylinder of the scattering device 4 is a fourth cylindrical surface, and the lower end surface of the fourth cylinder of the scattering device 4 is a fourth lower end circular plane;

the axis of a revolving body of the scattering device 4 coincides with the axis of a revolving body of the shell 1, explosives are arranged in the scattering device 4, the scattering device 4 is an energy source for scattering ten-ton-level solid-liquid mixed fuel, the scattering device 4 is positioned in the shell 1, the upper end of a fourth cylindrical surface of the scattering device 4 is hermetically connected with a second central circular hole of the upper end cover 2, a fourth upper end circular plane of the scattering device 4 is coplanar with a second upper end circular plane of the upper end cover 2, and a fourth lower end circular plane of the scattering device 4 is in contact with a third upper end circular plane of the lower end cover 3;

the baffle 5 is in the shape of a fifth rectangular plate, the front and the back of the fifth rectangular plate of the baffle 5 are rectangular, the upper end face of the fifth rectangular plate of the baffle 5 is a fifth upper narrow and long plane, the lower end face of the fifth rectangular plate of the baffle 5 is a fifth lower narrow and long plane, the left end face of the fifth rectangular plate of the baffle 5 is a fifth left narrow and long plane, the right end face of the fifth rectangular plate of the baffle 5 is a fifth right narrow and long plane, and the number of the baffles 5 is twelve;

the baffle 5 is positioned in the shell 1, twelve baffles 5 are uniformly distributed in the circumferential direction around the axis of the revolving body of the shell 1, the baffle 5 is positioned at the lower end of the upper end cover 2, a fifth upper end narrow and long plane of the baffle 5 is in sealing connection with a second lower end circular plane of the upper end cover 2, twelve second peripheral circular holes of the upper end cover 2 and twelve baffles 5 are arranged in a staggered manner in space, a baffle 5 is arranged between every two adjacent second peripheral circular holes of the upper end cover 2, a second peripheral circular hole of the upper end cover 2 is arranged between every two adjacent baffles 5, the baffle 5 is positioned at the upper end of the lower end cover 3, a certain gap is formed between the fifth lower end narrow and long plane of the baffle 5 and a third upper end circular plane of the lower end cover 3, a fifth left end narrow and long plane of the baffle 5 is in sealing connection with a fourth cylindrical surface of the scattering device 4, and a fifth right end narrow and long plane of the baffle 5 is in sealing connection with a first inner circle of;

the solid-liquid phase mixed fuel 6 is a ten-ton grade solid-liquid phase mixed material, solid and liquid are layered under the action of gravity, and the solid and liquid are uniformly mixed by the method;

solid-liquid phase mixed fuel 6 is filled in a closed space formed by the shell 1, the upper end cover 2, the lower end cover 3 and the scattering device 4, and the solid-liquid phase mixed fuel 6 is divided into twelve uniform parts by the baffle 5;

the shape of the mixing chamber 7 is a seventh cavity cylinder, the seventh cavity cylinder of the mixing chamber 7 is a revolving body, the upper end surface of the seventh cavity cylinder of the mixing chamber 7 is a seventh upper end circular plane, the center of the seventh upper end circular plane of the mixing chamber 7 is provided with a seventh upper end circular through hole, the lower end surface of the seventh cavity cylinder of the mixing chamber 7 is a seventh lower end circular plane, the eccentric position of the seventh lower end circular plane of the mixing chamber 7 is provided with a seventh lower end circular through hole, and the axial distance between the seventh lower end circular through hole of the mixing chamber 7 and the revolving body axial line of the mixing chamber 7 is the same as the distribution radius of twelve second peripheral circular holes of the upper end cover 2;

the axis of a revolving body of the mixing chamber 7 is coincided with the axis of a revolving body of the upper end cover 2, the mixing chamber 7 is positioned at the upper end of the upper end cover 2, a certain gap is reserved between the seventh lower end circular plane of the mixing chamber 7 and the second upper end circular plane of the upper end cover 2, and the axis of a seventh lower end circular through hole of the mixing chamber 7 is coincided with one of twelve second peripheral circular hole axes;

the conduit 8 is in the shape of an eighth round pipe, and the eighth round pipe of the conduit 8 is a revolving body;

the axis of the revolving body of the guide pipe 8 is parallel to the axis of the revolving body of the upper end cover 2, the lower end of an eighth round pipe of the guide pipe 8 is connected with one of the second peripheral round holes of the upper end cover 2, and the upper end of the eighth round pipe of the guide pipe 8 is connected with a seventh lower end round through hole of the mixing chamber 7;

a gap between a fifth lower end narrow and long plane of the baffle 5 and a third upper end circular plane of the lower end cover 3 is 6-9 mm;

the distance between the front and the back of the fifth rectangular plate of the baffle 5 is the thickness of the fifth rectangular plate of the baffle 5, and the thickness of the fifth rectangular plate of the baffle 5 is 5-8 mm;

the ratio of the volume of the seventh hollow cylinder of the mixing chamber 7 to the total volume of the solid-liquid phase mixed fuel 6 is 1: 5-6;

the distance between the seventh lower end circular plane of the mixing chamber 7 and the second upper end circular plane of the upper end cover 2 is 11-14 mm;

the shell filled with ten-ton-grade solid-liquid phase mixed fuel and having a differential pressure stirring function comprises the following steps of:

step 1: assembling a shell 1, an upper end cover 2, a lower end cover 3, a scattering device 4 and a baffle 5 into a warhead shell, wherein the baffle 5 divides the inner space of the warhead shell into twelve intervals;

step 2: filling solid-liquid phase mixed fuel 6 into a closed space formed by the shell 1, the upper end cover 2, the lower end cover 3 and the scattering device 4;

and step 3: connecting the lower end of the eighth round tube of the guide tube 8 with one of the second peripheral round holes of the upper end cover 2;

and 4, step 4: connecting the upper end of an eighth round pipe of the guide pipe 8 with a seventh lower end round through hole of the mixing chamber 7;

and 5: vacuumizing a seventh upper-end circular through hole of the mixing chamber 7, reducing the air pressure in the inner cavity of the mixing chamber 7, reducing the air pressure in a second peripheral circular hole connected with the guide pipe 8 in twelve second peripheral circular holes of the upper end cover 2, and still keeping the ambient air pressure in other second peripheral circular holes, forming pressure difference in the inner cavity of the warhead shell, sucking the solid-liquid phase mixed fuel 6 in the interval of the second peripheral circular hole connected with the guide pipe 8 in the warhead shell into the inner cavity of the mixing chamber 7 through the guide pipe 8, and allowing the solid-liquid phase mixed fuel 6 in other intervals in the warhead shell to flow into the inner cavity of the mixing chamber 7 through a gap between a fifth lower-end narrow long plane of the baffle plate 5 and a third upper-end circular plane of the lower end cover 3;

step 6: after the inner cavity of the mixing chamber 7 is filled with the solid-liquid phase mixed fuel 6, stopping vacuumizing the seventh upper end circular through hole of the mixing chamber 7, enabling the solid-liquid phase mixed fuel 6 in the mixing chamber 7 to flow downwards and enter the inner cavity of the warhead shell again, and connecting the lower end of the eighth circular pipe of the guide pipe 8 with the second peripheral circular hole of the upper end cover 2 next to the pointer;

and 7: and (5) repeating the step (5) and the step (6), lifting the solid-liquid phase mixed fuel (6) into the mixing chamber (7), and then putting the solid-liquid phase mixed fuel back into the inner cavity of the warhead shell, so that the solid-liquid phase fuel and the liquid phase fuel in the solid-liquid phase mixed fuel (6) are in relative motion and are mixed again until all the components in the solid-liquid phase mixed fuel (6) are mixed uniformly, disassembling the mixing chamber (7) and the conduit (8), and completely plugging the second peripheral circular hole of the upper end cover (2).

Regarding the gap between the fifth lower end long and narrow plane of the baffle 5 and the third upper end circular plane of the lower end cap 3, the thickness of the fifth rectangular plate of the baffle 5, the ratio of the volume of the seventh hollow cylinder of the mixing chamber 7 to the total volume of the solid-liquid phase mixed fuel 6, and the distance between the seventh lower end circular plane of the mixing chamber 7 and the second upper end circular plane of the upper end cap 2, any one of the following 2 methods may be adopted:

implementation mode 1: the gap between the fifth lower end narrow-long plane of the baffle 5 and the third upper end circular plane of the lower end cover 3 is 6 mm;

the distance between the front and the back of the fifth rectangular plate of the baffle 5 is the thickness of the fifth rectangular plate of the baffle 5, and the thickness of the fifth rectangular plate of the baffle 5 is 5 mm;

the ratio of the volume of the seventh hollow cylinder of the mixing chamber 7 to the total volume of the solid-liquid phase mixed fuel 6 is 1: 5;

the seventh lower circular plane of the mixing chamber 7 is at a distance of 11mm from the second upper circular plane of the upper end cap 2.

Implementation mode 2: the gap between the fifth lower end narrow-long plane of the baffle 5 and the third upper end circular plane of the lower end cover 3 is 9 mm;

the distance between the front and the back of the fifth rectangular plate of the baffle 5 is the thickness of the fifth rectangular plate of the baffle 5, and the thickness of the fifth rectangular plate of the baffle 5 is 8 mm;

the ratio of the volume of the seventh hollow cylinder of the mixing chamber 7 to the total volume of the solid-liquid phase mixed fuel 6 is 1: 6;

the seventh lower circular plane of the mixing chamber 7 is at a distance of 14mm from the second upper circular plane of the upper end cap 2.

The shell filled with ten-ton-grade solid-liquid phase mixed fuel and having the differential pressure stirring function has the following technical effects:

the internal space of the warhead shell is divided into twelve intervals, fuel in each interval is sucked into the mixing chamber by using pressure difference, layered solid-phase fuel and layered liquid-phase fuel are mixed again until the mixture is uniform, and the concentration ratio of each component reaches the design value. The invention uniformly stirs the fuel at any position in the shell without dead angle, the stirring work is completed within three days before the explosion of the warhead, the separation of each component is limited within three days after the stirring, the concentration ratio of each position is still within the allowable range, the fuel can participate in the detonation with the better concentration ratio when the warhead is detonated, and the power of the warhead can be ensured. The mass center offset of the body detonation warhead is within an acceptable error range, so that the influence of the mass center offset of the warhead on the trajectory is avoided, and the target hitting precision is guaranteed.

Drawings

Fig. 1 is a schematic structural diagram of a casing filled with ten-ton-grade solid-liquid phase mixed fuel and having a differential pressure stirring function. 1. The device comprises a shell, 2, an upper end cover, 3, a lower end cover, 4, a throwing device, 5, a baffle, 6, solid-liquid phase mixed fuel, 7, a mixing chamber, 8 and a guide pipe.

Detailed Description

The present invention is further described in detail with reference to the drawings and examples, it should be noted that the present invention is not limited to the following examples, and equivalent changes based on the technical scheme of the present invention are within the scope of the present invention.

Example 1:

as shown in fig. 1, this embodiment provides a casing filled with ten tons of solid-liquid phase mixed fuel and having a differential pressure stirring function. The device comprises a shell 1, an upper end cover 2, a lower end cover 3, a scattering device 4 and a solid-liquid phase mixed fuel 6, and is characterized by also comprising a baffle 5, a mixing chamber 7 and a conduit 8;

the using method and the working principle of the invention are as follows:

The working principle of the invention is as follows:

the solid-phase fuel and the liquid-phase fuel in the solid-liquid phase mixed fuel 6 are layered under the action of gravity, and the solid-phase fuel and the liquid-phase fuel in the solid-liquid phase mixed fuel 6 are subjected to relative motion, convection occurs, and the solid-phase fuel and the liquid-phase fuel are mixed again, so that the aim of uniform mixing can be fulfilled. The difficulty is that all solid-phase fuel and liquid-phase fuel in the solid-liquid phase mixed fuel 6 are required to be mixed, and the mixing needs a certain speed, and the mixing speed is enough to have enough mutual impact, so that the aim of uniform mixing can be achieved. The inner cavity of the warhead is divided into twelve sections, the upper end of one section is vacuumized, due to the pressure difference existing in the inner cavity of the warhead, solid-liquid phase mixed fuel 6 in the vacuumized section naturally flows upwards to enter a mixing chamber 7, the liquid level of solid-liquid phase mixed fuel 6 in other sections moves downwards, and solid-phase materials in the solid-liquid phase mixed fuel 6 are deposited at the lower end under the action of gravity, so that the solid-liquid phase mixed fuel 6 in other sections flows to the vacuumized section through a narrow gap between a baffle 5 and a lower end cover 3, the solid-phase materials deposited in the solid-liquid phase mixed fuel 6 at the lower end are impacted by the liquid flow in the solid-liquid phase mixed fuel 6, and the solid-liquid phase fuel and the liquid phase fuel in the solid-liquid phase mixed fuel 6 are relatively moved, and mixed. Because the solid-liquid phase mixed fuel 6 in the vacuumized interval in the inner cavity of the warhead is completely sucked into the mixing chamber 7, the liquid phase fuel and the solid phase fuel in the interval are all mixed, and through the other intervals which are vacuumized next to each other, finally, some fuel is mixed again, so that no dead angle can be ensured. The solid-liquid phase mixed fuel 6 which is uniformly re-mixed still can be layered under the action of gravity, but the layering has a time process, and experiments show that the liquid phase fuel has a certain year, is mixed with the solid phase fuel, the layering amount is limited within three days after the liquid phase fuel and the solid phase fuel are uniformly re-mixed, the concentration ratio of each position is still within an allowable range, and the mass center offset of the body detonation warhead is within an acceptable error range, so the solid-liquid phase mixed fuel has practical use significance.

When the gap between the fifth lower end long narrow plane of the baffle 5 and the third upper end circular plane of the lower end cover 3 is too large, the resistance to the flow of the solid-liquid phase fuel mixture 6 through the gap is reduced, the total flow rate of the solid-liquid phase fuel mixture 6 is the same, the gap is larger, the flow resistance of the solid-liquid phase fuel mixture 6 is smaller, the flow speed of the solid-liquid phase fuel mixture 6 is lower, the solid-liquid phase fuel in the solid-liquid phase fuel mixture 6 can be curled up and mixed with the liquid phase fuel in the solid-liquid phase fuel mixture 6 only if the flow speed of the solid-liquid phase fuel mixture 6 is sufficient because the solid phase fuel in the solid-liquid phase fuel mixture 6 is deposited at the lower end, that is, the gap is mainly located between the fifth lower end long narrow plane of the baffle 5 and the third upper end circular plane of the lower end cover 3, and if the flow speed of the solid-liquid phase fuel mixture 6 is too low, the solid phase fuel in, when the gap between the fifth lower end narrow long plane of the baffle 5 and the third upper end circular plane of the lower end cover 3 is too small, the resistance of the solid-liquid phase mixed fuel 6 flowing through the gap is too large, the gap is too small, the flow rate in unit time is too small, the working time is increased, and on the other hand, if the gap is too small, the solid phase mixed fuel in the solid-liquid phase mixed fuel 6 is easily and completely blocked, and the invention is invalid. Through a large amount of experiments, when the clearance between the narrow long plane of fifth lower extreme of baffle 5 and the third upper end circle plane of lower extreme lid 3 is 6 ~ 9mm, above-mentioned problem all can be avoided, and above-mentioned function all can be realized, satisfies the operation requirement.

In this embodiment, the gap between the fifth lower end narrow-long plane of the baffle 5 and the third upper end circular plane of the lower end cover 3 is 6 mm;

the distance between the front and the back of the fifth rectangular plate of the baffle 5 is the thickness of the fifth rectangular plate of the baffle 5, when the thickness of the fifth rectangular plate of the baffle 5 is too small, the strength of the fifth rectangular plate of the baffle 5 is insufficient, because the solid-liquid phase mixed fuel 6 is mixed by pressure difference, the inner layer and the outer layer of the fifth rectangular plate of the baffle 5 are subjected to different pressures, if the strength is insufficient, the rupture can occur, the failure of the invention can be caused, when the thickness of the fifth rectangular plate of the baffle 5 is too large, the cloud cluster formed by the subsequent fuel scattering of the warhead can be obstructed, and the power of the warhead can be reduced. A large number of experiments find that when the thickness of the fifth rectangular plate of the baffle 5 is 5-8 mm, the problems can be avoided, the functions can be realized, and the use requirement is met.

In this embodiment, the thickness of the fifth rectangular plate of the baffle 5 is 5 mm;

when the ratio of the volume of the seventh cavity cylinder of the mixing chamber 7 to the total volume of the solid-liquid phase mixed fuel 6 is too small, the volume of the seventh cavity cylinder of the mixing chamber 7 is too small, the solid-liquid phase mixed fuel 6 is sucked into the inner cavity of the seventh cavity cylinder of the mixing chamber 7 and then released for mixing, if the volume of the seventh cavity cylinder of the mixing chamber 7 is too small, the amount of mixing in each time is too small, the effect of uniform mixing cannot be achieved, and if the ratio of the volume of the seventh cavity cylinder of the mixing chamber 7 to the total volume of the solid-liquid phase mixed fuel 6 is too large, the volume of the solid-liquid phase mixed fuel 6 sucked into the inner cavity of the seventh cavity cylinder of the mixing chamber 7 is too large, and the time of each suction is too long, because the invention starts within 3 days before the experiment and needs to complete the mixing operation rapidly, the time is too long, which causes the invention to be. Through a large number of experiments, the ratio of the volume of the seventh hollow cylinder of the mixing chamber 7 to the total volume of the solid-liquid phase mixed fuel 6 is 1: 5-6, the problems can be avoided, the functions can be realized, and the use requirements are met.

In this embodiment, the ratio of the volume of the seventh hollow cylinder of the mixing chamber 7 to the total volume of the solid-liquid phase mixed fuel 6 is 1: 5;

in the invention, the solid-liquid phase mixed fuel 6 is mixed mainly by sucking the solid-liquid phase mixed fuel 6 into the inner cavity of the mixing chamber 7 and then putting the solid-liquid phase mixed fuel back into the inner cavity of the shell of the warhead part, if the gravitational potential energy increment is too small, the speed of putting the solid-liquid phase mixed fuel 6 back into the inner cavity of the shell of the warhead part is too small, the mixing effect is reduced, and the effect of full mixing cannot be achieved. When the distance between the seventh lower end circular plane of the mixing chamber 7 and the second upper end circular plane of the upper end cover 2 is too large, the solid-liquid phase mixed fuel 6 is lifted to the inner cavity of the mixing chamber 7, the increase of gravitational potential energy is too large, the speed of the solid-liquid phase mixed fuel 6 being put back to the inner cavity of the shell of the warhead is too large, the solid-liquid phase mixed fuel 6 easily overflows from the second peripheral circular holes of other upper end covers 2, and the total fuel amount filled in the warhead is reduced. A large number of experiments find that when the distance between the seventh lower end circular plane of the mixing chamber 7 and the second upper end circular plane of the upper end cover 2 is 11-14 mm, the problems can be avoided, the functions can be realized, and the use requirements are met.

In this embodiment, the distance from the seventh lower end circular plane of the mixing chamber 7 to the second upper end circular plane of the upper end cover 2 is 11 mm;

processing an original scheme of ten-ton-level warhead shell, filling solid-liquid phase mixed fuel 6, standing for one month, measuring the mass center of the warhead shell, and measuring the concentration distribution of each part of the warhead shell. The experimental result shows that the mass center offset exceeds 23% of the total length of the warhead, and the maximum deviation of concentration distribution of different parts exceeds 61%.

Ten warhead shells filled with ten tons of powder are processed, solid-liquid phase mixed fuel 6 is filled, the warhead shells are kept still for one month, the mass center of the warhead shells is measured, and the concentration distribution of each part of the warhead shells is measured, but the solid-liquid phase mixed fuel 6 is remixed by the invention three days before the measurement. The experimental result shows that the mass center offset is lower than 1% of the total length of the warhead, and the maximum deviation of concentration distribution of different parts exceeds 5%.

Example 2:

the using method and the working principle of the invention are as follows:

The working principle of the invention is as follows:

In this embodiment, the gap between the fifth lower end narrow-long plane of the baffle 5 and the third upper end circular plane of the lower end cover 3 is 9 mm;

In this embodiment, the thickness of the fifth rectangular plate of the baffle 5 is 8 mm;

In this embodiment, the ratio of the volume of the seventh hollow cylinder of the mixing chamber 7 to the total volume of the solid-liquid phase mixed fuel 6 is 1: 6;

In this embodiment, the distance from the seventh lower end circular plane of the mixing chamber 7 to the second upper end circular plane of the upper end cover 2 is 14 mm;

Claims

1. A shell filled with ten-ton-grade solid-liquid phase mixed fuel and having a differential pressure stirring function. The device comprises a shell (1), an upper end cover (2), a lower end cover (3), a scattering device (4) and solid-liquid phase mixed fuel (6), and is characterized by also comprising a baffle (5), a mixing chamber (7) and a guide pipe (8);

the shape of the shell (1) is a first cylinder, the first cylinder of the shell (1) is a revolving body, the inner side surface of the first cylinder of the shell (1) is a first inner cylindrical surface, the upper end surface of the first cylinder of the shell (1) is a first upper end concentric circular ring surface, and the lower end surface of the first cylinder of the shell (1) is a first lower end concentric circular ring surface;

the axis of the revolving body of the shell (1) is vertical to the ground, and the shell (1) is an outer shell filled with ten-ton solid-liquid mixed materials;

the upper end cover (2) is in a second circular plate shape, the second circular plate of the upper end cover (2) is a revolving body, the upper end face of the second circular plate of the upper end cover (2) is a second upper end circular plane, the lower end face of the second circular plate of the upper end cover (2) is a second lower end circular plane, the center of the upper end cover (2) is provided with a second central circular hole, and the periphery of the upper end cover (2) is provided with twelve second peripheral circular holes which are uniformly distributed in the circumferential direction;

the axis of the revolving body of the upper end cover (2) is superposed with the axis of the revolving body of the shell (1), the upper end cover (2) is positioned at the upper end of the shell (1), the diameter of a second circular plate of the upper end cover (2) is the same as the outer diameter of a first cylinder of the shell (1), and the edge of a second lower end circular plane of the upper end cover (2) is hermetically connected with a first upper end concentric circular ring surface of the shell (1);

the lower end cover (3) is in a shape of a third circular plate, the third circular plate of the lower end cover (3) is a revolving body, and the upper end surface of the third circular plate of the lower end cover (3) is a third upper end circular plane;

the axis of a revolving body of the lower end cover (3) is superposed with the axis of a revolving body of the shell (1), the lower end cover (3) is positioned at the lower end of the shell (1), the diameter of a third circular plate of the lower end cover (3) is the same as the outer diameter of a first cylinder of the shell (1), and the edge of a third upper end circular plane of the lower end cover (3) is hermetically connected with a first lower end concentric circular ring surface of the shell (1);

the throwing device (4) is in the shape of a fourth cylinder, the fourth cylinder of the throwing device (4) is a revolving body, the upper end surface of the fourth cylinder of the throwing device (4) is a fourth upper end circular plane, the side surface of the fourth cylinder of the throwing device (4) is a fourth cylindrical surface, and the lower end surface of the fourth cylinder of the throwing device (4) is a fourth lower end circular plane;

the axis of a revolving body of the scattering device (4) is coincident with the axis of a revolving body of the shell (1), explosives are arranged in the scattering device (4), the scattering device (4) is an energy source for scattering ten tons of solid-liquid mixed fuel, the scattering device (4) is positioned in the shell (1), the upper end of a fourth cylindrical surface of the scattering device (4) is hermetically connected with a second central circular hole of the upper end cover (2), a fourth upper end circular plane of the scattering device (4) is coplanar with a second upper end circular plane of the upper end cover (2), and a fourth lower end circular plane of the scattering device (4) is contacted with a third upper end circular plane of the lower end cover (3);

the baffle (5) is in a fifth rectangular plate shape, the front and the back of the fifth rectangular plate of the baffle (5) are rectangular, the upper end face of the fifth rectangular plate of the baffle (5) is a fifth upper-end narrow and long plane, the lower end face of the fifth rectangular plate of the baffle (5) is a fifth lower-end narrow and long plane, the left end face of the fifth rectangular plate of the baffle (5) is a fifth left-end narrow and long plane, the right end face of the fifth rectangular plate of the baffle (5) is a fifth right-end narrow and long plane, and the number of the baffles (5) is twelve;

the baffle plates (5) are positioned inside the shell (1), twelve baffle plates (5) are uniformly distributed in the circumferential direction around the axis of the revolution body of the shell (1), the baffle plates (5) are positioned at the lower end of the upper end cover (2), a fifth upper end narrow long plane of the baffle plates (5) is in sealing connection with a second lower end circular plane of the upper end cover (2), twelve second peripheral circular holes of the upper end cover (2) and the twelve baffle plates (5) are spatially arranged in a staggered manner, one baffle plate (5) is arranged between every two adjacent second peripheral circular holes of the upper end cover (2), a second peripheral circular hole of the upper end cover (2) is arranged between every two adjacent baffle plates (5), the baffle plates (5) are positioned at the upper end of the lower end cover (3), a certain gap is formed between a fifth lower end narrow long plane of the baffle plates (5) and a third upper end circular plane of the lower end cover (3), a fifth left end long plane of the baffle plates (5) is in sealing connection with a fourth cylindrical surface of the throwing device (4), the fifth right end narrow and long plane of the baffle (5) is hermetically connected with the first inner cylindrical surface of the shell (1);

the solid-liquid phase mixed fuel (6) is ten tons of solid-liquid phase mixed materials, solid and liquid are layered under the action of gravity, and the solid and liquid are uniformly mixed by the invention;

the solid-liquid phase mixed fuel (6) is filled in a closed space formed by the shell (1), the upper end cover (2), the lower end cover (3) and the scattering device (4), and the solid-liquid phase mixed fuel (6) is divided into twelve uniform parts by the baffle (5);

the shape of the mixing chamber (7) is a seventh cavity cylinder, the seventh cavity cylinder of the mixing chamber (7) is a revolving body, the upper end surface of the seventh cavity cylinder of the mixing chamber (7) is a seventh upper end circular plane, the center of the seventh upper end circular plane of the mixing chamber (7) is provided with a seventh upper end circular through hole, the lower end surface of the seventh cavity cylinder of the mixing chamber (7) is a seventh lower end circular plane, the eccentric position of the seventh lower end circular plane of the mixing chamber (7) is provided with a seventh lower end circular through hole, and the distance from the axis of the seventh lower end circular through hole of the mixing chamber (7) to the axis of the revolving body of the mixing chamber (7) is the same as the radius of the twelve second peripheral circular holes of the upper end cover (2);

the axis of a revolving body of the mixing chamber (7) is superposed with the axis of a revolving body of the upper end cover (2), the mixing chamber (7) is positioned at the upper end of the upper end cover (2), a certain gap is reserved between the seventh lower end circular plane of the mixing chamber (7) and the second upper end circular plane of the upper end cover (2), and the axis of a seventh lower end circular through hole of the mixing chamber (7) is superposed with one of the twelve second peripheral circular hole axes;

the shape of the conduit (8) is an eighth round pipe, and the eighth round pipe of the conduit (8) is a revolving body;

the axis of a revolving body of the guide pipe (8) is parallel to the axis of a revolving body of the upper end cover (2), the lower end of an eighth round pipe of the guide pipe (8) is connected with one of the second peripheral round holes of the upper end cover (2), and the upper end of the eighth round pipe of the guide pipe (8) is connected with a seventh lower end round through hole of the mixing chamber (7);

a gap between a fifth lower end narrow and long plane of the baffle (5) and a third upper end circular plane of the lower end cover (3) is 6-9 mm;

the distance between the front and the back of the fifth rectangular plate of the baffle plate (5) is the thickness of the fifth rectangular plate of the baffle plate (5), and the thickness of the fifth rectangular plate of the baffle plate (5) is 5-8 mm;

the ratio of the volume of the seventh cavity cylinder of the mixing chamber (7) to the total volume of the solid-liquid phase mixed fuel (6) is 1: 5-6;

the distance between the seventh lower end circular plane of the mixing chamber (7) and the second upper end circular plane of the upper end cover (2) is 11-14 mm;

step 1: assembling a shell (1), an upper end cover (2), a lower end cover (3), a scattering device (4) and a baffle (5) into a warhead shell, wherein the baffle (5) divides the inner space of the warhead shell into twelve intervals;

step 2: filling solid-liquid phase mixed fuel (6) in a closed space formed by the shell (1), the upper end cover (2), the lower end cover (3) and the scattering device (4);

and step 3: connecting the lower end of the eighth round pipe of the guide pipe (8) with one of the second peripheral round holes of the upper end cover (2);

and 4, step 4: the upper end of an eighth round pipe of the guide pipe (8) is connected with a seventh lower end round through hole of the mixing chamber (7);

and 5: vacuumizing a seventh upper end circular through hole of the mixing chamber (7), reducing the air pressure in an inner cavity of the mixing chamber (7), reducing the air pressure in a second peripheral circular hole connected with the guide pipe (8) in twelve second peripheral circular holes of the upper end cover (2), and keeping the ambient air pressure in other second peripheral circular holes, forming pressure difference in an inner cavity of the warhead shell, sucking solid-liquid phase mixed fuel (6) in a section of the second peripheral circular hole connected with the guide pipe (8) in the warhead shell into the inner cavity of the mixing chamber (7) through the guide pipe (8), and allowing the solid-liquid phase mixed fuel (6) in other sections in the warhead shell to flow to the inner cavity of the mixing chamber (7) through a gap between a fifth lower end narrow long plane of the baffle plate (5) and a third upper end circular plane of the lower end cover (3);

step 6: after the inner cavity of the mixing chamber (7) is filled with the solid-liquid phase mixed fuel (6), stopping vacuumizing the seventh upper-end circular through hole of the mixing chamber (7), enabling the solid-liquid phase mixed fuel (6) in the mixing chamber (7) to flow downwards and enter the inner cavity of the warhead shell again, and connecting the lower end of an eighth circular pipe of the guide pipe (8) with a second peripheral circular hole of an upper end cover (2) next to the pointer;

and 7: and (5) repeating the step (5) and the step (6), lifting the solid-liquid phase mixed fuel (6) into the mixing chamber (7), and then putting the solid-liquid phase mixed fuel back into the inner cavity of the warhead shell, so that the solid-liquid phase fuel and the liquid phase fuel in the solid-liquid phase mixed fuel (6) perform relative motion and are mixed again until all components in the solid-liquid phase mixed fuel (6) are completely and uniformly mixed, disassembling the mixing chamber (7) and the conduit (8), and completely blocking the second peripheral circular hole of the upper end cover (2).

2. The shell filled with ten-ton-grade solid-liquid phase mixed fuel and having the differential pressure stirring function as claimed in claim 1, wherein the gap between the fifth lower end long narrow plane of the baffle plate (5) and the third upper end circular plane of the lower end cover (3) is 6 mm;

the distance between the front and the back of the fifth rectangular plate of the baffle plate (5) is the thickness of the fifth rectangular plate of the baffle plate (5), and the thickness of the fifth rectangular plate of the baffle plate (5) is 5 mm;

the ratio of the volume of the seventh cavity cylinder of the mixing chamber (7) to the total volume of the solid-liquid phase mixed fuel (6) is 1: 5;

the distance between the seventh lower end circular plane of the mixing chamber (7) and the second upper end circular plane of the upper end cover (2) is 11 mm.

3. The shell filled with ten-ton-grade solid-liquid phase mixed fuel and having the differential pressure stirring function as claimed in claim 1, wherein the gap between the fifth lower end long narrow plane of the baffle plate (5) and the third upper end circular plane of the lower end cover (3) is 9 mm;

the distance between the front and the back of the fifth rectangular plate of the baffle plate (5) is the thickness of the fifth rectangular plate of the baffle plate (5), and the thickness of the fifth rectangular plate of the baffle plate (5) is 8 mm;

the ratio of the volume of the seventh cavity cylinder of the mixing chamber (7) to the total volume of the solid-liquid phase mixed fuel (6) is 1: 6;

the distance between the seventh lower end circular plane of the mixing chamber (7) and the second upper end circular plane of the upper end cover (2) is 14 mm.