US20040232274A1 - Fiber reinforced hybrid composite winding core - Google Patents
Fiber reinforced hybrid composite winding core Download PDFInfo
- Publication number
- US20040232274A1 US20040232274A1 US10/850,951 US85095104A US2004232274A1 US 20040232274 A1 US20040232274 A1 US 20040232274A1 US 85095104 A US85095104 A US 85095104A US 2004232274 A1 US2004232274 A1 US 2004232274A1
- Authority
- US
- United States
- Prior art keywords
- winding core
- layers
- recited
- core
- wall
- Prior art date
- Legal status (The legal status 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 status listed.)
- Abandoned
Links
- 238000004804 winding Methods 0.000 title claims abstract description 73
- 239000000835 fiber Substances 0.000 title claims description 40
- 239000002131 composite material Substances 0.000 title description 3
- 239000010410 layer Substances 0.000 claims abstract description 71
- 239000000463 material Substances 0.000 claims abstract description 26
- 239000011241 protective layer Substances 0.000 claims abstract description 18
- 230000003014 reinforcing effect Effects 0.000 claims abstract description 6
- 229920005989 resin Polymers 0.000 claims description 17
- 239000011347 resin Substances 0.000 claims description 17
- 238000005452 bending Methods 0.000 claims description 12
- 239000011159 matrix material Substances 0.000 claims description 7
- 239000011152 fibreglass Substances 0.000 claims description 6
- 239000003365 glass fiber Substances 0.000 claims description 6
- -1 polyethylene Polymers 0.000 claims description 5
- 229920000049 Carbon (fiber) Polymers 0.000 claims description 3
- 239000004698 Polyethylene Substances 0.000 claims description 3
- 239000004917 carbon fiber Substances 0.000 claims description 3
- 239000003822 epoxy resin Substances 0.000 claims description 3
- 229920000647 polyepoxide Polymers 0.000 claims description 3
- 229920000573 polyethylene Polymers 0.000 claims description 3
- 229920001187 thermosetting polymer Polymers 0.000 claims description 3
- 229920001567 vinyl ester resin Polymers 0.000 claims description 3
- 244000198134 Agave sisalana Species 0.000 claims description 2
- 244000025254 Cannabis sativa Species 0.000 claims description 2
- 235000012766 Cannabis sativa ssp. sativa var. sativa Nutrition 0.000 claims description 2
- 235000012765 Cannabis sativa ssp. sativa var. spontanea Nutrition 0.000 claims description 2
- 240000000797 Hibiscus cannabinus Species 0.000 claims description 2
- 229920000271 Kevlar® Polymers 0.000 claims description 2
- 235000009120 camo Nutrition 0.000 claims description 2
- 235000005607 chanvre indien Nutrition 0.000 claims description 2
- 239000004744 fabric Substances 0.000 claims description 2
- 239000011487 hemp Substances 0.000 claims description 2
- 239000004761 kevlar Substances 0.000 claims description 2
- 239000000203 mixture Substances 0.000 claims description 2
- 229920001568 phenolic resin Polymers 0.000 claims description 2
- 239000005011 phenolic resin Substances 0.000 claims description 2
- 229920001225 polyester resin Polymers 0.000 claims description 2
- 239000004645 polyester resin Substances 0.000 claims description 2
- 229920000642 polymer Polymers 0.000 claims description 2
- 239000002952 polymeric resin Substances 0.000 claims description 2
- 229920003002 synthetic resin Polymers 0.000 claims description 2
- 229920005992 thermoplastic resin Polymers 0.000 claims description 2
- OKTJSMMVPCPJKN-UHFFFAOYSA-N Carbon Chemical compound [C] OKTJSMMVPCPJKN-UHFFFAOYSA-N 0.000 claims 1
- 229910052799 carbon Inorganic materials 0.000 claims 1
- 239000011521 glass Substances 0.000 claims 1
- LNEPOXFFQSENCJ-UHFFFAOYSA-N haloperidol Chemical compound C1CC(O)(C=2C=CC(Cl)=CC=2)CCN1CCCC(=O)C1=CC=C(F)C=C1 LNEPOXFFQSENCJ-UHFFFAOYSA-N 0.000 claims 1
- 229920002430 Fibre-reinforced plastic Polymers 0.000 abstract description 3
- 239000011151 fibre-reinforced plastic Substances 0.000 abstract description 3
- 239000012792 core layer Substances 0.000 abstract description 2
- 239000011162 core material Substances 0.000 description 88
- 238000000034 method Methods 0.000 description 4
- 238000005520 cutting process Methods 0.000 description 3
- 238000004519 manufacturing process Methods 0.000 description 3
- 238000003860 storage Methods 0.000 description 3
- PXKLMJQFEQBVLD-UHFFFAOYSA-N bisphenol F Chemical compound C1=CC(O)=CC=C1CC1=CC=C(O)C=C1 PXKLMJQFEQBVLD-UHFFFAOYSA-N 0.000 description 2
- 238000006243 chemical reaction Methods 0.000 description 2
- 238000009730 filament winding Methods 0.000 description 2
- 239000004848 polyfunctional curative Substances 0.000 description 2
- 229920001131 Pulp (paper) Polymers 0.000 description 1
- 239000000853 adhesive Substances 0.000 description 1
- 230000001070 adhesive effect Effects 0.000 description 1
- 230000002411 adverse Effects 0.000 description 1
- 150000008064 anhydrides Chemical class 0.000 description 1
- 239000011324 bead Substances 0.000 description 1
- 239000004841 bisphenol A epoxy resin Substances 0.000 description 1
- 239000004842 bisphenol F epoxy resin Substances 0.000 description 1
- 238000010276 construction Methods 0.000 description 1
- 238000004132 cross linking Methods 0.000 description 1
- 239000003733 fiber-reinforced composite Substances 0.000 description 1
- 239000002657 fibrous material Substances 0.000 description 1
- 239000003292 glue Substances 0.000 description 1
- 239000002184 metal Substances 0.000 description 1
- VNWKTOKETHGBQD-UHFFFAOYSA-N methane Chemical compound C VNWKTOKETHGBQD-UHFFFAOYSA-N 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 239000004033 plastic Substances 0.000 description 1
- 229920003023 plastic Polymers 0.000 description 1
- 229920000728 polyester Polymers 0.000 description 1
- 238000009987 spinning Methods 0.000 description 1
- 239000012815 thermoplastic material Substances 0.000 description 1
- 238000005303 weighing Methods 0.000 description 1
Images
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B65—CONVEYING; PACKING; STORING; HANDLING THIN OR FILAMENTARY MATERIAL
- B65H—HANDLING THIN OR FILAMENTARY MATERIAL, e.g. SHEETS, WEBS, CABLES
- B65H75/00—Storing webs, tapes, or filamentary material, e.g. on reels
- B65H75/02—Cores, formers, supports, or holders for coiled, wound, or folded material, e.g. reels, spindles, bobbins, cop tubes, cans, mandrels or chucks
- B65H75/04—Kinds or types
- B65H75/08—Kinds or types of circular or polygonal cross-section
- B65H75/10—Kinds or types of circular or polygonal cross-section without flanges, e.g. cop tubes
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B65—CONVEYING; PACKING; STORING; HANDLING THIN OR FILAMENTARY MATERIAL
- B65H—HANDLING THIN OR FILAMENTARY MATERIAL, e.g. SHEETS, WEBS, CABLES
- B65H2701/00—Handled material; Storage means
- B65H2701/50—Storage means for webs, tapes, or filamentary material
- B65H2701/51—Cores or reels characterised by the material
- B65H2701/512—Cores or reels characterised by the material moulded
- B65H2701/5122—Plastics
Definitions
- This invention relates to web winding cores for use in winding web material such as tissue paper, paper toweling, and the like. More particularly, the invention is related to a fiber reinforced polymer winding core.
- the tissue making process entails winding the finished tissue product onto a cylindrical tube, commonly called a “core”.
- the core is supported by a mandrel that is inserted into the core.
- the mandrel rotates the winding core to a velocity with a surface speed that matches the linear speed of the tissue material moving through the end of the tissue machine.
- an adhesive is typically sprayed onto the winding core and the mandrel-driven winding core is brought into contact with the moving tissue material, which adheres to the winding core and begins to be wound onto the winding core.
- tissue winding is complete, the tissue material is cut and the tissue-wound core is brought to a stop by the mandrel.
- a table or similar means is brought into support for the tissue-wound core and the mandrel is extracted from the core.
- the tissue-wound core is then either transported to a storage facility or to a converting machine for conversion, i.e., unwinding, transverse perforation and rewinding into commercial sized rolls.
- the tissue-wound core may be stored either horizontally or vertically.
- a plug is inserted into each end of the tissue-wound core.
- the tissue-wound core is then raised by a mechanical hoist attached to the plugs and lowered into the converting machine.
- the plugs support the tissue-wound core as it is rotated to unwind most of the tissue material that was previously wound onto the core.
- the last several layers of tissue are discarded by cutting them off the core with a sharp knife. The knife often causes damage to the core.
- the core is transported back to the tissue machine where the winding process is repeated. During transportation, the core may be handled manually or with handling equipment.
- the fiber core is also commonly damaged through the cutting action of the knife that is used to remove the scrap tissue at the end of an unwind operation. During each cutting procedure, the knife penetrates several layers of the fiber core and makes a deep cut over the entire length of the core. After several reuses, the number of cuts becomes great enough that, when the winding core is rotated by the mandrel at high velocity just before the start of a wind operation, the fiber core may begin to delaminate and self-destruct.
- the integral wall thickness of the fiber core must be such that the winding core can withstand the centrifugal forces caused by high speed spinning and the structural forces caused by the weight of the tissue roll that the winding core must support.
- the present invention provides a unique solution to the major drawbacks of prior art winding cores.
- the invention disclosed is a hybrid fiber reinforced polymer core consisting of several layers of different materials that, when combined in a specific sequence and in specific relative quantities, result in a winding core with characteristics superior to prior art cores.
- the invention winding core weighs approximately the same as fiber cores, but has significantly increased crush strength, crush stiffness, bending strength, bending stiffness, hoop strength, hoop stiffness, impact resistance, cut resistance, moisture resistance, and abuse tolerance.
- the present invention hybrid composite winding core has properties which have been specifically tailored to exhibit a high degree of stiffness, strength and resistance to abuse without increasing mass over the prior art.
- the present invention core is particularly useful when used in conjunction with large-scale tissue manufacturing operations.
- FIG. 1 is a side view, partly in section, of a winding core constructed according to the present invention.
- FIG. 2 is a cross sectional side view of the portion of the winding core shown in FIG. 1 as area 2 .
- FIG. 3 is a close up cross sectional view of an end cap.
- FIG. 4 is a perspective view of a winding core with textured outer surface.
- a winding core 10 constructed according to the principles of the invention.
- the invention example shown pertains to a core with a sixteen inch nominal inside diameter with a nominal length of one hundred inches.
- a prior art fiber core of this size would typically require a wall thickness of between five-eighths inches to three-quarters inches, and would weigh approximately one hundred pounds in order to provide adequate strength, stiffness and resistance to abuse.
- the invention winding core is not limited to this particular core size, but applies to cores of virtually any size.
- the winding core 10 of the present invention is constructed of multiple layers of polymer impregnated fibrous materials forming a cylindrically-shaped, hollow winding core 10 with two open ends 2 , a wall 3 connecting both ends 2 , said wall 3 having an exterior surface 4 and an inner surface 5 .
- the wall 3 is comprised of said layers.
- the wall layers are formed preferably through filament winding, but could also be formed other known manufacturing methods, including by hand by means of a roll table.
- the winding core layers are constructed so that structural reinforcing layers are sandwiched between outer protective layers.
- the outermost protective layer and innermost protective layer define the outer wall surface 4 and inner wall surface 5 of the winding core.
- the winding core has a wall comprised of nine layers, starting with the innermost layer 11 to the outermost layer 19 .
- the innermost 11 and outermost layers 19 are comprised of a composition with a high percentage of polymer resin, i.e., approximately sixty to eighty percent.
- the innermost 11 and outermost 19 layers act as sealers protecting the other layers from fraying damage.
- the thickness of each of these layers, i.e., innermost 11 and outermost 19 is approximately one hundredth to two hundredth inches in thickness.
- the outermost layer 19 defines the winding core wall exterior surface 4 and the innermost layer 11 defines the winding core inner surface 5 .
- next layers in i.e., second layer 12 and eighth layer 18
- second layer 12 and eighth layer 18 are comprised of woven fiberglass cloth with approximately equal amounts of fiber in the warp and fill directions. These layers have a lower resin content than the innermost 11 and outermost 19 layers.
- the thickness of each of these layers, i.e., second layer 12 and eighth layer 18 is approximately one hundredth to two hundredth inches in thickness and each contains approximately thirty to fifty percent resin.
- the second layer 12 and eighth layer 18 provide resistance to knife cuts and damage from core plugs.
- the third through seventh layers 13 - 17 are the structural layers providing resistance to longitudinal bending and radial crushing. Specifically, the third layer 13 and seventh layer 17 contain carbon fiber primarily oriented in the circumferential (hoop) direction. The third 13 and seventh 17 layers are each approximately one hundredth to two hundredth inches in thickness and each contains approximately twenty to forty percent resin. The purpose of the third 13 and seventh 17 layers is to provide extra resistance to crushing.
- the fourth layer 14 and sixth layer 16 contain glass fibers oriented in the circumferential (hoop) direction.
- the fourth 14 and sixth 16 layers are each approximately three hundredth to six hundredth inches in thickness and each contains approximately twenty to forty percent resin.
- the purpose of the fourth 14 and sixth 16 layers is to resist crushing.
- the middle layer 15 i.e., fifth layer, contains glass fibers primarily oriented in a longitudinal direction, i.e., parallel with a winding core longitudinal axis.
- the middle layer 15 is approximately four hundredth to eight hundredth inches in thickness and contains approximately twenty to forty percent resin.
- the purpose of the middle layer 15 is to resist longitudinal bending. Although this layer is described as the middle layer, it could actually be located at any layer position and provide equivalent resistance to longitudinal bending. However, in the preferred embodiment this layer is centered as the middle layer 15 within the wall thickness. In doing so, the crushing stiffness is maximized. If the fifth layer were placed at any other location, the bending and hoop properties of the tube would not be significantly changed, but the crush properties of the structure would be significantly adversely affected.
- Each layer is typically combined with wet resin, in the percentage ranges indicated above, as the layer is wound over a cylindrical tool commonly called a mandrel. After winding on the mandrel, the resin is cured at an elevated temperature to initiate cross-linking and provide a rigid structure.
- the resin that is typically used is a Bisphenol F or Bisphenol A epoxy resin combined with an anhydride type hardener. Other types of epoxy resin/hardeners combinations could work as well.
- the applicable resin systems include, but are not limited to, polyester resins, vinyl ester resins, phenolic resins, or other generally acceptable thermosetting resins suitable for use with filament winding equipment. Thermoplastic resins could also be used with some modifications to manufacturing equipment.
- the core could also be made with pre-impregnated materials.
- a pre-manufactured plastic or metal end cap 20 is mechanically or adhesively (or a combination of both) fastened to either end of the winding core providing further enhanced strength, stiffness and abuse resistance properties.
- the innermost 11 , outermost 19 , second 12 and eighth layers 18 are removed near the winding core end to be capped, and the cap 20 slid over the end of the winding core wall.
- a post-formed bead 22 may be formed on the outside portion 21 of the cap 20 to mechanically attach the cap 20 to the winding core 10 .
- a molded texture 9 could be formed on the outermost layer 19 of the winding core 10 to assist in gripping the tissue material during the start of a wind.
- the texture could also be sprayed or painted on.
- the invention winding core material is typically two to four times as great as that of a prior art fiber core
- the invention winding core for the example described above only requires a wall thickness of approximately one-fourth to one-half that of a typical fiber core.
- the invention core construction provides a resistance to both crushing and bending forces which is considerably greater than that of a prior art fiber core. This results in a winding core with superior crush and bending properties while weighing essentially the same as a prior art fiber core. Along with superior crush and bending properties comes substantially increased resistance to knife damage and abuse damage from winding and unwinding.
- a significant portion of this invention are the layers that comprise the structural portion of the winding core. These layers are identified with the reference numerals as 13 - 17 in FIG. 2. The orientation and location of the fibers is of paramount importance in these layers. It is preferably to have the fibers that resist longitudinal bending located in the center of the wall thickness and the fibers that resist crushing forces located as near to the inner and outer wall surfaces as possible. The remaining layers are essentially protective layers, though they do add a small amount of structural strength and stiffness.
- Fiber reinforced material is a preferred choice because the properties of fibers are inherently directional. Applicant has chosen to use primarily glass and carbon fibers in the example shown, but there are many other variable choices, including Kevlar, polyethylene, basalt, hemp, kenaf, and sisal, or other organic fibers.
- the material that holds the fibers of a fiber reinforced composite together is called the “matrix”.
- Applicants have chosen an epoxy resin as a preferred matrix.
- other materials that could serve as the matrix for this invention including other thermoset polymers like polyester or vinylester, or thermoplastic materials such as polyethylene.
Landscapes
- Storage Of Web-Like Or Filamentary Materials (AREA)
Abstract
A hybrid fiber reinforced polymer winding core consisting of several layers of different materials. The winding core layers are constructed so that structural reinforcing layers are sandwiched between outer protective layers. The outermost protective layer and innermost protective layer define the outer wall surface and inner wall surface of the winding core.
Description
- Applicant claims the priority benefits of U.S. Provisional Patent Application No. 60/472,608, filed May 22, 2003.
- This invention relates to web winding cores for use in winding web material such as tissue paper, paper toweling, and the like. More particularly, the invention is related to a fiber reinforced polymer winding core.
- The tissue making process entails winding the finished tissue product onto a cylindrical tube, commonly called a “core”. The core is supported by a mandrel that is inserted into the core. The mandrel rotates the winding core to a velocity with a surface speed that matches the linear speed of the tissue material moving through the end of the tissue machine. At the start of the winding process an adhesive is typically sprayed onto the winding core and the mandrel-driven winding core is brought into contact with the moving tissue material, which adheres to the winding core and begins to be wound onto the winding core. When tissue winding is complete, the tissue material is cut and the tissue-wound core is brought to a stop by the mandrel. A table or similar means is brought into support for the tissue-wound core and the mandrel is extracted from the core. The tissue-wound core is then either transported to a storage facility or to a converting machine for conversion, i.e., unwinding, transverse perforation and rewinding into commercial sized rolls.
- In the storage facility, the tissue-wound core may be stored either horizontally or vertically. On the converting machines, a plug is inserted into each end of the tissue-wound core. The tissue-wound core is then raised by a mechanical hoist attached to the plugs and lowered into the converting machine. In the converting machine, the plugs support the tissue-wound core as it is rotated to unwind most of the tissue material that was previously wound onto the core. The last several layers of tissue are discarded by cutting them off the core with a sharp knife. The knife often causes damage to the core. After the unwind operation, the core is transported back to the tissue machine where the winding process is repeated. During transportation, the core may be handled manually or with handling equipment.
- The vast majority of prior art winding cores used in tissue making and conversion are constructed from multiple layers of wood pulp fiber (sometimes called paper, board, core board or fiber) and glue that are wound together in a spiral fashion to form a cylindrical tube. Fiber cores can typically be reused on the order of 5-20 times before they are damaged to such an extent that they are no longer usable. Damage to the fiber cores is most commonly caused by storage of the tissue-wound core on its end. The end of the fiber core becomes distorted and crushed when the tissue-wound core is stored in a vertical orientation. After several reuses, the fiber core can become so distorted that the winding core will no longer fit over a mandrel or plugs will no longer fit into its ends. The fiber core is also commonly damaged through the cutting action of the knife that is used to remove the scrap tissue at the end of an unwind operation. During each cutting procedure, the knife penetrates several layers of the fiber core and makes a deep cut over the entire length of the core. After several reuses, the number of cuts becomes great enough that, when the winding core is rotated by the mandrel at high velocity just before the start of a wind operation, the fiber core may begin to delaminate and self-destruct. The integral wall thickness of the fiber core must be such that the winding core can withstand the centrifugal forces caused by high speed spinning and the structural forces caused by the weight of the tissue roll that the winding core must support.
- In the prior art fiberglass composite cores have been utilized in winding applications. However, for the large diameter cores used in winding tissue materials, a typical fiberglass core with adequate resistance to crushing forces imparted by a wound roll weighs considerably more than fiber cores. While a fiber core may weigh one hundred pounds, a comparable fiberglass core will weigh from two hundred to three hundred pounds. This creates safety as well as handling problems. The fiberglass cores used in the prior art for winding applications have been typically constructed from a number of layers of resin impregnated glass fiber wound at a substantially constant angle, i.e., usually 50 to 60 degrees from the axial direction, throughout the wall thickness of the core.
- The present invention provides a unique solution to the major drawbacks of prior art winding cores. The invention disclosed is a hybrid fiber reinforced polymer core consisting of several layers of different materials that, when combined in a specific sequence and in specific relative quantities, result in a winding core with characteristics superior to prior art cores. The invention winding core weighs approximately the same as fiber cores, but has significantly increased crush strength, crush stiffness, bending strength, bending stiffness, hoop strength, hoop stiffness, impact resistance, cut resistance, moisture resistance, and abuse tolerance. In summary, the present invention hybrid composite winding core has properties which have been specifically tailored to exhibit a high degree of stiffness, strength and resistance to abuse without increasing mass over the prior art. The present invention core is particularly useful when used in conjunction with large-scale tissue manufacturing operations.
- These together with other objects of the invention, along with various features of novelty which characterize the invention, are pointed out with particularity in this disclosure. For a better understanding of the invention, its operating advantages and the specific objects attained by its uses, reference should be had to the accompanying drawings and descriptive matter in which there is illustrated a preferred embodiment of the invention.
- FIG. 1 is a side view, partly in section, of a winding core constructed according to the present invention.
- FIG. 2 is a cross sectional side view of the portion of the winding core shown in FIG. 1 as
area 2. - FIG. 3 is a close up cross sectional view of an end cap.
- FIG. 4 is a perspective view of a winding core with textured outer surface.
- Referring to the drawings in detail wherein like elements are indicated by like numerals, there is shown a
winding core 10 constructed according to the principles of the invention. The invention example shown pertains to a core with a sixteen inch nominal inside diameter with a nominal length of one hundred inches. A prior art fiber core of this size would typically require a wall thickness of between five-eighths inches to three-quarters inches, and would weigh approximately one hundred pounds in order to provide adequate strength, stiffness and resistance to abuse. The invention winding core is not limited to this particular core size, but applies to cores of virtually any size. - The winding
core 10 of the present invention is constructed of multiple layers of polymer impregnated fibrous materials forming a cylindrically-shaped, hollow windingcore 10 with twoopen ends 2, awall 3 connecting bothends 2, saidwall 3 having anexterior surface 4 and aninner surface 5. Thewall 3 is comprised of said layers. The wall layers are formed preferably through filament winding, but could also be formed other known manufacturing methods, including by hand by means of a roll table. The winding core layers are constructed so that structural reinforcing layers are sandwiched between outer protective layers. The outermost protective layer and innermost protective layer define theouter wall surface 4 andinner wall surface 5 of the winding core. - In a preferred embodiment shown in the drawings the winding core has a wall comprised of nine layers, starting with the innermost layer11 to the
outermost layer 19. The innermost 11 andoutermost layers 19 are comprised of a composition with a high percentage of polymer resin, i.e., approximately sixty to eighty percent. The innermost 11 and outermost 19 layers act as sealers protecting the other layers from fraying damage. The thickness of each of these layers, i.e., innermost 11 and outermost 19, is approximately one hundredth to two hundredth inches in thickness. Theoutermost layer 19 defines the winding core wallexterior surface 4 and the innermost layer 11 defines the winding coreinner surface 5. - The next layers in, i.e., second layer12 and
eighth layer 18, are comprised of woven fiberglass cloth with approximately equal amounts of fiber in the warp and fill directions. These layers have a lower resin content than the innermost 11 and outermost 19 layers. The thickness of each of these layers, i.e., second layer 12 andeighth layer 18, is approximately one hundredth to two hundredth inches in thickness and each contains approximately thirty to fifty percent resin. The second layer 12 andeighth layer 18 provide resistance to knife cuts and damage from core plugs. - The third through seventh layers13-17 are the structural layers providing resistance to longitudinal bending and radial crushing. Specifically, the
third layer 13 andseventh layer 17 contain carbon fiber primarily oriented in the circumferential (hoop) direction. The third 13 and seventh 17 layers are each approximately one hundredth to two hundredth inches in thickness and each contains approximately twenty to forty percent resin. The purpose of the third 13 and seventh 17 layers is to provide extra resistance to crushing. - The
fourth layer 14 andsixth layer 16 contain glass fibers oriented in the circumferential (hoop) direction. The fourth 14 and sixth 16 layers are each approximately three hundredth to six hundredth inches in thickness and each contains approximately twenty to forty percent resin. The purpose of the fourth 14 and sixth 16 layers is to resist crushing. - The
middle layer 15, i.e., fifth layer, contains glass fibers primarily oriented in a longitudinal direction, i.e., parallel with a winding core longitudinal axis. Themiddle layer 15 is approximately four hundredth to eight hundredth inches in thickness and contains approximately twenty to forty percent resin. The purpose of themiddle layer 15 is to resist longitudinal bending. Although this layer is described as the middle layer, it could actually be located at any layer position and provide equivalent resistance to longitudinal bending. However, in the preferred embodiment this layer is centered as themiddle layer 15 within the wall thickness. In doing so, the crushing stiffness is maximized. If the fifth layer were placed at any other location, the bending and hoop properties of the tube would not be significantly changed, but the crush properties of the structure would be significantly adversely affected. - Each layer is typically combined with wet resin, in the percentage ranges indicated above, as the layer is wound over a cylindrical tool commonly called a mandrel. After winding on the mandrel, the resin is cured at an elevated temperature to initiate cross-linking and provide a rigid structure. The resin that is typically used is a Bisphenol F or Bisphenol A epoxy resin combined with an anhydride type hardener. Other types of epoxy resin/hardeners combinations could work as well. The applicable resin systems include, but are not limited to, polyester resins, vinyl ester resins, phenolic resins, or other generally acceptable thermosetting resins suitable for use with filament winding equipment. Thermoplastic resins could also be used with some modifications to manufacturing equipment. The core could also be made with pre-impregnated materials.
- In another embodiment of the invention, a pre-manufactured plastic or
metal end cap 20 is mechanically or adhesively (or a combination of both) fastened to either end of the winding core providing further enhanced strength, stiffness and abuse resistance properties. In the example shown, the innermost 11, outermost 19, second 12 andeighth layers 18 are removed near the winding core end to be capped, and thecap 20 slid over the end of the winding core wall. Apost-formed bead 22 may be formed on theoutside portion 21 of thecap 20 to mechanically attach thecap 20 to the windingcore 10. - In another embodiment of the invention, a molded
texture 9 could be formed on theoutermost layer 19 of the windingcore 10 to assist in gripping the tissue material during the start of a wind. The texture could also be sprayed or painted on. - While the mass density of the invention winding core material is typically two to four times as great as that of a prior art fiber core, the invention winding core for the example described above only requires a wall thickness of approximately one-fourth to one-half that of a typical fiber core. The invention core construction provides a resistance to both crushing and bending forces which is considerably greater than that of a prior art fiber core. This results in a winding core with superior crush and bending properties while weighing essentially the same as a prior art fiber core. Along with superior crush and bending properties comes substantially increased resistance to knife damage and abuse damage from winding and unwinding.
- It is understood that the above-described embodiment is merely illustrative of the application. Other embodiments may be readily devised by those skilled in the art which will embody the principles of the invention and fall within the spirit and scope thereof. A significant portion of this invention are the layers that comprise the structural portion of the winding core. These layers are identified with the reference numerals as13-17 in FIG. 2. The orientation and location of the fibers is of paramount importance in these layers. It is preferably to have the fibers that resist longitudinal bending located in the center of the wall thickness and the fibers that resist crushing forces located as near to the inner and outer wall surfaces as possible. The remaining layers are essentially protective layers, though they do add a small amount of structural strength and stiffness.
- Making the structural layers from a fiber reinforced material is a preferred choice because the properties of fibers are inherently directional. Applicant has chosen to use primarily glass and carbon fibers in the example shown, but there are many other variable choices, including Kevlar, polyethylene, basalt, hemp, kenaf, and sisal, or other organic fibers.
- The material that holds the fibers of a fiber reinforced composite together is called the “matrix”. Applicants have chosen an epoxy resin as a preferred matrix. However, there are many other materials that could serve as the matrix for this invention including other thermoset polymers like polyester or vinylester, or thermoplastic materials such as polyethylene.
Claims (14)
1. A hybrid, fiber reinforced, polymer, web winding core for use in winding web material, comprising:
a cylindrical, hollow winding core wall having two ends, said two ends defining a winding core longitudinal axis, said wall having an exterior surface and an inner surface, said exterior surface and inner surface defining a wall thickness, said wall being comprised of a plurality of layers made from fiber reinforced material, said plurality of layers having a plurality of structural reinforcing layers sandwiched between a plurality of outer protective layers, said plurality of structural reinforcing layers adapted to provide resistance to longitudinal bending and radial crushing, said outer protective layers having an outermost protective layer defining the wall exterior surface and an innermost protective layer defining the wall inner surface.
2. A winding core as recited in claim 1 , wherein:
a plurality of the plurality of structural reinforcing layers contains material with fibers primarily oriented in a longitudinal direction parallel with the winding core longitudinal axis, said layer adapted to resist longitudinal bending.
3. A winding core as recited in claim 2 , wherein:
a plurality of the plurality of structural reinforcing layers contains material with fibers primarily oriented in a circumferential direction, said layers adapted to resist crushing.
4. A winding core as recited in claim 3 , wherein:
said plurality of layers containing material with fibers primarily oriented in a longitudinal direction are located in the center of the wall thickness; and
said plurality of layers containing material with fibers primarily oriented in a circumferential direction are located near to the inner and outer wall surfaces.
5. A winding core as recited in claim 4 , further comprising:
an end cap slidably positioned over and fastened to each end of the winding core wall.
6. A winding core as recited in claim 5 , further comprising:
a molded texture formed on said outermost protective layer.
7. A winding core as recited in claim 6 , wherein:
said fiber reinforced material is held in a matrix formed from the following classes of materials:
thermoset polymers such as epoxy resins, polyester resins, or vinyl ester resins, phenolic resins and thermoplastic resins.
8. A winding core as recited in claim 7 , wherein:
said fiber reinforced material contain fibers made from the following classes of materials: glass, carbon, Kevlar, polyethylene, basalt, hemp, kenaf, and sisal.
9. A winding core as recited in claim 8 , wherein:
said plurality of layers containing material with fibers primarily oriented in a longitudinal direction contain glass fibers in a matrix containing twenty to forty percent resin.
10. A winding core as recited in claim 9 , wherein:
a plurality of layers containing material with fibers primarily oriented in a circumferential direction contain carbon fibers in a matrix containing twenty to forty percent resin.
11. A winding core as recited in claim 10 , wherein:
a plurality of layers containing material with fibers primarily oriented in a circumferential direction contain glass fibers in a matrix containing twenty to forty percent resin.
12. A winding core as recited in claim 11 , wherein:
the outermost and innermost protective layers are comprised of a composition with sixty to eighty percent polymer resin, said innermost and outermost protective layers adapted to act as sealers protecting the other layers from fraying damage.
13. A winding core as recited in claim 12 , wherein:
a plurality of protective layers being comprised of woven fiberglass cloth with approximately equal amounts of fiber in warp and fill directions, said protective layers containing thirty to fifty percent resin.
14. A winding core as recited in claim 13 , wherein:
a portion of said outer protective layers are removed near the winding core end and said cap positioned over that portion of the winding core wall without the outer protective layers.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US10/850,951 US20040232274A1 (en) | 2003-05-22 | 2004-05-21 | Fiber reinforced hybrid composite winding core |
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US47260803P | 2003-05-22 | 2003-05-22 | |
US10/850,951 US20040232274A1 (en) | 2003-05-22 | 2004-05-21 | Fiber reinforced hybrid composite winding core |
Publications (1)
Publication Number | Publication Date |
---|---|
US20040232274A1 true US20040232274A1 (en) | 2004-11-25 |
Family
ID=33457361
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
US10/850,951 Abandoned US20040232274A1 (en) | 2003-05-22 | 2004-05-21 | Fiber reinforced hybrid composite winding core |
Country Status (1)
Country | Link |
---|---|
US (1) | US20040232274A1 (en) |
Cited By (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US20050184191A1 (en) * | 2004-02-25 | 2005-08-25 | Sonoco Development, Inc. | Winding core and associated method |
WO2006062852A1 (en) * | 2004-12-06 | 2006-06-15 | Sonoco Development, Inc. | High-stiffness winding core |
WO2007015092A1 (en) * | 2005-08-04 | 2007-02-08 | Ultra-Core Ltd. | Web-winding core |
US20070059505A1 (en) * | 2005-09-12 | 2007-03-15 | Ford Global Technologies, Llc | A method for forming molding compounds and articles therefrom |
US20160153080A1 (en) * | 2014-12-01 | 2016-06-02 | Inometa Gmbh & Co. Kg | Method for producing a coated component and a coated component |
US11370628B1 (en) | 2021-10-15 | 2022-06-28 | Abzac Canada Inc. | Convolute cardboard tube, apparatus and method for manufacturing the same |
Citations (15)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US1560192A (en) * | 1925-05-12 | 1925-11-03 | Ewen M Allan | Core tip |
US1648399A (en) * | 1925-10-12 | 1927-11-08 | Cons Water Power & Paper Co | Core tip |
US1651705A (en) * | 1927-02-05 | 1927-12-06 | Cons Water Power & Paper Co | Core tip |
US1687586A (en) * | 1927-04-16 | 1928-10-16 | Brown Co | Fiber core |
US1929035A (en) * | 1932-11-22 | 1933-10-03 | Elixman Paper Core Co Inc | End cap for paper cores |
US1929034A (en) * | 1932-11-22 | 1933-10-03 | Elixman Paper Core Co Inc | End cap for paper cores |
US1929033A (en) * | 1932-04-01 | 1933-10-03 | Elixman Paper Core Co Inc | End cap for paper cores |
US1929036A (en) * | 1932-11-22 | 1933-10-03 | Elixman Paper Core Co Inc | End cap for paper cores |
US3451639A (en) * | 1966-07-12 | 1969-06-24 | Dyson Kissner Corp | Textile tube |
US5236141A (en) * | 1992-03-25 | 1993-08-17 | Kewin Daniel D | Tubular core assemblies for rolls of paper or other sheet material |
US5393582A (en) * | 1993-06-04 | 1995-02-28 | Sonoco Products Company | Enhanced crush strength construction multi-grade paperboard tubes |
US5505395A (en) * | 1993-06-04 | 1996-04-09 | Sonoco Products Company | Multi-grade paperboard winding cores for yarns and films having enhanced resistance to inside diameter reduction |
US5908173A (en) * | 1996-01-10 | 1999-06-01 | Agfa-Gevaert | Winding core |
US20020066824A1 (en) * | 2000-12-01 | 2002-06-06 | Floyd, Arnold B. | Composite core |
US6405974B1 (en) * | 1998-08-12 | 2002-06-18 | F. John Herrington | Ribbed core dual wall structure |
-
2004
- 2004-05-21 US US10/850,951 patent/US20040232274A1/en not_active Abandoned
Patent Citations (15)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US1560192A (en) * | 1925-05-12 | 1925-11-03 | Ewen M Allan | Core tip |
US1648399A (en) * | 1925-10-12 | 1927-11-08 | Cons Water Power & Paper Co | Core tip |
US1651705A (en) * | 1927-02-05 | 1927-12-06 | Cons Water Power & Paper Co | Core tip |
US1687586A (en) * | 1927-04-16 | 1928-10-16 | Brown Co | Fiber core |
US1929033A (en) * | 1932-04-01 | 1933-10-03 | Elixman Paper Core Co Inc | End cap for paper cores |
US1929034A (en) * | 1932-11-22 | 1933-10-03 | Elixman Paper Core Co Inc | End cap for paper cores |
US1929035A (en) * | 1932-11-22 | 1933-10-03 | Elixman Paper Core Co Inc | End cap for paper cores |
US1929036A (en) * | 1932-11-22 | 1933-10-03 | Elixman Paper Core Co Inc | End cap for paper cores |
US3451639A (en) * | 1966-07-12 | 1969-06-24 | Dyson Kissner Corp | Textile tube |
US5236141A (en) * | 1992-03-25 | 1993-08-17 | Kewin Daniel D | Tubular core assemblies for rolls of paper or other sheet material |
US5393582A (en) * | 1993-06-04 | 1995-02-28 | Sonoco Products Company | Enhanced crush strength construction multi-grade paperboard tubes |
US5505395A (en) * | 1993-06-04 | 1996-04-09 | Sonoco Products Company | Multi-grade paperboard winding cores for yarns and films having enhanced resistance to inside diameter reduction |
US5908173A (en) * | 1996-01-10 | 1999-06-01 | Agfa-Gevaert | Winding core |
US6405974B1 (en) * | 1998-08-12 | 2002-06-18 | F. John Herrington | Ribbed core dual wall structure |
US20020066824A1 (en) * | 2000-12-01 | 2002-06-06 | Floyd, Arnold B. | Composite core |
Cited By (9)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US20050184191A1 (en) * | 2004-02-25 | 2005-08-25 | Sonoco Development, Inc. | Winding core and associated method |
WO2006062852A1 (en) * | 2004-12-06 | 2006-06-15 | Sonoco Development, Inc. | High-stiffness winding core |
US20060163420A1 (en) * | 2004-12-06 | 2006-07-27 | Sonoco Development, Inc. | High-stiffness winding core |
WO2007015092A1 (en) * | 2005-08-04 | 2007-02-08 | Ultra-Core Ltd. | Web-winding core |
US20070059505A1 (en) * | 2005-09-12 | 2007-03-15 | Ford Global Technologies, Llc | A method for forming molding compounds and articles therefrom |
US7968024B2 (en) * | 2005-09-12 | 2011-06-28 | Ford Global Technologies, Llc | Method for forming molding compounds and articles therefrom |
US20160153080A1 (en) * | 2014-12-01 | 2016-06-02 | Inometa Gmbh & Co. Kg | Method for producing a coated component and a coated component |
US11370628B1 (en) | 2021-10-15 | 2022-06-28 | Abzac Canada Inc. | Convolute cardboard tube, apparatus and method for manufacturing the same |
US12071317B2 (en) | 2021-10-15 | 2024-08-27 | Abzac Canada Inc. | Convolute cardboard tube, apparatus and method for manufacturing the same |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
US5188872A (en) | Composite structural member with high bending strength | |
USRE35081E (en) | Composite structural member with high bending strength | |
EP0487549B1 (en) | Composite structural member with high bending strength and method of manufacture | |
US4131701A (en) | Composite tubular elements | |
US4242160A (en) | Method of winding a wind turbine blade using a filament reinforced mandrel | |
CA1231883A (en) | Method of manufacturing a shape from a composite material and shapes manufactured in accordance with the method | |
US6586110B1 (en) | Contoured metal structural members and methods for making the same | |
US20090218435A1 (en) | Web-Winding Core | |
EP1301339A1 (en) | Contoured crushable composite structural members and methods for making the same | |
US5167994A (en) | Reusable core for paper rolls | |
US20040232274A1 (en) | Fiber reinforced hybrid composite winding core | |
EP2616375B1 (en) | Web-winding core | |
US4685241A (en) | Graphite fiber fishing rod | |
KR100298101B1 (en) | Fiber Reinforced Composite Material | |
EP0370147A1 (en) | Tubular composite construction | |
US20040052986A1 (en) | Reinforced paperboard tube | |
JPH085591B2 (en) | Carbon fiber reinforced plastic roll | |
JPS5953167B2 (en) | Manufacturing method of fiber reinforced plastic | |
JP3156130B2 (en) | Composite structural member having high bending strength and manufacturing method | |
JPH07102858B2 (en) | Composite tubular material | |
JPH0552264B2 (en) | ||
WO2024116982A1 (en) | Rotating electrical machine protection ring, method for producing same, rotating electrical machine, and electric mobility device | |
WO2024116983A1 (en) | Rotating electric machine protective ring, manufacturing method thereof, rotating electric machine , and electrically-driven mobility equipment | |
CA2211805A1 (en) | Rotors | |
JPH09262832A (en) | Prepreg |
Legal Events
Date | Code | Title | Description |
---|---|---|---|
STCB | Information on status: application discontinuation |
Free format text: ABANDONED -- FAILURE TO RESPOND TO AN OFFICE ACTION |