WO1991003378A1 - Thermoplastic honeycomb and methods of preparation - Google Patents
Thermoplastic honeycomb and methods of preparation Download PDFInfo
- Publication number
- WO1991003378A1 WO1991003378A1 PCT/US1990/005037 US9005037W WO9103378A1 WO 1991003378 A1 WO1991003378 A1 WO 1991003378A1 US 9005037 W US9005037 W US 9005037W WO 9103378 A1 WO9103378 A1 WO 9103378A1
- Authority
- WO
- WIPO (PCT)
- Prior art keywords
- thermoplastic
- open
- polymer
- cell grid
- laminated structure
- Prior art date
Links
- 229920001169 thermoplastic Polymers 0.000 title claims abstract description 18
- 239000004416 thermosoftening plastic Substances 0.000 title claims abstract description 7
- 238000000034 method Methods 0.000 title claims description 24
- 238000002360 preparation method Methods 0.000 title description 3
- 239000002904 solvent Substances 0.000 claims abstract description 27
- 239000000835 fiber Substances 0.000 claims abstract description 10
- 239000012815 thermoplastic material Substances 0.000 claims abstract description 7
- 230000015572 biosynthetic process Effects 0.000 claims abstract description 5
- 239000003365 glass fiber Substances 0.000 claims abstract description 4
- 229920000642 polymer Polymers 0.000 claims description 19
- 239000002243 precursor Substances 0.000 claims description 15
- 238000006243 chemical reaction Methods 0.000 claims description 12
- 239000004744 fabric Substances 0.000 claims description 12
- ZMXDDKWLCZADIW-UHFFFAOYSA-N N,N-Dimethylformamide Chemical compound CN(C)C=O ZMXDDKWLCZADIW-UHFFFAOYSA-N 0.000 claims description 6
- 238000000576 coating method Methods 0.000 claims description 6
- 239000011248 coating agent Substances 0.000 claims description 5
- IAZDPXIOMUYVGZ-UHFFFAOYSA-N Dimethylsulphoxide Chemical compound CS(C)=O IAZDPXIOMUYVGZ-UHFFFAOYSA-N 0.000 claims description 4
- SECXISVLQFMRJM-UHFFFAOYSA-N N-Methylpyrrolidone Chemical compound CN1CCCC1=O SECXISVLQFMRJM-UHFFFAOYSA-N 0.000 claims description 4
- 239000002253 acid Substances 0.000 claims description 4
- KZTYYGOKRVBIMI-UHFFFAOYSA-N diphenyl sulfone Chemical compound C=1C=CC=CC=1S(=O)(=O)C1=CC=CC=C1 KZTYYGOKRVBIMI-UHFFFAOYSA-N 0.000 claims description 4
- 238000010438 heat treatment Methods 0.000 claims description 3
- SRPWOOOHEPICQU-UHFFFAOYSA-N trimellitic anhydride Chemical compound OC(=O)C1=CC=C2C(=O)OC(=O)C2=C1 SRPWOOOHEPICQU-UHFFFAOYSA-N 0.000 claims description 3
- MQJKPEGWNLWLTK-UHFFFAOYSA-N Dapsone Chemical compound C1=CC(N)=CC=C1S(=O)(=O)C1=CC=C(N)C=C1 MQJKPEGWNLWLTK-UHFFFAOYSA-N 0.000 claims description 2
- FXHOOIRPVKKKFG-UHFFFAOYSA-N N,N-Dimethylacetamide Chemical compound CN(C)C(C)=O FXHOOIRPVKKKFG-UHFFFAOYSA-N 0.000 claims description 2
- RLSSMJSEOOYNOY-UHFFFAOYSA-N m-cresol Chemical compound CC1=CC=CC(O)=C1 RLSSMJSEOOYNOY-UHFFFAOYSA-N 0.000 claims 2
- 229920005989 resin Polymers 0.000 abstract description 41
- 239000011347 resin Substances 0.000 abstract description 41
- 238000007598 dipping method Methods 0.000 abstract description 8
- CSCPPACGZOOCGX-UHFFFAOYSA-N Acetone Chemical compound CC(C)=O CSCPPACGZOOCGX-UHFFFAOYSA-N 0.000 description 9
- 239000000463 material Substances 0.000 description 7
- 238000004519 manufacturing process Methods 0.000 description 5
- -1 poly(butylene terephthalate) Polymers 0.000 description 4
- 239000007787 solid Substances 0.000 description 4
- 229920005992 thermoplastic resin Polymers 0.000 description 4
- XEKOWRVHYACXOJ-UHFFFAOYSA-N Ethyl acetate Chemical compound CCOC(C)=O XEKOWRVHYACXOJ-UHFFFAOYSA-N 0.000 description 3
- 239000003085 diluting agent Substances 0.000 description 3
- 239000004033 plastic Substances 0.000 description 3
- 229920003023 plastic Polymers 0.000 description 3
- 229920005575 poly(amic acid) Polymers 0.000 description 3
- DLFVBJFMPXGRIB-UHFFFAOYSA-N Acetamide Chemical compound CC(N)=O DLFVBJFMPXGRIB-UHFFFAOYSA-N 0.000 description 2
- FZERHIULMFGESH-UHFFFAOYSA-N N-phenylacetamide Chemical compound CC(=O)NC1=CC=CC=C1 FZERHIULMFGESH-UHFFFAOYSA-N 0.000 description 2
- 239000002131 composite material Substances 0.000 description 2
- JHIVVAPYMSGYDF-UHFFFAOYSA-N cyclohexanone Chemical compound O=C1CCCCC1 JHIVVAPYMSGYDF-UHFFFAOYSA-N 0.000 description 2
- 238000005470 impregnation Methods 0.000 description 2
- 239000000203 mixture Substances 0.000 description 2
- 239000003495 polar organic solvent Substances 0.000 description 2
- 239000000047 product Substances 0.000 description 2
- 230000002787 reinforcement Effects 0.000 description 2
- 229920001187 thermosetting polymer Polymers 0.000 description 2
- JJHHIJFTHRNPIK-UHFFFAOYSA-N Diphenyl sulfoxide Chemical compound C=1C=CC=CC=1S(=O)C1=CC=CC=C1 JJHHIJFTHRNPIK-UHFFFAOYSA-N 0.000 description 1
- 239000004593 Epoxy Substances 0.000 description 1
- BRDWIEOJOWJCLU-LTGWCKQJSA-N GS-441524 Chemical compound C=1C=C2C(N)=NC=NN2C=1[C@]1(C#N)O[C@H](CO)[C@@H](O)[C@H]1O BRDWIEOJOWJCLU-LTGWCKQJSA-N 0.000 description 1
- 239000004952 Polyamide Substances 0.000 description 1
- 229960001413 acetanilide Drugs 0.000 description 1
- 150000007513 acids Chemical class 0.000 description 1
- 239000000654 additive Substances 0.000 description 1
- 230000000996 additive effect Effects 0.000 description 1
- 239000000853 adhesive Substances 0.000 description 1
- 230000001070 adhesive effect Effects 0.000 description 1
- 125000000217 alkyl group Chemical group 0.000 description 1
- 150000004945 aromatic hydrocarbons Chemical class 0.000 description 1
- 125000003710 aryl alkyl group Chemical group 0.000 description 1
- 125000003118 aryl group Chemical group 0.000 description 1
- 125000001797 benzyl group Chemical group [H]C1=C([H])C([H])=C(C([H])=C1[H])C([H])([H])* 0.000 description 1
- 238000003490 calendering Methods 0.000 description 1
- 239000000919 ceramic Substances 0.000 description 1
- 230000001427 coherent effect Effects 0.000 description 1
- 238000005520 cutting process Methods 0.000 description 1
- LTYMSROWYAPPGB-UHFFFAOYSA-N diphenyl sulfide Chemical compound C=1C=CC=CC=1SC1=CC=CC=C1 LTYMSROWYAPPGB-UHFFFAOYSA-N 0.000 description 1
- 238000004924 electrostatic deposition Methods 0.000 description 1
- 230000008020 evaporation Effects 0.000 description 1
- 238000001704 evaporation Methods 0.000 description 1
- 239000012467 final product Substances 0.000 description 1
- 238000013467 fragmentation Methods 0.000 description 1
- 238000006062 fragmentation reaction Methods 0.000 description 1
- 230000004927 fusion Effects 0.000 description 1
- 239000003292 glue Substances 0.000 description 1
- 239000007788 liquid Substances 0.000 description 1
- 238000011068 loading method Methods 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 125000001624 naphthyl group Chemical group 0.000 description 1
- 239000004745 nonwoven fabric Substances 0.000 description 1
- 125000001997 phenyl group Chemical group [H]C1=C([H])C([H])=C(*)C([H])=C1[H] 0.000 description 1
- XMGMFRIEKMMMSU-UHFFFAOYSA-N phenylmethylbenzene Chemical group C=1C=CC=CC=1[C]C1=CC=CC=C1 XMGMFRIEKMMMSU-UHFFFAOYSA-N 0.000 description 1
- 229920002647 polyamide Polymers 0.000 description 1
- 229920001707 polybutylene terephthalate Polymers 0.000 description 1
- 229920000515 polycarbonate Polymers 0.000 description 1
- 239000004417 polycarbonate Substances 0.000 description 1
- 238000010094 polymer processing Methods 0.000 description 1
- 229920006324 polyoxymethylene Polymers 0.000 description 1
- 229920006380 polyphenylene oxide Polymers 0.000 description 1
- 239000000843 powder Substances 0.000 description 1
- 238000001556 precipitation Methods 0.000 description 1
- 230000002028 premature Effects 0.000 description 1
- HNJBEVLQSNELDL-UHFFFAOYSA-N pyrrolidin-2-one Chemical compound O=C1CCCN1 HNJBEVLQSNELDL-UHFFFAOYSA-N 0.000 description 1
- 238000005096 rolling process Methods 0.000 description 1
- 238000002791 soaking Methods 0.000 description 1
- 239000000126 substance Substances 0.000 description 1
- 230000002195 synergetic effect Effects 0.000 description 1
- 229920002994 synthetic fiber Polymers 0.000 description 1
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 description 1
- 239000002759 woven fabric Substances 0.000 description 1
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29B—PREPARATION OR PRETREATMENT OF THE MATERIAL TO BE SHAPED; MAKING GRANULES OR PREFORMS; RECOVERY OF PLASTICS OR OTHER CONSTITUENTS OF WASTE MATERIAL CONTAINING PLASTICS
- B29B15/00—Pretreatment of the material to be shaped, not covered by groups B29B7/00 - B29B13/00
- B29B15/08—Pretreatment of the material to be shaped, not covered by groups B29B7/00 - B29B13/00 of reinforcements or fillers
- B29B15/10—Coating or impregnating independently of the moulding or shaping step
-
- 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
- B32B5/22—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 the presence of two or more layers which are next to each other and are fibrous, filamentary, formed of particles or foamed
- B32B5/24—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 the presence of two or more layers which are next to each other and are fibrous, filamentary, formed of particles or foamed one layer being a fibrous or filamentary layer
- B32B5/26—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 the presence of two or more layers which are next to each other and are fibrous, filamentary, formed of particles or foamed one layer being a fibrous or filamentary layer another layer next to it also being fibrous or filamentary
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29B—PREPARATION OR PRETREATMENT OF THE MATERIAL TO BE SHAPED; MAKING GRANULES OR PREFORMS; RECOVERY OF PLASTICS OR OTHER CONSTITUENTS OF WASTE MATERIAL CONTAINING PLASTICS
- B29B15/00—Pretreatment of the material to be shaped, not covered by groups B29B7/00 - B29B13/00
- B29B15/08—Pretreatment of the material to be shaped, not covered by groups B29B7/00 - B29B13/00 of reinforcements or fillers
- B29B15/10—Coating or impregnating independently of the moulding or shaping step
- B29B15/105—Coating or impregnating independently of the moulding or shaping step of reinforcement of definite length with a matrix in solid form, e.g. powder, fibre or sheet form
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29D—PRODUCING PARTICULAR ARTICLES FROM PLASTICS OR FROM SUBSTANCES IN A PLASTIC STATE
- B29D99/00—Subject matter not provided for in other groups of this subclass
- B29D99/0089—Producing honeycomb structures
-
- 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
- B32B37/00—Methods or apparatus for laminating, e.g. by curing or by ultrasonic bonding
- B32B37/14—Methods or apparatus for laminating, e.g. by curing or by ultrasonic bonding characterised by the properties of the layers
- B32B37/146—Methods or apparatus for laminating, e.g. by curing or by ultrasonic bonding characterised by the properties of the layers whereby one or more of the layers is 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
- B32B38/00—Ancillary operations in connection with laminating processes
- B32B38/08—Impregnating
-
- 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
- B32B2260/00—Layered product comprising an impregnated, embedded, or bonded layer wherein the layer comprises an impregnation, embedding, or binder material
- B32B2260/02—Composition of the impregnated, bonded or embedded layer
- B32B2260/021—Fibrous or filamentary layer
- B32B2260/023—Two or more layers
-
- 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
- B32B2260/00—Layered product comprising an impregnated, embedded, or bonded layer wherein the layer comprises an impregnation, embedding, or binder material
- B32B2260/04—Impregnation, embedding, or binder material
- B32B2260/046—Synthetic resin
-
- 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
- B32B2305/00—Condition, form or state of the layers or laminate
- B32B2305/02—Cellular or porous
- B32B2305/024—Honeycomb
Definitions
- This invention lies in the fields of honeycomb structures and polymer processing techniques.
- the particular area addressed by this invention is that relating to honeycomb structures formed of fabric-reinforced polymer.
- Honeycomb has long been known for use in structural elements where a combination of lightness and strength are desirable.
- nonmetallic materials such as ceramics and plastics offers additional advantages in terms of processing characteristics and the appearance and properties of the final product.
- Thermoset plastics have been used in the manufacture of honeycomb, by fusing together corrugated ribbons of the plastic as well as by fusing together ribbons of fabric impregnated with thermosetting resin prior to the final cure. Difficulties with such materials include limitations on the manufacturing techniques, as well as minimal damage resistance with the result that the product is highly susceptible to damage during fabrication and lay-up, as well as fragmentation upon handling.
- honeycomb structures can be prepared which have the strength, impact resistance and processing characteristics of thermoplastic materials and yet offer high temperature resistance and solvent resistance characteristics which permit such processing steps as the application of multiple coatings for purposes of density adjustment and the formation of composite layers.
- a thermoplastic resin which has a soluble form and can be converted to an insoluble form.
- a fiber web is initially impregnated with the resin in its soluble form, using any of a variety of techniques, thereby fusing the fibers together into a stable coherent structure.
- the resulting impregnated web in the form of ribbons or sheets, is arranged in a stack, in which adjacent ribbons or sheets are fused together along transverse node lines to render the stack expandable into the open-cell structure which forms the honeycomb, the expansion facilitated by heating the stack up to the softening point of the resin.
- the thermoplastic character of the insoluble resin permits this expansion to occur without damage to the resin, and the character of being insoluble permits further applications of the resin subsequent to the initial expansion.
- the soluble form of the resin permits these applications to be made by dipping the expanded structure in a solution of the resin followed by removal of the solvent and conversion to the insoluble form. Expansion can be done in stages, with further applications of resin in between each stage.
- the technique can also be used to apply layers of different resins or coating materials to form for example a composite structure with a specified combination of properties.
- the initial impregnation is also done by dipping the fiber web in a solution of the resin in its soluble form.
- the present invention has wide applicability in terms of the types of honeycomb which can be formed and the various procedural steps and different types and numbers of layers to be applied as well as the means by which they are applied.
- the invention is of particular interest however as applied to thermoplastic-impregnated fabric in unexpanded stacks of ribbons or sheets which are then expanded into open-cell honeycomb panels to which further thermoplastic resin is applied by dipping the expanded honeycomb into a solution of the resin.
- a wide variety of resins can be used, subject to the description in the preceding section. The choice of resin can thus depend on the choice of solvents.
- the resin serving as the fabric impregnant may be the same as or different than the resin ' in the dip solution, and where more than one dip solution is used, the resins in the solutions themselves may be the same or different.
- the resins must be compatible with each other. Compatibility in this context denotes the tendency of two resins to fuse together as one cures over a cured layer of the other, to the extent that the two are not easily separated by physical or mechanical means. The combining of two or more resins in this fashion permits the formation of hybrid structures and the achievement of useful as well as synergistic properties.
- the resin serving as the fabric impregnant may be one which is applied in the same manner as the subsequent resin layers, i.e., by dipping followed by solvent removal and thermal conversion to a state permitting further processing.
- the fabric impregnant may be applied by other techniques known to those skilled in the art. Examples of other techniques are electrostatic deposition of the resin directly onto the fiber web in dry powder form followed by thermal fusion, and hot calendering of the resin in solid form directly onto the fabric.
- thermoplastic resins which are soluble in a given solvent but which are capable of thermal conversion to a form which is insoluble in the same solvent.
- thermal conversion and related terms are used herein to denote a chemical reaction, such as curing or chain lengthening, which occurs at elevated temperature. Any thermoplastic resin which meets this description may be used.
- thermoplastic polymers may be used as the resins.
- examples include polyamides, poly(amide- imide) ⁇ , polyacetals, polycarbonates, poly(butylene terephthalate)s, poly(phenylene oxide)s and poly(phenylene sulphoxide)s.
- Preferred polymers for both the initial fabric impregnant and the dipping solution(s) are poly(amide-imides) , particularly those of the following formula
- R is alkyl, preferably C,-C 6 , straight-chain or branched-chain; aryl, preferably phenyl, naphthyl, diphenyl sulfide, diphenyl sulfoxide or diphenyl sulfone; or aryl-alkyl combinations such as benzyl and diphenylmethylene.
- the formula shown above represents the polymer in reacted form, insoluble in any of a variety of polar organic solvents.
- the prepolymer is any precursor form of the above which is soluble in the same solvents.
- the precursor may be a partially polymerized analogue of the insoluble polymer, particularly one with a sufficient number of free acid groups remaining which render it solubEe.
- One possibility for the precursor is a poly(amic acid) represented by the formula
- a particularly preferred polymer within the scope of formula I above is one represented by the formula
- This poly(amic acid) is formed by the reaction between diamino diphenyl sulfone and trimellitic anhydride.
- Preferred poly(amic acids) within this formula as well as precursors in general to the polymer of formula II above are those having an acid number ranging from about 50 to about 100 when dissolved in a solvent as a 25% solution by weight.
- a prepolymer which has been found to be particularly effective i a product defined as AI-10 Polymer, supplied by Amoco Chemical Corporation, Chicago, Illinois, which undergoes conversion at temperatures of 350°F and above.
- the choice of solvent is not critical and may vary widely, provided that it dissolves the resin prior to its conversion to the insoluble state.
- Polar organic solvents are preferred, and examples are dimethylformamide, dimethylacetamide, dimethyl sulfoxide, N-methylpyrrolidone and j ⁇ -cresol.
- the properties of the solution may be modified by the use of a diluent, which may be any liquid which is miscibl with the solvent, does not cause premature precipitation of th unconverted resin, and yet does not dissolve the converted polymer.
- diluents compatible with the solvents listed above are aromatic hydrocarbons, ethyl acetate, acetone, cyclohexanone, acetamide and acetanilide.
- the diluent may serve as an aid in removing the solvent, as for example by evaporation, or as an additive for adjusting the viscosity of the solution, or both.
- the concentration of resin in the solution may also vary, and will be chosen in accordance with the desired viscosity of the solution and other processing characteristics. In most applications, best results will be obtained using solutions having a dissolved solids content (i.e., the resin) of about 10% to about 30% by weight, preferably from about 15% to about 25% by weight.
- a solution which has been found to be effective is a solution of the AI-10 polymer in a mixture of 40% acetone and 60% N-methylpyrrolidone, with a solids content of about 18% to 22% by weight.
- the web or reinforcement may be any material capable of impregnation by a resin. Both woven and nonwoven fabrics may be used, including both natural and synthetic materials. Reinforcements made from glass fibers are particularly useful.
- the porosity and weight of the fabric may also vary widely. In most cases, fabrics having a weight ranging from about 0.3 to about 3.0 ounces per square yard (10 to 100 grams per square meter) , preferably from about 0.5 to about 2.0 ounces per square yard (17 to 68 grams per square meter) will provide the best results.
- honeycomb is used herein to denote any open-cell grid structure, and particularly such open-cell structures which are formed from fused sheet stacks which are expanded or drawn apart. Examples of such stacks and the honeycomb panels which they form upon expansion are found in Steele, R.C., et al., U.S. Patent No. 2,674,295 (April 6, 1954); Holland, K.M. , U.S. Patent No. 3,006,798 (October 31, 1961); Anderson, D.C., et al., U.S. Patent No. 3,466,957 (September 16, 1969); Noble, R.G., et al., U.S. Patent No. 3,598,676 (August 10, 1971); and Taylor, R.S., U.S. Patent No. 3,819,439 (June 25, 1974). The disclosures of these patents are incorporated herein by reference.
- the fused stacks which are expanded into open-cell honeycomb structures may be of various dimensions of thickness, length and width. As addressed by the present invention, these stacks may be formed from components which range from long, narrow strips or ribbons, to relatively wide sheets. In practice, ribbon stacks are generally formed from sheet stacks by cutting with a band saw or similar equipment. Other methods of preparation are possible, however, and the present invention is not contemplated to be limited to any particular method or any particular configuration of the stack itself. For purposes of convenience, ribbons and sheets will be referred to herein generically as "layers.” As one example of a fabrication procedure, a roll of glass fiber fabric, typically 2 to 4 mils in thickness, is impregnated with a solution of the resin in its soluble state.
- An example is the AI-10 polymer dissolved in a 40/60 mixture of acetone and N-methylpyrrolidone at a solids content of about 20% by weight.
- the impregnated roll is then passed through an oven at a temperature of about 400°F (204°C) for 5 to 8 minutes, which results in the acetone and N-methyl ⁇ pyrrolidone being flashed off and the remaining resin being partially cured to a tack-free state.
- the roll is then cut into sheets. In one embodiment the roll is cut into sheets about 36 inches (91 cm) in width, on a 45" bias, i.e., in a direction such that the fibers are aligned at an angle of approximately 45° with respect to the lateral edges of the sheets.
- the longitudinal edges of the sheets are then overlapped, glued together and heat sealed. This is followed by rolling the sheets into rolls and heat soaking the rolls at about 350°F (177°C) for at least one hour for final curing of the glue.
- the rolls are unrolled and node lines, typically of a nylon-modified epoxy, are printed on the at regular intervals using a standard gravure technique.
- the rolls are then cut into rectangular sheets which are stacked t a thickness of about 4 to 5 inches (10 to 13 cm) .
- the stacks are then placed in a press where they are heated to a temperature of about 350 ⁇ F (177°C) under a pressure of about
- the unexpanded honeycomb block may be expanded to the desired dimensions, and restrained in the expanded state by a jig or frame.
- expansion may occur at room temperature. In most applications, however, particularly those involving anything other than very low resin loadings, expansion is best done with the aid of heat, such as by the use of steam and/or hot water.
- the honeycomb may be dipped in fresh AI-10 solution to form a film over the cured surface of the honeycomb. The solvent is then removed from the film and the resin converted to the final cured state in the same manner as the web impregnant. The dipping procedure may be repeated as often as desired to achieve a final honeycomb of the desired density and other characteristics.
- the initial expansion is done to less than a full expansion, opening the cells only part way to their maximum opening. This prevents excessive strain on the node bonds.
- the first dip followed by solvent removal and cure is then performed while the cells are still only partially opened.
- the panel is then heated once again and expanded to its full expansion, opening the cells to their maximum opening, the node bonds being strengthened by the coating laid down by the dip.
- the expansion ratio prior to the dip is not critical, and may range from about 20% to about 80% depending on the materials, conditions and dimensions of the system, although in most cases, an initial expansion ratio (i.e., the percent of total expansion) of about 50% will provide the best results.
- the dipping process may be repeated several times, the number depending on the cell size and the desired final density.
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- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Laminated Bodies (AREA)
Abstract
Thermoplastic honeycomb capable of formation by expansion of a compacted ribbon stack and of repeated dips in resin solution to form densified honeycomb panels is prepared by impregnating a fiber web with a thermoplastic material which has a soluble form and an insoluble form, and is readily converted from the former to the latter. Poly(amide-imide)s are an example of a suitable resin. The invention is particularly useful in forming compacted ribbon stacks of resin-impregnated glass fiber, expanding the stacks at an elevated temperature to a partial expansion sufficient to expose the cell interiors, then dipping the partially expanded stacks in resin solution, removing the solvent from the resulting film and curing the film, then expanding the stacks further at an elevated temperature to their full expansion, following by further dips to the final desired density.
Description
THERMOPLASTIC HONEYCOMB AND METHODS OF PREPARATION
This invention lies in the fields of honeycomb structures and polymer processing techniques. The particular area addressed by this invention is that relating to honeycomb structures formed of fabric-reinforced polymer.
BACKGROUND AND SUMMARY OF THE INVENTION Honeycomb has long been known for use in structural elements where a combination of lightness and strength are desirable. The use of nonmetallic materials such as ceramics and plastics offers additional advantages in terms of processing characteristics and the appearance and properties of the final product.
Thermoset plastics have been used in the manufacture of honeycomb, by fusing together corrugated ribbons of the plastic as well as by fusing together ribbons of fabric impregnated with thermosetting resin prior to the final cure. Difficulties with such materials include limitations on the manufacturing techniques, as well as minimal damage resistance with the result that the product is highly susceptible to damage during fabrication and lay-up, as well as fragmentation upon handling.
The present invention provides honeycomb based on plastic materials, the honeycomb being of acceptable mechanical properties and capable of being fabricated and handled by simpler and more versatile techniques. As described herein, honeycomb structures can be prepared which have the strength, impact resistance and processing characteristics of thermoplastic materials and yet offer high temperature resistance and solvent resistance characteristics which permit such processing steps as the application of multiple coatings for purposes of density adjustment and the formation of composite layers.
Central to the invention is the selection of a thermoplastic resin which has a soluble form and can be converted to an insoluble form. A fiber web is initially impregnated with the resin in its soluble form, using any of a variety of techniques, thereby fusing the fibers together into a stable coherent structure. The resulting impregnated web, in the form of ribbons or sheets, is arranged in a stack, in which adjacent ribbons or sheets are fused together along transverse node lines to render the stack expandable into the open-cell structure which forms the honeycomb, the expansion facilitated by heating the stack up to the softening point of the resin. The thermoplastic character of the insoluble resin permits this expansion to occur without damage to the resin, and the character of being insoluble permits further applications of the resin subsequent to the initial expansion. The soluble form of the resin permits these applications to be made by dipping the expanded structure in a solution of the resin followed by removal of the solvent and conversion to the insoluble form. Expansion can be done in stages, with further applications of resin in between each stage. The technique can also be used to apply layers of different resins or coating materials to form for example a composite structure with a specified combination of properties. In preferred embodiments, the initial impregnation is also done by dipping the fiber web in a solution of the resin in its soluble form.
Other advantages, features and embodiments of the invention will be apparent from the description which follows.
DETAILED DESCRIPTION OF THE INVENTION AND PREFERRED EMBODIMENTS
The present invention has wide applicability in terms of the types of honeycomb which can be formed and the various procedural steps and different types and numbers of layers to be applied as well as the means by which they are applied. The invention is of particular interest however as applied to thermoplastic-impregnated fabric in unexpanded stacks of ribbons or sheets which are then expanded into open-cell honeycomb panels to which further thermoplastic resin is
applied by dipping the expanded honeycomb into a solution of the resin. In accordance with this application, a wide variety of resins can be used, subject to the description in the preceding section. The choice of resin can thus depend on the choice of solvents.
The resin serving as the fabric impregnant may be the same as or different than the resin 'in the dip solution, and where more than one dip solution is used, the resins in the solutions themselves may be the same or different. When different resins are combined in either of these two ways in a single honeycomb structure, the resins must be compatible with each other. Compatibility in this context denotes the tendency of two resins to fuse together as one cures over a cured layer of the other, to the extent that the two are not easily separated by physical or mechanical means. The combining of two or more resins in this fashion permits the formation of hybrid structures and the achievement of useful as well as synergistic properties.
The resin serving as the fabric impregnant may be one which is applied in the same manner as the subsequent resin layers, i.e., by dipping followed by solvent removal and thermal conversion to a state permitting further processing. Alternatively, the fabric impregnant may be applied by other techniques known to those skilled in the art. Examples of other techniques are electrostatic deposition of the resin directly onto the fiber web in dry powder form followed by thermal fusion, and hot calendering of the resin in solid form directly onto the fabric.
The resins used in the practice of the present invention are thermoplastic resins which are soluble in a given solvent but which are capable of thermal conversion to a form which is insoluble in the same solvent. The term "thermal conversion" and related terms are used herein to denote a chemical reaction, such as curing or chain lengthening, which occurs at elevated temperature. Any thermoplastic resin which meets this description may be used.
A wide variety of thermoplastic polymers may be used as the resins. Examples include polyamides, poly(amide-
imide)ε, polyacetals, polycarbonates, poly(butylene terephthalate)s, poly(phenylene oxide)s and poly(phenylene sulphoxide)s. Preferred polymers for both the initial fabric impregnant and the dipping solution(s) are poly(amide-imides) , particularly those of the following formula
in which R is alkyl, preferably C,-C6, straight-chain or branched-chain; aryl, preferably phenyl, naphthyl, diphenyl sulfide, diphenyl sulfoxide or diphenyl sulfone; or aryl-alkyl combinations such as benzyl and diphenylmethylene.
The formula shown above represents the polymer in reacted form, insoluble in any of a variety of polar organic solvents. The prepolymer is any precursor form of the above which is soluble in the same solvents. The precursor may be a partially polymerized analogue of the insoluble polymer, particularly one with a sufficient number of free acid groups remaining which render it solubEe. One possibility for the precursor is a poly(amic acid) represented by the formula
A particularly preferred polymer within the scope of formula I above is one represented by the formula
or which the corresponding soluble poly(amic acid) prepolymer is as follows:
This poly(amic acid) is formed by the reaction between diamino diphenyl sulfone and trimellitic anhydride. Preferred poly(amic acids) within this formula as well as precursors in general to the polymer of formula II above are those having an acid number ranging from about 50 to about 100 when dissolved in a solvent as a 25% solution by weight. A prepolymer which has been found to be particularly effective i a product defined as AI-10 Polymer, supplied by Amoco Chemical Corporation, Chicago, Illinois, which undergoes conversion at temperatures of 350°F and above.
The choice of solvent is not critical and may vary widely, provided that it dissolves the resin prior to its conversion to the insoluble state. Polar organic solvents are preferred, and examples are dimethylformamide, dimethylacetamide, dimethyl sulfoxide, N-methylpyrrolidone and jπ-cresol. The properties of the solution may be modified by the use of a diluent, which may be any liquid which is miscibl with the solvent, does not cause premature precipitation of th unconverted resin, and yet does not dissolve the converted
polymer. Examples of diluents compatible with the solvents listed above are aromatic hydrocarbons, ethyl acetate, acetone, cyclohexanone, acetamide and acetanilide. The diluent may serve as an aid in removing the solvent, as for example by evaporation, or as an additive for adjusting the viscosity of the solution, or both.
The concentration of resin in the solution may also vary, and will be chosen in accordance with the desired viscosity of the solution and other processing characteristics. In most applications, best results will be obtained using solutions having a dissolved solids content (i.e., the resin) of about 10% to about 30% by weight, preferably from about 15% to about 25% by weight. One solution which has been found to be effective is a solution of the AI-10 polymer in a mixture of 40% acetone and 60% N-methylpyrrolidone, with a solids content of about 18% to 22% by weight.
The web or reinforcement may be any material capable of impregnation by a resin. Both woven and nonwoven fabrics may be used, including both natural and synthetic materials. Reinforcements made from glass fibers are particularly useful. The porosity and weight of the fabric may also vary widely. In most cases, fabrics having a weight ranging from about 0.3 to about 3.0 ounces per square yard (10 to 100 grams per square meter) , preferably from about 0.5 to about 2.0 ounces per square yard (17 to 68 grams per square meter) will provide the best results.
Fabrication of the honeycomb may be done in accordance with known procedures. The term "honeycomb" is used herein to denote any open-cell grid structure, and particularly such open-cell structures which are formed from fused sheet stacks which are expanded or drawn apart. Examples of such stacks and the honeycomb panels which they form upon expansion are found in Steele, R.C., et al., U.S. Patent No. 2,674,295 (April 6, 1954); Holland, K.M. , U.S. Patent No. 3,006,798 (October 31, 1961); Anderson, D.C., et al., U.S. Patent No. 3,466,957 (September 16, 1969); Noble, R.G., et al., U.S. Patent No. 3,598,676 (August 10, 1971); and Taylor, R.S., U.S.
Patent No. 3,819,439 (June 25, 1974). The disclosures of these patents are incorporated herein by reference.
The fused stacks which are expanded into open-cell honeycomb structures may be of various dimensions of thickness, length and width. As addressed by the present invention, these stacks may be formed from components which range from long, narrow strips or ribbons, to relatively wide sheets. In practice, ribbon stacks are generally formed from sheet stacks by cutting with a band saw or similar equipment. Other methods of preparation are possible, however, and the present invention is not contemplated to be limited to any particular method or any particular configuration of the stack itself. For purposes of convenience, ribbons and sheets will be referred to herein generically as "layers." As one example of a fabrication procedure, a roll of glass fiber fabric, typically 2 to 4 mils in thickness, is impregnated with a solution of the resin in its soluble state. An example, as stated above, is the AI-10 polymer dissolved in a 40/60 mixture of acetone and N-methylpyrrolidone at a solids content of about 20% by weight. The impregnated roll is then passed through an oven at a temperature of about 400°F (204°C) for 5 to 8 minutes, which results in the acetone and N-methyl¬ pyrrolidone being flashed off and the remaining resin being partially cured to a tack-free state. The roll is then cut into sheets. In one embodiment the roll is cut into sheets about 36 inches (91 cm) in width, on a 45" bias, i.e., in a direction such that the fibers are aligned at an angle of approximately 45° with respect to the lateral edges of the sheets. The longitudinal edges of the sheets are then overlapped, glued together and heat sealed. This is followed by rolling the sheets into rolls and heat soaking the rolls at about 350°F (177°C) for at least one hour for final curing of the glue.
Once the rolls are cured, they are unrolled and node lines, typically of a nylon-modified epoxy, are printed on the at regular intervals using a standard gravure technique. The rolls are then cut into rectangular sheets which are stacked t a thickness of about 4 to 5 inches (10 to 13 cm) . The stacks
are then placed in a press where they are heated to a temperature of about 350βF (177°C) under a pressure of about
•**>
500 to 600 psi (35 to 42 kg/cm ) to cure the node adhesive, thus bonding the sheets together at the node lines. The result is a stack ready for expansion into a honeycomb structure.
Since the cured resin is a thermoplastic material, the unexpanded honeycomb block may be expanded to the desired dimensions, and restrained in the expanded state by a jig or frame. For blocks made from webs with low resin content, expansion may occur at room temperature. In most applications, however, particularly those involving anything other than very low resin loadings, expansion is best done with the aid of heat, such as by the use of steam and/or hot water. Thus expanded, the honeycomb may be dipped in fresh AI-10 solution to form a film over the cured surface of the honeycomb. The solvent is then removed from the film and the resin converted to the final cured state in the same manner as the web impregnant. The dipping procedure may be repeated as often as desired to achieve a final honeycomb of the desired density and other characteristics.
In particularly preferred embodiments, the initial expansion is done to less than a full expansion, opening the cells only part way to their maximum opening. This prevents excessive strain on the node bonds. The first dip followed by solvent removal and cure is then performed while the cells are still only partially opened. The panel is then heated once again and expanded to its full expansion, opening the cells to their maximum opening, the node bonds being strengthened by the coating laid down by the dip. The expansion ratio prior to the dip is not critical, and may range from about 20% to about 80% depending on the materials, conditions and dimensions of the system, although in most cases, an initial expansion ratio (i.e., the percent of total expansion) of about 50% will provide the best results. The dipping process may be repeated several times, the number depending on the cell size and the desired final density. The most typical cells are hexagonal in shape, with a width of about one-quarter inch (0.6 cm) or less.
The foregoing is offered primarily for purposes of illustration. It will be readily apparent to those skilled in the art that modifications and variations may be made in the materials, proportions, conditions and procedures used without departing from the spirit and scope of the invention.
Claims
1. A laminated structure expandable into an open- cell grid structure, comprising layers of fabric fused together at node lines periodically spaced along each said layer, said layers impregnated with a thermoplastic material which is insoluble in a selected solvent and capable of formation from a precursor by thermal conversion, said precursor being one which is soluble in said solvent.
2. A laminated structure in accordance with claim 1 in which said selected solvent is a member selected from the group consisting of dimethylformamide, dimethylacetamide, dimethyl sulfoxide, N-methylpyrrolidone and m-cresol.
3. A laminated structure in accordance with claim 1 in which said thermoplastic material is a poly(amide-imide) .
4. A laminated structure in accordance with claim 1 in which said thermoplastic material is a poly(amide-imide) formed by the reaction between a dia ino diphenyl sulfone and trimellitic anhydride.
5. A laminated structure in accordance with claim 1 in which said thermoplastic material is a poly(amide-imide) and said precursor is a prepolymer thereof having an acid number ranging from about 50 to about 100.
6. A laminated structure in accordance with claim 1 in which said fabric is a glass fiber web.
7. A method for preparing a fiber-reinforced thermoplastic laminate expandable into open-cell grid structure, said method comprising: (a) impregnating a fiber web with a thermoplastic polymer which is insoluble in a selected solvent and capable of formation from a prepolymer by thermal conversion, said prepolymer being one which is soluble in said solvent; and
(b) fusing together a plurality of layers of said fiber web so impregnated, at node lines periodically spaced along each said layer, to form a laminated structure.
8. A method in accordance with claim 7 in which said thermoplastic polymer is a poly(amide-imide) formed by the reaction between a diamino diphenyl sulfone and trimellitic anhydride.
9. A method for preparing an open-cell grid structure comprised of a fiber-reinforced thermoplastic laminate, said method comprising:
(a) impregnating a fiber web with a first thermoplastic polymer which is insoluble in a selected solvent;
(b) fusing together a plurality of layers of said fiber web so impregnated, at node lines periodically spaced along each said layer, to form a laminated structure;
(c) heating said laminated structure to a temperature at which said first thermoplastic polyme softens sufficiently to permit expansion of said laminated structure into an open-cell grid structure, and expanding said laminated structure so heated;
(d) immersing said expanded laminate so heated and expanded into a solution of a polymer precursor in said selected solvent, said polymer precursor being thermally convertible to a second thermoplasti polymer which is compatible with said first thermoplastic polymer and insoluble in said selected solvent to coat said open-cell grid structure with a film of said solution; and
(e) removing said solvent from said film and thermally converting said polymer precursor to form coating of said second thermoplastic polymer over said layers.
10. A method in accordance with claim 9 in which the expansion of step (c) is a partial expansion resulting in an open-cell grid structure whose cells are partially opened, and said solution, polymer precursor and film are defined as a first solution, a first polymer precursor and a first film, respectively, and said method further comprises: (f) heating said open-cell grid structure subsequent to step (d) to a temperature at which said first and second thermoplastic polymers soften sufficiently to permit further expansion of said open-cell grid structure, and further expanding said open-cell grid structure so heated;
(g) immersing said open-cell grid structure thus further expanded in a second solution of a second polymer precursor in said selected solvent, said second polymer precursor being thermally convertible to a third thermoplastic polymer which is compatible with said second thermoplastic polymer and insoluble in said selected solvent to coat said open- cell grid structure with a second film of said second solution; and (h) removing said solvent from said second film and thermally converting said polymer precursor to form a coating of said third thermoplastic polymer over said coating of said second thermoplastic polymer.
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US404,240 | 1982-08-02 | ||
US40424089A | 1989-09-07 | 1989-09-07 |
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WO1991003378A1 true WO1991003378A1 (en) | 1991-03-21 |
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ID=23598769
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
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PCT/US1990/005037 WO1991003378A1 (en) | 1989-09-07 | 1990-09-06 | Thermoplastic honeycomb and methods of preparation |
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AU (1) | AU6624390A (en) |
WO (1) | WO1991003378A1 (en) |
Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
EP1008566A1 (en) * | 1998-12-10 | 2000-06-14 | Showa Aircraft Industry Co., Ltd. | Honeycomb structure and method for preparing the same |
WO2001030718A1 (en) * | 1999-10-22 | 2001-05-03 | Air & Refrigeration Corp | Media for evaporative cooler |
US8440290B2 (en) | 1999-10-22 | 2013-05-14 | Anne Yaeger | Contact media for evaporative coolers |
Citations (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3899626A (en) * | 1972-09-11 | 1975-08-12 | Rhone Poulenc Sa | Composite articles based on heat-resistant resins |
US4710432A (en) * | 1985-08-08 | 1987-12-01 | Teijin Limited | Base material for honeycomb core structure and process for producing the same |
-
1990
- 1990-09-06 AU AU66243/90A patent/AU6624390A/en not_active Abandoned
- 1990-09-06 WO PCT/US1990/005037 patent/WO1991003378A1/en unknown
Patent Citations (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3899626A (en) * | 1972-09-11 | 1975-08-12 | Rhone Poulenc Sa | Composite articles based on heat-resistant resins |
US4710432A (en) * | 1985-08-08 | 1987-12-01 | Teijin Limited | Base material for honeycomb core structure and process for producing the same |
Cited By (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
EP1008566A1 (en) * | 1998-12-10 | 2000-06-14 | Showa Aircraft Industry Co., Ltd. | Honeycomb structure and method for preparing the same |
US6331340B1 (en) | 1998-12-10 | 2001-12-18 | Showa Aircraft Industry Co., Ltd. | Honeycomb structure and method for preparing the same |
EP1544179A3 (en) * | 1998-12-10 | 2006-06-07 | Showa Aircraft Industry Co., Ltd. | Honeycomb structure and method for preparing the same |
WO2001030718A1 (en) * | 1999-10-22 | 2001-05-03 | Air & Refrigeration Corp | Media for evaporative cooler |
US8440290B2 (en) | 1999-10-22 | 2013-05-14 | Anne Yaeger | Contact media for evaporative coolers |
Also Published As
Publication number | Publication date |
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AU6624390A (en) | 1991-04-08 |
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