CN115388722A - Automatic internal pressure adjusting device with movable end cover - Google Patents
Automatic internal pressure adjusting device with movable end cover Download PDFInfo
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- CN115388722A CN115388722A CN202211011837.7A CN202211011837A CN115388722A CN 115388722 A CN115388722 A CN 115388722A CN 202211011837 A CN202211011837 A CN 202211011837A CN 115388722 A CN115388722 A CN 115388722A
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- detonation warhead
- movable end
- shell
- end cover
- body detonation
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F42—AMMUNITION; BLASTING
- F42B—EXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
- F42B33/00—Manufacture of ammunition; Dismantling of ammunition; Apparatus therefor
- F42B33/02—Filling cartridges, missiles, or fuzes; Inserting propellant or explosive charges
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F42—AMMUNITION; BLASTING
- F42B—EXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
- F42B33/00—Manufacture of ammunition; Dismantling of ammunition; Apparatus therefor
- F42B33/02—Filling cartridges, missiles, or fuzes; Inserting propellant or explosive charges
- F42B33/0278—Safety arrangements therefor
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- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02E—REDUCTION OF GREENHOUSE GAS [GHG] EMISSIONS, RELATED TO ENERGY GENERATION, TRANSMISSION OR DISTRIBUTION
- Y02E30/00—Energy generation of nuclear origin
- Y02E30/30—Nuclear fission reactors
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- General Engineering & Computer Science (AREA)
- Pressure Vessels And Lids Thereof (AREA)
Abstract
The invention discloses a movable end cover type internal pressure automatic adjusting device which comprises fuel, a body detonation warhead shell, a movable end cover and two-section type scattering devices, wherein the upper parts of the two-section type scattering devices are in the shape of a third upper end cylinder, the lower parts of the two-section type scattering devices are in the shape of a third lower end cylinder, the upper ends of third soft ropes are connected with the lower end face of the third upper end cylinder, and the lower ends of the third soft ropes are connected with the upper end face of the third lower end cylinder; the axis of a revolving body of the two-section type scattering device is superposed with the axis of a revolving body of the shell of the body detonation warhead, the upper end surface of a third upper end cylinder of the two-section type scattering device is connected with the lower end surface of a first circular plate of the shell of the body detonation warhead, and the lower end surface of a third lower end cylinder of the two-section type scattering device is connected with the upper end surface of a second circular plate of the movable end cover; the device adopts the movable end cover to adjust the volume of the inner cavity by moving up and down, compensates the volume change of fuel caused by thermal expansion and cold contraction, avoids overlarge internal stress and ensures the safety of the shell of the body detonation warhead.
Description
Technical Field
The invention belongs to the technical field of adjusting devices, relates to an internal pressure adjusting device, and particularly relates to an automatic movable end cover type internal pressure adjusting device.
Background
The body detonation warhead is internally filled with high-energy fuel, the high-energy fuel is thrown into the air under the action of explosive detonation throwing driving action, the high-energy fuel is mixed with the air to form a large-range active cloud cluster, and the active cloud cluster generates body detonation and releases strong shock waves after secondary detonation of the explosive, so that the body detonation warhead is one of weapons with the greatest power.
The body detonation warhead can normally work at the ambient temperature of minus 40-70 ℃, and the expansion coefficient of the high-energy fuel is (1.24 multiplied by 10) -3 ) Warhead case (1.22X 10) -5 ) The high-energy fuel is an incompressible material, the internal stress of the shell of the warhead part after the high-energy fuel expands at high temperature is very high, the shell is usually of a thin-wall structure in order not to influence the throwing range of the high-energy fuel, and the warhead part is damaged at a weak position due to the too high internal stress, so that liquid agent leakage is caused, and major accidents are caused.
The Chinese patent application ' isobaric adjusting device for compensating the volume change of liquid-phase charges at different temperatures ' (application number: 201911033140.8, 10 months in 2019) ', discloses an isobaric adjusting device for compensating the volume change of liquid-phase charges at different temperatures, when the volume of liquid changes after expansion with heat and contraction with cold, the volume change of an inner cavity caused by the movement of a piston is compensated, the pressure of the inner cavity and the external pressure are always kept the same in the movement process of the piston, and the strength of a shell is ensured.
The standard document "experimental study of FAE fuel and explosive throwing and fire-leaping failure" (academic report of explosives and powders, 2001, 3 rd 37 pages): in the process of throwing the body detonation warhead, if three elements of fuel consumption are met: temperature, fuel, oxygen, will take place to ignite in advance, and the ignition in advance will lead to the body detonation warhead power very big reduction.
Since the patent is the subject of earlier research by the applicant, the following problems occur in the popularization and application process of the device:
the device contains air, is placed in an inner cavity of a shell of the body detonation warhead and is wrapped by high-energy fuel, when explosive is thrown in an explosion mode, the air wrapped by the high-energy fuel is compressed, the temperature rises rapidly, three burning-up factors (temperature, fuel and oxygen) are met simultaneously, and the phenomenon of pre-ignition is generated. Accordingly, there is a need for improvements to the above patents.
Disclosure of Invention
Aiming at the technical problem of pre-ignition phenomenon in the body detonation warhead throwing process in the prior art, the invention aims to provide an automatic pressure regulating device with a movable end cover.
In order to realize the task, the invention adopts the following technical solution:
the utility model provides a pressure automatic regulating apparatus in movable end cap formula, includes fuel, its characterized in that still includes body detonation warhead casing, movable end cap 2 and two sections formula throwing device 3, wherein:
the shell 1 of the body detonation warhead part is a revolving body, and the axis of the revolving body is vertical to the ground;
the body detonation warhead shell 1 consists of an upper part, a middle part and a lower part, wherein the upper part is a first circular plate, the middle part is a first cylinder, and the other part is a first concentric circular plate;
the inner side of the upper end surface of the first concentric circular plate is provided with a circle of first upper end annular boss, the inner side of the lower end surface of the first concentric circular plate is provided with a circle of first lower end annular boss, and the middle part of the inner side cylindrical surface of the first concentric circular plate is provided with a circle of first annular groove;
the movable end cover is in the shape of a second circular plate and is a revolving body;
the revolving body axis of the movable end cover is superposed with the revolving body axis of the body detonation warhead shell, the movable end cover is positioned in the first annular groove of the body detonation warhead shell, and the thickness of the second circular plate of the movable end cover is smaller than the width of the first annular groove of the body detonation warhead shell;
the two-section type scattering device is a revolving body, and the axis of the revolving body is superposed with the axis of the revolving body of the shell of the detonation warhead;
the two-section type throwing device consists of an upper part, a middle part and a lower part, wherein the upper part is in the shape of a third upper end cylinder, the lower part is in the shape of a third lower end cylinder, and the middle part is in the shape of a third soft rope; the upper end of the third soft rope is connected with the lower end face of the third upper end cylinder, and the lower end of the third soft rope is connected with the upper end face of the third lower end cylinder;
the two-section type scattering device is positioned in the inner cavity of the body detonation warhead shell, the upper end surface of a third upper end cylinder of the two-section type scattering device is connected with the lower end surface of a first circular plate of the body detonation warhead shell, and the lower end surface of a third lower end cylinder of the two-section type scattering device is connected with the upper end surface of a second circular plate of the movable end cover;
the fuel is the scattered explosive and the fuel and is filled in a sealed space formed by the shell of the body detonation warhead and the movable end cover;
the ratio of the distance between the lower end face of the first annular groove and the lower end face of the first lower end annular boss of the body detonation warhead shell and the thickness of the second circular plate of the movable end cover is 1:0.8 to 0.85.
The use method of the movable end cap type automatic internal pressure adjusting device. The method is characterized by comprising the following steps:
step 1: assembling the two-section type throwing device with a body detonation warhead shell;
step 2: filling fuel into an inner cavity of a shell of the detonation warhead;
and 3, step 3: assembling a movable end cover with a two-section type scattering device and a body detonation warhead shell, wherein the upper end face of a second circular plate of the movable end cover is 5mm away from the upper end face of a first annular groove of the body detonation warhead shell, and the lower end face of the second circular plate of the movable end cover is 14mm away from the lower end face of the first annular groove of the body detonation warhead shell;
and 4, step 4: when the environmental temperature rises, the fuel is heated, the volume of the fuel is increased, the movable end cover moves downwards, the volume of a sealed space formed by the body detonation warhead shell and the movable end cover is increased, the internal stress of the fuel is not too large, the first cylinder body of the body detonation warhead shell is not propped up, and the safety of the body detonation warhead shell is ensured;
when the ambient temperature reduces, the shrinkage takes place for the fuel, and the volume of fuel reduces, and movable end cover moves upwards, and the confined space volume that body detonation warhead casing and movable end cover are constituteed reduces, and the internal stress of fuel is unlikely to too big, and the first cylinder of body detonation warhead casing is unlikely to be propped up badly, has guaranteed the security of body detonation warhead casing.
Regarding the ratio of the distance between the lower end surface of the first annular groove and the lower end surface of the first lower end annular boss of the body detonation warhead shell and the thickness of the second circular plate of the movable end cover, any one of the following 2 modes can be adopted:
implementation mode 1: the ratio of the distance between the lower end face of the first annular groove and the lower end face of the first lower end annular boss of the shell of the body detonation warhead and the thickness of the second circular plate of the movable end cover 2 is 1:0.8.
implementation mode 2: the ratio of the distance between the lower end face of the first annular groove and the lower end face of the first lower end annular boss of the shell of the body detonation warhead and the thickness of the second circular plate of the movable end cover is 1:0.85.
the invention relates to a movable end cover type automatic internal pressure adjusting device, which brings technical innovation that:
the movable end cover in the movable end cover type internal pressure automatic regulating device regulates the volume of the inner cavity by moving up and down, compensates the volume change of fuel caused by thermal expansion and cold contraction, avoids overlarge internal stress and ensures the safety of the shell. Meanwhile, air is not in the inner cavity of the shell, when explosive is exploded and scattered, no air is compressed in the fuel, the three factors of fuel consumption are not satisfied, the phenomenon of pre-ignition cannot occur, and the power of the detonation warhead cannot be influenced.
Drawings
Fig. 1 is a schematic structural diagram of the automatic internal pressure regulating device with a movable end cover of the invention. The symbols in the figures represent: 1. the body detonation warhead comprises a body detonation warhead shell part, 2, a movable end cover, 3, a two-section type scattering device, 4 and fuel.
The present invention will be described in further detail with reference to the accompanying drawings and examples.
Detailed Description
First, the following examples are preferred examples of the present invention. The present invention is not limited to the following examples, and any additions and equivalent changes based on the technical solution of the present invention are within the scope of the present invention.
Example 1:
as shown in fig. 1, the present embodiment provides an automatic internal pressure adjusting device with a movable end cap, which includes a body detonation warhead housing 1, a movable end cap 2, a two-section type scattering device 3 and fuel 4, wherein:
the shell 1 of the body detonation warhead part is a revolving body, and the axis of the revolving body is vertical to the ground;
the body detonation warhead shell 1 consists of an upper part, a middle part and a lower part:
the shape of the upper part of the body detonation warhead casing 1 is a first circular plate;
the shape of the middle part of the body detonation warhead shell 1 is a first cylinder;
the shape of the lower part of the body detonation warhead shell 1 is a first concentric circular plate;
the inner side of the upper end surface of a first concentric circular plate of the body detonation warhead shell 1 is provided with a circle of first upper end annular boss, the inner side of the lower end surface of the first concentric circular plate is provided with a circle of first lower end annular boss, and the middle part of the inner side cylindrical surface of the first concentric circular plate is provided with a circle of first annular groove;
the shape of the movable end cover 2 is a second circular plate and is a revolving body;
the revolving body axis of the movable end cover 2 is superposed with the revolving body axis of the body detonation warhead shell 1, the movable end cover 2 is positioned in a first annular groove of the body detonation warhead shell 1, and the thickness of a second circular plate of the movable end cover 2 is smaller than the width of the first annular groove of the body detonation warhead shell 1;
the two-section type scattering device 3 is a revolving body, and the two-section type scattering device 3 consists of an upper part, a middle part and a lower part: the upper part is in the shape of a third upper end cylinder, the lower part is in the shape of a third lower end cylinder, and the middle part is in the shape of a third soft rope;
the upper end of the third soft rope is connected with the lower end face of the third upper end cylinder, and the lower end of the third soft rope is connected with the upper end face of the third lower end cylinder;
the axis of a revolving body of the two-section type scattering device 3 is superposed with the axis of a revolving body of the shell body detonation warhead 1, the two-section type scattering device 3 is positioned in the inner cavity of the shell body detonation warhead 1, the upper end surface of a third upper end cylinder of the two-section type scattering device 3 is connected with the lower end surface of a first circular plate of the shell body detonation warhead 1, and the lower end surface of a third lower end cylinder of the two-section type scattering device 3 is connected with the upper end surface of a second circular plate of the movable end cover 2;
the fuel 4 is the scattered explosive and the fuel and is filled in a sealed space formed by the body detonation warhead shell 1 and the movable end cover 2.
The use method of the movable end cover type automatic internal pressure adjusting device comprises the following steps:
step 1: assembling a two-section throwing device 3 with a body detonation warhead housing 1;
step 2: filling fuel 4 into the inner cavity of the body detonation warhead shell 1;
and step 3: assembling a movable end cover 2 with a two-section type throwing device 3 and a body detonation warhead shell 1, wherein the upper end surface of a second circular plate of the movable end cover 2 is 5mm away from the upper end surface of a first annular groove of the in-vitro detonation warhead shell 1, and the lower end surface of the second circular plate of the movable end cover 2 is 4mm away from the lower end surface of the body detonation warhead shell 1 of the in-vitro detonation warhead shell 1;
and 4, step 4: when the environmental temperature rises, the fuel 4 is heated, the volume of the fuel 4 is increased, the movable end cover 2 moves downwards, the volume of a sealed space formed by the body detonation warhead shell 1 and the movable end cover 2 is increased, the internal stress of the fuel 4 is not too large, the first cylinder of the body detonation warhead shell 1 is not damaged by being supported, and the safety of the body detonation warhead shell 1 is ensured;
when the ambient temperature reduces, the shrinkage takes place for fuel 4, and the volume of fuel 4 reduces, and movable end cover 2 rebound, and the confined space volume that body detonation warhead casing 1 and movable end cover 2 constitute reduces, and the internal stress of fuel 4 is unlikely to too big, and the first cylinder of body detonation warhead casing 1 is unlikely to be propped up badly, has guaranteed the security of body detonation warhead casing 1.
The working principle of the automatic adjusting device for the internal pressure of the movable end cover is as follows:
the shell of the body detonation warhead is a thin-wall shell, the internal pressure bearing capacity is lower, and the volume expansion coefficient of the high-energy fuel in the body detonation warhead is larger than that of the shell, so that after the temperature is increased, the high-energy fuel expands to generate internal stress which is enough to break the shell.
In order to solve the problem of excessive internal stress after temperature rise, the movable end cover type internal pressure automatic regulating device of the embodiment adopts the movable end cover 2 which can move up and down in the first annular groove of the body detonation warhead shell 1, during upward movement, the space of high-energy fuel becomes smaller, during downward movement, the space of the high-energy fuel becomes larger, that is, the volume of the body detonation warhead shell 1 of the embodiment can be freely regulated, through regulating the volume, the volume is consistent with the volume of the high-energy fuel after thermal expansion and cold contraction, the generation of the internal stress is avoided, and the body detonation warhead shell is protected.
However, if air exists in the shell of the body detonation warhead, the air is wrapped by high-energy fuel, and when the explosive is thrown, the air is compressed to form hot spots, so that fire leaps are caused.
Because the inner cavity of the shell of the body detonation warhead is not provided with air, the fire leaping factor is avoided.
After the explosive is exploded and thrown, the temperature of the explosion product of the explosive is air but no fuel, the three burning factors are not satisfied, the high-energy fuel moves outwards to form a cloud cluster, the fuel is air but no temperature, and the three burning factors are not satisfied, so that the occurrence of fire leaping can be avoided.
In this embodiment, the body detonation warhead casing 1 is a casing of a body detonation warhead, and is used for loading and throwing explosives and fuel.
The movable end cap 2 is an innovation of the automatic adjusting device for the internal pressure of the movable end cap in the embodiment, the volume is adjusted by moving the movable cover plate 2 up and down, and air is not introduced into the shell 1 of the body detonation warhead.
The two-section type scattering device 3 contains explosives which are a power source for scattering fuel to form a cloud cluster, the two-section type scattering device 3 is composed of an upper section and a lower section, a third soft rope is a detonating cord and can propagate explosion, and the upper section and the lower section of the two-section type scattering device 3 are connected through the third soft rope.
The fuel 4 is a throwing explosive and fuel (also called high-energy fuel) filled inside the body detonation warhead.
The movable end cover 2 is assembled with the two-section type throwing device 3 and the body detonation warhead shell 1, the upper end face of a second circular plate of the movable end cover 2 is 5mm away from the upper end face of a first annular groove of the body detonation warhead shell 1, and the lower end face of the second circular plate of the movable end cover 2 is 14mm away from the lower end face of the first annular groove of the body detonation warhead shell 1. The installation is that considering thermal expansion and cold contraction simultaneously, the second plectane of movable end cover 2 can upwards remove also can downwards remove, considers actual conditions, and the temperature is reduced to minimum, and high energy fuel volume contracts to minimum, and movable end cover 2 upwards removes 5mm, and the volume of body detonation warhead casing 1 just is unanimous with fuel 4 volume, therefore design so. Similarly, the temperature is raised to the maximum, the volume of the high-energy fuel is increased to the maximum, the movable end cover 2 moves downwards by 14mm, and the volume of the body detonation warhead shell 1 is exactly consistent with the volume of the fuel, so the design is carried out. If the margin is too large, the stiffness is too large, and if the margin is insufficient, the adjusting capability is insufficient, and the internal stress is generated.
The inventor finds in tests that after the two-section type scattering device 3 explodes, the fuel 4 is scattered to form a cloud cluster, the shell 1 of the body detonation warhead part is impacted by explosive explosion in the two-section type scattering device 3 and moves upwards, the movable end cover 2 is impacted by explosive explosion in the two-section type scattering device 3 and moves downwards, and when the cloud cluster is flat, the subsequent power is the largest, and if the cloud cluster is irregular in shape, the explosion power is also influenced.
When the ratio of the distance between the lower end face of the first annular groove and the lower end face of the first lower annular boss of the body detonation warhead shell 1 to the thickness of the second circular plate of the movable end cover 2 is too small, the distance between the lower end face of the first annular groove and the lower end face of the first lower annular boss of the body detonation warhead shell 1 is too small, the movable end cover 2 is supported by the thickness of the part, namely, the supporting capacity for the movable end cover 2 is insufficient, the movable end cover 2 moves downwards after being impacted by explosive, and when the supported force of the movable end cover 2 is insufficient, the movable end cover 2 is firstly damaged, shells above and below a cloud cluster are damaged asymmetrically, a regular flat cylindrical cloud cluster cannot be formed, and the subsequent power is influenced.
When the ratio of the distance between the lower end surface of the first annular groove and the lower end surface of the first lower annular boss of the body detonation warhead shell 1 to the thickness of the second circular plate of the movable end cover 2 is too large, the distance between the lower end surface of the first annular groove and the lower end surface of the first lower annular boss of the body detonation warhead shell 1 is too large, which causes the stiffness to be too large and influences the fuel loading amount.
Through partial theoretical calculation, workers with relevant working experience are summoned to conduct collective consultation and discussion, the problems are resolved, and each module is subjected to experimental evaluation independently. The final experimental evaluation results show that the ratio of the distance between the lower end surface of the first annular groove and the lower end surface of the first lower end annular boss of the body detonation warhead shell 1 and the thickness of the second circular plate of the movable end cover 2 is 1: 0.8-0.85, the above problems can be avoided, the design advantages of the automatic movable end cap type internal pressure adjusting device of the present embodiment can be embodied, so that the functions can be well exerted, and the technical problems can be well solved by using the automatic movable end cap type internal pressure adjusting device of the present embodiment.
In this embodiment, the ratio of the distance between the lower end surface of the first annular groove and the lower end surface of the first lower annular boss of the body detonation warhead housing 1 and the thickness of the second circular plate of the movable end cap 2 is designed to be 1:0.8;
the ten movable end cover type internal pressure automatic adjusting devices of the embodiment are processed and used according to the using method of the device, and are respectively stored in the environment of +80 ℃ and-60 ℃, the shell 1 of the body detonation warhead is not damaged, the cloud cluster formed by the detonation two-section type throwing device 3 is flat and cylindrical, and fire leaping does not occur, so that the effect of the movable end cover type internal pressure automatic adjusting devices of the embodiment is proved.
According to the movable end cover type internal pressure automatic adjusting device, the movable end cover is adopted to adjust the volume of the inner cavity through up and down movement, so that the volume change caused by thermal expansion and cold contraction of fuel is compensated, the overlarge internal stress is avoided, and the safety of the shell of the body detonation warhead is ensured. Meanwhile, air does not exist in the inner cavity of the shell of the body detonation warhead, when explosive is thrown in an explosion mode, air is not compressed inside fuel, the three burning factors are not satisfied, the phenomenon of pre-ignition cannot occur, and the power of the body detonation warhead cannot be influenced.
Example 2:
example 2 differs from example 1 in that:
in this embodiment, the ratio of the distance between the lower end surface of the first annular groove and the lower end surface of the first lower annular boss of the body detonation warhead housing 1 and the thickness of the second circular plate of the movable end cap 2 is 1:0.85;
the ten movable end cover type internal pressure automatic adjusting devices of the embodiment are processed and used according to the using method of the device, and are respectively stored in the environment of +80 ℃ and-60 ℃, the shell 1 of the body detonation warhead is not damaged, the cloud cluster formed by the detonation two-section type throwing device 3 is flat and cylindrical, and fire leaping does not occur, so that the effect of the movable end cover type internal pressure automatic adjusting devices of the embodiment is proved.
According to the automatic internal pressure adjusting device with the movable end cover, the volume of the inner cavity is adjusted by the movable end cover through moving up and down, so that the volume change caused by thermal expansion and cold contraction of fuel is compensated, the overlarge internal stress is avoided, and the safety of the shell of the body detonation warhead is ensured. Meanwhile, air does not exist in the inner cavity of the shell of the body detonation warhead, when explosive is thrown in an explosion mode, air is not compressed inside fuel, the three burning factors are not satisfied, the phenomenon of pre-ignition cannot occur, and the power of the body detonation warhead cannot be influenced.
Claims (4)
1. The utility model provides a pressure automatic regulating apparatus in movable end cap formula, includes fuel (4), its characterized in that still includes body detonation warhead casing (1), movable end cap (2) and two sections formula scattering device (3), wherein:
the shell (1) of the body detonation warhead part is a revolving body, and the axis of the revolving body is vertical to the ground;
the shell (1) of the body detonation warhead consists of an upper part, a middle part and a lower part, wherein the upper part is in the shape of a first circular plate, the middle part is in the shape of a first cylinder, and the lower part is in the shape of a first concentric circular plate;
the inner side of the upper end surface of the first concentric circular plate is provided with a circle of first upper end annular boss, the inner side of the lower end surface of the first concentric circular plate is provided with a circle of first lower end annular boss, and the middle part of the inner side cylindrical surface of the first concentric circular plate is provided with a circle of first annular groove;
the shape of the movable end cover (2) is a second circular plate and is a revolving body;
the revolving body axis of the movable end cover (2) is superposed with the revolving body axis of the body detonation warhead shell (1), the movable end cover (2) is positioned in a first annular groove of the body detonation warhead shell (1), and the thickness of a second circular plate of the movable end cover (2) is smaller than the width of the first annular groove of the body detonation warhead shell (1);
the two-section type throwing device (3) is a revolving body, and the axis of the revolving body is superposed with the axis of the revolving body of the shell (1) of the detonation warhead part;
the two-section type throwing device (3) consists of an upper part, a middle part and a lower part, wherein the upper part is in the shape of a third upper end cylinder, the lower part is in the shape of a third lower end cylinder, and the middle part is in the shape of a third soft rope; the upper end of the third soft rope is connected with the lower end face of the third upper end cylinder, and the lower end of the third soft rope is connected with the upper end face of the third lower end cylinder;
the two-section type scattering device (3) is positioned in the inner cavity of the body detonation warhead shell (1), the upper end surface of a third upper end cylinder of the two-section type scattering device (3) is connected with the lower end surface of a first circular plate of the body detonation warhead shell (1), and the lower end surface of a third lower end cylinder of the two-section type scattering device (3) is connected with the upper end surface of a second circular plate of the movable end cover (2);
the fuel (4) is a scattered explosive and a fuel and is filled in a sealed space formed by the body detonation warhead shell (1) and the movable end cover (2);
the ratio of the distance between the lower end face of the first annular groove and the lower end face of the first lower end annular boss of the body detonation warhead shell (1) and the thickness of the second circular plate of the movable end cover (2) is 1:0.8 to 0.85.
2. The automatic adjusting device for internal pressure of movable end cap type according to claim 1, wherein the ratio of the distance between the lower end surface of the first annular groove and the lower end surface of the first lower annular boss of the body detonation warhead shell (1) and the thickness of the second circular plate of the movable end cap (2) is 1:0.8.
3. the automatic adjusting device for internal pressure of movable end cap type according to claim 1, wherein the ratio of the distance between the lower end surface of the first annular groove and the lower end surface of the first lower annular boss of the body detonation warhead shell (1) and the thickness of the second circular plate of the movable end cap (2) is 1:0.85.
4. the use method of the automatic adjusting device for the internal pressure of the movable end cover type as claimed in one of the claims 1 to 3 is characterized by comprising the following steps:
step 1: assembling a two-section throwing device (3) with a body detonation warhead housing (1);
step 2: filling fuel (4) into the inner cavity of the body detonation warhead shell (1);
and step 3: assembling a movable end cover (2), a two-section type scattering device (3) and a body detonation warhead shell (1), wherein the upper end face of a second circular plate of the movable end cover (2) is 5mm away from the upper end face of a first annular groove of the body detonation warhead shell (1), and the lower end face of the second circular plate of the movable end cover (2) is 5mm away from the lower end face of the first annular groove of the body detonation warhead shell (1) for fuel (4) of the body detonation warhead shell (1);
and 4, step 4: when the environmental temperature rises, the fuel (4) is heated to expand, the volume of the fuel (4) is increased, the movable end cover (2) moves downwards, the volume of a sealed space formed by the body detonation warhead shell (1) and the movable end cover (2) is increased, the internal stress of the fuel (4) is not too large, the first cylinder of the body detonation warhead shell (1) is not broken by support, and the safety of the body detonation warhead shell (1) is ensured;
when the ambient temperature is reduced, the fuel (4) is shrunk, the volume of the fuel (4) is reduced, the movable end cover (2) moves upwards, the volume of a sealed space formed by the body detonation warhead shell (1) and the movable end cover (2) is reduced, the internal stress of the fuel (4) is not too large, the first cylinder of the body detonation warhead shell (1) is not damaged by being supported, and the safety of the body detonation warhead shell (1) is ensured.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202211011837.7A CN115388722B (en) | 2022-08-23 | 2022-08-23 | Automatic regulating device for pressure in movable end cover |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202211011837.7A CN115388722B (en) | 2022-08-23 | 2022-08-23 | Automatic regulating device for pressure in movable end cover |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CN115388722A true CN115388722A (en) | 2022-11-25 |
| CN115388722B CN115388722B (en) | 2023-06-09 |
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| CN202211011837.7A Active CN115388722B (en) | 2022-08-23 | 2022-08-23 | Automatic regulating device for pressure in movable end cover |
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Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN105043172A (en) * | 2015-06-04 | 2015-11-11 | 西安近代化学研究所 | Internal stress release device for liquid-phase charging payload |
| CN110645846A (en) * | 2019-10-28 | 2020-01-03 | 西安近代化学研究所 | Isobaric adjusting device for compensating liquid-phase charging volume changes at different temperatures |
| CN112229279A (en) * | 2020-09-18 | 2021-01-15 | 西安近代化学研究所 | Liquid-phase charging warhead shell without using counterweight block, without changing charging amount and capable of adjusting mass center of mass |
| CN113154961A (en) * | 2021-04-12 | 2021-07-23 | 西安近代化学研究所 | Fluid antigravity flow device under air cushion drive |
| CN113175849A (en) * | 2021-04-02 | 2021-07-27 | 西安近代化学研究所 | Device capable of driving suspended bubbles in fluid to move radially |
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2022
- 2022-08-23 CN CN202211011837.7A patent/CN115388722B/en active Active
Patent Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN105043172A (en) * | 2015-06-04 | 2015-11-11 | 西安近代化学研究所 | Internal stress release device for liquid-phase charging payload |
| CN110645846A (en) * | 2019-10-28 | 2020-01-03 | 西安近代化学研究所 | Isobaric adjusting device for compensating liquid-phase charging volume changes at different temperatures |
| CN112229279A (en) * | 2020-09-18 | 2021-01-15 | 西安近代化学研究所 | Liquid-phase charging warhead shell without using counterweight block, without changing charging amount and capable of adjusting mass center of mass |
| CN113175849A (en) * | 2021-04-02 | 2021-07-27 | 西安近代化学研究所 | Device capable of driving suspended bubbles in fluid to move radially |
| CN113154961A (en) * | 2021-04-12 | 2021-07-23 | 西安近代化学研究所 | Fluid antigravity flow device under air cushion drive |
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| 许志峰;曹玉武;王世英;宋玉江;顾晓峰;: "云爆战斗部密封接口机械结构设计研究", 火工品 * |
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| CN115388722B (en) | 2023-06-09 |
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