WO2020062691A1 - 蜂窝结构贴版套筒及其加工方法 - Google Patents

蜂窝结构贴版套筒及其加工方法 Download PDF

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Publication number
WO2020062691A1
WO2020062691A1 PCT/CN2018/125300 CN2018125300W WO2020062691A1 WO 2020062691 A1 WO2020062691 A1 WO 2020062691A1 CN 2018125300 W CN2018125300 W CN 2018125300W WO 2020062691 A1 WO2020062691 A1 WO 2020062691A1
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layer
glass fiber
reinforced plastic
fiber reinforced
mounting sleeve
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PCT/CN2018/125300
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English (en)
French (fr)
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归霆
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澳科利高新技术（无锡）有限公司
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    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B32—LAYERED PRODUCTS
    • B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B27/00—Layered products comprising a layer of synthetic resin
    • B32B27/18—Layered products comprising a layer of synthetic resin characterised by the use of special additives
    • B32B27/20—Layered products comprising a layer of synthetic resin characterised by the use of special additives using fillers, pigments, thixotroping agents
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B32—LAYERED PRODUCTS
    • B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B1/00—Layered products having a non-planar shape
    • B32B1/08—Tubular products
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B32—LAYERED PRODUCTS
    • B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B27/00—Layered products comprising a layer of synthetic resin
    • B32B27/06—Layered products comprising a layer of synthetic resin as the main or only constituent of a layer, which is next to another layer of the same or of a different material
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B32—LAYERED PRODUCTS
    • B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B27/00—Layered products comprising a layer of synthetic resin
    • B32B27/12—Layered products comprising a layer of synthetic resin next to a fibrous or filamentary layer
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B32—LAYERED PRODUCTS
    • B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B27/00—Layered products comprising a layer of synthetic resin
    • B32B27/34—Layered products comprising a layer of synthetic resin comprising polyamides
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B32—LAYERED PRODUCTS
    • B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B3/00—Layered products comprising a layer with external or internal discontinuities or unevennesses, or a layer of non-planar shape; Layered products comprising a layer having particular features of form
    • B32B3/02—Layered products comprising a layer with external or internal discontinuities or unevennesses, or a layer of non-planar shape; Layered products comprising a layer having particular features of form characterised by features of form at particular places, e.g. in edge regions
    • B32B3/08—Layered products comprising a layer with external or internal discontinuities or unevennesses, or a layer of non-planar shape; Layered products comprising a layer having particular features of form characterised by features of form at particular places, e.g. in edge regions characterised by added members at particular parts
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B32—LAYERED PRODUCTS
    • B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B3/00—Layered products comprising a layer with external or internal discontinuities or unevennesses, or a layer of non-planar shape; Layered products comprising a layer having particular features of form
    • B32B3/10—Layered products comprising a layer with external or internal discontinuities or unevennesses, or a layer of non-planar shape; Layered products comprising a layer having particular features of form characterised by a discontinuous layer, i.e. formed of separate pieces of material
    • B32B3/12—Layered products comprising a layer with external or internal discontinuities or unevennesses, or a layer of non-planar shape; Layered products comprising a layer having particular features of form characterised by a discontinuous layer, i.e. formed of separate pieces of material characterised by a layer of regularly- arranged cells, e.g. a honeycomb structure
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B32—LAYERED PRODUCTS
    • B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B33/00—Layered products characterised by particular properties or particular surface features, e.g. particular surface coatings; Layered products designed for particular purposes not covered by another single class
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B32—LAYERED PRODUCTS
    • B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B37/00—Methods or apparatus for laminating, e.g. by curing or by ultrasonic bonding
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B32—LAYERED PRODUCTS
    • B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B5/00—Layered products characterised by the non- homogeneity or physical structure, i.e. comprising a fibrous, filamentary, particulate or foam layer; Layered products characterised by having a layer differing constitutionally or physically in different parts
    • B32B5/02—Layered products characterised by the non- homogeneity or physical structure, i.e. comprising a fibrous, filamentary, particulate or foam layer; Layered products characterised by having a layer differing constitutionally or physically in different parts characterised by structural features of a fibrous or filamentary layer
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B32—LAYERED PRODUCTS
    • B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B2255/00—Coating on the layer surface
    • B32B2255/10—Coating on the layer surface on synthetic resin layer or on natural or synthetic rubber layer
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B32—LAYERED PRODUCTS
    • B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B2255/00—Coating on the layer surface
    • B32B2255/20—Inorganic coating
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B32—LAYERED PRODUCTS
    • B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B2255/00—Coating on the layer surface
    • B32B2255/20—Inorganic coating
    • B32B2255/205—Metallic coating
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B32—LAYERED PRODUCTS
    • B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B2262/00—Composition or structural features of fibres which form a fibrous or filamentary layer or are present as additives
    • B32B2262/02—Synthetic macromolecular fibres
    • B32B2262/0261—Polyamide fibres
    • B32B2262/0269—Aromatic polyamide fibres
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B32—LAYERED PRODUCTS
    • B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B2262/00—Composition or structural features of fibres which form a fibrous or filamentary layer or are present as additives
    • B32B2262/10—Inorganic fibres
    • B32B2262/101—Glass fibres
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B32—LAYERED PRODUCTS
    • B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B2307/00—Properties of the layers or laminate
    • B32B2307/50—Properties of the layers or laminate having particular mechanical properties
    • B32B2307/558—Impact strength, toughness
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B32—LAYERED PRODUCTS
    • B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B2307/00—Properties of the layers or laminate
    • B32B2307/70—Other properties
    • B32B2307/718—Weight, e.g. weight per square meter
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B32—LAYERED PRODUCTS
    • B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B2307/00—Properties of the layers or laminate
    • B32B2307/70—Other properties
    • B32B2307/732—Dimensional properties
    • B32B2307/734—Dimensional stability
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B32—LAYERED PRODUCTS
    • B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B2597/00—Tubular articles, e.g. hoses, pipes

Definitions

  • the invention belongs to the technical field of a plate mounting sleeve, and particularly relates to a plate mounting sleeve for a flexible printing honeycomb structure and a processing method thereof.
  • the technical problem to be solved by the present invention is to provide a honeycomb structure mounting sleeve and a processing method thereof, which reduce the quality, improve the structural strength and stability, facilitate loading and unloading, and prolong the service life.
  • the technical solution adopted by the present invention to solve its technical problem is to provide a honeycomb structured mounting sleeve, which has a hollow cylindrical shape, and the mounting sleeve is a glass fiber reinforced plastic inner sleeve in order from the inside to the outside.
  • the FRP inner jacket layer may also be a plastic inner jacket layer.
  • the technical solution adopted by the present invention to solve its technical problem is to provide a method for processing the above-mentioned honeycomb structure mounting sleeve, which includes the following steps:
  • a fiberglass tape containing resin is wound on a core rod mold, and the FRP inner jacket layer is obtained by curing and demoulding, and the thickness of the single side of the FRP inner jacket layer is 0.7mm-1.7mm. ;
  • honeycomb panel filling structure layer The thickness of the honeycomb panel filling structure layer is determined according to the outer diameter of the mounting sleeve, and the cut honeycomb panel is wrapped around the outer surface of the FRP bonding and fixing layer to obtain a honeycomb. Plate filling structure layer;
  • Wrapped FRP bonding and strengthening layer Wrap a glass fiber ribbon or glass fiber containing resin on the outer surface of the honeycomb panel filling structure layer to obtain a FRP bonding and strengthening layer;
  • Composite outer cover layer Select the sleeve surface material, and compound the outer cover layer on the outer surface of the glass fiber reinforced plastic bonding and reinforcement layer;
  • the honeycomb panel is an aramid honeycomb panel.
  • the surface material of the plate roller in the step (6) is a metal alloy, and a metal transition coating is sprayed on the outer surface of the FRP bonding and reinforcing layer by a thermal spraying method.
  • the surface material of the plate roller in the step (6) is polyurethane or synthetic resin, and a polyurethane or synthetic resin layer is poured on the outer surface of the glass fiber reinforced plastic bonding and reinforcing layer by a spin casting method and cured.
  • the surface material of the plate roller in step (6) is ceramic.
  • a thermal spraying method is used to spray a metal transition coating on the outer surface of the FRP bonding and reinforcing layer, and then a thermal spraying method is used to spray a ceramic coating on the outer surface of the metal transition coating.
  • Floor is used to spray a ceramic coating on the outer surface of the metal transition coating.
  • the surface material of the plate roller is synthetic rubber. After the outer surface of the glass fiber reinforced plastic bonding and reinforcing layer is textured, the rubber is coated, and then the wrapped synthetic rubber is vulcanized.
  • the inner layer of the mounting sleeve of the present invention uses a glass fiber reinforced plastic inner covering layer or a plastic inner covering layer with a certain elastic tension, which can force the mounting sleeve to expand outward to achieve a certain diameter expansion effect when the mounting sleeve is loaded and unloaded. , So as to facilitate the mounting and dismounting between the plate mounting sleeve and the sleeve mandrel.
  • the elastomer layer has compressible resilience, and is arranged on the outer surface of the glass fiber reinforced plastic inner cover layer, which can absorb the expansion and contraction of the glass fiber reinforced plastic inner cover layer (or plastic inner cover layer), which is beneficial to maintaining the stability of the size sleeve Sex.
  • the honeycomb panel filling structure layer serves as the main structure layer of the mounting sleeve, and supports the strength, rigidity and toughness of the mounting sleeve.
  • the outer diameter of the sleeve can be controlled, and the radial size of the sleeve core rod can be reduced.
  • the honeycomb hollow structure of the honeycomb panel filling structure layer can greatly reduce the mounting sleeve. The quality is conducive to reducing the energy consumption of the plate roll.
  • the honeycomb structure of the honeycomb plate filling structure layer has strong stability, which can improve the structural strength and toughness of the mounting sleeve, which is conducive to extending the service life of the sleeve.
  • the honeycomb body structure also helps to realize the ultra-thick patch sleeve, which can get rid of the thickness limitation of the existing sleeve.
  • the honeycomb panel filling structure layer has a very small thermal expansion performance as the main structure layer, which can keep the structure stable when heated. At the same time, it can strengthen the inner glass fiber reinforced plastic structural layer, so that its expansion deformation is absorbed by the elastomer layer, thereby maintaining the overall dimensional stability of the mounting sleeve when heated.
  • FIG. 1 is a schematic structural diagram of a mounting sleeve according to the present invention.
  • FIG. 2 is a schematic structural diagram of a sleeve mandrel of the present invention.
  • FIG. 3 is a schematic structural diagram of a plate-making plate roller according to the present invention.
  • FIG. 4 is a schematic axial sectional view of a printing plate of a mounting sleeve according to the present invention.
  • FIG. 5 is a schematic side structural view of a printing plate of a mounting sleeve according to the present invention.
  • the following provides a method for processing the honeycomb structure mounting sleeve, which includes the following steps:
  • Wrapped FRP inner jacket layer 1 Wrapped fiberglass yarn ribbon containing resin on the core rod mold, solidified and demoulded to obtain FRP inner jacket layer 1, FRP inner jacket layer 1 thickness 0.7mm ⁇ 1.7 mm;
  • make a plastic inner cover layer make a plastic inner cover layer on a core rod mold, and the thickness of the plastic inner cover layer is 0.7 to 1.7 mm;
  • Wrapped FRP bonding and reinforcing layer 5 Wrap fiberglass tape or fiberglass on the outer surface of the honeycomb panel filling structure layer 4 to obtain the FRP bonding and reinforcing layer 5;
  • Composite outer plate surface layer 6 Select the surface material of the plate roller, and compound the outer plate surface layer 6 on the outer surface of the FRP bonding and reinforcing layer 5;
  • a plate mounting roller includes the above-mentioned honeycomb structure plate mounting sleeve and a sleeve mandrel 7.
  • the structure of the sleeve mandrel 7 is shown in FIG. 2 and includes a hollow roller 701 and roller supports 702 on the left and right sides.
  • An air inlet hole 703 communicating with the hollow cavity of the roller 701 is opened in the roller support 702 on the side of the sleeve core rod 7, and the position of the opposite end of the roller 701 and the air inlet hole 703 near the end edge is along the roller 701.
  • a plurality of air outlet holes 704 are formed in the circumferential direction through the inside and outside of the roller 701, and the inner end of the air outlet holes 704 communicates with the hollow cavity of the roller 701.
  • the mounting sleeve is closely attached to the outer surface of the roller 701 of the sleeve core rod 7 without a gap.
  • a photosensitive plate 9 is bonded to the outer surface of the mounting sleeve through a double-sided tape 8.
  • the photosensitive plate 9 may be a photosensitive resin plate, a photosensitive rubber plate, or other flexible thin photosensitive plate.
  • the following provides a method for loading and unloading the above-mentioned mounting sleeve, which includes the following steps:
  • Wrapped FRP inner sheath layer 1 Wrapped fiberglass yarn containing resin on a core rod mold, cured and demoulded to obtain FRP inner sheath layer 1, and the single-sided thickness of FRP inner sheath layer 0.7 is 0.7mm;
  • the thickness of the honeycomb panel filling structure layer 4 is determined to be 3.4 mm according to the outer diameter of the mounting sleeve, and the cut honeycomb panel is wrapped in a glass fiber reinforced plastic bonding and fixing layer A honeycomb panel filling structure layer 4 is obtained on the outer surface of 3, and the honeycomb panel is an aramid honeycomb panel;
  • Wrapped FRP bonding and reinforcing layer 5 Wrap a glass fiber tape containing resin on the outer surface of the honeycomb panel filling structure layer 4 with a thickness of 5 mm on one side to obtain a FRP bonding and reinforcing layer 5;
  • Composite outer cover layer 6 Select the surface material of the plate roller as a metal alloy, and spray the metal transition coating on the outer surface of the FRP bonding and reinforcement layer 5 by thermal spraying, with a single-sided thickness of 1.5mm to obtain a composite outer surface of the metal alloy.
  • Wrapped FRP inner sheath layer 1 Wrapped fiberglass yarn ribbon containing resin on a core rod mold, solidified and demoulded to obtain FRP inner sheath layer 1, and the single-sided thickness of FRP inner sheath layer 1 is 1.0 mm;
  • the thickness of the honeycomb panel filling structure layer 4 is determined to be 4.7mm according to the outer diameter of the mounting sleeve, and the cut honeycomb panel is wrapped in a glass fiber reinforced plastic bonding and fixing layer A honeycomb panel filling structure layer 4 is obtained on the outer surface of 3, and the honeycomb panel is an aramid honeycomb panel;
  • Wrapped FRP bonding and reinforcing layer 5 Wrap a glass fiber tape containing resin on the outer surface of the honeycomb panel filling structural layer 4 with a thickness of 4 mm on one side to obtain a FRP bonding and reinforcing layer 5;
  • Composite outer plate surface layer 6 The surface material of the plate roller is selected from polyurethane, and the outer surface of the glass fiber reinforced plastic bonding and reinforcement layer 5 is poured with a rotary casting method, and the thickness of one side is 4 mm, and the polyurethane layer is cured;
  • Wrapped FRP inner jacket layer 1 Wrapped fiberglass yarn ribbon containing resin on a core rod mold, cured and demoulded to obtain FRP inner jacket layer 1, and the single-sided thickness of FRP inner jacket layer 1 is 0.8 mm;
  • the thickness of the honeycomb panel filling structure layer 4 is determined to be 4.3 mm according to the outer diameter of the mounting sleeve.
  • the cut honeycomb panel is wrapped in a glass fiber reinforced plastic bonding and fixing layer.
  • a honeycomb panel filling structure layer 4 is obtained on the outer surface of 3, and the honeycomb panel is an aramid honeycomb panel;
  • Wrapped FRP bonding and strengthening layer 5 Wrap the glass fiber filament containing resin on the outer surface of the honeycomb panel filling structure layer 4 with a thickness of 4 mm on one side to obtain the FRP bonding and strengthening layer 5;
  • Composite outer plate surface layer 6 Select the surface material of the plate roll as synthetic resin, and apply the spin-casting method to cast synthetic resin on the outer surface of the FRP bonding and reinforcement layer 5 with a thickness of 1 mm on one side and cure to obtain a synthetic resin layer;
  • Wrapped FRP inner sheath layer 1 Wrapped fiberglass yarn containing resin on the core rod mold, solidified and demoulded to obtain FRP inner sheath layer 1, and the thickness of the single side of FRP inner sheath layer 1 is 1.7mm;
  • the thickness of the honeycomb panel filling structure layer 4 is determined to be 5.5mm according to the outer diameter of the mounting sleeve, and the cut honeycomb panel is wrapped in a glass fiber reinforced plastic bonding and fixing layer A honeycomb panel filling structure layer 4 is obtained on the outer surface of 3, and the honeycomb panel is an aramid honeycomb panel;
  • Wrapped FRP bonding and reinforcing layer 5 Wrap a glass fiber filament containing resin on the outer surface of the honeycomb panel filling structure layer 4 with a thickness of 5 mm on one side to obtain a FRP bonding and reinforcing layer 5;
  • Composite outer plate surface layer 6 Select the surface material of the plate roller as ceramic, first use a thermal spray method to spray a metal transition coating on the outer surface of the glass fiber reinforced plastic bonding and reinforcement layer 5 with a single-sided thickness of 2 mm, and then use thermal spray method The outer surface of the transition coating is sprayed with a ceramic coating, and the thickness of the ceramic coating on one side is 0.3mm;
  • Wrapped FRP inner jacket layer 1 Wrapped fiberglass yarn ribbon containing resin on a core rod mold, cured and demoulded to obtain FRP inner jacket layer 1, and the single-sided thickness of FRP inner jacket layer 1 is 1.2 mm;
  • the thickness of the honeycomb panel filling structure layer 4 is determined to be 5.1 mm according to the outer diameter of the mounting sleeve, and the cut honeycomb panel is wrapped in a glass fiber reinforced plastic bonding and fixing layer.
  • a honeycomb panel filling structure layer 4 is obtained on the outer surface of 3, and the honeycomb panel is an aramid honeycomb panel;
  • Wrapped FRP bonding and strengthening layer 5 Wrap a glass fiber tape containing resin on the outer surface of the honeycomb panel filling structure layer 4 with a thickness of 6 mm on one side to obtain a FRP bonding and strengthening layer 5;
  • Composite outer plate surface layer 6 Select the surface material of the plate roller as synthetic rubber. First, coat the outer surface of the glass fiber reinforced plastic reinforcement layer 5 after lapping, and then cover it with a thickness of 25 mm. Then, vulcanize the wrapped rubber. Obtaining a synthetic rubber layer;
  • Wrapped FRP inner jacket layer 1 Wrapped fiberglass yarn ribbon containing resin on a core rod mold, cured and demoulded to obtain FRP inner jacket layer 1, and the thickness of the single side of FRP inner jacket layer 1 is 1.1 mm;
  • the thickness of the honeycomb panel filling structure layer 4 is determined to be 20 mm according to the outer diameter of the mounting sleeve, and the cut honeycomb panel is wrapped around the glass fiber reinforced plastic fixing layer 3
  • the outer surface of the honeycomb panel is filled with a structural layer 4, and the honeycomb panel is an aramid honeycomb panel;
  • Wrapped FRP bonding and reinforcing layer 5 Wrapped on the outer surface of the honeycomb panel filling structure layer 4 is a glass fiber tape containing resin, with a thickness of 4 mm on one side, and coarsely ground to the required size after curing to obtain the FRP bonding and reinforcing layer 5 ;
  • Composite outer plate surface layer 6 The surface material of the plate roll is selected from synthetic resin, and a synthetic resin layer is poured on the outer surface of the glass fiber reinforced plastic bonding and reinforcement layer 5 by a rotary pouring method with a thickness of 1 mm on one side.
  • plastic inner jacket layer is obtained by injection molding on a core rod mold, and the thickness of the plastic inner jacket layer is 1.2 mm;
  • the thickness of the honeycomb panel filling structure layer 4 is determined to be 40 mm according to the outer diameter of the mounting sleeve, and the cut honeycomb panel is wrapped around the FRP bonding and fixing layer 3
  • the outer surface of the honeycomb panel is filled with a structural layer 4, and the honeycomb panel is an aramid honeycomb panel;
  • Wrapped FRP bonding and strengthening layer 5 Wrap a glass fiber tape containing resin on the outer surface of the honeycomb panel filling structure layer 4 with a thickness of 1 mm on one side to obtain a FRP bonding and strengthening layer 5;
  • Composite outer plate surface layer 6 The surface material of the plate roll is selected from polyurethane, and the outer surface of the glass fiber reinforced plastic bonding and reinforcement layer 5 is poured with a rotary casting method, and the thickness of one side is 4 mm. The polyurethane layer is obtained after curing;
  • Wrapped FRP inner jacket layer 1 Wrapped fiberglass yarn ribbon containing resin on a core rod mold, cured and demoulded to obtain FRP inner jacket layer 1, and the single-sided thickness of FRP inner jacket layer 1 is 1.2 mm;
  • the thickness of the honeycomb panel filling structure layer 4 is determined to be 15 mm according to the outer diameter of the mounting sleeve, and the cut honeycomb panel is wrapped around the glass fiber reinforced plastic bonding and fixing layer 3
  • the outer surface of the honeycomb panel is filled with a structural layer 4, and the honeycomb panel is an aramid honeycomb panel;
  • Wrapped FRP bonding and reinforcing layer 5 Wrap a glass fiber tape containing resin on the outer surface of the honeycomb panel filling structure layer 4 with a thickness of 3 mm on one side, and then grind to the size required after curing to obtain the FRP bonding and reinforcing layer 5 ;
  • Composite outer plate layer 6 Select the surface material of the plate roller as a metal alloy, and spray the metal coating on the outer surface of the FRP bonding and reinforcement layer 5 by thermal spraying, with a thickness of 1.2 mm on one side to obtain a metal alloy layer;
  • Wrapped FRP inner jacket layer 1 Wrapped fiberglass yarn ribbon containing resin on a core rod mold, solidified and demoulded to obtain FRP inner jacket layer 1, and the thickness of the single side of FRP inner jacket layer 1.3 is 1.3mm;
  • the thickness of the honeycomb panel filling structure layer 4 is determined to be 70mm according to the outer diameter of the mounting sleeve, and the cut honeycomb panel is wrapped around the FRP bonding and fixing layer 3
  • the outer surface of the honeycomb panel is filled with a structural layer 4, and the honeycomb panel is an aramid honeycomb panel;
  • Wrapped FRP bonding and reinforcing layer 5 Wrapped on the outer surface of the honeycomb panel filling structure layer 4 is a glass fiber tape containing resin, with a thickness of 4 mm on one side, and coarsely ground to the required size after curing to obtain the FRP bonding and reinforcing layer 5 ;
  • Composite outer plate surface layer 6 Select the surface material of the plate roller as ceramic, first use a thermal spray method to spray a metal transition coating on the outer surface of the glass fiber reinforced plastic bonding and reinforcement layer 5 with a thickness of 1 mm on one side, and then apply the metal to the metal by thermal spray method. The outer surface of the transition coating is sprayed with a single-sided ceramic coating thickness of 0.3 mm to obtain a ceramic layer;
  • Wrapped FRP inner sheath layer 1 Wrapped fiberglass yarn ribbon containing resin on a core rod mold, solidified and demoulded to obtain FRP inner sheath layer 1, and the single-sided thickness of FRP inner sheath layer 1 is 1.5 mm;
  • the thickness of the honeycomb panel filling structure layer 4 is determined to be 160 mm according to the outer diameter dimension of the mounting sleeve, and the cut honeycomb panel is wrapped around the FRP bonding and fixing layer 3
  • the outer surface of the honeycomb panel is filled with a structural layer 4, and the honeycomb panel is an aramid honeycomb panel;
  • Wrapped FRP bonding and strengthening layer 5 Wrap a glass fiber ribbon containing resin on the outer surface of the honeycomb panel filling structure layer 4 with a thickness of 5 mm on one side. After curing, it is coarsely ground to size requirements to obtain the FRP bonding and strengthening layer 5 ;
  • Composite outer plate surface layer 6 Select the surface material of the plate roller as synthetic rubber, first coat the outer surface of the FRP bonding and reinforcement layer 5 after lapping, and cover the thickness of 25mm. A synthetic rubber layer is obtained after vulcanization;
  • the mounting sleeve of the invention has the characteristics of light weight, high strength, good fatigue resistance and impact resistance, good dimensional stability, long service life, and can be easily loaded and unloaded with a sleeve mandrel.

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  • Laminated Bodies (AREA)

Abstract

一种蜂窝结构贴版套筒及其加工方法，该贴版套筒呈中空圆柱形，贴版套筒由内至外依次为玻璃钢内套层（1）或者塑料内套层、弹性体层（2）、玻璃钢粘结固定层（3）、蜂窝板填充结构层（4）、玻璃钢粘结加固层（5）和外版面层（6）。加工方法包括以下步骤：绕制玻璃钢内套层（1）或制作塑料内套层；包绕弹性体层（2）；包绕玻璃钢粘结固定层（3）；包绕蜂窝板填充结构层（4）；包绕玻璃钢粘结加固层（5）；复合外版面层（6）；对贴版套筒进行磨削、抛光处理。

Description

蜂窝结构贴版套筒及其加工方法 技术领域
本发明属于贴版套筒的技术领域，特别是涉及一种柔性版印刷蜂窝结构贴版套筒及其加工方法。
背景技术
现有的柔性版印刷贴版套筒，为了减重，有采用发泡聚氨酯或者发泡合成橡胶作为填充层，但是这种贴版套筒整体上存在结构强度低、尺寸稳定性差和加工污染大等弊端。
发明内容
本发明所要解决的技术问题是提供一种蜂窝结构贴版套筒及其加工方法，降低质量，提高结构强度和稳定性，方便装卸，延长使用寿命。
本发明解决其技术问题所采用的技术方案是提供一种蜂窝结构贴版套筒，该贴版套筒呈中空圆柱形，所述贴版套筒由内至外依次为玻璃钢内套层、弹性体层、玻璃钢粘结固定层、蜂窝板填充结构层、玻璃钢粘结加固层和外版面层。
所述玻璃钢内套层也可以是塑料内套层。
本发明解决其技术问题所采用的技术方案是提供一种上述蜂窝结构贴版套筒的加工方法，包括以下步骤：
(1)绕制玻璃钢内套层：在芯棒模具上绕制含有树脂的玻璃纤维纱带，固化脱模裁切得到玻璃钢内套层，所述玻璃钢内套层单边厚度0.7mm～1.7mm；
(2)包绕弹性体层：将经过裁切的厚度为0.3mm～3.0mm的弹性体片状薄带包绕在玻璃钢内套层外表面得到弹性体层；
(3)包绕玻璃钢粘结固定层：将经过裁切的含有树脂的玻璃钢带/片包绕在弹性体层外表面得到玻璃钢粘结固定层；
(4)包绕蜂窝板填充结构层：根据贴版套筒的外径尺寸确定蜂窝板填充结构层的厚度，将经过裁切的蜂窝板片包绕在玻璃钢粘结固定层的外表面得到蜂窝板填充结构层；
(5)包绕玻璃钢粘结加固层：在蜂窝板填充结构层的外表面包绕含有树脂的玻璃纤维带或者玻璃纤维丝得到玻璃钢粘结加固层；
(6)复合外版面层：选择套筒表面材料，在玻璃钢粘结加固层的外表面复合外版面 层；
(7)对贴版套筒的外表面进行磨削、抛光处理至到达设计外径尺寸。
所述蜂窝板片采用芳纶蜂窝板片。
所述步骤(6)的版辊表面材料为金属合金，采用热喷涂法在玻璃钢粘结加固层的外表面喷涂金属过渡涂层。
所述步骤(6)的版辊表面材料为聚氨酯或者合成树脂，采用旋转浇筑法在玻璃钢粘结加固层的外表面浇淋聚氨酯或者合成树脂并固化得到聚氨酯层或者合成树脂层。
所述步骤(6)的版辊表面材料为陶瓷，先采用热喷涂法在玻璃钢粘结加固层的外表面喷涂金属过渡涂层，再通过热喷涂法在金属过渡涂层的外表面喷涂陶瓷涂层。
所述步骤(6)的版辊表面材料为合成橡胶，先在玻璃钢粘结加固层的外表面毛化处理后包胶，再对包裹的合成橡胶进行硫化成型。
有益效果
第一，本发明的贴版套筒内层采用具有一定弹性张力的玻璃钢内套层或塑料内套层，能够在贴版套筒装卸时通过气流压迫使其向外膨胀达到一定的扩径作用，从而能够方便贴版套筒与套筒芯棒之间的装卸。
第二，弹性体层具有可压缩回弹性，设置于玻璃钢内套层的外表面，能够吸收玻璃钢内套层(或者塑料内套层)的膨胀和收缩，有利于保持贴版套筒尺寸的稳定性。
第三，蜂窝板填充结构层作为贴版套筒的主体结构层，支撑着贴版套筒的强度、刚性和韧性度。通过对蜂窝板填充结构层厚度设计可以对套筒的外径尺寸进行控制，可以降低套筒芯棒的径向尺寸，蜂窝板填充结构层的蜂窝状空心结构，能够大大降低贴版套筒的质量，有利于降低版辊的使用能耗；蜂窝板填充结构层的蜂窝状组织架构，稳定性强，能够提高贴版套筒的结构强度和韧性，有利于延长套筒的使用寿命，稳定的蜂窝状主体结构同样有助于超厚贴版套筒的实现，摆脱现有套筒的厚度限制；蜂窝板填充结构层作为主体结构层具有非常小的热膨胀性能，能够在受热时保持结构的稳定性，同时能够加固内侧的玻璃钢结构层，使其膨胀形变量由弹性体层吸收，从而保持了贴版套筒受热时整体尺寸的稳定性。
附图说明
图1为本发明贴版套筒的结构示意图。
图2为本发明套筒芯棒的结构示意图。
图3为本发明贴版版辊的结构示意图。
图4为本发明贴版套筒粘贴印版的轴向剖视示意图。
图5为本发明贴版套筒粘贴印版的侧面结构示意图。
具体实施方式
下面结合具体实施例，进一步阐述本发明。应理解，这些实施例仅用于说明本发明而不用于限制本发明的范围。此外应理解，在阅读了本发明讲授的内容之后，本领域技术人员可以对本发明作各种改动或修改，这些等价形式同样落于本申请所附权利要求书所限定的范围。
如图1所示的一种蜂窝结构贴版套筒，该贴版套筒呈中空圆柱形，贴版套筒由内至外依次为玻璃钢内套层1或者塑料内套层、弹性体层2、玻璃钢粘结固定层3、蜂窝板填充结构层4、玻璃钢粘结加固层5和外版面层6。
下面提供一种上述的蜂窝结构贴版套筒的加工方法，包括以下步骤：
(1)绕制玻璃钢内套层1：在芯棒模具上绕制含有树脂的玻璃纤维纱带，固化脱模裁切得到玻璃钢内套层1，玻璃钢内套层1单边厚度0.7mm～1.7mm；
或者制作塑料内套层：在芯棒模具上制作塑料内套层，塑料内套层的厚度为0.7～1.7mm；
(2)包绕弹性体层2：将经过裁切的厚度为0.3mm～3.0mm的弹性体片状薄带包绕在玻璃钢内套层1(或者塑料内套层)外表面得到弹性体层2；
(3)包绕玻璃钢粘结固定层3：将经过裁切的玻璃钢带/片包绕在弹性体层2外表面得到玻璃钢粘结固定层3；
(4)包绕蜂窝板填充结构层4：根据贴版套筒的外径尺寸确定蜂窝板填充结构层4的厚度，将经过裁切的蜂窝板片包绕在玻璃钢粘结固定层3的外表面得到蜂窝板填充结构层4；
(5)包绕玻璃钢粘结加固层5：在蜂窝板填充结构层4的外表面包绕玻璃纤维带或者玻璃纤维丝得到玻璃钢粘结加固层5；
(6)复合外版面层6：选择版辊表面材料，在玻璃钢粘结加固层5的外表面复合外版面层6；
(7)对贴版套筒的外表面进行磨削、抛光处理至到达设计外径尺寸。
如图3所示的一种贴版版辊，包括上述的蜂窝结构贴版套筒和套筒芯棒7。
套筒芯棒7的结构如图2所示，包括中空辊筒701和左右两侧的辊撑702。套筒芯棒7一侧的辊撑702内开有与辊筒701的中空腔连通的进气孔703，辊筒701与进气孔703的相对端靠近端部边缘的位置沿辊筒701的周向开有若干贯通辊筒701内外的出气孔704，出气孔704的内端连通到辊筒701的中空腔。
贴版套筒无间隙紧密贴合在套筒芯棒7的辊筒701的外表面。如图4换热图5所示，贴版套筒的外表面通过双面胶带8粘接有感光印版9，感光印版9可以为感光树脂版、感光橡胶版或者其他柔性薄感光版。
下面提供一种上述的贴版套筒的装卸方法，包括以下步骤：
(1)在进行贴版套筒装套时，通过进气孔703向套筒芯棒7内通入压缩空气，出气孔704的气流压迫贴版套筒的内壁膨胀，贴版套筒套装到位后泄去压缩空气，贴版套筒向内回弹后无间隙紧密贴合在套筒芯棒7的辊筒701的外表面形成一体的贴版版辊；
(2)在进行贴版套筒卸套时，通过进气孔703向套筒芯棒7内通入压缩空气，出气孔704的气流压迫贴版套筒的内壁膨胀与套筒芯棒7脱离贴合，将贴版套筒从辊筒701外表面拉出完成贴版套筒的卸套。
下面提供10种贴版套筒的具体加工方法的实施例：
实施例1
(1)绕制玻璃钢内套层1：在芯棒模具上绕制含有树脂的玻璃纤维纱带，固化脱模裁切得到玻璃钢内套层1，玻璃钢内套层1单边厚度为0.7mm；
(2)包绕弹性体层2：将经过裁切的厚度为0.5mm的弹性体片状薄带包绕在玻璃钢内套层1外表面得到弹性体层2；
(3)包绕玻璃钢粘结固定层3：将经过裁切的含有树脂的玻璃钢带包绕在弹性体层2外表面，得到单边厚度为1.5mm的玻璃钢粘结固定层3；
(4)包绕蜂窝板填充结构层4：根据贴版套筒的外径尺寸确定蜂窝板填充结构层4的厚度为3.4mm，将经过裁切的蜂窝板片包绕在玻璃钢粘结固定层3的外表面得到蜂窝板填充结构层4，蜂窝板片采用芳纶蜂窝板片；
(5)包绕玻璃钢粘结加固层5：在蜂窝板填充结构层4的外表面包绕含有树脂的玻璃纤维带，单边厚度5mm，得到玻璃钢粘结加固层5；
(6)复合外版面层6：选择版辊表面材料为金属合金，采用热喷涂法在玻璃钢粘结 加固层5的外表面喷涂金属过渡涂层，单边厚度1.5mm，得到金属合金的复合外版面层6；
(7)对贴版套筒的外表面进行磨削、抛光处理至到达设计外径尺寸。
实施例2
(1)绕制玻璃钢内套层1：在芯棒模具上绕制含有树脂的玻璃纤维纱带，固化脱模裁切得到玻璃钢内套层1，玻璃钢内套层1单边厚度为1.0mm；
(2)包绕弹性体层2：将经过裁切的厚度为1.0mm的弹性体片状薄带包绕在玻璃钢内套层1外表面得到弹性体层2；
(3)包绕玻璃钢粘结固定层3：将经过裁切的含有树脂的玻璃钢带包绕在弹性体层2外表面，得到单边厚度为2mm的玻璃钢粘结固定层3；
(4)包绕蜂窝板填充结构层4：根据贴版套筒的外径尺寸确定蜂窝板填充结构层4的厚度为4.7mm，将经过裁切的蜂窝板片包绕在玻璃钢粘结固定层3的外表面得到蜂窝板填充结构层4，蜂窝板片采用芳纶蜂窝板片；
(5)包绕玻璃钢粘结加固层5：在蜂窝板填充结构层4的外表面包绕含有树脂的玻璃纤维带，单边厚度4mm，得到玻璃钢粘结加固层5；
(6)复合外版面层6：选择版辊表面材料为聚氨酯，采用旋转浇筑法在玻璃钢粘结加固层5的外表面浇淋聚氨酯，单边厚度4mm，固化得到聚氨酯层；
(7)对贴版套筒的外表面进行磨削、抛光处理至到达设计外径尺寸。
实施例3
(1)绕制玻璃钢内套层1：在芯棒模具上绕制含有树脂的玻璃纤维纱带，固化脱模裁切得到玻璃钢内套层1，玻璃钢内套层1单边厚度为0.8mm；
(2)包绕弹性体层2：将经过裁切的厚度为1.1mm的弹性体片状薄带包绕在玻璃钢内套层1外表面得到弹性体层2；
(3)包绕玻璃钢粘结固定层3：将经过裁切的含有树脂的玻璃钢带包绕在弹性体层2外表面，单边厚度2.5mm，得到玻璃钢粘结固定层3；
(4)包绕蜂窝板填充结构层4：根据贴版套筒的外径尺寸确定蜂窝板填充结构层4的厚度为4.3mm，将经过裁切的蜂窝板片包绕在玻璃钢粘结固定层3的外表面得到蜂窝板填充结构层4，蜂窝板片采用芳纶蜂窝板片；
(5)包绕玻璃钢粘结加固层5：在蜂窝板填充结构层4的外表面包绕含有树脂的玻 璃纤维丝，单边厚度4mm，得到玻璃钢粘结加固层5；
(6)复合外版面层6：选择版辊表面材料为合成树脂，采用旋转浇筑法在玻璃钢粘结加固层5的外表面浇淋合成树脂，单边厚度1mm，固化得到合成树脂层；
(7)对贴版套筒的外表面进行磨削、抛光处理至到达设计外径尺寸。
实施例4
(1)绕制玻璃钢内套层1：在芯棒模具上绕制含有树脂的玻璃纤维纱带，固化脱模裁切得到玻璃钢内套层1，玻璃钢内套层1单边厚度为1.7mm；
(2)包绕弹性体层2：将经过裁切的厚度为2.0mm的弹性体片状薄带包绕在玻璃钢内套层1外表面得到弹性体层2；
(3)包绕玻璃钢粘结固定层3：将经过裁切的含有树脂的玻璃钢带包绕在弹性体层2外表面，单边厚度3mm，得到玻璃钢粘结固定层3；
(4)包绕蜂窝板填充结构层4：根据贴版套筒的外径尺寸确定蜂窝板填充结构层4的厚度为5.5mm，将经过裁切的蜂窝板片包绕在玻璃钢粘结固定层3的外表面得到蜂窝板填充结构层4，蜂窝板片采用芳纶蜂窝板片；
(5)包绕玻璃钢粘结加固层5：在蜂窝板填充结构层4的外表面包绕含有树脂的玻璃纤维丝，单边厚度5mm，得到玻璃钢粘结加固层5；
(6)复合外版面层6：选择版辊表面材料为陶瓷，先采用热喷涂法在玻璃钢粘结加固层5的外表面喷涂金属过渡涂层，单边厚度2mm，再通过热喷涂法在金属过渡涂层的外表面喷涂陶瓷涂层，陶瓷涂层单边厚度0.3mm；
(7)对贴版套筒的外表面进行磨削、抛光处理至到达设计外径尺寸。
实施例5
(1)绕制玻璃钢内套层1：在芯棒模具上绕制含有树脂的玻璃纤维纱带，固化脱模裁切得到玻璃钢内套层1，玻璃钢内套层1单边厚度为1.2mm；
(2)包绕弹性体层2：将经过裁切的厚度为1.3mm的弹性体片状薄带包绕在玻璃钢内套层1外表面得到弹性体层2；
(3)包绕玻璃钢粘结固定层3：将经过裁切的含有树脂的玻璃钢带包绕在弹性体层2外表面，单边厚度5mm，得到玻璃钢粘结固定层3；
(4)包绕蜂窝板填充结构层4：根据贴版套筒的外径尺寸确定蜂窝板填充结构层4的厚度为5.1mm，将经过裁切的蜂窝板片包绕在玻璃钢粘结固定层3的外表面 得到蜂窝板填充结构层4，蜂窝板片采用芳纶蜂窝板片；
(5)包绕玻璃钢粘结加固层5：在蜂窝板填充结构层4的外表面包绕含有树脂的玻璃纤维带，单边厚度6mm，得到玻璃钢粘结加固层5；
(6)复合外版面层6：选择版辊表面材料为为合成橡胶，先在玻璃钢粘结加固层5的外表面毛化处理后包胶，包胶厚度25mm，再对包裹的橡胶进行硫化成型得到合成橡胶层；
(7)对贴版套筒的外表面进行磨削、抛光处理至到达设计外径尺寸。
实施例6
(1)绕制玻璃钢内套层1：在芯棒模具上绕制含有树脂的玻璃纤维纱带，固化脱模裁切得到玻璃钢内套层1，玻璃钢内套层1单边厚度为1.1mm；
(2)包绕弹性体层2：将经过裁切的厚度为1.5mm的弹性体片状薄带包绕在玻璃钢内套层1外表面得到弹性体层2；
(3)包绕玻璃钢粘结固定层3：将经过裁切的含有树脂的玻璃钢带包绕在弹性体层2外表面，得到单边厚度为1.0mm的玻璃钢粘结固定层3；
(4)包绕蜂窝板填充结构层4：根据贴版套筒的外径尺寸确定蜂窝板填充结构层4的厚度为20mm，将经过裁切的蜂窝板片包绕在玻璃钢粘结固定层3的外表面得到蜂窝板填充结构层4，蜂窝板片采用芳纶蜂窝板片；
(5)包绕玻璃钢粘结加固层5：在蜂窝板填充结构层4的外表面包绕含有树脂的玻璃纤维带，单边厚度4mm，固化后粗磨至尺寸要求，得到玻璃钢粘结加固层5；
(6)复合外版面层6：选择版辊表面材料为合成树脂，采用旋转浇淋法在玻璃钢粘结加固层5的外表面浇淋合成树脂，单边厚度1mm，固化后得到合成树脂层；
(7)对贴版套筒的外表面进行磨削、抛光处理至到达设计外径尺寸。
实施例7
(1)制作塑料内套层：在芯棒模具上注塑得到塑料内套层，塑料内套层的厚度为1.2mm；
(2)包绕弹性体层2：将经过裁切的厚度为1.5mm的弹性体片状薄带包绕在塑料内套层外表面得到弹性体层2；
(3)包绕玻璃钢粘结固定层3：将经过裁切的含有树脂的玻璃钢带包绕在弹性体层2外表面，得到单边厚度为2.0mm的玻璃钢粘结固定层3；
(4)包绕蜂窝板填充结构层4：根据贴版套筒的外径尺寸确定蜂窝板填充结构层4的厚度为40mm，将经过裁切的蜂窝板片包绕在玻璃钢粘结固定层3的外表面得到蜂窝板填充结构层4，蜂窝板片采用芳纶蜂窝板片；
(5)包绕玻璃钢粘结加固层5：在蜂窝板填充结构层4的外表面包绕含有树脂的玻璃纤维带，单边厚度1mm，得到玻璃钢粘结加固层5；
(6)复合外版面层6：选择版辊表面材料为聚氨酯，采用旋转浇筑法在玻璃钢粘结加固层5的外表面浇淋聚氨酯，单边厚度4mm，固化后得到聚氨酯层；
(7)对贴版套筒的外表面进行磨削、抛光处理至到达设计外径尺寸。
实施例8
(1)绕制玻璃钢内套层1：在芯棒模具上绕制含有树脂的玻璃纤维纱带，固化脱模裁切得到玻璃钢内套层1，玻璃钢内套层1单边厚度为1.2mm；
(2)包绕弹性体层2：将经过裁切的厚度为1.5mm的弹性体片状薄带包绕在玻璃钢内套层1外表面得到弹性体层2；
(3)包绕玻璃钢粘结固定层3：将经过裁切的含有树脂的玻璃钢带包绕在弹性体层2外表面，得到单边厚度为0.5mm的玻璃钢粘结固定层3；
(4)包绕蜂窝板填充结构层4：根据贴版套筒的外径尺寸确定蜂窝板填充结构层4的厚度为15mm，将经过裁切的蜂窝板片包绕在玻璃钢粘结固定层3的外表面得到蜂窝板填充结构层4，蜂窝板片采用芳纶蜂窝板片；
(5)包绕玻璃钢粘结加固层5：在蜂窝板填充结构层4的外表面包绕含有树脂的玻璃纤维带，单边厚度3mm，固化后粗磨至尺寸要求，得到玻璃钢粘结加固层5；
(6)复合外版面层6：选择版辊表面材料为金属合金，采用热喷涂法在玻璃钢粘结加固层5的外表面喷涂金属涂层，单边厚度1.2mm，得到金属合金层；
(7)对贴版套筒的外表面进行磨削、抛光处理至到达设计外径尺寸。
实施例9
(1)绕制玻璃钢内套层1：在芯棒模具上绕制含有树脂的玻璃纤维纱带，固化脱模裁切得到玻璃钢内套层1，玻璃钢内套层1单边厚度为1.3mm；
(2)包绕弹性体层2：将经过裁切的厚度为2.0mm的弹性体片状薄带包绕在玻璃钢内套层1外表面得到弹性体层2；
(3)包绕玻璃钢粘结固定层3：将经过裁切的含有树脂的玻璃钢带包绕在弹性体层2 外表面，得到单边厚度为3.0mm的玻璃钢粘结固定层3；
(4)包绕蜂窝板填充结构层4：根据贴版套筒的外径尺寸确定蜂窝板填充结构层4的厚度为70mm，将经过裁切的蜂窝板片包绕在玻璃钢粘结固定层3的外表面得到蜂窝板填充结构层4，蜂窝板片采用芳纶蜂窝板片；
(5)包绕玻璃钢粘结加固层5：在蜂窝板填充结构层4的外表面包绕含有树脂的玻璃纤维带，单边厚度4mm，固化后粗磨至尺寸要求，得到玻璃钢粘结加固层5；
(6)复合外版面层6：选择版辊表面材料为陶瓷，先采用热喷涂法在玻璃钢粘结加固层5的外表面喷涂金属过渡涂层，单边厚度1mm，再通过热喷涂法在金属过渡涂层的外表面喷涂单边陶瓷涂层厚度0.3mm，得到陶瓷层；
(7)对贴版套筒的外表面进行磨削、抛光处理至到达设计外径尺寸。
实施例10
(1)绕制玻璃钢内套层1：在芯棒模具上绕制含有树脂的玻璃纤维纱带，固化脱模裁切得到玻璃钢内套层1，玻璃钢内套层1单边厚度为1.5mm；
(2)包绕弹性体层2：将经过裁切的厚度为2.0mm的弹性体片状薄带包绕在玻璃钢内套层1外表面得到弹性体层2；
(3)包绕玻璃钢粘结固定层3：将经过裁切的含有树脂的玻璃钢带包绕在弹性体层2外表面，得到单边厚度为5.0mm的玻璃钢粘结固定层3；
(4)包绕蜂窝板填充结构层4：根据贴版套筒的外径尺寸确定蜂窝板填充结构层4的厚度为160mm，将经过裁切的蜂窝板片包绕在玻璃钢粘结固定层3的外表面得到蜂窝板填充结构层4，蜂窝板片采用芳纶蜂窝板片；
(5)包绕玻璃钢粘结加固层5：在蜂窝板填充结构层4的外表面包绕含有树脂的玻璃纤维带，单边厚度5mm，固化后粗磨至尺寸要求，得到玻璃钢粘结加固层5；
(6)复合外版面层6：选择版辊表面材料为合成橡胶，先在玻璃钢粘结加固层5的外表面毛化处理后包胶，包胶厚度25mm，再对包裹的贴版套筒进行硫化成型后得到合成橡胶层；
(7)对贴版套筒的外表面进行磨削、抛光处理至到达设计外径尺寸。
本发明的贴版套筒具有质量轻、强度高、抗疲劳性和耐冲击性好、尺寸稳定性好的特点，使用寿命长，且能够方便地与套筒芯棒进行装卸。

Claims (8)

  1. 一种蜂窝结构贴版套筒，该贴版套筒呈中空圆柱形，其特征在于：所述贴版套筒由内至外依次为玻璃钢内套层(1)、弹性体层(2)、玻璃钢粘结固定层(3)、蜂窝板填充结构层(4)、玻璃钢粘结加固层(5)和外版面层(6)。
  2. 根据权利要求1所述的一种蜂窝结构贴版套筒，其特征在于：所述玻璃钢内套层(1)也可以是塑料内套层。
  3. 一种权利要求1所述的蜂窝结构贴版套筒的加工方法，包括以下步骤：
    (1)绕制玻璃钢内套层(1)：在芯棒模具上绕制含有树脂的玻璃纤维纱带，固化脱模裁切得到玻璃钢内套层(1)，所述玻璃钢内套层(1)单边厚度0.7mm～1.7mm；
    (2)包绕弹性体层(2)：将经过裁切的厚度为0.3mm～3.0mm的弹性体片状薄带包绕在玻璃钢内套层(1)外表面得到弹性体层(2)；
    (3)包绕玻璃钢粘结固定层(3)：将经过裁切的含有树脂的玻璃钢带/片包绕在弹性体层(2)外表面得到玻璃钢粘结固定层(3)；
    (4)包绕蜂窝板填充结构层(4)：根据贴版套筒的外径尺寸确定蜂窝板填充结构层(4)的厚度，将经过裁切的蜂窝板片包绕在玻璃钢粘结固定层(3)的外表面得到蜂窝板填充结构层(4)；
    (5)包绕玻璃钢粘结加固层(5)：在蜂窝板填充结构层(4)的外表面包绕含有树脂的玻璃纤维带或者玻璃纤维丝得到玻璃钢粘结加固层(5)；
    (6)复合外版面层(6)：选择套筒表面材料，在玻璃钢粘结加固层(5)的外表面复合外版面层(6)；
    (7)对贴版套筒的外表面进行磨削、抛光处理至到达设计外径尺寸。
  4. 根据权利要求3所述的一种蜂窝结构贴版套筒的加工方法，其特征在于：所述蜂窝板片采用芳纶蜂窝板片。
  5. 根据权利要求3所述的一种蜂窝结构贴版套筒的加工方法，其特征在于：所述步骤(6)的版辊表面材料为金属合金，采用热喷涂法在玻璃钢粘结加固层(5)的外表面喷涂金属过渡涂层。
  6. 根据权利要求3所述的一种蜂窝结构贴版套筒的加工方法，其特征在于：所述步骤(6)的版辊表面材料为聚氨酯或者合成树脂，采用旋转浇筑法在玻璃钢粘结加固层(5)的外表面浇淋聚氨酯或者合成树脂并固化得到聚氨酯层或者合成树脂层。
  7. 根据权利要求3所述的一种蜂窝结构贴版套筒的加工方法，其特征在于：所述步骤(6)的版辊表面材料为陶瓷，先采用热喷涂法在玻璃钢粘结加固层(5)的外表面喷涂金属 过渡涂层，再通过热喷涂法在金属过渡涂层的外表面喷涂陶瓷涂层。
  8. 根据权利要求3所述的一种蜂窝结构贴版套筒的加工方法，其特征在于：所述步骤(6)的版辊表面材料为合成橡胶，先在玻璃钢粘结加固层(5)的外表面毛化处理后包胶，再对包裹的合成橡胶进行硫化成型。
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