WO2021259342A1 - Prestress constrained block and composite armor structure - Google Patents

Prestress constrained block and composite armor structure Download PDF

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Publication number
WO2021259342A1
WO2021259342A1 PCT/CN2021/101945 CN2021101945W WO2021259342A1 WO 2021259342 A1 WO2021259342 A1 WO 2021259342A1 CN 2021101945 W CN2021101945 W CN 2021101945W WO 2021259342 A1 WO2021259342 A1 WO 2021259342A1
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WO
WIPO (PCT)
Prior art keywords
ring
filling platform
filling
prestressed
prestress
Prior art date
Application number
PCT/CN2021/101945
Other languages
French (fr)
Chinese (zh)
Inventor
王子国
孙宇雁
王文杰
Original Assignee
青岛理工大学
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by 青岛理工大学 filed Critical 青岛理工大学
Priority to JP2022505641A priority Critical patent/JP7203472B2/en
Publication of WO2021259342A1 publication Critical patent/WO2021259342A1/en

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Classifications

    • EFIXED CONSTRUCTIONS
    • E04BUILDING
    • E04CSTRUCTURAL ELEMENTS; BUILDING MATERIALS
    • E04C1/00Building elements of block or other shape for the construction of parts of buildings
    • E04C1/39Building elements of block or other shape for the construction of parts of buildings characterised by special adaptations, e.g. serving for locating conduits, for forming soffits, cornices, or shelves, for fixing wall-plates or door-frames, for claustra
    • EFIXED CONSTRUCTIONS
    • E04BUILDING
    • E04BGENERAL BUILDING CONSTRUCTIONS; WALLS, e.g. PARTITIONS; ROOFS; FLOORS; CEILINGS; INSULATION OR OTHER PROTECTION OF BUILDINGS
    • E04B1/00Constructions in general; Structures which are not restricted either to walls, e.g. partitions, or floors or ceilings or roofs
    • E04B1/62Insulation or other protection; Elements or use of specified material therefor
    • E04B1/92Protection against other undesired influences or dangers

Definitions

  • the invention belongs to armor technology, and specifically relates to a prestressed restraint block and a composite armor structure.
  • the anti-penetration performance of composite armor using ceramic materials mainly depends on the ceramic's compressive strength and hardness, crushing characteristics, fragment flow friction and particle abrasion; the high compressive strength of ceramics improves the anti-penetration performance to a certain extent; ceramics Energy absorption in the surface area of the crushing zone is an important factor for ceramic anti-penetration; for thick and strictly constrained ceramic blocks, the flow friction of ceramic fragments is the most important factor for anti-penetration.
  • Studies have shown that after the ceramic target is laterally constrained, when the projectile penetrates the constrained ceramic, the confinement ring will exert a constraining force on the ceramic target plate, which can effectively curb the crack propagation of the ceramic material, thereby improving the resistance of the ceramic material. Penetration performance. With the deepening of research, more and more people have begun to study the effect of applying internal stress to ceramics in advance on the anti-penetration performance of ceramic materials.
  • Prestressing the ceramic material of the composite armor can effectively inhibit the initiation and propagation of cracks in the target body. Even if fracture occurs inside the ceramic under high-speed impact, the ceramic fragments are still squeezed relatively tightly, and there are only cracks without expansion, so that there is a large penetration resistance inside the broken ceramic area. The reverse movement of the ceramic particles and the projectile will have an abrasion effect on the quality of the projectile, and make the energy dissipation mechanism such as mutual friction play a role, effectively improving the anti-penetration performance of the ceramic.
  • Both heat and cold shrinkage or mechanical pressure can be used to generate prestress inside the ceramic.
  • a stable pre-stress is required and the pre-stress size can be adjusted.
  • the heat treatment of the hot charging method will have an adverse effect on the strength of the metal.
  • the temperature is controlled to adjust the internal pre-stress of the ceramic
  • the method of stress magnitude is difficult to achieve the long rod impact test, so the mechanical extrusion method is mostly used in the test, and the mechanical pressure device requires uniform lateral pressure from the periphery of the ceramic material, and the assembly size between the ceramic material and the restraint structure
  • the machining accuracy is high, and multiple surfaces are pressurized at the same time.
  • the equipment structure is relatively complicated, but it is difficult to apply in actual engineering and is only limited to research.
  • the technical problem solved by the present invention is to provide a prestressed restraint block and a composite armor structure that can be quickly assembled in a room temperature environment in view of the above-mentioned problems existing in the mechanical extrusion method and the hot charging method of applying prestress to the existing composite armor .
  • the pre-stressed constraining block includes a filling platform 11 and a constraining ring 12.
  • the filling platform 11 has a cross section of the same shape as the inner ring of the constraining ring 12, and is fixedly embedded in the inner ring of the constraining ring 12.
  • the filling platform The outer side wall of the body 11 and the inner ring wall of the constraining ring 12 are wedged tightly through taper fit;
  • the outer side wall of the filling platform 11 and the inner wall of the confinement ring 12 are respectively matched conical surfaces or matched polygonal pyramid surfaces.
  • the diameters of the large end and the small end of the outer side wall of the filling platform 11 are respectively d 1 and d 2
  • the diameters of the large end and the small end of the inner wall of the confinement ring 12 are respectively R 1 and R 2 satisfy R 2 ⁇ d 2 ⁇ R 1 ⁇ d 1
  • the heights of the filling platform 11 and the confinement ring 12 are h1 and h2, respectively, where h1 ⁇ h2.
  • the inclination angle ⁇ of the cone surface of the outer side wall of the filling platform 11 ranges from 1° to 10°, preferably 3° to 6°.
  • the range of ⁇ is 1° ⁇ 10°, preferably 3° ⁇ 6°.
  • There is an angular difference ⁇ between the outer side wall of the filling table body 11 and the inner wall of the confinement ring 12, ⁇ ⁇ - ⁇ , the value of ⁇
  • the range is 0° ⁇ 0.5°, preferably 0° ⁇ 0.2°.
  • the diameter-to-thickness ratio d 1 /h 1 of the filling table body 11 is 0.5-40, preferably 3-12.
  • the filling platform 11 is a frustum with a conical surface or an outer side wall of a polygonal pyramid surface
  • the cylinder or prism of the first reducing ring 14 is fixed externally, and the outer side wall of the first reducing ring 14 is a conical surface or a polygonal pyramid surface.
  • the constraining ring 12 is a reduced-diameter ring body with an inner ring wall of a conical surface or a polygonal pyramid surface,
  • the filling platform 11 has a layered structure and includes at least two layers of fixed and stacked filling blocks.
  • the outer surface of the filling platform body 11 is wrapped with a wrapping layer 17.
  • the small end of the inner wall of the restraining ring 12 or the second reducing ring 13 is provided with a bottom plate structure, and the bottom plate structure is a restraining groove bottom plate 16 integrally structured with the restraining ring 12, Or the cushion is mounted on the cushion layer 15 at the small end of the filling platform 11.
  • the filling platform 11 is made of ceramic, concrete or glass material
  • the restraining ring 12 is made of metal or fiber reinforced composite material.
  • the inner wall of the constraining ring 12 is provided with a clamping groove 18, and the clamping groove 18 is equipped with a wedge for the filling platform 11 to axially limit the constraining ring 12 Snap ring 19.
  • the present invention also discloses a composite armored structure, including at least one layer of armor plate, the armor plate includes a plurality of the above-mentioned prestressed restraint blocks of the present invention, the prestressed restraint blocks are spliced by a plurality of split restraint rings 12, or A confinement ring 12 with an integrated honeycomb structure is adopted.
  • the composite armor structure in the above solution also includes a cover plate 2 and a back plate 3 respectively attached to cover both sides of the composite armor.
  • the present invention presses the filling platform body made of ceramic, concrete or glass into the inner ring of the confinement ring made of metal or fiber reinforced composite material to obtain the prestressed constraining block, wherein the confinement ring and the filling platform body are matched by a cone Wedge tightening, according to the hoop restraint principle, the inner ring of the confinement ring and the filling platform are wedge tightly tightened through the tapered surface to have a self-tightening function.
  • the generated radial hoop force increases with the increase of vertical pressure, so that the strength of the filling platform becomes larger, and the elastic restoring force of the confinement ring exerts a lateral prestress on the filling platform, which increases the resistance of the restraining block. Thorough and anti-explosive shock performance.
  • the prestressed constraining block of the present invention can very simply apply radial prestress to brittle materials such as ceramics, concrete or glass at room temperature.
  • the prestress can be filled with the depth of the inner ring of the constrained ring or the filling of the table body by the wedge of the table body.
  • the taper inclination angle between the wedge and the constraining ring is controlled, which is suitable for prestressing of various sizes of filling platform components.
  • the prestressed constraining block of the present invention does not need to change the relative size of the components by heating like the hot charging method, it can also be applied to the fiber reinforced composite material confinement ring, concrete material or glass material filling table body which is difficult to apply to the hot charging method. In the present invention.
  • a single prestressed restraint block is assembled into a larger area composite armor structure, which can be assembled into a single-layer protective armor plate, or a single-layer protective armor plate can be misplaced and stacked into a multi-layer protective armor plate to reduce weak points and further increase the protective effect.
  • the confinement ring can be made into an integral structure to increase the integrity of the confinement ring and the bending resistance of the armor plate.
  • the prestressed restraint block of the present invention is more tolerant than the hot-fitting method. It is easier to assemble, the size of the table body and the confinement ring components has a larger tolerance range, and it is more environmentally friendly. Damaged or damaged components are easy to replace. In armed helicopters, armored vehicles, ships, tanks, aircraft caverns and missile manhole covers, etc. A variety of protection fields have broader application prospects.
  • the prestressing method of the present invention is not only applied to protective materials such as armor, but also to brittle material components such as ceramic mirrors, lenses, transparent windows, etc. of aviation and aerospace devices.
  • the prestressing of these components is improved by applying prestress through the confinement ring. Strength and reduce structural weight.
  • Fig. 1 is a schematic diagram of the assembly of the circular cross-section pre-stressed restraint block in the first embodiment.
  • Figure 2 is a schematic diagram of the assembly of the pre-stressed restraint block with a regular hexagonal cross-section in the first embodiment.
  • Fig. 3 is an anatomical view of the filling table body and the constraining ring in the first embodiment.
  • Fig. 4 is a schematic diagram of pre-stress application during the assembly process of the filling table body and the confinement ring in the first embodiment.
  • Figures 5a, 5b, and 5c are respectively schematic diagrams of prestressing application during the assembly process of the three filling platform bodies and the confinement ring in the second embodiment.
  • Fig. 6 is a schematic diagram of prestressing application during the assembly process of the filling table body and the confinement ring in the third embodiment.
  • Figures 7a and 7b are schematic diagrams of prestressing application during the two assembly processes of the filling platform body and the confinement ring in the fourth embodiment.
  • Fig. 8 is a schematic diagram of prestressing application during the assembly process of the filling table body and the confinement ring in the fifth embodiment.
  • Fig. 9 is a schematic diagram of prestressing application during the assembly process of the filling table body and the confinement ring in the sixth embodiment.
  • Fig. 10 is a schematic diagram of prestressing application during the assembly process of the filling platform body and the confinement ring in the seventh embodiment.
  • Figures 11a, 11b and 11c are schematic diagrams of assembling composite armor in the eighth embodiment.
  • Figures 12a, 12b and 12c are schematic cross-sectional views of three types of cover plates of the composite armor in the ninth embodiment.
  • 13a, 13b, and 13c are schematic cross-sectional views of three types of back plates of composite armor in the ninth embodiment.
  • 14a, 14b, 14c, 14d, and 14e are schematic cross-sectional views of five types of composite armor in the ninth embodiment.
  • Fig. 15 is a sectional dimension drawing of the frustum and the axis of the confinement ring planned in the first embodiment.
  • Fig. 16 is a 1/4 finite element model diagram of the planned size in the first embodiment.
  • Fig. 17 is the prestress-depression depth relation curve of the prestress restraint block in the prestress simulation process in the first embodiment.
  • FIG. 18 is a damage cloud diagram of the filling table body during the penetration simulation process of the prestressed restraint block in the first embodiment.
  • Figure 19 is the penetration depth-prestress relationship curve of the filled platform body in the penetration simulation process of the prestressed restraint block in the first embodiment
  • 3-back plate 31-collision layer; 32-energy-absorbing layer; 33-resistance layer.
  • the prestressed constraining block 1 shown in the figure includes a filling platform 11 and a confinement ring 12.
  • the filling platform 11 has a cross section of the same shape as the inner ring of the confinement ring 12, as shown in Figure 1 as a circular cross section.
  • the filling platform 11 is fixedly embedded in the inner ring of the confinement ring 12, and the outer side wall of the filling platform 11 and the inner ring wall of the confinement ring 12 are wedged tightly with each other through a taper fit.
  • the filling platform 11 and the constraining ring 12 in this embodiment are both integral structures, and the two are wedge tightly with a conical surface.
  • the inner wall of the confinement ring 12 is also a section of conical surface.
  • the cross section of the filling platform 11 in Fig. 2 is a regular hexagon, and its outer side wall is a section of a hexagonal pyramidal reducing ring.
  • the inner wall of the confinement ring 12 is also a section of a hexagonal pyramid. Spliced into a continuous armor layer, other polygonal pyramid surfaces can also be used in practical applications, including but not limited to triangles, quadrilaterals, and pentagons.
  • the size between the filling platform 11 and the confinement ring 12 should meet the following conditions:
  • the outer side wall of the filling platform 11 is a tapered surface, that is, the filling platform 11 is set to a large end and a small end at both ends in the axial direction.
  • the diameter of the large end is d 1
  • the diameter of the small end of the filling station body 11 is d 2
  • the diameter referred to here is the outer diameter of the cross section of the filling station body 11 in Fig. 1 and the filling station in Fig.
  • the diameter of the large end is R 1
  • the diameter of the small end of the confinement ring 12 is R 2
  • the diameter referred to here is the inner circle diameter of the inner wall of the inner ring wall of the confinement ring 12 in Fig. 1 and the confinement ring in Fig. 2 12
  • the diameter of the circumscribed circle of the regular hexagon of the inner ring wall cross section preferably, R 2 ⁇ d 2 ⁇ R 1 ⁇ d 1 .
  • the taper angle ⁇ of the outer side wall of the filling platform 11 ranges from 1° to 10°, preferably 3° to 6°.
  • the cone inclination angle ⁇ ranges from 1° to 10°, preferably 3° to 6°.
  • the cone inclination angle referred to here is the conical generatrix and vertical direction of the outer wall of the filling platform 11 and the inner wall of the confinement ring 12 in Fig. 1 2 or the angle between the outer wall of the filling platform 11 and the inner wall of the constraining ring 12 in the vertical direction.
  • the axial heights of the filling platform 11 and the confinement ring 12 are h 1 and h 2 , respectively, where h 1 ⁇ h 2 .
  • FIG. 1 The assembly diagram of the circular prestressed constraining block and the hexagonal prestressed constraining block are shown in Figures 1 and 2, respectively.
  • the filling platform 11 with a circular cross section or the filling platform 11 with a hexagonal cross section is placed in the corresponding constraint.
  • the large end of the inner ring of the confinement ring 12 is generally opened upward, and the small end of the filling platform 11 is pressed into the inner ring of the constraining ring 12 downward, and then the filling platform 11 is pressed along A downward pushing force is applied in the height direction, and the elastic restoring force of the confinement ring 12 squeezes the pre-stressed filling platform 11 inward, and applies a pre-compression stress in its radial direction. Larger, the greater the radial pre-compression stress applied by the constraining ring 12 to the filling platform 11, and the pre-stressed constraining block is obtained after the filling platform is pressed into a predetermined position.
  • the filling platform 11 can be pressed in by jack, hydraulic press or bolt fastening. In order to reduce the pressing resistance, temporary lubricant can be applied to the contact cone surface of the two, and the lubricant can be removed after being pressed into a predetermined position.
  • the radial prestress of the filling platform 11 can be designed to adjust the included angle between the conical generatrix or pyramid ridge line of the external side wall of the platform and the height of the filling platform, as well as the depression depth of the filling platform. When the included angle is constant, the restraining ring 12 does not yield. Or before failure, the greater the depression depth of the filling platform 11, the greater the prestress.
  • the table body and the confinement ring can be bonded with an adhesive to prevent slippage, or they can be in direct contact, and the friction between the two can be stabilized.
  • the filling table body 11 may be made of ceramic, concrete or glass material, and the confinement ring 12 is made of metal or fiber reinforced composite material, and the fiber reinforced composite material includes fiber reinforced metal matrix composite material or fiber reinforced polymer.
  • the confinement ring 12 can be used as a template for pouring and molding of the filling platform 11.
  • the inner side of the confinement ring 12 should be painted with isolation oil or arranged isolation Membrane, the bottom of the confinement ring 12 retains the press-in space after the concrete is formed.
  • the filling platform 11 is further pressed into the confinement ring 12, so that the filling platform 11 generates a radial pre-tension. stress.
  • the diameter-to-thickness ratio or the diameter-to-height ratio d 1 /h 1 of the filling table body 11 is 0.5-40, preferably 3-12.
  • the ring wall of the confinement ring 12 may have a variable thickness or a uniform thickness, that is, the top wall thickness t1 of the confinement ring 12 ⁇ the bottom wall thickness t2.
  • the wall thickness and yield strength of the confinement ring 12 are determined according to the prestress that needs to be applied to the filling table body 11. The greater the potential for constrained prestress that can be provided. Affected by the inconsistency of the diameter of the upper and lower cross-sections of the filling platform 11 and the inconsistency of the wall thickness in the height direction of the confinement ring 12, the prestress of the filling platform 11 is uneven in the height direction.
  • the outer wall cone clamp of the filling platform 11 can be adjusted by design. The slight difference between the angle ⁇ and the angle ⁇ of the conical surface of the inner ring wall of the confinement ring 12 is used to adjust the upper and lower prestress changes.
  • the prestress of the prestressed constraining block gradually increases from top to bottom, and the angle difference ⁇ between ⁇ and ⁇ is appropriately adjusted to reduce the upper and lower prestress of the platform. Difference, the value range of ⁇ is 0° ⁇ 0.5°, preferably 0° ⁇ 0.2°.
  • the contact stress between the outer side wall of the filling platform 11 and the inner ring wall of the confinement ring 12 is very small.
  • the difference is h3, and the height difference between the bottom surface of the platform and the bottom surface of the confinement ring is h4.
  • the filling table body 11 in FIG. 1 is a truncated cone body, and the inner wall of the confinement ring 12 is a truncated cone cavity.
  • the material of the filling table body 11 is one of ceramics, concrete or glass, and the material of the confinement ring 12 is steel, aluminum alloy, titanium alloy or fiber reinforced polymer material.
  • the assembly method is: place the confinement ring 12 on the platform, apply epoxy resin, glass glue or vacancies on the inner wall of the confinement ring 12 and the outer side wall of the filling platform 11, and then put the filling platform 11 into the confinement ring 12 In the circle, before the thrust is applied, there is no contact force between the two contact surfaces.
  • a jack or a press is used to apply thrust to the upper surface of the round-table filling platform, and the filling platform 11 is pressed down on the inner ring of the confinement ring 12 to obtain the pre-stressed constraining block 1. Due to the gap between the filling platform 11 and the confinement ring 12, The elastic restoring force of the confinement ring 12 squeezes the pre-tensioned filling platform 11 and applies a pre-compression stress in its radial direction.
  • the filling table body 11 in FIG. 2 is a regular hexagonal pyramid frustum body, and the inner wall of the confinement ring 12 is a regular hexagonal pyramid frustum cavity.
  • the material of the filling table body 11 is one of ceramics, concrete or glass, and the material of the confinement ring 12 is steel, aluminum alloy, titanium alloy or fiber reinforced polymer material.
  • the assembly method is as follows: place the confinement ring 12 on the platform, apply epoxy resin, glass glue or vacancies on the inner wall of the confinement ring 12 and the outer side wall of the filling platform 11, and then put the filling platform 11 into the confinement ring
  • the big end of 12 is open. Before thrust is applied, there is no contact force between the two contact surfaces.
  • a jack or a press is used to apply a vertical downward thrust to the upper surface of the filling platform 11, and the filling platform 11 is pushed down on the inner ring of the confinement ring 12 to obtain the prestressed restraint block 1. Due to the difference between the filling platform 11 and the confinement ring 12, the elastic restoring force of the confinement ring 12 squeezes the pre-tensioning the filling platform 11 and applies a pre-compression stress in its radial direction.
  • the filling platform 11 and the confinement ring 12 adopts a combined structure.
  • the filling platform 11 can be a combined platform, which is composed of a first reducing ring 14 and a cylinder or prism, and the column is embedded in the first reducing ring 14;
  • the constraining ring 12 can be a combined ring structure, consisting of
  • the second reducing ring 13 is constituted by a cylindrical ring or prismatic ring of equal cross section, and the second reducing ring 13 is embedded and fixed in the cylindrical ring or prismatic ring of equal cross section.
  • the axial cross-sections of the first reducing ring 14 and the second reducing ring 13 are both wedge-shaped cross-sections, and the outer side wall of the first reducing ring 14 and the inner wall of the second reducing ring 13 enclose a conical surface or a pyramid surface.
  • the filling table body 11 in the figure adopts the same truncated cone or pyramid body as in the first embodiment
  • the constraining ring 12 adopts a cylindrical ring or prismatic ring in which the second reducing ring 13 is fixed and embedded inside, and the second The inner wall of the reducing ring 13 is the conical surface or the inner wall of the polygonal pyramid surface of the constraining ring 12.
  • the filling platform 11 in the figure adopts a cylindrical or prism body that is externally fixed and fitted with the first reducing ring 14, and the outer side wall of the first reducing ring 14, that is, the filling platform 11 is a conical surface or a polygonal pyramid
  • the confinement ring 12 adopts the same integral reducing ring body with a conical surface or a polygonal pyramid surface inner ring wall as in the first embodiment.
  • the filling platform 11 in the figure adopts a cylindrical or prism body that is externally fixed and fitted with the first reducing ring 14, and the outer side wall of the first reducing ring 14, that is, the filling platform 11 is a conical surface or a polygonal pyramid
  • the constraining ring 12 adopts a cylindrical ring or a prismatic ring in which the second reducing ring 13 is fixed and embedded inside.
  • the inner wall of the second reducing ring 13 is the conical or polygonal pyramid surface of the constraining ring 12.
  • the second reducing ring 13 is used to adjust the inclination angle of the inner wall of the equal cross-section confinement ring 12, and the first reducing ring 14 is used to adjust the inclination angle of the outer side surface of the equal cross-section filling table body 11.
  • the ring turns the equal cross-section confinement ring and the equal cross-section filling block into a combined confinement ring and a combined filling platform respectively, and the dimensions of the formed combined confinement ring and combined filling platform refer to Embodiment 1.
  • the reducing ring is fixed with the table body or the constraining ring by means of nesting, welding or adhesive bonding.
  • the material of the reducing ring can be made of elastic-plastic materials such as metal with better toughness and greater rigidity, or fiber-reinforced polymer, such as aluminum alloy and low-strength steel, which produces an appropriate amount of compression deformation during the extrusion process, so that the filling block and The restraint ring fits better.
  • a wrapping layer 17 is wrapped on the outer surface of the filling platform body 11.
  • a thinner layer of metal is wrapped on its outer surface, such as a metal material such as a molten aluminum alloy or iron alloy, or a fiber-reinforced polymer material is pasted and wrapped on its surface.
  • the table body 11 is pressed into the inner ring of the confinement ring 12.
  • the filling platform 11 in this embodiment uses multiple layers of filling materials.
  • the filling platform 11 includes a first filling block 111, an interlayer 113, and a second
  • the filling block 112 the first filling block 111 and the second filling block 112 are made of the same material of the filling platform, and there is an interlayer or gap between the two filling blocks.
  • the method shown in Fig. 7a can be used.
  • the second filler block 112 below is pressed into the inner ring of the confinement ring 12, and then the interlayer 113 is arranged or missing on the surface, and then the first filler block 111 is pressed into it.
  • the first filling block 111, the interlayer 113, and the second filling block 112 are mounted and glued in order to form an integral filling platform body 11, and then the filling platform The body 11 is integrally pressed into the inner ring of the confinement ring 12.
  • the material of the interlayer 113 can be at least one of foamed metal, metal layer, graphite retention layer, rubber, polymer porous material, resin binder, or air layer, and the foamed metal is preferably foamed aluminum.
  • the filling table body with a multi-layer filling block structure can reduce the impact damage range and damage degree of the filling block.
  • two or more multi-layer filling blocks can be used to fill according to the armor thickness.
  • the material of the filling block can be ceramic or concrete.
  • At least one of glass and metal materials, and the surface layer on the outside is preferably a ceramic material.
  • the surface of the filling platform 11 using multiple layers of filling materials can also be provided with a wrapping layer 17 on the entire surface of the filling platform 11 in the manner of the fourth embodiment.
  • the pyramid body 11 when the filling platform body 11 adopts a polygonal pyramid structure, in order to reduce the damage range, the pyramid body can be assembled from a plurality of small prisms in a plane arrangement to form a large pyramid filling platform body, and the combined large prism body The pre-stress is applied by inserting and squeezing into the restraining ring 12.
  • the upper surface or the lower surface of the filling table body 11 may be flat, or may be provided as spherical crown-shaped protrusions, or pyramid-shaped protrusions, or other stacking methods.
  • the confinement ring 12 is provided with a bottom plate structure. As shown in Figure 8, the height of the confinement ring 12 in this embodiment is greater than the thickness of the filling platform 11, and the bottom of the confinement ring 12 in the first embodiment or the second A cushion layer 15 is provided at the opening at the small end of the bottom of the reducing ring 13. Before the filling table body 11 is pressed into the inner ring of the constraining ring 12, the energy-absorbing cushion layer 15 is filled at the bottom of the inner ring of the constraining ring 12, and then pressed into the filling table. The body 11 is prestressed.
  • the cushion layer 15 can be made of porous material or foamed metal, such as foamed aluminum, or a polymer material such as rubber as a cushioning material.
  • the confinement ring 12 in this embodiment is a confinement groove bottom plate 16 integrated with the confinement ring 12, that is, the confinement groove bottom plate 16 and The outer wall of the confinement ring 12 is an integral structure.
  • the bottom small end of the confinement ring 12 is sealed by the confinement groove bottom plate 16 to form a groove-shaped confinement ring.
  • the confinement groove bottom plate 16 Fill the upper surface of a thinner foam aluminum cushion layer, and then press into the filling table body 11, the foam aluminum cushion layer makes the bottom surface of the filling table body 11 and the constraining groove bottom plate 16 more closely fit.
  • the constraining groove bottom plate 16 increases the bending rigidity of the prestressed constraining block to a certain extent, and plays the role of an armor back plate to a certain extent.
  • the constraining ring 12 in this embodiment is provided with a ring of clamping grooves 18 inside the large end of the inner ring wall, and the filling table 11 is pressed into the inner ring of the constraining ring 12.
  • a snap ring 19 is installed in the groove 18 of the ring 12 to axially limit the filling platform 11.
  • the size of the large end of the filling platform 11 is much larger than the opening of the small end of the inner ring of the constraining ring 12, it is tightly wedge
  • the rear filling platform 11 cannot escape from the small end of the confinement ring 12.
  • Assembling a snap ring 19 on the inner wall of the large end of the confinement ring 12 can effectively prevent the filling platform 11 from moving away from the large end of the confinement ring 12 when it is impacted. Slide out.
  • the snap ring 19 adopts an elastic opening snap ring that is easy to install.
  • the filling table body 11 is damaged, by taking out the snap ring 19, the damaged filling table body 11 is pushed back from the small end of the inner ring of the restraining ring to the large port, and replaced
  • the new filling platform 11 can quickly repair damaged or destroyed armored structures.
  • the surface of the filling table body 11 will be lower than the top surface of the confinement ring 12, and a metal plate, epoxy resin or polyurea can be further used. Material filling and leveling.
  • This embodiment can be applied to the prestressed constraining blocks in the first to sixth embodiments, and the corresponding circular split snap ring or polygonal bayonet snap ring can be selected according to the transverse cross-sectional shape of the filling platform and the constraining ring.
  • the composite armor structure includes a layer of armor plate formed by splicing a plurality of prestressed restraining blocks 1.
  • the prestressed constraining block 1 adopts a filling platform 11 and a constraining ring 12 with a regular hexagon in cross section, and spreads and spreads in the transverse direction to form a continuous armor plate.
  • the confinement ring 12 is made of high-strength steel, and the regular hexagonal filling table body 11 is made of any one or more of ceramic, concrete or glass.
  • Fig. 11b discloses a composite armor structure including two layers of armor plates in Fig. 11a.
  • the prestressed restraint blocks 11 between the armor plates are misaligned.
  • the prestressed constrained blocks 11 separated by dislocation are used to compensate for the prestress of the single-layer composite armored structure.
  • the weakened areas of protection at the joints of the stress-constrained blocks increase the protective effect of the composite armor structure.
  • different layers of armor plates can be stacked according to the protection requirements and the overall thickness of the armor.
  • the spliced prestressed restraint blocks 1 are all separate restraint rings, that is, all the restraint rings 12 and the filling platform 11 are assembled into a single prestressed restraint block 11. , All the prestressed restraint blocks 11 are spliced and laid. Fig.
  • 11c discloses another way of paving the armor plate, that is, all the confinement rings 12 of the prestressed constraining block 1 adopt an integrated honeycomb structure, and all the confinement rings 12 are connected into an integral conjoined confinement ring 121, which can be welded Fix them together or directly process all the hexagonal inner walls of the confinement ring 12 on a whole plate structure to form a honeycomb plate structure, and then assemble all the filling table bodies 11 into the inner ring of the corresponding confinement ring one by one.
  • the conjoined confinement ring 121 of the structure increases the integrity of the armor plate.
  • This example discloses a further specific implementation of the composite armor structure of the present invention.
  • this example covers the cover plate 2 and the back plate 3 on both sides of the armor plate, respectively.
  • the cover plate 2 is used for the appearance of the outer side of the armor and improves the protective effect of the armor to a certain extent, and the back plate 3 increases the impact resistance of the inner side of the armor.
  • the installation method of the cover plate 2 or the back plate 3 can be combined with the pre-stressed restraint block 1 of the armor plate by an adhesive, or the cover plate 2 or the back plate 3 and the armor plate can be anchored by bolts, wherein the bolts can pass through the cover plate.
  • the plate 2 or the reserved hole of the back plate 3 is anchored.
  • the cover plate 2 is divided into a single-layer, double-layer or multi-layer composite board. Specifically, as shown in Figures 12a, 12b and 12c, the optional cover plate 2 in this embodiment is divided into three forms: a single-layer protective layer, a protective surface layer + a holding layer, and a two-layer protective layer + a holding layer.
  • the cover plate 2 of the single-layer protective surface layer is shown in FIG. 12a.
  • the first protective surface layer 21 is preferably made of metal materials such as steel plates, aluminum alloys, titanium alloys, or polymer materials or fiber-reinforced polymer materials, such as polyurea. Coating, polycarbonate coating, and the composite armor structure in FIG. 14a and FIG. 14c are all directly attached to the first protective surface layer 21 as the cover plate 2 on the outer surface of the armor plate.
  • the cover 2 of the double-layer structure of the protective surface layer + the containment layer is shown in FIG.
  • Materials, such as polyurea coating and polycarbonate coating, the retaining layer 22 is made of graphite material, which is attached to the prestressed constraining block.
  • the composite armor structures in Figure 14b, Figure 14d and Figure 14e are all pasted on the outer surface of the armor plate.
  • the cover plate 2 is attached to the outer side of the armor plate in the order of the first protective surface layer of the steel plate + the graphite holding layer.
  • the three-layer structure cover plate 2 of three forms of two-layer protective layer + storage layer is shown in Figure 12c.
  • the first protective layer 21 is preferably made of metal materials such as steel plate, aluminum alloy, titanium alloy, or polymer material. Or fiber-reinforced polymer materials, such as polyurea coating or polycarbonate coating, the retaining layer 22 is made of graphite material, which is attached to the prestressed constraining block, and the second protective surface layer 23 is made of copper alloy material from the prestressed constraining block. From the distal end to the proximal end, the cover plate 2 of the three-layer structure is attached to the outer side of the armor plate in the order of a steel plate first protective surface layer + a copper plate second protective surface layer + a graphite holding layer.
  • the backplane 3 is divided into a single-layer, double-layer or multi-layer composite board, including at least one layer of a collision layer 31, an energy absorption layer 32, and a resistance layer 33, as shown in FIGS. 13a, 13b, and 13c.
  • the backplane 3 in Figure 13a has a single-layer resistance layer 33 structure.
  • the resistance layer 33 uses one or more of metal materials such as steel plates, aluminum alloys, and titanium alloys, or uses polymer materials or fiber-reinforced polymer materials.
  • the composite armor structure in 14a and 14b is directly attached to the resistance layer 33 as the back plate 3 on the inner surface of the armor plate.
  • the backplane 3 in Figure 13b has a double-layer structure of an energy absorbing layer 32 + a resistance layer 33.
  • the resistance layer 33 is made of one or more of metal materials such as steel plates, aluminum alloys, titanium alloys, or polymer materials or fibers. Reinforced polymer material, the energy-absorbing layer 32 is made of one or more of foamed metal and rubber.
  • the composite armor structure in Figure 14c and Figure 14d is attached to the double-layer backplane 3 in Figure 13b on the inner surface of the armor plate. , The energy-absorbing layer 32 is arranged close to the armor plate.
  • the back plate 3 in Figure 13c is a three-layer structure of collision layer 31 + energy absorption layer 32 + resistance layer 33.
  • the resistance layer 33 is made of one or more of metal materials such as steel plate, aluminum alloy, titanium alloy, or polymer. Material or fiber-reinforced polymer material, the energy absorbing layer 32 is made of one or more of foamed metal and rubber, and the collision layer 31 is made of one or more of metal materials such as steel plate, aluminum alloy, titanium alloy, or Using polymer materials or fiber-reinforced polymer materials, the composite armor structure in FIG. 14e is attached to the three-layer backplane 3 in FIG. 13c on the inner surface of the armor plate, and the collision layer 31 is arranged close to the armor plate.
  • the armor plate spliced by the prestressed restraint block 1 can be used alone as armor, but in order to obtain a better protective effect, the cover plate 2 and the back plate 3 are installed on its surface, and the cover plate 2 is attached to the two surfaces of the prestressed restraint block It is preferable to install one side close to the large end of the filling platform, and install the back plate 3 on the other side.
  • the cover plate 2 and the back plate 3 and the pre-stressed restraint block can be bonded by a resin adhesive, or anchored by bolts.
  • a specific size of the filling table body and the confinement ring in the first embodiment is drawn as shown in FIG.
  • the height h1 of the filling platform is 40mm, and the height h2 of the confinement ring 12 is 50mm;
  • the diameter d 1 of the large end of the top surface of the filling platform 11 is 100mm, and the diameter d 2 of the small end of the bottom surface is 95.8mm; the inner diameter R 1 of the large end of the inner ring wall of the confinement ring 12 is 100mm, and the inner diameter R 2 of the small end of the bottom surface is 94.8mm ;
  • the difference between the outer diameter of the small end of the bottom surface of the filling platform 11 and the inner diameter of the small end of the bottom surface of the confinement ring 12 is 1mm, because the height of the confinement ring is greater than the height of the filling platform, and the inclination of the inner wall of the confinement ring and the outer side of the filling platform The wall inclination is the same.
  • the outer diameter of the large end of the top surface of the filling platform 11 and the inner wall of the confinement ring 12 will be the same as the small end.
  • the surplus difference; the outer diameter of the confinement ring 12 is 110mm, the top wall thickness of the confinement ring 12 is 5mm, and the bottom wall thickness is 7.6mm.
  • the material of the filling table body 11 is one of ceramics, concrete or glass, and the material of the confinement ring 12 is steel, aluminum alloy, titanium alloy or fiber reinforced polymer material.
  • the explicit finite element program LS-DYNA is used for the prestressed restraint block to establish a three-dimensional numerical model of the concrete circular table pressing into the steel restraining ring to impose prestress and bullet penetration.
  • the finite element model and mesh division of the prestressed constraining block are established according to the geometric dimensions of the filling platform and the confinement ring. As shown in Figure 16, the model is composed of a circular constraining ring, a round table, a bullet, a backing plate and a thrust block, with 8 knots
  • the point solid hexahedral element (*SECTION_SOLID) is modeled. According to the symmetry condition, only a 1/4 model that is symmetrical along the zy plane and the zx plane is established.
  • the average size of the truncated cone unit and the confinement ring unit is about 1.25mm, the total number of concrete truncated cone units is 49152, and the total number of confinement ring units is 10240.
  • the average grid size of the bullet is 1.25mm and it is divided into 300 units.
  • the boundary condition of the backing plate is fixed, and surface contact (keyword *CONTACT_AUTOMATIC_SURFACE_TO_SURFACE) is adopted between the confinement ring, round table, backing plate, and thrust block.
  • the static friction coefficient between the two is 0.08, and the dynamic friction coefficient is 0.06.
  • the contact between the bullet and the concrete is realized with the keyword *CONTACT_ERODING_SURFACE_TO_SURFACE.
  • the concrete material adopts the HJC model, the concrete density is 2400kg/m 3 , the strength is 170MPa, and the specific parameters are shown in Table 1.
  • the *MAT_ADD_EROSION erosion failure criterion is introduced, and the maximum principal strain is used to control the failure of the element.
  • the maximum principal strain of an element of the target body exceeds the strain value during the simulation process, the element is considered to be invalid and deleted, and the failure strain is set to 0.1.
  • the material of the confinement ring and the flat-headed bullet adopts the *MAT_PLASTIC_KINEMATIC material model.
  • the main parameters of the material model are shown in Table 2.
  • the loading system and test process are divided into two stages.
  • the first stage pushes down the round table to apply pre-stress simulation test, and then the second stage conducts anti-penetration simulation test.
  • the keyword *BOUNDARY_PRESCRIBED_MOTION_SET is used to give the thrust block displacement to push the concrete circular platform to the specified depth of the steel ring
  • the loading rate is 200mm/s
  • the stability is 10ms
  • the corresponding restart file is generated.
  • the bullet does not move in the first phase.
  • the bullet is a flat-headed bullet with a diameter of 7.62mm, a length of 20mm, and an initial velocity of 600m/s.
  • the pushing depth of the filling table body in the inner ring of the confinement ring is from 0 to 10mm, and the pushing down displacement is divided into 10 levels.
  • the radial prestress of the round table gradually increases.
  • the damage cloud diagram of the filled platform concrete cylindrome at various levels of depression depth is shown in Figure 18.
  • the use of the prestressed restraint block of the present invention to apply a reasonable prestress value can greatly improve the anti-penetration performance of the composite armor component.

Abstract

A prestress constrained block and a composite armor structure. The prestress constrained block comprises a filling platform body (11) and a constraint ring (12). The filling platform body (11) has a cross section of the same shape as that of an inner ring of the constraint ring (12), and is fixedly embedded in the inner ring of the constraint ring (12), an outer side wall of the filling platform body (11) and an inner ring wall of the constraint ring (12) being wedged tightly by means of the fit of conical surfaces or polygonal pyramid surfaces. The composite armor structure comprises at least one layer of armor plates. The armor plates comprise several prestress constrained blocks. For the prestress constrained blocks, several separate constrain rings that are spliced are used or a constraint ring with an integrated honeycomb structure is used. The prestress constrained block can apply a radial prestress to fragile materials such as ceramics, concrete or glass in a room temperature condition, and can adjust and control the magnitude of the prestress; and the prestress constrained block is suitable for applying prestress to components of various sizes and is easier to assemble, and damaged or broken components can be easily replaced, so that the prestress constrained block is applied to a plurality of protection fields such as armed helicopters, armored vehicles, ships, tanks, aircraft warehouses and missile-well covers.

Description

预应力约束块和复合装甲结构Prestressed restraint block and composite armor structure 技术领域Technical field
本发明属于装甲技术,具体涉及一种预应力约束块和复合装甲结构。The invention belongs to armor technology, and specifically relates to a prestressed restraint block and a composite armor structure.
背景技术Background technique
采用陶瓷材料的复合装甲的抗侵彻性能主要取决于陶瓷的抗压强度和硬度、粉碎特征、碎片流动摩擦性和碎粒磨蚀;陶瓷的高抗压强度在一定程度提高抗侵彻性能;陶瓷表面积粉碎区能量吸收是陶瓷抗侵彻一种重要因素;对于厚而严格约束的陶瓷块,陶瓷碎片的流动摩擦作用是抗侵彻的最重要因素。研究表明,在对陶瓷靶进行侧向约束后,弹体侵彻约束陶瓷的过程中,约束环会对陶瓷靶板产生约束力,这样可以有效遏制陶瓷材料裂纹的扩展,从而提高陶瓷材料的抗侵彻性能。随着研究的深入,越来越多的人开始研究对陶瓷提前施加内部应力,对陶瓷材料抗侵彻性能的影响。The anti-penetration performance of composite armor using ceramic materials mainly depends on the ceramic's compressive strength and hardness, crushing characteristics, fragment flow friction and particle abrasion; the high compressive strength of ceramics improves the anti-penetration performance to a certain extent; ceramics Energy absorption in the surface area of the crushing zone is an important factor for ceramic anti-penetration; for thick and strictly constrained ceramic blocks, the flow friction of ceramic fragments is the most important factor for anti-penetration. Studies have shown that after the ceramic target is laterally constrained, when the projectile penetrates the constrained ceramic, the confinement ring will exert a constraining force on the ceramic target plate, which can effectively curb the crack propagation of the ceramic material, thereby improving the resistance of the ceramic material. Penetration performance. With the deepening of research, more and more people have begun to study the effect of applying internal stress to ceramics in advance on the anti-penetration performance of ceramic materials.
对于复合装甲的陶瓷材料进行施加预应力,可以有效抑制靶体内部裂纹萌生和扩展。即使在高速冲击下陶瓷内部发生断裂,但陶瓷各裂块之间仍挤压得较为紧密,只有裂纹而没有扩容,使得破碎陶瓷区域内部存在较大侵彻阻力。陶瓷颗粒与弹丸的逆向运动会对弹丸质量产生磨蚀作用,并且使相互的摩擦等耗能机制发挥作用,有效的提高陶瓷的抗侵彻性能。Prestressing the ceramic material of the composite armor can effectively inhibit the initiation and propagation of cracks in the target body. Even if fracture occurs inside the ceramic under high-speed impact, the ceramic fragments are still squeezed relatively tightly, and there are only cracks without expansion, so that there is a large penetration resistance inside the broken ceramic area. The reverse movement of the ceramic particles and the projectile will have an abrasion effect on the quality of the projectile, and make the energy dissipation mechanism such as mutual friction play a role, effectively improving the anti-penetration performance of the ceramic.
技术问题technical problem
目前国内外的学者对陶瓷施加预应力方法主要有:机械挤压法和热装法,机械挤压法是从陶瓷材料的侧面加压,对陶瓷材料内部形成横向的压紧预应力;热装法是将陶瓷材料和金属材料的约束结构在高温下相互固定,然后整体降温,热膨胀系数较大收缩更快的金属压缩陶瓷施加预应力,如申请号为201810777211.4的中国专利申请公开的一种约束陶瓷-金属复合防弹装甲板及其制备方法。At present, scholars at home and abroad mainly apply prestressing methods to ceramics: mechanical extrusion and hot packing. The mechanical extrusion method presses on the side of the ceramic material to form a transverse compression prestress on the inside of the ceramic material; hot packing The method is to fix the constrained structure of the ceramic material and the metal material at high temperature, and then the overall temperature is lowered, and the metal compression ceramic with a larger thermal expansion coefficient and faster shrinkage is applied to prestress, such as a constraint disclosed in the Chinese patent application with application number 201810777211.4 Ceramic-metal composite bulletproof armor plate and preparation method thereof.
采用热冷缩或者机械加压的方式均可以使陶瓷内部产生预应力。在对复合装甲进行预应力试验中需要稳定的预应力且预应力大小可调整,在实际试验条件限制下,热装法热处理时对金属的强度将产生不利影响,通过控制温度以调节陶瓷内部预应力大小的方式难以实现长杆弹撞击试验,因此试验中大多采用机械挤压法,而机械施加压力装置要求从陶瓷材料的四周均匀侧向加压,对陶瓷材料和约束结构之间的装配尺寸加工精度要求高,并且多个面同时施压,设备构造比较复杂,但很难在实际工程中应用,仅仅限于研究。Both heat and cold shrinkage or mechanical pressure can be used to generate prestress inside the ceramic. In the pre-stress test of composite armor, a stable pre-stress is required and the pre-stress size can be adjusted. Under the limitation of actual test conditions, the heat treatment of the hot charging method will have an adverse effect on the strength of the metal. The temperature is controlled to adjust the internal pre-stress of the ceramic The method of stress magnitude is difficult to achieve the long rod impact test, so the mechanical extrusion method is mostly used in the test, and the mechanical pressure device requires uniform lateral pressure from the periphery of the ceramic material, and the assembly size between the ceramic material and the restraint structure The machining accuracy is high, and multiple surfaces are pressurized at the same time. The equipment structure is relatively complicated, but it is difficult to apply in actual engineering and is only limited to research.
技术解决方案Technical solutions
本发明解决的技术问题是:针对现有复合装甲施加预应力的机械挤压法和热装法存在的上述问题,提供一种能够在室温环境下实现快速装配的预应力约束块和复合装甲结构。The technical problem solved by the present invention is to provide a prestressed restraint block and a composite armor structure that can be quickly assembled in a room temperature environment in view of the above-mentioned problems existing in the mechanical extrusion method and the hot charging method of applying prestress to the existing composite armor .
本发明采用如下技术方案实现:The present invention adopts the following technical solutions to achieve:
预应力约束块,包括填充台体11和约束环12,所述填充台体11具有和约束环12内圈相同形状的横截面,并固定嵌装于约束环12的内圈,所述填充台体11的外侧壁和约束环12的内圈壁之间通过锥面配合而楔紧;The pre-stressed constraining block includes a filling platform 11 and a constraining ring 12. The filling platform 11 has a cross section of the same shape as the inner ring of the constraining ring 12, and is fixedly embedded in the inner ring of the constraining ring 12. The filling platform The outer side wall of the body 11 and the inner ring wall of the constraining ring 12 are wedged tightly through taper fit;
所述填充台体11的外侧壁和约束环12的内圈壁分别为相匹配的圆锥面,或相匹配的多边形棱锥面。The outer side wall of the filling platform 11 and the inner wall of the confinement ring 12 are respectively matched conical surfaces or matched polygonal pyramid surfaces.
上述方案中的预应力约束块中,所述填充台体11外侧壁的大端和小端直径分别为d 1和d 2,所述约束环12内圈壁的大端和小端直径分别为R 1和R 2,满足R 2<d 2<R 1≤d 1,所述填充台体11和约束环12的高分别为h1和h2,其中h1≤h2。 In the prestressed restraint block in the above solution, the diameters of the large end and the small end of the outer side wall of the filling platform 11 are respectively d 1 and d 2 , and the diameters of the large end and the small end of the inner wall of the confinement ring 12 are respectively R 1 and R 2 satisfy R 2 ≦d 2 ≦R 1 ≦d 1 , and the heights of the filling platform 11 and the confinement ring 12 are h1 and h2, respectively, where h1≦h2.
上述方案中的预应力约束块中,所述填充台体11外侧壁的锥面倾角α范围为1°~10°,优选3°~6°,所述约束环12内圈壁的锥面倾角β范围为1°~10°,优选3°~6°,所述填充台体11的外侧壁和约束环12的内圈壁之间存在角度差Δα,Δα=α-β,Δα的取值范围为0°~0.5°,优选0°~0.2°。In the prestressed restraint block in the above solution, the inclination angle α of the cone surface of the outer side wall of the filling platform 11 ranges from 1° to 10°, preferably 3° to 6°. The range of β is 1°~10°, preferably 3°~6°. There is an angular difference Δα between the outer side wall of the filling table body 11 and the inner wall of the confinement ring 12, Δα=α-β, the value of Δα The range is 0°~0.5°, preferably 0°~0.2°.
上述方案中的预应力约束块中,所述填充台体11的径厚比d 1/h 1为0.5~40,优选3~12。 In the prestressed constraining block in the above solution, the diameter-to-thickness ratio d 1 /h 1 of the filling table body 11 is 0.5-40, preferably 3-12.
上述方案中的预应力约束块中,所述填充台体11为具有圆锥面或多边形棱锥面外侧壁的锥台体,In the prestressed constraining block in the above solution, the filling platform 11 is a frustum with a conical surface or an outer side wall of a polygonal pyramid surface,
或外部固定套装第一变径环14的圆柱体或棱柱体,所述第一变径环14的外侧壁为圆锥面或多边形棱锥面。Or, the cylinder or prism of the first reducing ring 14 is fixed externally, and the outer side wall of the first reducing ring 14 is a conical surface or a polygonal pyramid surface.
上述方案中的预应力约束块中,所述约束环12为具有圆锥面或多边形棱锥面内圈壁的变径环体,In the prestressed constraining block in the above solution, the constraining ring 12 is a reduced-diameter ring body with an inner ring wall of a conical surface or a polygonal pyramid surface,
或内部固定嵌装第二变径环13的圆柱环或棱柱环,所述第二变径环13的内圈壁为圆锥面或多边形棱锥面。Or a cylindrical ring or a prismatic ring in which the second reducing ring 13 is fixed and embedded, and the inner wall of the second reducing ring 13 is a conical surface or a polygonal pyramid surface.
上述方案中的预应力约束块中,所述填充台体11为分层结构,包括至少两层固定叠装的填充块。In the prestressed constraining block in the above solution, the filling platform 11 has a layered structure and includes at least two layers of fixed and stacked filling blocks.
上述方案中的预应力约束块中,所述填充台体11外表面包裹设有包裹层17。In the prestressed constraining block in the above solution, the outer surface of the filling platform body 11 is wrapped with a wrapping layer 17.
上述方案中的预应力约束块中,所述约束环12或第二变径环13内圈壁的小端设有底板结构,所述底板结构为与约束环12一体结构的约束槽底板16,或垫装在填充台体11小端的垫层15。In the prestressed restraining block in the above solution, the small end of the inner wall of the restraining ring 12 or the second reducing ring 13 is provided with a bottom plate structure, and the bottom plate structure is a restraining groove bottom plate 16 integrally structured with the restraining ring 12, Or the cushion is mounted on the cushion layer 15 at the small end of the filling platform 11.
上述方案中的预应力约束块中,所述填充台体11为陶瓷、混凝土或者玻璃材料,所述约束环12为金属或者纤维增强复合材料。In the prestressed restraint block in the above solution, the filling platform 11 is made of ceramic, concrete or glass material, and the restraining ring 12 is made of metal or fiber reinforced composite material.
在本发明的预应力约束块中,所述约束环12的内壁开设有卡槽18,所述卡槽18内装配用于楔紧后的填充台体11在约束环12内轴向限位的卡环19。In the prestressed constraining block of the present invention, the inner wall of the constraining ring 12 is provided with a clamping groove 18, and the clamping groove 18 is equipped with a wedge for the filling platform 11 to axially limit the constraining ring 12 Snap ring 19.
本发明还公开了一种复合装甲结构,包括至少一层装甲板,所述装甲板包括若干本发明上述的预应力约束块,所述预应力约束块采用若干分体的约束环12拼接,或采用一体蜂窝结构的约束环12。The present invention also discloses a composite armored structure, including at least one layer of armor plate, the armor plate includes a plurality of the above-mentioned prestressed restraint blocks of the present invention, the prestressed restraint blocks are spliced by a plurality of split restraint rings 12, or A confinement ring 12 with an integrated honeycomb structure is adopted.
上述方案中的复合装甲结构中,还包括分别贴合覆盖复合装甲两侧表面的盖板2和背板3。The composite armor structure in the above solution also includes a cover plate 2 and a back plate 3 respectively attached to cover both sides of the composite armor.
有益效果Beneficial effect
本发明具有如下有益效果:The present invention has the following beneficial effects:
本发明将陶瓷、混凝土或者玻璃等材质的填充台体压入金属或者纤维增强复合材料制成的约束环内圈中得到预应力约束块,其中的约束环和填充台体之间通过锥面配合楔紧,根据套箍约束原理,约束环内圈与填充台体之间通过锥面楔紧具有自紧功能,当填充台体在约束环内圈越压越紧,约束力的锥面斜面上产生的径向套箍力随着竖直压力的增大而增大,这样填充台体的强度变大,约束环的弹性恢复力对填充台体施加侧向预应力,增加约束块的抗侵彻和抗爆炸冲击性能。The present invention presses the filling platform body made of ceramic, concrete or glass into the inner ring of the confinement ring made of metal or fiber reinforced composite material to obtain the prestressed constraining block, wherein the confinement ring and the filling platform body are matched by a cone Wedge tightening, according to the hoop restraint principle, the inner ring of the confinement ring and the filling platform are wedge tightly tightened through the tapered surface to have a self-tightening function. The generated radial hoop force increases with the increase of vertical pressure, so that the strength of the filling platform becomes larger, and the elastic restoring force of the confinement ring exerts a lateral prestress on the filling platform, which increases the resistance of the restraining block. Thorough and anti-explosive shock performance.
本发明的预应力约束块可以在室温条件下非常简便地对陶瓷、混凝土或者玻璃等脆性材料施加径向预应力,预应力可以通过填充台体的楔入约束环内圈的深度或者填充台体和约束环之间楔紧的锥面倾角大小控制,适合各种尺寸的填充台体构件施加预应力。The prestressed constraining block of the present invention can very simply apply radial prestress to brittle materials such as ceramics, concrete or glass at room temperature. The prestress can be filled with the depth of the inner ring of the constrained ring or the filling of the table body by the wedge of the table body. The taper inclination angle between the wedge and the constraining ring is controlled, which is suitable for prestressing of various sizes of filling platform components.
由于本发明预应力约束块不需要像热装法一样通过加热改变构件的相对尺寸,对于热装法很难适用的纤维增强复合材料的约束环、混凝土材料或玻璃材料的填充台体也可以适用于本发明。Since the prestressed constraining block of the present invention does not need to change the relative size of the components by heating like the hot charging method, it can also be applied to the fiber reinforced composite material confinement ring, concrete material or glass material filling table body which is difficult to apply to the hot charging method. In the present invention.
单个预应力约束块拼装成更大面积的复合装甲结构,可以拼装成单层防护装甲板,或者将单层防护装甲板错位叠合成多层防护装甲板,减少薄弱部位,进一步增加防护效果。约束环可以制成整体结构,增加约束环的整体性和装甲板的抗弯能力。A single prestressed restraint block is assembled into a larger area composite armor structure, which can be assembled into a single-layer protective armor plate, or a single-layer protective armor plate can be misplaced and stacked into a multi-layer protective armor plate to reduce weak points and further increase the protective effect. The confinement ring can be made into an integral structure to increase the integrity of the confinement ring and the bending resistance of the armor plate.
在填充台体装入约束环的过程中,由于填充台体的小端外径尺寸比约束环内圈的大端口径具有更大的容差,因此本发明的预应力约束块比热装法更容易装配,台体和约束环部件的尺寸容许误差范围更大,更为环保,受损或者破坏的部件而且容易更换,在武装直升机、装甲车、舰船、坦克、飞机洞库和导弹井盖等多种防护领域具有更为广阔的应用前景。本发明预应力方法除了应用到装甲等防护性材料上,还可以应用到航空、航天器件的陶瓷反射镜、透镜、透明窗户等脆性材料构件上,通过约束环施加预应力提高这些构件的抗弯强度和减轻结构重量。In the process of installing the filling table body into the confinement ring, since the outer diameter of the small end of the filling table body has a larger tolerance than the large port diameter of the inner ring of the confinement ring, the prestressed restraint block of the present invention is more tolerant than the hot-fitting method. It is easier to assemble, the size of the table body and the confinement ring components has a larger tolerance range, and it is more environmentally friendly. Damaged or damaged components are easy to replace. In armed helicopters, armored vehicles, ships, tanks, aircraft caverns and missile manhole covers, etc. A variety of protection fields have broader application prospects. The prestressing method of the present invention is not only applied to protective materials such as armor, but also to brittle material components such as ceramic mirrors, lenses, transparent windows, etc. of aviation and aerospace devices. The prestressing of these components is improved by applying prestress through the confinement ring. Strength and reduce structural weight.
以下结合附图和具体实施方式对本发明作进一步说明。The present invention will be further described below in conjunction with the drawings and specific embodiments.
附图说明Description of the drawings
图1为实施例一中圆形截面预应力约束块的装配示意图。Fig. 1 is a schematic diagram of the assembly of the circular cross-section pre-stressed restraint block in the first embodiment.
图2为实施例一中正六边形截面预应力约束块的装配示意图。Figure 2 is a schematic diagram of the assembly of the pre-stressed restraint block with a regular hexagonal cross-section in the first embodiment.
图3为实施例一中的填充台体和约束环分解剖视图。Fig. 3 is an anatomical view of the filling table body and the constraining ring in the first embodiment.
图4为实施例一中的填充台体和约束环装配过程预应力施加示意图。Fig. 4 is a schematic diagram of pre-stress application during the assembly process of the filling table body and the confinement ring in the first embodiment.
图5a、5b、5c分别为实施例二中的三种填充台体和约束环的装配过程预应力施加示意图。Figures 5a, 5b, and 5c are respectively schematic diagrams of prestressing application during the assembly process of the three filling platform bodies and the confinement ring in the second embodiment.
图6为实施例三中的填充台体和约束环的装配过程预应力施加示意图。Fig. 6 is a schematic diagram of prestressing application during the assembly process of the filling table body and the confinement ring in the third embodiment.
图7a、7b为实施例四中的填充台体和约束环的两种装配过程预应力施加示意图。Figures 7a and 7b are schematic diagrams of prestressing application during the two assembly processes of the filling platform body and the confinement ring in the fourth embodiment.
图8为实施例五中的填充台体和约束环的装配过程预应力施加示意图。Fig. 8 is a schematic diagram of prestressing application during the assembly process of the filling table body and the confinement ring in the fifth embodiment.
图9为实施例六中的填充台体和约束环的装配过程预应力施加示意图。Fig. 9 is a schematic diagram of prestressing application during the assembly process of the filling table body and the confinement ring in the sixth embodiment.
图10为实施例七中的填充台体和约束环的装配过程预应力施加示意图。Fig. 10 is a schematic diagram of prestressing application during the assembly process of the filling platform body and the confinement ring in the seventh embodiment.
图11a、11b和11c为实施例八中复合装甲装配示意图。Figures 11a, 11b and 11c are schematic diagrams of assembling composite armor in the eighth embodiment.
图12a、12b和12c为实施例九中复合装甲的三种盖板剖面示意图。Figures 12a, 12b and 12c are schematic cross-sectional views of three types of cover plates of the composite armor in the ninth embodiment.
图13a、13b和13c为实施例九中复合装甲的三种背板剖面示意图。13a, 13b, and 13c are schematic cross-sectional views of three types of back plates of composite armor in the ninth embodiment.
图14a、14b、14c、14d、14e为实施例九中五种复合装甲的剖面示意图。14a, 14b, 14c, 14d, and 14e are schematic cross-sectional views of five types of composite armor in the ninth embodiment.
图15为实施例一中拟定的圆台与约束环轴线剖面尺寸图。Fig. 15 is a sectional dimension drawing of the frustum and the axis of the confinement ring planned in the first embodiment.
图16为实施例一中拟定尺寸的1/4有限元模型图。Fig. 16 is a 1/4 finite element model diagram of the planned size in the first embodiment.
图17为实施例一中的预应力约束块在预应力模拟过程中的预应力-下压深度关系曲线。Fig. 17 is the prestress-depression depth relation curve of the prestress restraint block in the prestress simulation process in the first embodiment.
图18为实施例一中的预应力约束块在侵彻模拟过程中的填充台体损伤云图。FIG. 18 is a damage cloud diagram of the filling table body during the penetration simulation process of the prestressed restraint block in the first embodiment.
图19为实施例一中的预应力约束块在侵彻模拟过程中的填充台体的侵彻深度-预应力关系曲线Figure 19 is the penetration depth-prestress relationship curve of the filled platform body in the penetration simulation process of the prestressed restraint block in the first embodiment
图中标号:1-预应力约束块;11-填充台体;111-第一填充块;112-第二填充块;113-夹层;12-约束环;121-连体约束环;13-第二变径环;14-第一变径环;15-垫层;16-约束槽底板;17-包裹层;18-卡槽;19-卡环;Numbers in the figure: 1-prestressed restraint block; 11-filled platform body; 111-first filled block; 112-second filled block; 113-sandwich; 12-confined ring; 121-conjoined constrained ring; 13-section Second reducing ring; 14-first reducing ring; 15-cushion layer; 16-constraint groove bottom plate; 17-wrapping layer; 18-slot; 19-snap ring;
2-盖板;21-第一护面层;22-容留层;23-第二护面层;2-cover plate; 21-first protective surface layer; 22-accommodating layer; 23-second protective surface layer;
3-背板;31-碰撞层;32-吸能层;33-抵抗层。3-back plate; 31-collision layer; 32-energy-absorbing layer; 33-resistance layer.
本发明的实施方式Embodiments of the present invention
实施例一Example one
参见图1-4,图示中的预应力约束块1包括填充台体11和约束环12,填充台体11具有和约束环12内圈相同形状的横截面,如图1中的圆形截面和图2中的正六边形截面,填充台体11固定嵌装在约束环12的内圈内,填充台体11的外侧壁和约束环12的内圈壁之间通过锥面配合相互楔紧,利用套箍约束原理,当填充台体11压入约束环12的内圈过程中,约束环12的弹性恢复力反作用到填充台体11上,从填充台体11的外侧壁侧将填充台体11施加挤压预应力。Referring to Figures 1-4, the prestressed constraining block 1 shown in the figure includes a filling platform 11 and a confinement ring 12. The filling platform 11 has a cross section of the same shape as the inner ring of the confinement ring 12, as shown in Figure 1 as a circular cross section. As with the regular hexagonal section in Figure 2, the filling platform 11 is fixedly embedded in the inner ring of the confinement ring 12, and the outer side wall of the filling platform 11 and the inner ring wall of the confinement ring 12 are wedged tightly with each other through a taper fit. , Using the hoop restraint principle, when the filling platform 11 is pressed into the inner ring of the constraining ring 12, the elastic restoring force of the constraining ring 12 reacts to the filling platform 11, and the filling platform is moved from the outer side wall of the filling platform 11 The body 11 is prestressed by extrusion.
本实施例中的填充台体11和约束环12均为整体结构,两者之间通过锥面楔紧,图1中的填充台体11横截面为圆形,其外侧壁为一段圆锥面的台体结构,约束环12的内圈壁同样为一段圆锥面。图2中的填充台体11横截面为正六边形,其外侧壁为一段六棱锥面的变径环体,约束环12的内圈壁同样为一段六棱锥面,多边形截面的约束环12便于拼接成连续的装甲层,实际应用中也可以采用其他多边形棱锥面,包括但不限于三角形、四边形、五边形。The filling platform 11 and the constraining ring 12 in this embodiment are both integral structures, and the two are wedge tightly with a conical surface. The filling platform 11 in FIG. For the platform structure, the inner wall of the confinement ring 12 is also a section of conical surface. The cross section of the filling platform 11 in Fig. 2 is a regular hexagon, and its outer side wall is a section of a hexagonal pyramidal reducing ring. The inner wall of the confinement ring 12 is also a section of a hexagonal pyramid. Spliced into a continuous armor layer, other polygonal pyramid surfaces can also be used in practical applications, including but not limited to triangles, quadrilaterals, and pentagons.
具体参见图3,为了保证填充台体11压嵌到约束环12内部能够产生挤压预应力,填充台体11和约束环12之间的尺寸应当满足以下条件:For details, referring to Fig. 3, in order to ensure that the filling platform 11 is press-fitted into the confinement ring 12 to generate extrusion prestress, the size between the filling platform 11 and the confinement ring 12 should meet the following conditions:
对于填充台体11和约束环12的横截面尺寸,填充台体11外侧壁为锥面,即填充台体11在轴向两端分别设定为大端和小端,其中填充台体11的大端直径为d 1,填充台体11的小端直径为d 2,d 1>d 2,这里所指的直径为图1中填充台体11横截面的外圆直径和图2中填充台体11横截面的正六边形外接圆直径;同样的,约束环12内圈壁为锥面,在约束环12内圈壁轴向两端分别设定大端和小端,其中约束环12的大端直径为R 1,约束环12的小端直径为R 2,R 1>R 2,这里所指的直径为图1中约束环12内圈壁横截面内圆直径和图2中约束环12内圈壁横截面的正六边形外接圆直径,优选,R 2<d 2<R 1≤d 1Regarding the cross-sectional dimensions of the filling platform 11 and the constraining ring 12, the outer side wall of the filling platform 11 is a tapered surface, that is, the filling platform 11 is set to a large end and a small end at both ends in the axial direction. The diameter of the large end is d 1 , the diameter of the small end of the filling station body 11 is d 2 , d 1 >d 2 , and the diameter referred to here is the outer diameter of the cross section of the filling station body 11 in Fig. 1 and the filling station in Fig. 2 The diameter of the circumscribed circle of the regular hexagon of the cross-section of the body 11; similarly, the inner wall of the constraining ring 12 is a tapered surface, and the large end and the small end are respectively set at the two axial ends of the inner ring wall of the constraining ring 12. The diameter of the large end is R 1 , the diameter of the small end of the confinement ring 12 is R 2 , R 1 > R 2 , and the diameter referred to here is the inner circle diameter of the inner wall of the inner ring wall of the confinement ring 12 in Fig. 1 and the confinement ring in Fig. 2 12 The diameter of the circumscribed circle of the regular hexagon of the inner ring wall cross section, preferably, R 2 <d 2 <R 1 ≤ d 1 .
对于填充台体11和约束环12楔合的锥面倾角尺寸,填充台体11外侧壁的锥面倾角α范围为1°~10°,优选3°~6°,约束环12内圈壁的锥面倾角β范围为1°~10°,优选3°~6°,这里所指的锥面倾角为图1中填充台体11外侧壁和约束环12内圈壁的圆锥母线与竖直方向的夹角或图2中填充台体11外侧壁和约束环12内圈壁的棱锥棱线与竖直方向的夹角。For the size of the taper inclination angle between the filling platform 11 and the confinement ring 12, the taper angle α of the outer side wall of the filling platform 11 ranges from 1° to 10°, preferably 3° to 6°. The cone inclination angle β ranges from 1° to 10°, preferably 3° to 6°. The cone inclination angle referred to here is the conical generatrix and vertical direction of the outer wall of the filling platform 11 and the inner wall of the confinement ring 12 in Fig. 1 2 or the angle between the outer wall of the filling platform 11 and the inner wall of the constraining ring 12 in the vertical direction.
对于填充台体11和约束环12的轴向尺寸,填充台体11和约束环12的轴向高度分别为h 1和h 2,其中h 1≤h 2Regarding the axial dimensions of the filling platform 11 and the confinement ring 12, the axial heights of the filling platform 11 and the confinement ring 12 are h 1 and h 2 , respectively, where h 1h 2 .
预应力约束块装配方法和预应力基本原理具体如下:The assembly method of prestressed restraint block and the basic principle of prestress are as follows:
圆形预应力约束块和六边形预应力约束块装配示意图分别如图1和2所示,圆形横截面的填充台体11或者六边形横截面的填充台体11放入对应的约束环12内圈内,为了便于施压,一般将约束环12的内圈大端开口朝上,填充台体11的小端朝下压入约束环12的内圈,然后对填充台体11沿高度方向施加下压推力,约束环12的弹性恢复力向内挤压预紧填充台体11,在其径向施加预压应力,填充台体11在约束环12内圈中的下压深度越大,约束环12施加到填充台体11径向预压应力就越大,填充台体压入预定位置后即得到预应力约束块。填充台体11压入的方式可以采用千斤顶、液压机或者螺栓紧固等方式,为了减少压入阻力,可以在两者的接触锥面涂抹临时润滑剂,待压入预定位置后,去除润滑剂。填充台体11的径向预应力大小可以通过设计调整台体外侧壁圆锥母线或者棱锥棱线与高的夹角,以及填充台体的下压深度,当夹角一定,在约束环12未屈服或者未失效之前,填充台体11的下压深度越大,预应力就越大。台体和约束环可以采用粘结剂粘结,以防止滑移,或者直接接触,通过两者的摩擦力稳定。The assembly diagram of the circular prestressed constraining block and the hexagonal prestressed constraining block are shown in Figures 1 and 2, respectively. The filling platform 11 with a circular cross section or the filling platform 11 with a hexagonal cross section is placed in the corresponding constraint. In the inner ring of the ring 12, in order to facilitate pressure, the large end of the inner ring of the confinement ring 12 is generally opened upward, and the small end of the filling platform 11 is pressed into the inner ring of the constraining ring 12 downward, and then the filling platform 11 is pressed along A downward pushing force is applied in the height direction, and the elastic restoring force of the confinement ring 12 squeezes the pre-stressed filling platform 11 inward, and applies a pre-compression stress in its radial direction. Larger, the greater the radial pre-compression stress applied by the constraining ring 12 to the filling platform 11, and the pre-stressed constraining block is obtained after the filling platform is pressed into a predetermined position. The filling platform 11 can be pressed in by jack, hydraulic press or bolt fastening. In order to reduce the pressing resistance, temporary lubricant can be applied to the contact cone surface of the two, and the lubricant can be removed after being pressed into a predetermined position. The radial prestress of the filling platform 11 can be designed to adjust the included angle between the conical generatrix or pyramid ridge line of the external side wall of the platform and the height of the filling platform, as well as the depression depth of the filling platform. When the included angle is constant, the restraining ring 12 does not yield. Or before failure, the greater the depression depth of the filling platform 11, the greater the prestress. The table body and the confinement ring can be bonded with an adhesive to prevent slippage, or they can be in direct contact, and the friction between the two can be stabilized.
填充台体11可以采用陶瓷、混凝土或者玻璃材料,约束环12为金属或者纤维增强复合材料,纤维增强复合材料包括纤维增强金属基复合材料或纤维增强聚合物。The filling table body 11 may be made of ceramic, concrete or glass material, and the confinement ring 12 is made of metal or fiber reinforced composite material, and the fiber reinforced composite material includes fiber reinforced metal matrix composite material or fiber reinforced polymer.
对于采用混凝土材质的填充台体11的预应力约束块,可以直接以约束环12为模板进行填充台体11的浇筑成型,在混凝土浇筑之前,事先在约束环12内侧涂刷隔离油或者布置隔离薄膜,约束环12底部保留混凝土成型后的压入空间,待混凝土达到强度,支承或者固定约束环的底部,将填充台体11进一步压入约束环12内,使填充台体11产生径向预应力。For the prestressed constraining block of the filling platform 11 made of concrete, the confinement ring 12 can be used as a template for pouring and molding of the filling platform 11. Before the concrete is poured, the inner side of the confinement ring 12 should be painted with isolation oil or arranged isolation Membrane, the bottom of the confinement ring 12 retains the press-in space after the concrete is formed. When the concrete reaches the strength, the bottom of the confinement ring is supported or fixed, and the filling platform 11 is further pressed into the confinement ring 12, so that the filling platform 11 generates a radial pre-tension. stress.
结合图4,填充台体11和约束环12在装配过程中,填充台体11的底面小端直径d2<约束环12内圈顶部的大端开口直径R1,以便于台体装入约束环内。填充台体11的径厚比或者径高比d 1/h 1为0.5~40,优选3~12。约束环12的环壁可以为变厚度,也可以为等厚度,即约束环12的顶部壁厚t1 ≤底部壁厚t2。根据填充台体11需要施加的预应力确定约束环12的壁厚和屈服强度,约束环12的壁厚与填充台体11的直径之比t/d越大,以及约束环12的屈服强度越大,可提供的约束预应力的潜力就越大。受到填充台体11上下横截面直径不一致和约束环12高度方向壁厚不一致的因素影响,填充台体11的预应力在高度方向不均匀,可以通过设计调整填充台体11的外侧壁锥面夹角α与约束环12的内圈壁锥面夹角β的微小差别来调整上下预应力大小变化。将填充台体11压入约束环12内的过程中,预应力约束块的预应力从上至下逐渐增加,适当调大α和β之间的角度差Δα,可以减少台体的上下预应力差距,Δα的取值范围为0°~0.5°,优选0°~0.2°。当α=β,填充台体11放入约束环12内,填充台体11的外侧壁和约束块12内圈壁接触面贴合。将填充台体11放入约束环12内,填充台体11外侧壁与约束环12内圈壁接触应力非常小,此时填充台体11的顶面与约束环12的顶面之间的高差为h3,台体的底面与约束环的底面之间的高差为h4。 With reference to Figure 4, during the assembly process of the filling table body 11 and the confinement ring 12, the diameter d2 of the small end of the bottom surface of the filling table body 11<the large end opening diameter R1 at the top of the inner ring of the confinement ring 12, so that the table body can be fitted into the confinement ring . The diameter-to-thickness ratio or the diameter-to-height ratio d 1 /h 1 of the filling table body 11 is 0.5-40, preferably 3-12. The ring wall of the confinement ring 12 may have a variable thickness or a uniform thickness, that is, the top wall thickness t1 of the confinement ring 12 ≤ the bottom wall thickness t2. The wall thickness and yield strength of the confinement ring 12 are determined according to the prestress that needs to be applied to the filling table body 11. The greater the potential for constrained prestress that can be provided. Affected by the inconsistency of the diameter of the upper and lower cross-sections of the filling platform 11 and the inconsistency of the wall thickness in the height direction of the confinement ring 12, the prestress of the filling platform 11 is uneven in the height direction. The outer wall cone clamp of the filling platform 11 can be adjusted by design. The slight difference between the angle α and the angle β of the conical surface of the inner ring wall of the confinement ring 12 is used to adjust the upper and lower prestress changes. In the process of pressing the filling platform 11 into the confinement ring 12, the prestress of the prestressed constraining block gradually increases from top to bottom, and the angle difference Δα between α and β is appropriately adjusted to reduce the upper and lower prestress of the platform. Difference, the value range of Δα is 0°~0.5°, preferably 0°~0.2°. When α=β, the filling platform 11 is put into the confinement ring 12, and the contact surface of the outer side wall of the filling platform 11 and the inner wall of the constraining block 12 are attached. Put the filling platform 11 into the confinement ring 12. The contact stress between the outer side wall of the filling platform 11 and the inner ring wall of the confinement ring 12 is very small. The difference is h3, and the height difference between the bottom surface of the platform and the bottom surface of the confinement ring is h4.
具体的,图1中的填充台体11为圆台体,约束环12的内圈壁为圆台空腔。填充台体11的材质为陶瓷、混凝土或者玻璃中的一种,约束环12中的材质为钢材、铝合金、钛合金或者纤维增强聚合物材料。其装配方法为:将约束环12置于平台上,在约束环12的内壁和填充台体11的外侧壁涂抹环氧树脂、玻璃胶或者空缺,然后将填充台体11放入约束环12内圈内,未施加推力之前,两者接触面无接触力。采用千斤顶或者压力机对圆台填充台体的上表面施加推力,将填充台体11在约束环12内圈下压,得到预应力约束块1,由于填充台体11与约束环12的盈差,约束环12的弹性恢复力挤压预紧填充台体11,在其径向施加预压应力。Specifically, the filling table body 11 in FIG. 1 is a truncated cone body, and the inner wall of the confinement ring 12 is a truncated cone cavity. The material of the filling table body 11 is one of ceramics, concrete or glass, and the material of the confinement ring 12 is steel, aluminum alloy, titanium alloy or fiber reinforced polymer material. The assembly method is: place the confinement ring 12 on the platform, apply epoxy resin, glass glue or vacancies on the inner wall of the confinement ring 12 and the outer side wall of the filling platform 11, and then put the filling platform 11 into the confinement ring 12 In the circle, before the thrust is applied, there is no contact force between the two contact surfaces. A jack or a press is used to apply thrust to the upper surface of the round-table filling platform, and the filling platform 11 is pressed down on the inner ring of the confinement ring 12 to obtain the pre-stressed constraining block 1. Due to the gap between the filling platform 11 and the confinement ring 12, The elastic restoring force of the confinement ring 12 squeezes the pre-tensioned filling platform 11 and applies a pre-compression stress in its radial direction.
具体的,图2中的填充台体11为正六棱锥台体,约束环12的内圈壁为正六棱锥台空腔。填充台体11的材质为陶瓷、混凝土或者玻璃中的一种,约束环12中的材质为钢材、铝合金、钛合金或者纤维增强聚合物材料。其装配方法为:将约束环12置于平台上,在约束环12的内圈壁和填充台体11的外侧壁涂抹环氧树脂、玻璃胶或者空缺,然后将填充台体11放入约束环12的大端开口,未施加推力之前,两者接触面无接触力。采用千斤顶或者压力机对填充台体11的上表面施加竖直向下的推力,将填充台体11在约束环12内圈下推,得到预应力约束块1。由于填充台体11与约束环12的盈差,约束环12的弹性恢复力挤压预紧填充台体11,在其径向施加预压应力。Specifically, the filling table body 11 in FIG. 2 is a regular hexagonal pyramid frustum body, and the inner wall of the confinement ring 12 is a regular hexagonal pyramid frustum cavity. The material of the filling table body 11 is one of ceramics, concrete or glass, and the material of the confinement ring 12 is steel, aluminum alloy, titanium alloy or fiber reinforced polymer material. The assembly method is as follows: place the confinement ring 12 on the platform, apply epoxy resin, glass glue or vacancies on the inner wall of the confinement ring 12 and the outer side wall of the filling platform 11, and then put the filling platform 11 into the confinement ring The big end of 12 is open. Before thrust is applied, there is no contact force between the two contact surfaces. A jack or a press is used to apply a vertical downward thrust to the upper surface of the filling platform 11, and the filling platform 11 is pushed down on the inner ring of the confinement ring 12 to obtain the prestressed restraint block 1. Due to the difference between the filling platform 11 and the confinement ring 12, the elastic restoring force of the confinement ring 12 squeezes the pre-tensioning the filling platform 11 and applies a pre-compression stress in its radial direction.
实施例二Example two
本实施例中的填充台体11和约束环12中至少一个采用组合结构。填充台体11可以为组合式台体,由第一变径环14和圆柱体或棱柱体构成,柱体嵌固在第一变径环14内;约束环12可以为组合式环结构,由第二变径环13和等横截面圆柱环或棱柱环构成,第二变径环13嵌固在等横截面圆柱环或棱柱环内。第一变径环14和第二变径环13的轴线截面均为楔形截面,第一变径环14的外侧壁和第二变径环13的内圈壁围成圆锥面或棱锥面。In this embodiment, at least one of the filling platform 11 and the confinement ring 12 adopts a combined structure. The filling platform 11 can be a combined platform, which is composed of a first reducing ring 14 and a cylinder or prism, and the column is embedded in the first reducing ring 14; the constraining ring 12 can be a combined ring structure, consisting of The second reducing ring 13 is constituted by a cylindrical ring or prismatic ring of equal cross section, and the second reducing ring 13 is embedded and fixed in the cylindrical ring or prismatic ring of equal cross section. The axial cross-sections of the first reducing ring 14 and the second reducing ring 13 are both wedge-shaped cross-sections, and the outer side wall of the first reducing ring 14 and the inner wall of the second reducing ring 13 enclose a conical surface or a pyramid surface.
参见图5a,图示中的填充台体11采用与实施例一相同的圆锥台体或棱锥台体,约束环12采用内部固定嵌装第二变径环13的圆柱环或棱柱环,第二变径环13的内圈壁即约束环12的圆锥面或多边形棱锥面内圈壁。Referring to Figure 5a, the filling table body 11 in the figure adopts the same truncated cone or pyramid body as in the first embodiment, and the constraining ring 12 adopts a cylindrical ring or prismatic ring in which the second reducing ring 13 is fixed and embedded inside, and the second The inner wall of the reducing ring 13 is the conical surface or the inner wall of the polygonal pyramid surface of the constraining ring 12.
参见图5b,图示中的填充台体11采用外部固定套装第一变径环14的圆柱体或棱柱体,第一变径环14的外侧壁即填充台体11的为圆锥面或多边形棱锥面外侧壁,约束环12采用与实施例一相同的具有圆锥面或多边形棱锥面内圈壁的整体变径环体。Referring to Figure 5b, the filling platform 11 in the figure adopts a cylindrical or prism body that is externally fixed and fitted with the first reducing ring 14, and the outer side wall of the first reducing ring 14, that is, the filling platform 11 is a conical surface or a polygonal pyramid On the outer side wall, the confinement ring 12 adopts the same integral reducing ring body with a conical surface or a polygonal pyramid surface inner ring wall as in the first embodiment.
参见图5c,图示中的填充台体11采用外部固定套装第一变径环14的圆柱体或棱柱体,第一变径环14的外侧壁即填充台体11的为圆锥面或多边形棱锥面外侧壁,约束环12采用内部固定嵌装第二变径环13的圆柱环或棱柱环,第二变径环13的内圈壁即约束环12的圆锥面或多边形棱锥面内圈壁。Referring to Figure 5c, the filling platform 11 in the figure adopts a cylindrical or prism body that is externally fixed and fitted with the first reducing ring 14, and the outer side wall of the first reducing ring 14, that is, the filling platform 11 is a conical surface or a polygonal pyramid On the outer side wall, the constraining ring 12 adopts a cylindrical ring or a prismatic ring in which the second reducing ring 13 is fixed and embedded inside. The inner wall of the second reducing ring 13 is the conical or polygonal pyramid surface of the constraining ring 12.
本实施例中的第二变径环13用于调节等横截面约束环12内壁的倾斜角,第一变径环14用于调节等横截面填充台体11外侧面的倾斜角,通过变径环将等横截面约束环和等横截面填充块分别变成组合式约束环和组合式填充台体,形成的组合式约束环和组合式填充台体尺寸参考实施例一。变径环采用嵌套、焊接或者粘结剂粘合的连接手段与台体或者约束环的结合固定。变径环的材质可以采用韧性较好、刚度较大的金属或者纤维增强聚合物等弹塑性材料,例如采用铝合金、低强度钢,在挤压过程中产生适量的压缩变形,使填充块与约束环更为贴合。In this embodiment, the second reducing ring 13 is used to adjust the inclination angle of the inner wall of the equal cross-section confinement ring 12, and the first reducing ring 14 is used to adjust the inclination angle of the outer side surface of the equal cross-section filling table body 11. The ring turns the equal cross-section confinement ring and the equal cross-section filling block into a combined confinement ring and a combined filling platform respectively, and the dimensions of the formed combined confinement ring and combined filling platform refer to Embodiment 1. The reducing ring is fixed with the table body or the constraining ring by means of nesting, welding or adhesive bonding. The material of the reducing ring can be made of elastic-plastic materials such as metal with better toughness and greater rigidity, or fiber-reinforced polymer, such as aluminum alloy and low-strength steel, which produces an appropriate amount of compression deformation during the extrusion process, so that the filling block and The restraint ring fits better.
实施例三Example three
参见图6,在实施例一的基础上,本实施例中在填充台体11外表面包裹设有包裹层17。实施例在填充台体11压入约束环12之前,在其外表包裹一层较薄的金属,如涂覆熔融的铝合金或者铁合金等金属材料,或者在其表面粘贴包裹纤维增强聚合物材料,如碳纤维、玻璃纤维、凯夫拉纤维或者超高分子量聚乙烯纤维增强环氧树脂、纤维增强酚醛树脂等聚合物材料,形成填充台体11的包裹层17,然后将包裹有包裹层17的填充台体11压入约束环12的内圈。通过在填充台体11外侧包裹韧性材料形成包裹层17,可以增加填充台体11抗多次打击能力,防止填充台体11的材质受到冲击后发生飞溅而造成二次伤害。Referring to FIG. 6, on the basis of the first embodiment, in this embodiment, a wrapping layer 17 is wrapped on the outer surface of the filling platform body 11. In the embodiment, before the filling table body 11 is pressed into the confinement ring 12, a thinner layer of metal is wrapped on its outer surface, such as a metal material such as a molten aluminum alloy or iron alloy, or a fiber-reinforced polymer material is pasted and wrapped on its surface. Such as carbon fiber, glass fiber, Kevlar fiber or ultra-high molecular weight polyethylene fiber-reinforced epoxy resin, fiber-reinforced phenolic resin and other polymer materials to form the packing layer 17 that fills the table body 11, and then fill the packing layer 17 with the packing layer 17 The table body 11 is pressed into the inner ring of the confinement ring 12. By wrapping a flexible material on the outside of the filling platform 11 to form the wrapping layer 17, the ability of the filling platform 11 to resist multiple blows can be increased, and the material of the filling platform 11 can be prevented from splashing after being impacted and causing secondary damage.
实施例四Embodiment four
如图7a和图7b所示,本实施例中的填充台体11采用多层填充材料,填充台体11从上至下包括依次叠装贴合的第一填充块111、夹层113和第二填充块112,第一填充块111和第二填充块112为填充台体相同材质制成,两块填充块之间存在夹层或者空隙。As shown in Figures 7a and 7b, the filling platform 11 in this embodiment uses multiple layers of filling materials. The filling platform 11 includes a first filling block 111, an interlayer 113, and a second The filling block 112, the first filling block 111 and the second filling block 112 are made of the same material of the filling platform, and there is an interlayer or gap between the two filling blocks.
装配时,可以采用图7a中的方式,先将下方的第二填充块112压入约束环12内圈中后,再在其表面布置夹层113或者缺失,然后再压入第一填充块111,得到预应力约束块1;也可以采用图7b中的方式,先将第一填充块111、夹层113和第二填充块112按照次序依次贴装粘合成整体填充台体11,然后将填充台体11整体压入约束环12内圈中。夹层113的材质可以选用泡沫金属、金属层、石墨容留层、橡胶、聚合物多孔材料、树脂粘结剂、或者空气层等材质中的至少一种,泡沫金属优选泡沫铝。When assembling, the method shown in Fig. 7a can be used. The second filler block 112 below is pressed into the inner ring of the confinement ring 12, and then the interlayer 113 is arranged or missing on the surface, and then the first filler block 111 is pressed into it. Obtain the pre-stressed constraining block 1; it is also possible to use the method shown in Figure 7b. First, the first filling block 111, the interlayer 113, and the second filling block 112 are mounted and glued in order to form an integral filling platform body 11, and then the filling platform The body 11 is integrally pressed into the inner ring of the confinement ring 12. The material of the interlayer 113 can be at least one of foamed metal, metal layer, graphite retention layer, rubber, polymer porous material, resin binder, or air layer, and the foamed metal is preferably foamed aluminum.
采用多层填充块结构的填充台体可以减少填充块的冲击损伤范围和破坏程度,实际应用中可以根据装甲厚度采用两层及以上的多层填充块填充,填充块的材质可以选择陶瓷、混凝土、玻璃、金属材质中的至少一种,位于外侧的面层优选陶瓷材料。The filling table body with a multi-layer filling block structure can reduce the impact damage range and damage degree of the filling block. In actual applications, two or more multi-layer filling blocks can be used to fill according to the armor thickness. The material of the filling block can be ceramic or concrete. , At least one of glass and metal materials, and the surface layer on the outside is preferably a ceramic material.
本实施例中采用多层填充材料的填充台体11表面也可以按照实施例四的方式在填充台体11整体表面设置包裹层17。In this embodiment, the surface of the filling platform 11 using multiple layers of filling materials can also be provided with a wrapping layer 17 on the entire surface of the filling platform 11 in the manner of the fourth embodiment.
另外,填充台体11在采用多边形棱锥台体结构时,为了减少损伤范围,可以将棱台体由多块小棱柱体平面排列拼装组合成大棱锥填充台体,将组合后的大棱台体嵌挤入约束环12内施加预应力。填充台体11的上表面或者下表面可以是平面,也可以设置成球冠形凸起,或者棱锥凸起,或者其它堆高方式。In addition, when the filling platform body 11 adopts a polygonal pyramid structure, in order to reduce the damage range, the pyramid body can be assembled from a plurality of small prisms in a plane arrangement to form a large pyramid filling platform body, and the combined large prism body The pre-stress is applied by inserting and squeezing into the restraining ring 12. The upper surface or the lower surface of the filling table body 11 may be flat, or may be provided as spherical crown-shaped protrusions, or pyramid-shaped protrusions, or other stacking methods.
实施例五Embodiment five
约束环12设有底板结构,如图8所示,本实施例中的约束环12的高度大于填充台体11的厚度,在实施例一中的约束环12底部或实施例二中的第二变径环13的底部小端开口处设置垫层15,在填充台体11压入约束环12内圈之前,先在约束环12内圈底部填充吸能垫层15,然后再压入填充台体11施加预应力。垫层15可以采用多孔材料或者泡沫金属,如泡沫铝,或者采用橡胶等聚合物材料作为缓冲材料。The confinement ring 12 is provided with a bottom plate structure. As shown in Figure 8, the height of the confinement ring 12 in this embodiment is greater than the thickness of the filling platform 11, and the bottom of the confinement ring 12 in the first embodiment or the second A cushion layer 15 is provided at the opening at the small end of the bottom of the reducing ring 13. Before the filling table body 11 is pressed into the inner ring of the constraining ring 12, the energy-absorbing cushion layer 15 is filled at the bottom of the inner ring of the constraining ring 12, and then pressed into the filling table. The body 11 is prestressed. The cushion layer 15 can be made of porous material or foamed metal, such as foamed aluminum, or a polymer material such as rubber as a cushioning material.
实施例六Example Six
如图9所示,本实施例中的约束环12的底板结构不同于实施例五,本实施例中的约束环12为与约束环12一体结构的约束槽底板16,即约束槽底板16与约束环12的外壁为一体结构,通过约束槽底板16将约束环12的底部小端封口,形成一个槽形约束环,填充台体11压入约束环12之前,还可以先在约束槽底板16的上表面填充较薄的泡沫铝垫层,然后压入填充台体11,泡沫铝垫层使填充台体11的底面与约束槽底板16更为贴合。约束槽底板16在一定程度上增大预应力约束块的抗弯刚度,一定程度上起到装甲背板的作用。As shown in Figure 9, the bottom structure of the confinement ring 12 in this embodiment is different from that of the fifth embodiment. The confinement ring 12 in this embodiment is a confinement groove bottom plate 16 integrated with the confinement ring 12, that is, the confinement groove bottom plate 16 and The outer wall of the confinement ring 12 is an integral structure. The bottom small end of the confinement ring 12 is sealed by the confinement groove bottom plate 16 to form a groove-shaped confinement ring. Before the filling table 11 is pressed into the confinement ring 12, the confinement groove bottom plate 16 Fill the upper surface of a thinner foam aluminum cushion layer, and then press into the filling table body 11, the foam aluminum cushion layer makes the bottom surface of the filling table body 11 and the constraining groove bottom plate 16 more closely fit. The constraining groove bottom plate 16 increases the bending rigidity of the prestressed constraining block to a certain extent, and plays the role of an armor back plate to a certain extent.
实施例七Example Seven
如图10所示,本实施例中的约束环12在内圈壁的大端内侧设有一圈卡槽18,将填充台体11压入约束环12的内圈,达到预定位置后,在约束环12的卡槽18内安装卡环19对填充台体11进行轴向限位,在轴向方向上,由于填充台体11的大端尺寸远大于约束环12内圈小端开口,楔紧后的填充台体11不能够从约束环12的小端脱出,在约束环12的大端内圈壁上装配卡环19可以有效防止填充台体11在受冲击时从约束环12的大端滑出。As shown in Figure 10, the constraining ring 12 in this embodiment is provided with a ring of clamping grooves 18 inside the large end of the inner ring wall, and the filling table 11 is pressed into the inner ring of the constraining ring 12. A snap ring 19 is installed in the groove 18 of the ring 12 to axially limit the filling platform 11. In the axial direction, because the size of the large end of the filling platform 11 is much larger than the opening of the small end of the inner ring of the constraining ring 12, it is tightly wedge The rear filling platform 11 cannot escape from the small end of the confinement ring 12. Assembling a snap ring 19 on the inner wall of the large end of the confinement ring 12 can effectively prevent the filling platform 11 from moving away from the large end of the confinement ring 12 when it is impacted. Slide out.
卡环19采用便于安装的弹性开口卡环,当填充台体11受损后,通过取出卡环19,从约束环内圈的小端向大端口反向推出受损的填充台体11,更换新的填充台体11,可以快速修复受损或者破坏装甲结构。The snap ring 19 adopts an elastic opening snap ring that is easy to install. When the filling table body 11 is damaged, by taking out the snap ring 19, the damaged filling table body 11 is pushed back from the small end of the inner ring of the restraining ring to the large port, and replaced The new filling platform 11 can quickly repair damaged or destroyed armored structures.
由于约束环12大端内圈壁加工卡槽,在装配卡环19后,填充台体11表面会要低于约束环12的顶面,可以进一步采用金属板、环氧树脂或者聚脲等聚合物材料填充调平。Since the inner wall of the large end of the confinement ring 12 is processed with a groove, after the snap ring 19 is assembled, the surface of the filling table body 11 will be lower than the top surface of the confinement ring 12, and a metal plate, epoxy resin or polyurea can be further used. Material filling and leveling.
本实施例可以应用在实施例一到六中的预应力约束块中,并且可以根据填充台体和约束环的横向截面形状选用对应的圆形开口卡环或多边形卡口卡环。This embodiment can be applied to the prestressed constraining blocks in the first to sixth embodiments, and the corresponding circular split snap ring or polygonal bayonet snap ring can be selected according to the transverse cross-sectional shape of the filling platform and the constraining ring.
实施例八Example eight
本实施例公开了本发明的复合装甲结构的一种具体实施方案,如图11a中所示,该复合装甲结构包括一层由若干预应力约束块1拼接而成的装甲板,本实施例中的预应力约束块1采用横截面为正六边形的填充台体11和约束环12,沿横向延展铺装成连续的装甲板。约束环12采用高强度钢材,正六棱填充台体11采用陶瓷、混凝土或者玻璃中的任意一种或者多种材质。This example discloses a specific implementation of the composite armor structure of the present invention. As shown in FIG. 11a, the composite armor structure includes a layer of armor plate formed by splicing a plurality of prestressed restraining blocks 1. In this example The prestressed constraining block 1 adopts a filling platform 11 and a constraining ring 12 with a regular hexagon in cross section, and spreads and spreads in the transverse direction to form a continuous armor plate. The confinement ring 12 is made of high-strength steel, and the regular hexagonal filling table body 11 is made of any one or more of ceramic, concrete or glass.
图11b中公开了包括两层图11a中装甲板的复合装甲结构,装甲板之间的预应力约束块11之间错位分布,通过错位分开的预应力约束块11弥补单层复合装甲结构的预应力约束块接缝处的防护薄弱区域,增加复合装甲结构的防护效果。实际应用中可以根据防护要求和装甲整体厚度采用不同层数的装甲板叠装。Fig. 11b discloses a composite armor structure including two layers of armor plates in Fig. 11a. The prestressed restraint blocks 11 between the armor plates are misaligned. The prestressed constrained blocks 11 separated by dislocation are used to compensate for the prestress of the single-layer composite armored structure. The weakened areas of protection at the joints of the stress-constrained blocks increase the protective effect of the composite armor structure. In practical applications, different layers of armor plates can be stacked according to the protection requirements and the overall thickness of the armor.
在图11a和图11b中的装甲板中,拼接的预应力约束块1均为分体的约束环,即先将所有的约束环12和填充台体11装配成单独的预应力约束块11后,在对所有的预应力约束块11进行拼接铺装。图11c中公开了另一种装甲板的铺装方式,即所有的预应力约束块1的约束环12采用一体蜂窝结构,所有约束环12连接成一个整体的连体约束环121,可以通过焊接固定在一起或者直接在一块整体板结构上加工所有约束环12的六边形内圈壁,形成蜂窝板结构,然后将所有填充台体11一一对应装配到对应约束环的内圈中,一体结构的连体约束环121增加了装甲板的整体性。In the armor plates in Figure 11a and Figure 11b, the spliced prestressed restraint blocks 1 are all separate restraint rings, that is, all the restraint rings 12 and the filling platform 11 are assembled into a single prestressed restraint block 11. , All the prestressed restraint blocks 11 are spliced and laid. Fig. 11c discloses another way of paving the armor plate, that is, all the confinement rings 12 of the prestressed constraining block 1 adopt an integrated honeycomb structure, and all the confinement rings 12 are connected into an integral conjoined confinement ring 121, which can be welded Fix them together or directly process all the hexagonal inner walls of the confinement ring 12 on a whole plate structure to form a honeycomb plate structure, and then assemble all the filling table bodies 11 into the inner ring of the corresponding confinement ring one by one. The conjoined confinement ring 121 of the structure increases the integrity of the armor plate.
实施例九Example 9
本实施例公开了本发明的复合装甲结构的进一步具体实施方案,在实施例七的基础上,本实施例在装甲板的两侧面分别覆盖贴合盖板2和背板3。其中盖板2用于装甲外侧美观,并且一定程度上提高装甲防护效果,背板3增加装甲内侧抗冲击强度。This example discloses a further specific implementation of the composite armor structure of the present invention. On the basis of Example 7, this example covers the cover plate 2 and the back plate 3 on both sides of the armor plate, respectively. The cover plate 2 is used for the appearance of the outer side of the armor and improves the protective effect of the armor to a certain extent, and the back plate 3 increases the impact resistance of the inner side of the armor.
盖板2或者背板3的安装方式可以采用粘结剂与装甲板的预应力约束块1进行结合,或者采用螺栓将盖板2或者背板3与装甲板进行锚固,其中螺栓可以穿过盖板2或者背板3的预留孔进行锚固。The installation method of the cover plate 2 or the back plate 3 can be combined with the pre-stressed restraint block 1 of the armor plate by an adhesive, or the cover plate 2 or the back plate 3 and the armor plate can be anchored by bolts, wherein the bolts can pass through the cover plate. The plate 2 or the reserved hole of the back plate 3 is anchored.
盖板2分为单层、双层或者多层复合板。具体如图12a、12b和12c中所示,本实施例中可选择的盖板2分为单层护面层、护面层+容留层、两层护面层+容留层三种形式。The cover plate 2 is divided into a single-layer, double-layer or multi-layer composite board. Specifically, as shown in Figures 12a, 12b and 12c, the optional cover plate 2 in this embodiment is divided into three forms: a single-layer protective layer, a protective surface layer + a holding layer, and a two-layer protective layer + a holding layer.
单层护面层的盖板2如图12a中所示,第一护面层21优选采用钢板、铝合金、钛合金等金属材料,或者采用聚合物材料或者纤维增强聚合物材料,如聚脲涂层、聚碳酸酯涂层,图14a和图14c中的复合装甲结构均在装甲板的外侧表面直接贴合第一护面层21作为盖板2。The cover plate 2 of the single-layer protective surface layer is shown in FIG. 12a. The first protective surface layer 21 is preferably made of metal materials such as steel plates, aluminum alloys, titanium alloys, or polymer materials or fiber-reinforced polymer materials, such as polyurea. Coating, polycarbonate coating, and the composite armor structure in FIG. 14a and FIG. 14c are all directly attached to the first protective surface layer 21 as the cover plate 2 on the outer surface of the armor plate.
护面层+容留层的双层结构的盖板2如图12b中所示,第一护面层21优选采用钢板、铝合金、钛合金等金属材料,或者采用聚合物材料或者纤维增强聚合物材料,如聚脲涂层、聚碳酸酯涂层,容留层22采用石墨材料,与预应力约束块贴合,图14b、图14d和图14e中的复合装甲结构均在装甲板的外侧表面贴合图12b中的盖板2,从预应力约束块的远端到近端的顺序,盖板2按照钢板的第一护面层+石墨容留层的顺序贴合在装甲板外侧。The cover 2 of the double-layer structure of the protective surface layer + the containment layer is shown in FIG. Materials, such as polyurea coating and polycarbonate coating, the retaining layer 22 is made of graphite material, which is attached to the prestressed constraining block. The composite armor structures in Figure 14b, Figure 14d and Figure 14e are all pasted on the outer surface of the armor plate. Combining the cover plate 2 in Fig. 12b, from the distal end to the proximal end of the prestressed restraint block, the cover plate 2 is attached to the outer side of the armor plate in the order of the first protective surface layer of the steel plate + the graphite holding layer.
两层护面层+容留层三种形式的三层结构的盖板2如图12c中所示,第一护面层21优选采用钢板、铝合金、钛合金等金属材料,或者采用聚合物材料或者纤维增强聚合物材料,如聚脲涂层、聚碳酸酯涂层,容留层22采用石墨材料,与预应力约束块贴合,第二护面层23采用铜合金材料,从预应力约束块的远端到近端的顺序,三层结构的盖板2采用一层钢板第一护面层+一层铜板第二护面层+石墨容留层的顺序贴合在装甲板外侧。The three-layer structure cover plate 2 of three forms of two-layer protective layer + storage layer is shown in Figure 12c. The first protective layer 21 is preferably made of metal materials such as steel plate, aluminum alloy, titanium alloy, or polymer material. Or fiber-reinforced polymer materials, such as polyurea coating or polycarbonate coating, the retaining layer 22 is made of graphite material, which is attached to the prestressed constraining block, and the second protective surface layer 23 is made of copper alloy material from the prestressed constraining block. From the distal end to the proximal end, the cover plate 2 of the three-layer structure is attached to the outer side of the armor plate in the order of a steel plate first protective surface layer + a copper plate second protective surface layer + a graphite holding layer.
背板3分为单层、双层或者多层复合板,包括碰撞层31、吸能层32、抵抗层33至少一层,具体如图13a、13b和13c中所示。图13a中的背板3为单层抵抗层33结构,抵抗层33采用钢板、铝合金、钛合金等金属材料中的一种或者多种,或者采用聚合物材料或者纤维增强聚合物材料,图14a和图14b中的复合装甲结构在装甲板的内侧表面直接贴合抵抗层33作为背板3。The backplane 3 is divided into a single-layer, double-layer or multi-layer composite board, including at least one layer of a collision layer 31, an energy absorption layer 32, and a resistance layer 33, as shown in FIGS. 13a, 13b, and 13c. The backplane 3 in Figure 13a has a single-layer resistance layer 33 structure. The resistance layer 33 uses one or more of metal materials such as steel plates, aluminum alloys, and titanium alloys, or uses polymer materials or fiber-reinforced polymer materials. The composite armor structure in 14a and 14b is directly attached to the resistance layer 33 as the back plate 3 on the inner surface of the armor plate.
图13b中的背板3为吸能层32+抵抗层33的双层结构,抵抗层33采用钢板、铝合金、钛合金等金属材料中的一种或者多种,或者采用聚合物材料或者纤维增强聚合物材料,吸能层32采用泡沫金属、橡胶中的一种或者多种材料,图14c和图14d中的复合装甲结构在装甲板的内侧表面贴合图13b中的双层背板3,吸能层32紧贴装甲板设置。The backplane 3 in Figure 13b has a double-layer structure of an energy absorbing layer 32 + a resistance layer 33. The resistance layer 33 is made of one or more of metal materials such as steel plates, aluminum alloys, titanium alloys, or polymer materials or fibers. Reinforced polymer material, the energy-absorbing layer 32 is made of one or more of foamed metal and rubber. The composite armor structure in Figure 14c and Figure 14d is attached to the double-layer backplane 3 in Figure 13b on the inner surface of the armor plate. , The energy-absorbing layer 32 is arranged close to the armor plate.
图13c中的背板3为碰撞层31+吸能层32+抵抗层33的三层结构,抵抗层33采用钢板、铝合金、钛合金等金属材料中的一种或者多种,或者采用聚合物材料或者纤维增强聚合物材料,吸能层32采用泡沫金属、橡胶中的一种或者多种材料,碰撞层31采用钢板、铝合金、钛合金等金属材料中的一种或者多种,或者采用聚合物材料或者纤维增强聚合物材料,图14e中的复合装甲结构在装甲板的内侧表面贴合图13c中的三层背板3,碰撞层31紧贴装甲板设置。The back plate 3 in Figure 13c is a three-layer structure of collision layer 31 + energy absorption layer 32 + resistance layer 33. The resistance layer 33 is made of one or more of metal materials such as steel plate, aluminum alloy, titanium alloy, or polymer. Material or fiber-reinforced polymer material, the energy absorbing layer 32 is made of one or more of foamed metal and rubber, and the collision layer 31 is made of one or more of metal materials such as steel plate, aluminum alloy, titanium alloy, or Using polymer materials or fiber-reinforced polymer materials, the composite armor structure in FIG. 14e is attached to the three-layer backplane 3 in FIG. 13c on the inner surface of the armor plate, and the collision layer 31 is arranged close to the armor plate.
预应力约束块1拼接的装甲板可以作为护甲单独使用,但为了取得更好的防护效果,在其表面安装盖板2和背板3,盖板2贴合在预应力约束块两个表面的任何的一面,优选靠近填充台体的大端一面安装,背板3则安装另外一面。盖板2和背板3与预应力约束块可以采用树脂类粘结剂粘合,或者采用螺栓锚固。The armor plate spliced by the prestressed restraint block 1 can be used alone as armor, but in order to obtain a better protective effect, the cover plate 2 and the back plate 3 are installed on its surface, and the cover plate 2 is attached to the two surfaces of the prestressed restraint block It is preferable to install one side close to the large end of the filling platform, and install the back plate 3 on the other side. The cover plate 2 and the back plate 3 and the pre-stressed restraint block can be bonded by a resin adhesive, or anchored by bolts.
上述仅为本发明的若干具体实施方式,但本发明的设计构思并不局限于此,凡利用此构思对本发明进行非实质性的改动,均应属于侵犯本发明保护的范围的行为。但凡是未脱离本发明技术方案的内容,依据本发明的技术实质对以上实施例所作的任何形式的简单修改、等同变化与改型,仍属于本发明技术方案的保护范围。The above are only a few specific embodiments of the present invention, but the design concept of the present invention is not limited to this. Any insubstantial modification of the present invention using this concept should be an act that violates the protection scope of the present invention. However, any simple modifications, equivalent changes and modifications made to the above embodiments according to the technical essence of the present invention without departing from the content of the technical solution of the present invention still belong to the protection scope of the technical solution of the present invention.
以下对实施例一中的预应力约束块的预应力施加和抗侵彻效果模拟进行实验验证:The following is an experimental verification of the pre-stress application and anti-penetration effect simulation of the pre-stress restraint block in the first embodiment:
(1)有限元模型(1) Finite element model
将实施例一中的填充台体和约束环拟定一种具体尺寸参见图15所示,填充台体为圆台体,约束环的内圈壁为圆台空腔。填充台体的台体高度h1为40mm,约束环12的高度h2为50mm;填充台体11的母线和约束环12内圈壁的母线均为直线,填充台体11的母线与高的夹角α =3°,约束环12内圈壁的母线与高的夹角β=3°。填充台体11顶面大端直径d 1为100mm,底面小端直径d 2为95.8mm;约束环12内圈壁的顶面大端内径R 1为100mm,底面小端内径R 2为94.8mm;填充台体11底面小端外径与约束环12底面小端内径的盈差为1mm,由于约束环的高度大于填充台体的高度,并且约束环的内圈壁倾角和填充台体的外侧壁倾角相同,随着填充台体向下压入约束环后至两者小端平齐,填充台体11顶面大端外径与约束环12的内圈壁之间会产生与小端相同的盈差;约束环12的外径为110mm,约束环12的顶面壁厚为5mm,底面壁厚为7.6mm。填充台体11的材质为陶瓷、混凝土或者玻璃中的一种,约束环12中的材质为钢材、铝合金、钛合金或者纤维增强聚合物材料。 A specific size of the filling table body and the confinement ring in the first embodiment is drawn as shown in FIG. The height h1 of the filling platform is 40mm, and the height h2 of the confinement ring 12 is 50mm; the generatrix of the filling platform 11 and the generatrix of the inner wall of the confinement ring 12 are both straight lines, and the angle between the generatrix of the filling platform 11 and the height α=3°, the angle β=3° between the generatrix of the inner wall of the confinement ring 12 and the height. The diameter d 1 of the large end of the top surface of the filling platform 11 is 100mm, and the diameter d 2 of the small end of the bottom surface is 95.8mm; the inner diameter R 1 of the large end of the inner ring wall of the confinement ring 12 is 100mm, and the inner diameter R 2 of the small end of the bottom surface is 94.8mm ; The difference between the outer diameter of the small end of the bottom surface of the filling platform 11 and the inner diameter of the small end of the bottom surface of the confinement ring 12 is 1mm, because the height of the confinement ring is greater than the height of the filling platform, and the inclination of the inner wall of the confinement ring and the outer side of the filling platform The wall inclination is the same. As the filling platform is pressed down into the confinement ring until the small ends of the two are flush, the outer diameter of the large end of the top surface of the filling platform 11 and the inner wall of the confinement ring 12 will be the same as the small end. The surplus difference; the outer diameter of the confinement ring 12 is 110mm, the top wall thickness of the confinement ring 12 is 5mm, and the bottom wall thickness is 7.6mm. The material of the filling table body 11 is one of ceramics, concrete or glass, and the material of the confinement ring 12 is steel, aluminum alloy, titanium alloy or fiber reinforced polymer material.
预应力约束块采用显式有限元程序LS-DYNA建立混凝土圆台压入钢约束环施加预应力和子弹侵彻的三维数值模型。根据填充台体和约束环的几何尺寸建立预应力约束块的有限元模型和网格划分如图16所示,模型由圆形约束环、圆台、子弹、垫板和推力块组成,以8结点实体六面体单元(*SECTION_SOLID)进行建模,根据对称条件,仅建立了沿zy平面和zx平面对称的1/4模型。圆台单元和约束环单元的平均尺寸约为1.25mm,混凝土圆台的单元总数为49152个,约束环单元总数为10240个。子弹的平均网格尺寸为1.25mm,共划分300个单元。垫板的边界条件为固定,约束环、圆台、垫板、推力块之间采用面面接触(关键字*CONTACT_AUTOMATIC_SURFACE_TO_SURFACE),两者之间的静摩擦系数为0.08,动摩擦系数为0.06。子弹与混凝土的接触采用关键字*CONTACT_ERODING_SURFACE_TO_SURFACE实现。The explicit finite element program LS-DYNA is used for the prestressed restraint block to establish a three-dimensional numerical model of the concrete circular table pressing into the steel restraining ring to impose prestress and bullet penetration. The finite element model and mesh division of the prestressed constraining block are established according to the geometric dimensions of the filling platform and the confinement ring. As shown in Figure 16, the model is composed of a circular constraining ring, a round table, a bullet, a backing plate and a thrust block, with 8 knots The point solid hexahedral element (*SECTION_SOLID) is modeled. According to the symmetry condition, only a 1/4 model that is symmetrical along the zy plane and the zx plane is established. The average size of the truncated cone unit and the confinement ring unit is about 1.25mm, the total number of concrete truncated cone units is 49152, and the total number of confinement ring units is 10240. The average grid size of the bullet is 1.25mm and it is divided into 300 units. The boundary condition of the backing plate is fixed, and surface contact (keyword *CONTACT_AUTOMATIC_SURFACE_TO_SURFACE) is adopted between the confinement ring, round table, backing plate, and thrust block. The static friction coefficient between the two is 0.08, and the dynamic friction coefficient is 0.06. The contact between the bullet and the concrete is realized with the keyword *CONTACT_ERODING_SURFACE_TO_SURFACE.
(2)混凝土材料模型(2) Concrete material model
混凝土材料采用HJC模型,混凝土密度为2400kg/m 3,强度为170MPa,具体参数如表1所示。为避免单元产生畸变,引起沙漏效应,影响计算的稳定性,引入*MAT_ADD_EROSION侵蚀失效准则,以最大主应变来控制单元的失效。当模拟过程中靶体某一单元最大主应变超过该应变值时,认为该单元失效,将其删除,失效应变设为0.1。 The concrete material adopts the HJC model, the concrete density is 2400kg/m 3 , the strength is 170MPa, and the specific parameters are shown in Table 1. In order to avoid element distortion, cause hourglass effect, and affect the stability of calculation, the *MAT_ADD_EROSION erosion failure criterion is introduced, and the maximum principal strain is used to control the failure of the element. When the maximum principal strain of an element of the target body exceeds the strain value during the simulation process, the element is considered to be invalid and deleted, and the failure strain is set to 0.1.
 To
 To
表1混凝土HJC本构模型参数Table 1 Concrete HJC constitutive model parameters
Figure 770727dest_path_image001
Figure 770727dest_path_image001
(3)钢材料模型(3) Steel material model
约束环与平头弹的材料采用*MAT_PLASTIC_KINEMATIC材料模型,材料模型主要参数如表2所示。The material of the confinement ring and the flat-headed bullet adopts the *MAT_PLASTIC_KINEMATIC material model. The main parameters of the material model are shown in Table 2.
表2 钢材材料参数Table 2 Steel material parameters
Figure 165936dest_path_image002
Figure 165936dest_path_image002
(4)加载制度(4) Loading system
加载制度和试验流程分为两个阶段,第一阶段下推圆台施加预应力模拟试验,然后第二阶段再进行抗侵彻模拟试验。第一阶段采用关键字*BOUNDARY_PRESCRIBED_MOTION_SET赋予推力块位移推动混凝土圆台到达钢环的指定深度,加载速率为200mm/s,稳定10ms,生成相应的重启文件。子弹在第一阶段不动,第一个阶段结束后,使用LS-DYNA中的全重启动功能进行第二阶段模拟,通过关键字*CHANGE_VELOCITY_GENERATION赋予子弹速度,同时通过关键字*STRESS_ INITIALIZATION将上一过程中各个部件的应力状态传递到重启动过程中相应部件上。子弹为平头弹,其直径为7.62mm,长度为20mm,初速度为600m/s。The loading system and test process are divided into two stages. The first stage pushes down the round table to apply pre-stress simulation test, and then the second stage conducts anti-penetration simulation test. In the first stage, the keyword *BOUNDARY_PRESCRIBED_MOTION_SET is used to give the thrust block displacement to push the concrete circular platform to the specified depth of the steel ring, the loading rate is 200mm/s, the stability is 10ms, and the corresponding restart file is generated. The bullet does not move in the first phase. After the first phase is over, use the full restart function in LS-DYNA to perform the second phase simulation. Use the keyword *CHANGE_VELOCITY_GENERATION to assign the bullet speed, and use the keyword *STRESS_ INITIALIZATION to move the previous The stress state of each component in the process is transferred to the corresponding component in the restart process. The bullet is a flat-headed bullet with a diameter of 7.62mm, a length of 20mm, and an initial velocity of 600m/s.
(4)预应力模拟结果与分析(4) Prestress simulation results and analysis
混凝土材质的填充台体下推10mm后,填充台体的圆心单元预应力-下压深度关系曲线如图17所示,随着下压深度的增大,圆台的内部应力逐步增大,下压深度为10mm时,圆台轴线单元的平均径向应力达到169MPa,因此可以证明本发明可以通过下压深度或者位移调整预应力大小,而且能够施加足够大的预应力。After the filled platform of concrete material is pushed down by 10mm, the prestress-depression depth relationship curve of the center element of the filled platform is shown in Figure 17. With the increase of the depression depth, the internal stress of the truncated cone gradually increases, and the downward pressure When the depth is 10 mm, the average radial stress of the truncated cone axis unit reaches 169 MPa. Therefore, it can be proved that the present invention can adjust the prestress by pressing down depth or displacement, and can apply sufficient prestress.
(5)侵彻模拟结果分析(5) Analysis of penetration simulation results
填充台体在约束环内圈下推深度从0~10mm,下推位移总共分为10级,随着下压深度的增加圆台的径向预应力逐渐增大,在600m/s的平头弹的正冲击下,各级下压深度的填充台体混凝土圆台其损伤云图如图18所示,结合图19所示的混凝土圆台的侵彻深度与预应力的关系曲线,可以看出,随着预应力的增加,侵彻深度逐渐减少,当下压深度为7mm,即施加在填充台体中心预应力为119MPa时,填充台体的侵彻深度下降了37.5%,抗侵彻性能达到最佳。而随着预应力的进一步增大,其抗侵彻性能则发生下降。因此采用本发明的预应力约束块施加合理的预应力值可以很大程度上提高复合装甲构件的抗侵彻性能。The pushing depth of the filling table body in the inner ring of the confinement ring is from 0 to 10mm, and the pushing down displacement is divided into 10 levels. With the increase of the depression depth, the radial prestress of the round table gradually increases. Under a positive impact, the damage cloud diagram of the filled platform concrete cylindrome at various levels of depression depth is shown in Figure 18. Combining the relationship curve between the penetration depth of the concrete cylindrome and the prestress shown in Figure 19, it can be seen that with the prestress As the stress increases, the penetration depth gradually decreases. When the depression depth is 7mm, that is, when the prestress applied to the center of the filling platform is 119MPa, the penetration depth of the filling platform decreases by 37.5%, and the anti-penetration performance reaches the best. With the further increase of the prestress, its anti-penetration performance will decrease. Therefore, the use of the prestressed restraint block of the present invention to apply a reasonable prestress value can greatly improve the anti-penetration performance of the composite armor component.

Claims (13)

  1. 一种预应力约束块,其特征在于:包括填充台体(11)和约束环(12),所述填充台体(11)具有和约束环(12)内圈相同形状的横截面,并固定嵌装于约束环(12)的内圈,所述填充台体(11)的外侧壁和约束环(12)的内圈壁之间通过锥面配合而楔紧;A prestressed constraining block, characterized in that it comprises a filling platform (11) and a confinement ring (12). The filling platform (11) has the same cross-section as the inner ring of the confinement ring (12) and is fixed Embedded in the inner ring of the constraining ring (12), the outer side wall of the filling platform (11) and the inner ring wall of the constraining ring (12) are wedged tightly through taper fit;
    所述填充台体(11)的外侧壁和约束环(12)的内圈壁分别为相匹配的圆锥面,或相匹配的多边形棱锥面。The outer side wall of the filling platform (11) and the inner ring wall of the confinement ring (12) are respectively matched conical surfaces or matched polygonal pyramid surfaces.
  2. 根据权利要求1所述的预应力约束块,所述填充台体(11)外侧壁的大端和小端直径分别为d 1和d 2,所述约束环(12)内圈壁的大端和小端直径分别为R 1和R 2,满足R 2<d 2<R 1≤d 1,所述填充台体(11)和约束环(12)的高分别为h1和h2,其中h1≤h2。 The prestressed restraint block according to claim 1, wherein the diameters of the large end and the small end of the outer side wall of the filling platform (11) are d 1 and d 2 respectively, and the large end of the inner wall of the restraining ring (12) The diameters of and the small end are R 1 and R 2 respectively , satisfying R 2 <d 2 <R 1 ≤d 1 , the heights of the filling platform (11) and the confinement ring (12) are h1 and h2, respectively, where h1≤ h2.
  3. 根据权利要求1所述的预应力约束块,所述填充台体(11)外侧壁的锥面倾角α范围为1°~10°,优选3°~6°,所述约束环(12)内圈壁的锥面倾角β范围为1°~10°,优选3°~6°,所述填充台体(11)的外侧壁和约束环(12)的内圈壁之间存在角度差Δα,Δα=α-β,Δα的取值范围为0°~0.5°,优选0°~0.2°。The prestressed restraint block according to claim 1, wherein the inclination angle α of the cone surface of the outer side wall of the filling platform (11) ranges from 1° to 10°, preferably 3° to 6°, and the confinement ring (12) The tapered surface inclination angle β of the ring wall ranges from 1° to 10°, preferably 3° to 6°. There is an angle difference Δα between the outer side wall of the filling platform (11) and the inner ring wall of the confinement ring (12), Δα=α-β, and the value range of Δα is 0°~0.5°, preferably 0°~0.2°.
  4. 根据权利要求2所述的预应力约束块,所述填充台体(11)的径厚比d 1/h 1为0.5~40,优选3~12。 The prestressed restraint block according to claim 2, wherein the diameter-to-thickness ratio d 1 /h 1 of the filling table body (11) is 0.5-40, preferably 3-12.
  5. 根据权利要求1所述的预应力约束块,所述填充台体(11)为具有圆锥面或多边形棱锥面外侧壁的锥台体,The prestressed constraining block according to claim 1, wherein the filling platform (11) is a frustum with a conical surface or an outer side wall of a polygonal pyramid surface,
    或外部固定套装第一变径环(14)的圆柱体或棱柱体,所述第一变径环(14)的外侧壁为圆锥面或多边形棱锥面。Or, the cylinder or prism of the first reducing ring (14) is externally fixed, and the outer side wall of the first reducing ring (14) is a conical surface or a polygonal pyramid surface.
  6. 根据权利要求5所述的预应力约束块,所述约束环(12)为具有圆锥面或多边形棱锥面内圈壁的变径环体,The prestressed restraint block according to claim 5, wherein the restraint ring (12) is a reduced-diameter ring body with an inner ring wall of a conical surface or a polygonal pyramid surface,
    或内部固定嵌装第二变径环(13)的圆柱环或棱柱环,所述第二变径环(13)的内圈壁为圆锥面或多边形棱锥面。Or a cylindrical ring or a prismatic ring in which the second reducing ring (13) is fixed and embedded inside, and the inner wall of the second reducing ring (13) is a conical surface or a polygonal pyramid surface.
  7. 根据权利要求5所述的预应力约束块,所述填充台体(11)为分层结构,包括至少两层固定叠装的填充块。The prestressed restraint block according to claim 5, wherein the filling platform body (11) is a layered structure and includes at least two fixed and stacked filling blocks.
  8. 根据权利要求5或7所述的预应力约束块,所述填充台体(11)外表面包裹设有包裹层(17)。The prestressed restraint block according to claim 5 or 7, wherein the outer surface of the filling platform (11) is wrapped with a wrapping layer (17).
  9. 根据权利要求6所述的预应力约束块,所述约束环(12)或第二变径环(13)内圈壁的小端设有底板结构,所述底板结构为与约束环(12)一体结构的约束槽底板(16),或垫装在填充台体(11)小端的垫层(15)。The prestressed restraint block according to claim 6, wherein the small end of the inner ring wall of the restraining ring (12) or the second reducing ring (13) is provided with a bottom plate structure, and the bottom plate structure is connected with the restraining ring (12) The constraining groove bottom plate (16) of an integral structure, or the cushion layer (15) installed on the small end of the filling platform body (11).
  10. 根据权利要求5-9中任一项所述的预应力约束块,所述约束环(12)的内壁开设有卡槽(18),所述卡槽(18)内装配用于楔紧后的填充台体(11)在约束环(12)内轴向限位的卡环(19)。The pre-stressed restraint block according to any one of claims 5-9, the inner wall of the restraint ring (12) is provided with a clamping groove (18), and the clamping groove (18) is assembled for tightening The filling platform (11) is axially limited by a snap ring (19) in the confinement ring (12).
  11. 根据权利要求1所述的预应力约束块,所述填充台体(11)为陶瓷、混凝土或者玻璃材料,所述约束环(12)为金属或者纤维增强复合材料。The prestressed restraint block according to claim 1, wherein the filling platform (11) is made of ceramic, concrete or glass material, and the restraining ring (12) is made of metal or fiber-reinforced composite material.
  12. 复合装甲结构,其特征在于:包括至少一层装甲板,所述装甲板包括若干权利要求1-11中的预应力约束块,所述预应力约束块采用若干分体的约束环(12)拼接,或采用一体蜂窝结构的约束环(12)。The composite armor structure is characterized in that it includes at least one layer of armor plate, the armor plate includes a plurality of prestressed restraint blocks in claims 1-11, and the prestressed restraint blocks are spliced by a plurality of separate restraining rings (12). , Or use a confinement ring (12) with an integrated honeycomb structure.
  13. 根据权利要求12所述的复合装甲结构,还包括分别贴合覆盖复合装甲两侧表面的盖板(2)和背板(3)。The composite armor structure according to claim 12, further comprising a cover plate (2) and a back plate (3) which are respectively attached to cover both sides of the composite armor.
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