Warhead charge and hoisting integrated tooling

Abstract

The application provides a warhead charging and hoisting integrated tool, which comprises a warhead support frame, the warhead support frame comprises a supporting base arranged in the horizontal direction, a plurality of auxiliary pipes are fixedly connected to the upper surface of the supporting base, the plurality of auxiliary pipes are uniformly arranged in the circumferential direction, and each auxiliary pipe is arranged in the vertical direction; a gasket sleeve is coaxially arranged on the supporting base, and the plurality of auxiliary pipes are arranged at the periphery of the gasket sleeve. A stepped blind hole-shaped cavity coaxially arranged in the gasket sleeve is a warhead mounting cavity, a warhead shell is coaxially sleeved in the warhead mounting cavity, and a charging sprue is coaxially sleeved in the warhead shell. A plurality of height adjusting supports are uniformly arranged in the circumferential direction on the outer side wall of the charging sprue, the vertical section of the height adjusting support is detachably connected with the auxiliary pipe, and the installation position can be adjusted. A plurality of horizontal bubble instruments are installed on the upper end surface of the charging sprue. The tool realizes the leveling of the charging sprue during charging, the safe and lossless hoisting and transfer of the warhead after charging, and can adapt to the requirements of warheads of various sizes.

Description

Technical Field

[0001] This invention belongs to the field of military ammunition manufacturing technology, and relates to propellant loading and hoisting, specifically to an integrated tooling for warhead propellant loading and hoisting. Background Technology

[0002] The warhead is the core component of various munitions for destroying targets, and the quality of the explosives inside directly determines the ultimate effectiveness of the weapon. Explosive injection is one of the mainstream filling processes for large-charge warheads. This process typically requires precisely fixing the warhead casing at a specific position, ensuring its injection port (i.e., riser) is strictly horizontal, and then injecting molten explosive into the casing cavity through the riser under vacuum or pressure, where it slowly solidifies to form a high-quality propellant charge.

[0003] In existing technologies, the loading and hoisting / transfer processes of warheads are generally separated, which has a series of inherent drawbacks:

[0004] First, the process is cumbersome: Firstly, a dedicated loading bracket or pit is needed to fix and initially level the warhead. After loading and allowing the explosive to initially solidify, the warhead is then lifted from the loading station using wire ropes, slings, or specialized lifting equipment and transferred to the curing room or the next assembly line. This process involves tooling changes and repeated positioning, which is not only time-consuming and labor-intensive but also increases operational complexity.

[0005] Secondly, the leveling accuracy and efficiency are low: the leveling of traditional charge holders relies heavily on shims, simple levels, and worker experience. The leveling process is cumbersome, and the accuracy is difficult to guarantee, resulting in low efficiency. An uneven riser may cause defects such as segregation and shrinkage cavities inside the charge, affecting the density and uniformity of the explosive charge, and thus endangering storage and use safety.

[0006] Third, there are safety hazards and quality risks: When hoisting a loaded warhead, collisions and slippage may occur during the change of lifting equipment. The wire ropes and other lifting equipment come into direct contact with the precision machined surfaces of the warhead (such as threads, centering parts, and coatings), which can easily cause surface scratches, paint peeling, or localized stress concentration, affecting the appearance, sealing, and long-term storage performance of the ammunition. It may even lead to unexpected risks due to friction or impact.

[0007] Fourth, poor tooling versatility: For warheads with different calibers, lengths and shapes, it is often necessary to design and manufacture special propellant supports and lifting devices, resulting in a wide variety of tooling, high management and maintenance costs, and large footprint.

[0008] Therefore, developing an integrated tooling that can deeply integrate the functions of propellant positioning and leveling with safe hoisting and transportation, and has good versatility and product protection capabilities, is of urgent practical need and has important military and economic benefits for improving the automation level of warhead production lines, ensuring product quality consistency, and improving production safety and efficiency. Summary of the Invention

[0009] In view of the shortcomings of the existing technology, the purpose of this invention is to provide an integrated tooling for warhead loading and hoisting, which solves the technical problem that it is difficult to simultaneously improve work efficiency and product quality when loading and hoisting warheads in the existing technology.

[0010] To solve the above-mentioned technical problems, the present invention adopts the following technical solution.

[0011] An integrated tooling for warhead loading and hoisting includes a warhead support frame. The warhead support frame includes a horizontally arranged support base, which is mirror-symmetrical with respect to its vertical plane. Multiple auxiliary tubes are fixedly connected to the upper surface of the support base near the outer wall. The multiple auxiliary tubes are evenly arranged circumferentially, and each auxiliary tube is arranged vertically. A padding sleeve is also coaxially arranged on the support base, and the multiple auxiliary tubes are arranged around the padding sleeve.

[0012] The aforementioned liner includes a liner body arranged vertically along its central axis. The bottom of the liner body is closed and the top is open. A stepped blind hole-shaped cavity coaxially arranged within the liner body serves as a warhead mounting cavity. A warhead housing is coaxially fitted within the warhead mounting cavity. A propellant riser is coaxially fitted within the warhead housing. The axial upper end face of the propellant riser extends vertically beyond the axial upper end face of both the liner body and the warhead housing.

[0013] The outer wall of the charge riser is also evenly provided with multiple L-shaped height adjustment brackets along the circumference. Each height adjustment bracket corresponds to an auxiliary tube. The end of the horizontal section of the height adjustment bracket is fixedly connected to the outer wall of the charge riser, and the end of the vertical section of the height adjustment bracket is detachably connected to the auxiliary tube. The installation position of the vertical section of the height adjustment bracket on the auxiliary tube can be adjusted vertically, thereby realizing the horizontal adjustment of the axial upper end face of the charge riser.

[0014] Multiple horizontal bubble levelers are also embedded in the upper surface of the charge riser. Each horizontal bubble leveler corresponds to a height adjustment bracket, thereby achieving horizontal calibration of the axial upper surface of the charge riser.

[0015] Specifically, the auxiliary tube has a first elongated hole that runs radially through the body of the liner sleeve near the upper part. The first elongated hole is arranged vertically and corresponds one-to-one with the auxiliary tube. The vertical section of the height adjustment bracket also has a second elongated hole that runs radially through the charging riser near the lower part. The second elongated hole is arranged vertically and corresponds one-to-one with the first elongated hole.

[0016] It also includes multiple bolts, with each bolt corresponding to a first elongated hole; the bolts pass radially through the first and second elongated holes and are installed, thereby achieving a detachable connection between the vertical section of the height adjustment bracket and the auxiliary pipe.

[0017] Specifically, the inner diameter of the warhead mounting cavity increases vertically from bottom to top.

[0018] The outer wall of the warhead casing is in contact with at least one section of the inner wall of the warhead mounting cavity along its axial direction.

[0019] Specifically, the number of height-adjustable brackets is even.

[0020] Each of the horizontal sections of the height adjustment bracket is also fixedly connected to a lifting handle. The number of lifting handles is less than or equal to the number of height adjustment brackets. The multiple lifting handles are arranged in a mirror-symmetrical manner with the axial section of the charge riser as the symmetrical plane.

[0021] Specifically, the supporting base is hollow.

[0022] Specifically, the outer diameter of the propellant riser is smaller than the inner diameter of the warhead casing.

[0023] Specifically, the material of the gasket body is polytetrafluoroethylene.

[0024] Specifically, the plurality of the aforementioned horizontal bubble gauges are mirror-symmetrical about the plane containing the axis of the aforementioned charge riser.

[0025] The aforementioned level bubble apparatus is a spirit level.

[0026] Compared with the prior art, the present invention has the following technical effects.

[0027] (I) The tooling in this invention enables rapid and accurate leveling of the propellant riser during the propellant loading process, safe and damage-free hoisting and transportation of the warhead after loading, and can adapt to the needs of warheads with various diameters and a certain height range. This effectively solves the problems of process separation, low efficiency, insufficient accuracy guarantee and damage risk in traditional processes during propellant loading and hoisting. At the same time, it reduces the number of special tooling, lowers the design, manufacturing, storage and management costs of tooling, and improves the utilization rate of the device.

[0028] (II) The tooling in this invention simplifies the process flow and realizes "one clamp for multiple uses". From the loading of the warhead to the transfer of the loaded warhead off the production line, the tooling does not need to be changed throughout the process. After the warhead is loaded with explosives on this tooling, it can be directly lifted and transported away, eliminating the intermediate lifting and conversion links, simplifying the operation procedures, shortening the production cycle, and improving the overall operation efficiency.

[0029] (III) The tooling in this invention significantly improves the leveling accuracy and work quality. The integrated high-precision horizontal bubble meter combined with the structure of four independent micro-adjustments in the circumferential direction makes the leveling operation of the propellant riser intuitive, precise and quantifiable. The leveling accuracy can easily reach within ±0.5°, which is far higher than the traditional gasket leveling method. This provides a reliable guarantee for ensuring the density uniformity of the propellant grains in the warhead and reducing internal defects. It directly improves the propellant loading quality and batch consistency of the warhead and can serve the propellant loading production line of medium-sized conventional warheads commonly used in the art.

[0030] (IV) The tooling in this invention uses a PTFE pad as a pad for full protection of the warhead, which effectively prevents scratches, wear and chemical contamination of the precision mechanical surface and coating of the warhead during loading and hoisting. The product protection effect is significant and helps to reduce rework or scrap losses caused by appearance damage.

[0031] (V) The tooling in this invention allows bolts to be installed into the first and second elongated holes manually or using known and commonly used tools, via nuts. This can be used to adjust the distance between the upper end face of the propellant riser and the upper surface of the support base, thereby achieving two main functions: First, macroscopically, by simultaneously adjusting the vertical position of the four nuts, the overall bearing height of the tooling can be changed to adapt to the needs of warheads of different lengths and specifications; second, microscopically, by differentially adjusting each nut, the spatial orientation of the propellant riser can be precisely adjusted, ultimately ensuring that the top propellant riser reaches the absolute horizontal state indicated by the horizontal bubble level, thus creating the preconditions for high-quality propellant loading of the warhead. Attached Figure Description

[0032] Figure 1 This is a schematic diagram of the overall structure of the tooling in the embodiment.

[0033] Figure 2 This is a schematic diagram of the structure of the warhead support frame.

[0034] Figure 3 This is a schematic diagram of the assembly structure between the warhead support frame and the bushing.

[0035] Figure 4 This is a cross-sectional view of the gasket.

[0036] Figure 5This is a schematic diagram of the assembly structure between the explosive riser and the height adjustment bracket.

[0037] Figure 6 for Figure 5 A top-view structural diagram.

[0038] Figure 7 for Figure 5 A cross-sectional structural diagram.

[0039] The meanings of the labels in the diagram are as follows: 1-warhead support frame, 2-shield sleeve, 3-warhead shell, 4-propellant riser, 5-height adjustment bracket, 6-level bubble level, 7-second elongated hole, 8-bolt, 9-lifting handle.

[0040] 101-Support base, 102-Auxiliary tube, 103-First elongated hole.

[0041] 201-Pad sleeve body, 202-Warhead mounting cavity.

[0042] The specific content of the present invention will be further described in detail below with reference to the embodiments. Detailed Implementation

[0043] It should be noted that, unless otherwise specified, all components and raw materials in this invention are commonly used in the art and are known in the prior art. For example, the auxiliary pipe is made of known steel pipe, and the raw material of the support base is made of commonly used steel.

[0044] Following the above technical solution, specific embodiments of the present invention are given below. It should be noted that the present invention is not limited to the following specific embodiments, and all equivalent modifications made on the basis of the technical solution of the present invention fall within the protection scope of the present invention.

[0045] Example: This embodiment provides an integrated tooling for warhead loading and hoisting, such as... Figures 1 to 3 As shown, the device includes a warhead support frame 1, which includes a horizontally arranged support base 101. The support base 101 is mirror-symmetrical about the vertical plane. Multiple auxiliary tubes 102 are fixedly connected to the upper surface of the support base 101 near the outer wall. The multiple auxiliary tubes 102 are evenly arranged circumferentially, and each auxiliary tube 102 is arranged vertically. A padding sleeve 2 is also coaxially arranged on the support base 101, and the multiple auxiliary tubes 102 are arranged around the padding sleeve 2.

[0046] like Figure 3 and Figure 4As shown, the liner sleeve 2 includes a liner sleeve body 201 arranged vertically along its central axis. The liner sleeve body 201 is closed in the circumference and bottom and open at the top. The stepped blind hole-shaped cavity arranged coaxially inside the liner sleeve body 201 is the warhead mounting cavity 202. The warhead housing 3 is coaxially fitted inside the warhead housing 202. The propellant riser 4 is coaxially fitted inside the warhead housing 3. The axial upper end face of the propellant riser 4 extends vertically to the outside of the axial upper end face of the liner sleeve body 201 and the warhead housing 3.

[0047] like Figures 5 to 7 As shown, multiple L-shaped height adjustment brackets 5 are evenly distributed along the circumference of the outer wall of the charge riser 4. Each height adjustment bracket 5 corresponds to an auxiliary tube 102. The end of the horizontal section of the height adjustment bracket 5 is fixedly connected to the outer wall of the charge riser 4, and the end of the vertical section of the height adjustment bracket 5 is detachably connected to the auxiliary tube 102. The installation position of the vertical section of the height adjustment bracket 5 on the auxiliary tube 102 can be adjusted vertically, thereby realizing the horizontal adjustment of the axial upper end face of the charge riser 4.

[0048] like Figure 5 As shown, multiple horizontal bubble levelers 6 are also embedded on the upper surface of the charge riser 4. The horizontal bubble levelers 6 correspond one-to-one with the height adjustment bracket 5, thereby achieving horizontal calibration of the axial upper surface of the charge riser 4.

[0049] The tooling in this embodiment has a mirror-symmetric structure with the vertical plane as the symmetry plane.

[0050] In this embodiment, the interior of the charge riser 4 is hollow and open at both ends along the axis. The charge riser 4 is used as a channel for injecting explosives. The charge riser 4 adopts a charge riser commonly known in the art, and the explosive adopts an explosive commonly known in the art. The warhead in this embodiment is a warhead commonly known in the art. The warhead includes a warhead shell 3 and explosives.

[0051] In this embodiment, the end of the horizontal section of the height adjustment bracket 5 is fixedly connected to the outer wall of the charge riser 4 using a continuous weld commonly known in the art.

[0052] In this embodiment, there are four height adjustment brackets 5. The four height adjustment brackets 5 are arranged in a mirror-symmetrical manner with the axial section of the charge riser 4 as the symmetrical plane. The four height adjustment brackets 5 are arranged around the charge riser 4 to form a stable four-point support leveling structure. The distance between the inner sidewalls of two radially opposite height adjustment brackets 5 is greater than the outer diameter of the liner body 201.

[0053] In this embodiment, the warhead casing 3 adopts a commonly used warhead casing known in the art.

[0054] In this embodiment, the internal cavity of the liner body 201 is stepped hole-shaped, which can be used for warhead shells 3 of various diameters; furthermore, in this embodiment, the shape of the internal cavity of the liner body 201 can be integrated and adjusted according to the external contour of the warhead shell 3 to adapt to warhead shells 3 of different specifications.

[0055] In this embodiment, there are four auxiliary tubes 102. The four auxiliary tubes 102 are arranged in a mirror-symmetrical manner with the plane containing the central axis of the supporting base 101 as the symmetrical plane. The four auxiliary tubes 102 form a shape that matches the cylindrical section of the warhead shell 3, thereby also achieving protection for the warhead shell 3 and the padding sleeve body 201 during transportation. The distance between the inner sidewalls of two radially opposite auxiliary tubes 102 is greater than the outer diameter of the padding sleeve body 201.

[0056] In this embodiment, the gasket 2 is bonded to the support base 101 using a high-temperature resistant silicone adhesive commonly known in the art.

[0057] In this embodiment, there are four horizontal bubblers 6, and the method of embedding the horizontal bubblers 6 on the upper surface of the charge riser 4 adopts a commonly known installation method in the art.

[0058] As a preferred embodiment of this invention, such as Figure 2 As shown, the auxiliary tube 102 has a first elongated hole 103 that runs radially through the liner body 201 near the upper part. The first elongated hole 103 is arranged vertically and corresponds one-to-one with the auxiliary tube 102. The vertical section of the height adjustment bracket 5 also has a second elongated hole 7 that runs radially through the charge riser 4 near the lower part. The second elongated hole 7 is arranged vertically and corresponds one-to-one with the first elongated hole 103.

[0059] It also includes multiple bolts 8, each of which corresponds to a first elongated hole 103; the bolts 8 pass radially through the first elongated hole 103 and the second elongated hole 7 and are installed, thereby achieving a detachable connection between the vertical section of the height adjustment bracket 5 and the auxiliary tube 102.

[0060] In this embodiment, the outer diameter of the shank of the bolt 8 is smaller than the length of the first elongated hole 103 and the length of the second elongated hole 7, respectively; the bolt 8 is fastened by a nut, thereby achieving detachable installation; by changing the installation position of the vertical section of the height adjustment bracket 5 on the auxiliary tube 102, the height of the entire tooling can be adjusted to adapt to different heights of the warhead shell 3; the nut corresponds one-to-one with the bolt 8, and the nut is a commonly used nut known in the art.

[0061] As a preferred embodiment of this invention, such as Figure 4As shown, the inner diameter of the warhead mounting cavity 202 increases vertically from bottom to top.

[0062] The outer wall of the warhead casing 3 is in contact with at least one section of the inner wall of the warhead mounting cavity 202 in the axial direction.

[0063] As a preferred embodiment of this invention, such as Figure 2 As shown, the number of height adjustment brackets 5 is even.

[0064] Each of the horizontal sections of the height adjustment bracket 5 is also fixedly connected to a lifting handle 9. The number of lifting handles 9 is less than or equal to the number of height adjustment brackets 5. The multiple lifting handles 9 are arranged in a mirror-symmetrical manner with the axial section of the charge riser 4 as the symmetrical plane.

[0065] In this embodiment, the lifting handle 9 is a lifting handle with a rectangular cross-section of its outer contour and a square hole inside. The lifting handle 9 provides a standard interface with external lifting equipment, which facilitates quick and stable hook attachment and clear force distribution. The external lifting equipment includes bridge cranes, overhead cranes, etc., which are commonly known in the art. The lifting handle adopts a lifting handle commonly known in the art. In this embodiment, the number of lifting handles 9 is 2.

[0066] As a preferred embodiment of this invention, such as Figure 2 As shown, the supporting base 101 is hollow.

[0067] As a preferred embodiment, the outer diameter of the propellant riser 4 is smaller than the inner diameter of the warhead casing 3.

[0068] As a preferred embodiment, the material of the liner body 201 is polytetrafluoroethylene.

[0069] In this embodiment, the thickness of the liner body 201 is 3 to 10 millimeters.

[0070] In this embodiment, polytetrafluoroethylene (PTFE), a material commonly known in the art, is selected as the material for the liner body 201 because: PTFE has an extremely low coefficient of friction, excellent chemical inertness, good high and low temperature resistance, and moderate flexibility. The extremely low coefficient of friction gives the liner body 201 self-lubricating properties, and the excellent chemical inertness gives the liner body 201 the characteristics of not corroding metals and not contaminating explosives. The liner body 201 can effectively isolate other commonly used rigid tooling from the surface of the warhead, completely avoiding scratches, bumps, and paint wear. At the same time, it allows the warhead to have slight self-centering adjustments during hoisting, improving the stress state.

[0071] As a preferred embodiment, the multiple horizontal bubble gauges 6 are mirror-symmetrical about the plane containing the axis of the charge riser 4.

[0072] The level bubble meter 6 is a level bubble.

[0073] In this embodiment, a circular level bubble, commonly known in the art, is used; the level bubble meter 6 provides the operator with intuitive and real-time visual feedback on the levelness, which serves as the basis for subsequent precise leveling.

[0074] When using the tooling in this embodiment, the specific steps include: The liner 2 is installed on the warhead support frame 1, the warhead housing 3 is placed inside the liner body 201, and then the explosive riser 4 is arranged inside the warhead housing 3.

[0075] By adjusting the vertical installation positions of the vertical sections of the four height adjustment brackets 5 on the corresponding auxiliary tubes 102 through the first elongated hole 103 and the second elongated hole 7, the warhead shell 3 of different heights can be adapted to fit. At the same time, by fine-tuning multiple bolts 8 and observing whether the bubbles of multiple horizontal bubble gauges 6 are within the corresponding central circles, the leveling and calibration of the charge riser 4 can be achieved, so that the charge riser 4 reaches a horizontal state. After the charge riser 4 is horizontal, the current posture is locked by bolts 8 and nuts.

[0076] The explosive riser 4 serves as the channel for injecting the explosive, and the explosive is vacuum-cast using commonly known processes and methods in the art. After loading, without any operational changes, the overhead crane is directly operated to smoothly and horizontally lift the entire tooling, along with the internal explosive warhead which is still in a liquid or semi-solid state, to a commonly known heat preservation and curing chamber in the art. Throughout the entire lifting process, there is no relative movement between the warhead and the tooling, and the surface of the warhead is always well protected by the gasket body 201.

Claims

1. A tooling integrating warhead loading and hoisting, comprising a warhead support frame (1), characterized in that, The warhead support frame (1) includes a horizontally arranged support base (101), which is mirror-symmetrical about the vertical plane. Multiple auxiliary tubes (102) are fixedly connected to the upper surface of the support base (101) near the outer wall. The multiple auxiliary tubes (102) are evenly arranged circumferentially, and each auxiliary tube (102) is arranged vertically. A padding sleeve (2) is also coaxially arranged on the support base (101), and the multiple auxiliary tubes (102) are arranged around the padding sleeve (2). The aforementioned padding sleeve (2) includes a padding sleeve body (201) arranged vertically along the central axis. The bottom of the padding sleeve body (201) is closed and the top is open. The stepped blind hole-shaped cavity arranged coaxially inside the padding sleeve body (201) is the warhead mounting cavity (202). The warhead housing (3) is coaxially fitted inside the warhead housing (3). The explosive riser (4) is coaxially fitted inside the warhead housing (3). The axial upper end face of the explosive riser (4) extends vertically to the outside of the axial upper end face of the padding sleeve body (201) and the warhead housing (3). The outer wall of the charge riser (4) is also evenly provided with multiple L-shaped height adjustment brackets (5) along the circumferential direction. The height adjustment brackets (5) correspond one-to-one with the auxiliary tube (102). The end of the horizontal section of the height adjustment bracket (5) is fixedly connected to the outer wall of the charge riser (4), and the end of the vertical section of the height adjustment bracket (5) is detachably connected to the auxiliary tube (102). The installation position of the vertical section of the height adjustment bracket (5) on the auxiliary tube (102) can be adjusted vertically, thereby realizing the horizontal adjustment of the axial upper end face of the charge riser (4). Multiple horizontal bubble levelers (6) are also embedded on the upper surface of the charge riser (4). The horizontal bubble levelers (6) correspond one-to-one with the height adjustment bracket (5), thereby achieving horizontal calibration of the axial upper surface of the charge riser (4).

2. The integrated tooling for warhead loading and hoisting as described in claim 1, characterized in that, The auxiliary tube (102) has a first elongated hole (103) that runs radially through the liner body (201) near the upper part. The first elongated hole (103) is arranged vertically and corresponds one-to-one with the auxiliary tube (102). The vertical section of the height adjustment bracket (5) also has a second elongated hole (7) that runs radially through the charge riser (4) near the lower part. The second elongated hole (7) is arranged vertically and corresponds one-to-one with the first elongated hole (103). It also includes multiple bolts (8), each of which corresponds to a first elongated hole (103); the bolts (8) are installed radially through the first elongated hole (103) and the second elongated hole (7), thereby achieving a detachable connection between the vertical section of the height adjustment bracket (5) and the auxiliary tube (102).

3. The integrated tooling for warhead loading and hoisting as described in claim 1, characterized in that, The inner diameter of the warhead mounting cavity (202) increases vertically from bottom to top; The outer side wall of the warhead housing (3) is in contact with at least one section of the inner side wall of the warhead mounting cavity (202) in the axial direction.

4. The integrated tooling for warhead loading and hoisting as described in claim 1, characterized in that, The number of height adjustment brackets (5) is even; On the upper surface of the horizontal section of the height adjustment bracket (5), a hoisting handle (9) is fixedly connected. The number of hoisting handles (9) is less than or equal to the number of height adjustment brackets (5). The multiple hoisting handles (9) are arranged in a mirror-symmetrical manner with the axial section of the charge riser (4) as the symmetrical plane.

5. The integrated tooling for warhead loading and hoisting as described in claim 1, characterized in that, The supporting base (101) is hollow.

6. The integrated tooling for warhead loading and hoisting as described in claim 1, characterized in that, The outer diameter of the explosive riser (4) is smaller than the inner diameter of the warhead casing (3).

7. The integrated tooling for warhead loading and hoisting as described in claim 1, characterized in that, The material of the liner body (201) is polytetrafluoroethylene.

8. The integrated tooling for warhead loading and hoisting as described in claim 1, characterized in that, The plurality of the horizontal bubble gauges (6) are mirror-symmetrical about the plane in which the axis of the charge riser (4) lies; The level bubble meter (6) is a level bubble.

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