EP0387468A2 - Stable amorphous hydrated metal oxide sizing for fibres in composites - Google Patents
Stable amorphous hydrated metal oxide sizing for fibres in composites Download PDFInfo
- Publication number
- EP0387468A2 EP0387468A2 EP89630216A EP89630216A EP0387468A2 EP 0387468 A2 EP0387468 A2 EP 0387468A2 EP 89630216 A EP89630216 A EP 89630216A EP 89630216 A EP89630216 A EP 89630216A EP 0387468 A2 EP0387468 A2 EP 0387468A2
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- EP
- European Patent Office
- Prior art keywords
- fiber
- composite
- composites
- metal oxide
- amorphous hydrated
- 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.)
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- 239000002131 composite material Substances 0.000 title claims abstract description 39
- 238000004513 sizing Methods 0.000 title description 16
- 229910044991 metal oxide Inorganic materials 0.000 title description 13
- 150000004706 metal oxides Chemical class 0.000 title description 13
- 239000000835 fiber Substances 0.000 claims abstract description 41
- 229910052751 metal Inorganic materials 0.000 claims abstract description 24
- 239000002184 metal Substances 0.000 claims abstract description 24
- 150000004703 alkoxides Chemical class 0.000 claims abstract description 23
- 238000000034 method Methods 0.000 claims abstract description 10
- 230000007062 hydrolysis Effects 0.000 claims abstract description 4
- 238000006460 hydrolysis reaction Methods 0.000 claims abstract description 4
- 230000001590 oxidative effect Effects 0.000 claims abstract description 4
- 230000008021 deposition Effects 0.000 claims abstract description 3
- 230000002787 reinforcement Effects 0.000 claims abstract description 3
- OKTJSMMVPCPJKN-UHFFFAOYSA-N Carbon Chemical group [C] OKTJSMMVPCPJKN-UHFFFAOYSA-N 0.000 claims description 10
- 229910052782 aluminium Inorganic materials 0.000 claims description 9
- 239000010439 graphite Substances 0.000 claims description 9
- 229910002804 graphite Inorganic materials 0.000 claims description 9
- XAGFODPZIPBFFR-UHFFFAOYSA-N aluminium Chemical compound [Al] XAGFODPZIPBFFR-UHFFFAOYSA-N 0.000 claims description 4
- 239000011159 matrix material Substances 0.000 claims description 4
- ZOXJGFHDIHLPTG-UHFFFAOYSA-N Boron Chemical compound [B] ZOXJGFHDIHLPTG-UHFFFAOYSA-N 0.000 claims description 2
- XUIMIQQOPSSXEZ-UHFFFAOYSA-N Silicon Chemical compound [Si] XUIMIQQOPSSXEZ-UHFFFAOYSA-N 0.000 claims description 2
- RTAQQCXQSZGOHL-UHFFFAOYSA-N Titanium Chemical compound [Ti] RTAQQCXQSZGOHL-UHFFFAOYSA-N 0.000 claims description 2
- 229910052796 boron Inorganic materials 0.000 claims description 2
- 239000011521 glass Substances 0.000 claims description 2
- 229910052710 silicon Inorganic materials 0.000 claims description 2
- 239000010703 silicon Substances 0.000 claims description 2
- HBMJWWWQQXIZIP-UHFFFAOYSA-N silicon carbide Chemical compound [Si+]#[C-] HBMJWWWQQXIZIP-UHFFFAOYSA-N 0.000 claims description 2
- 229910010271 silicon carbide Inorganic materials 0.000 claims description 2
- 239000010936 titanium Substances 0.000 claims description 2
- 229910052719 titanium Inorganic materials 0.000 claims description 2
- 229920003235 aromatic polyamide Polymers 0.000 claims 1
- 239000011347 resin Substances 0.000 description 12
- 229920005989 resin Polymers 0.000 description 12
- -1 i.e. Substances 0.000 description 7
- 238000006243 chemical reaction Methods 0.000 description 6
- 230000003647 oxidation Effects 0.000 description 6
- 238000007254 oxidation reaction Methods 0.000 description 6
- 230000008901 benefit Effects 0.000 description 5
- 238000000576 coating method Methods 0.000 description 5
- 239000003795 chemical substances by application Substances 0.000 description 4
- 239000011248 coating agent Substances 0.000 description 4
- 230000035882 stress Effects 0.000 description 4
- YXFVVABEGXRONW-UHFFFAOYSA-N Toluene Chemical compound CC1=CC=CC=C1 YXFVVABEGXRONW-UHFFFAOYSA-N 0.000 description 3
- 238000005516 engineering process Methods 0.000 description 3
- 229920001721 polyimide Polymers 0.000 description 3
- 229920000049 Carbon (fiber) Polymers 0.000 description 2
- 239000004593 Epoxy Substances 0.000 description 2
- XEEYBQQBJWHFJM-UHFFFAOYSA-N Iron Chemical compound [Fe] XEEYBQQBJWHFJM-UHFFFAOYSA-N 0.000 description 2
- PXHVJJICTQNCMI-UHFFFAOYSA-N Nickel Chemical compound [Ni] PXHVJJICTQNCMI-UHFFFAOYSA-N 0.000 description 2
- 239000004642 Polyimide Substances 0.000 description 2
- MCMNRKCIXSYSNV-UHFFFAOYSA-N Zirconium dioxide Chemical compound O=[Zr]=O MCMNRKCIXSYSNV-UHFFFAOYSA-N 0.000 description 2
- PNEYBMLMFCGWSK-UHFFFAOYSA-N aluminium oxide Inorganic materials [O-2].[O-2].[O-2].[Al+3].[Al+3] PNEYBMLMFCGWSK-UHFFFAOYSA-N 0.000 description 2
- 239000004917 carbon fiber Substances 0.000 description 2
- 238000002425 crystallisation Methods 0.000 description 2
- 230000008025 crystallization Effects 0.000 description 2
- 230000006353 environmental stress Effects 0.000 description 2
- 239000003733 fiber-reinforced composite Substances 0.000 description 2
- 238000004519 manufacturing process Methods 0.000 description 2
- 239000000203 mixture Substances 0.000 description 2
- 238000006116 polymerization reaction Methods 0.000 description 2
- 238000002360 preparation method Methods 0.000 description 2
- 230000003014 reinforcing effect Effects 0.000 description 2
- 239000002904 solvent Substances 0.000 description 2
- 239000007921 spray Substances 0.000 description 2
- 239000000758 substrate Substances 0.000 description 2
- 238000002411 thermogravimetry Methods 0.000 description 2
- 229910052726 zirconium Inorganic materials 0.000 description 2
- LFQSCWFLJHTTHZ-UHFFFAOYSA-N Ethanol Chemical compound CCO LFQSCWFLJHTTHZ-UHFFFAOYSA-N 0.000 description 1
- MXRIRQGCELJRSN-UHFFFAOYSA-N O.O.O.[Al] Chemical compound O.O.O.[Al] MXRIRQGCELJRSN-UHFFFAOYSA-N 0.000 description 1
- BPQQTUXANYXVAA-UHFFFAOYSA-N Orthosilicate Chemical compound [O-][Si]([O-])([O-])[O-] BPQQTUXANYXVAA-UHFFFAOYSA-N 0.000 description 1
- 229910019142 PO4 Inorganic materials 0.000 description 1
- QCWXUUIWCKQGHC-UHFFFAOYSA-N Zirconium Chemical compound [Zr] QCWXUUIWCKQGHC-UHFFFAOYSA-N 0.000 description 1
- 239000000654 additive Substances 0.000 description 1
- 150000001298 alcohols Chemical class 0.000 description 1
- 150000001408 amides Chemical class 0.000 description 1
- QVGXLLKOCUKJST-UHFFFAOYSA-N atomic oxygen Chemical compound [O] QVGXLLKOCUKJST-UHFFFAOYSA-N 0.000 description 1
- 230000015572 biosynthetic process Effects 0.000 description 1
- 229910052799 carbon Inorganic materials 0.000 description 1
- 230000015556 catabolic process Effects 0.000 description 1
- 238000011109 contamination Methods 0.000 description 1
- 238000000354 decomposition reaction Methods 0.000 description 1
- 230000007423 decrease Effects 0.000 description 1
- 230000007812 deficiency Effects 0.000 description 1
- 238000006731 degradation reaction Methods 0.000 description 1
- 230000002939 deleterious effect Effects 0.000 description 1
- 239000000539 dimer Substances 0.000 description 1
- 238000004821 distillation Methods 0.000 description 1
- 230000007613 environmental effect Effects 0.000 description 1
- 150000002118 epoxides Chemical class 0.000 description 1
- 125000001495 ethyl group Chemical group [H]C([H])([H])C([H])([H])* 0.000 description 1
- 239000003365 glass fiber Substances 0.000 description 1
- 238000010348 incorporation Methods 0.000 description 1
- 239000012784 inorganic fiber Substances 0.000 description 1
- 229910052742 iron Inorganic materials 0.000 description 1
- 239000004761 kevlar Substances 0.000 description 1
- 238000011068 loading method Methods 0.000 description 1
- CPLXHLVBOLITMK-UHFFFAOYSA-N magnesium oxide Inorganic materials [Mg]=O CPLXHLVBOLITMK-UHFFFAOYSA-N 0.000 description 1
- 239000000395 magnesium oxide Substances 0.000 description 1
- AXZKOIWUVFPNLO-UHFFFAOYSA-N magnesium;oxygen(2-) Chemical compound [O-2].[Mg+2] AXZKOIWUVFPNLO-UHFFFAOYSA-N 0.000 description 1
- 230000014759 maintenance of location Effects 0.000 description 1
- 239000000463 material Substances 0.000 description 1
- 150000002739 metals Chemical class 0.000 description 1
- 125000002496 methyl group Chemical group [H]C([H])([H])* 0.000 description 1
- 238000002156 mixing Methods 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 239000006082 mold release agent Substances 0.000 description 1
- 230000006740 morphological transformation Effects 0.000 description 1
- 238000000465 moulding Methods 0.000 description 1
- 229910052759 nickel Inorganic materials 0.000 description 1
- 229910052760 oxygen Inorganic materials 0.000 description 1
- 239000001301 oxygen Substances 0.000 description 1
- 239000010452 phosphate Substances 0.000 description 1
- NBIIXXVUZAFLBC-UHFFFAOYSA-K phosphate Chemical compound [O-]P([O-])([O-])=O NBIIXXVUZAFLBC-UHFFFAOYSA-K 0.000 description 1
- 239000009719 polyimide resin Substances 0.000 description 1
- 229920000642 polymer Polymers 0.000 description 1
- 229920002689 polyvinyl acetate Polymers 0.000 description 1
- 239000011118 polyvinyl acetate Substances 0.000 description 1
- 125000001436 propyl group Chemical group [H]C([*])([H])C([H])([H])C([H])([H])[H] 0.000 description 1
- 238000012827 research and development Methods 0.000 description 1
- 125000002914 sec-butyl group Chemical group [H]C([H])([H])C([H])([H])C([H])(*)C([H])([H])[H] 0.000 description 1
- 239000007858 starting material Substances 0.000 description 1
- 239000000126 substance Substances 0.000 description 1
- 238000012546 transfer Methods 0.000 description 1
- 239000013638 trimer Substances 0.000 description 1
- 239000003039 volatile agent Substances 0.000 description 1
- 230000004580 weight loss Effects 0.000 description 1
- 238000004804 winding Methods 0.000 description 1
Images
Classifications
-
- D—TEXTILES; PAPER
- D01—NATURAL OR MAN-MADE THREADS OR FIBRES; SPINNING
- D01F—CHEMICAL FEATURES IN THE MANUFACTURE OF ARTIFICIAL FILAMENTS, THREADS, FIBRES, BRISTLES OR RIBBONS; APPARATUS SPECIALLY ADAPTED FOR THE MANUFACTURE OF CARBON FILAMENTS
- D01F11/00—Chemical after-treatment of artificial filaments or the like during manufacture
- D01F11/10—Chemical after-treatment of artificial filaments or the like during manufacture of carbon
- D01F11/12—Chemical after-treatment of artificial filaments or the like during manufacture of carbon with inorganic substances ; Intercalation
- D01F11/123—Oxides
-
- D—TEXTILES; PAPER
- D06—TREATMENT OF TEXTILES OR THE LIKE; LAUNDERING; FLEXIBLE MATERIALS NOT OTHERWISE PROVIDED FOR
- D06M—TREATMENT, NOT PROVIDED FOR ELSEWHERE IN CLASS D06, OF FIBRES, THREADS, YARNS, FABRICS, FEATHERS OR FIBROUS GOODS MADE FROM SUCH MATERIALS
- D06M11/00—Treating fibres, threads, yarns, fabrics or fibrous goods made from such materials, with inorganic substances or complexes thereof; Such treatment combined with mechanical treatment, e.g. mercerising
- D06M11/32—Treating fibres, threads, yarns, fabrics or fibrous goods made from such materials, with inorganic substances or complexes thereof; Such treatment combined with mechanical treatment, e.g. mercerising with oxygen, ozone, ozonides, oxides, hydroxides or percompounds; Salts derived from anions with an amphoteric element-oxygen bond
- D06M11/36—Treating fibres, threads, yarns, fabrics or fibrous goods made from such materials, with inorganic substances or complexes thereof; Such treatment combined with mechanical treatment, e.g. mercerising with oxygen, ozone, ozonides, oxides, hydroxides or percompounds; Salts derived from anions with an amphoteric element-oxygen bond with oxides, hydroxides or mixed oxides; with salts derived from anions with an amphoteric element-oxygen bond
- D06M11/45—Oxides or hydroxides of elements of Groups 3 or 13 of the Periodic Table; Aluminates
-
- D—TEXTILES; PAPER
- D06—TREATMENT OF TEXTILES OR THE LIKE; LAUNDERING; FLEXIBLE MATERIALS NOT OTHERWISE PROVIDED FOR
- D06M—TREATMENT, NOT PROVIDED FOR ELSEWHERE IN CLASS D06, OF FIBRES, THREADS, YARNS, FABRICS, FEATHERS OR FIBROUS GOODS MADE FROM SUCH MATERIALS
- D06M11/00—Treating fibres, threads, yarns, fabrics or fibrous goods made from such materials, with inorganic substances or complexes thereof; Such treatment combined with mechanical treatment, e.g. mercerising
- D06M11/32—Treating fibres, threads, yarns, fabrics or fibrous goods made from such materials, with inorganic substances or complexes thereof; Such treatment combined with mechanical treatment, e.g. mercerising with oxygen, ozone, ozonides, oxides, hydroxides or percompounds; Salts derived from anions with an amphoteric element-oxygen bond
- D06M11/36—Treating fibres, threads, yarns, fabrics or fibrous goods made from such materials, with inorganic substances or complexes thereof; Such treatment combined with mechanical treatment, e.g. mercerising with oxygen, ozone, ozonides, oxides, hydroxides or percompounds; Salts derived from anions with an amphoteric element-oxygen bond with oxides, hydroxides or mixed oxides; with salts derived from anions with an amphoteric element-oxygen bond
- D06M11/46—Oxides or hydroxides of elements of Groups 4 or 14 of the Periodic Table; Titanates; Zirconates; Stannates; Plumbates
-
- D—TEXTILES; PAPER
- D06—TREATMENT OF TEXTILES OR THE LIKE; LAUNDERING; FLEXIBLE MATERIALS NOT OTHERWISE PROVIDED FOR
- D06M—TREATMENT, NOT PROVIDED FOR ELSEWHERE IN CLASS D06, OF FIBRES, THREADS, YARNS, FABRICS, FEATHERS OR FIBROUS GOODS MADE FROM SUCH MATERIALS
- D06M11/00—Treating fibres, threads, yarns, fabrics or fibrous goods made from such materials, with inorganic substances or complexes thereof; Such treatment combined with mechanical treatment, e.g. mercerising
- D06M11/77—Treating fibres, threads, yarns, fabrics or fibrous goods made from such materials, with inorganic substances or complexes thereof; Such treatment combined with mechanical treatment, e.g. mercerising with silicon or compounds thereof
- D06M11/79—Treating fibres, threads, yarns, fabrics or fibrous goods made from such materials, with inorganic substances or complexes thereof; Such treatment combined with mechanical treatment, e.g. mercerising with silicon or compounds thereof with silicon dioxide, silicic acids or their salts
-
- D—TEXTILES; PAPER
- D06—TREATMENT OF TEXTILES OR THE LIKE; LAUNDERING; FLEXIBLE MATERIALS NOT OTHERWISE PROVIDED FOR
- D06M—TREATMENT, NOT PROVIDED FOR ELSEWHERE IN CLASS D06, OF FIBRES, THREADS, YARNS, FABRICS, FEATHERS OR FIBROUS GOODS MADE FROM SUCH MATERIALS
- D06M2200/00—Functionality of the treatment composition and/or properties imparted to the textile material
- D06M2200/50—Modified hand or grip properties; Softening compositions
Definitions
- the field of art to which this invention pertains is methods for using composites.
- the fiber can be coated with an organic primer or sizing agent to produce a surface which with improved handling (i.e., weaveability) and less subject to contamination when combined with the matrix resin develops the strengths which meet application requirements.
- an organic primer or sizing agent i.e., weaveability
- a variety of sizing agents have been used to produce improved bondability including epoxy, polyimide and polyvinylacetate polymers.
- commonly assigned U.S. Patent No. 4,678,820 describes an amorphous hydrated metal oxide primer as a fiber size that provides improved wet strength to a fabricated composite.
- the invention is directed to a method of using a polymeric composite wherein the composite exhibits greater oxidative stability.
- the fiber reinforcement has a layer of amorphous hydrated metal alkoxide formed by deposition onto the fiber and subsequent hydrolysis of metal alkoxides.
- the improvement comprises exposing the composite to temperatures of about 100°C to about 975°C.
- This amorphous hydrated metal oxide sizing for composite fibers provides improved oxidation resistance at elevated temperatures.
- this invention makes a significant advance to the aerospace industry by providing new technology relating to structural composites.
- Any metal alkoxide that hydrolyzes to give an amorphous hydrated metal oxide may be used in the practice of this invention.
- Metal alkoxides having the formula M x (OR) y where x is 1 and y is 3 or 4 are preferred in forming the metal oxide primer of this disclosure, y being determined by the particular valence of the metal. Typically, a valence of at least 3 is preferable to form a monohydroxy metal oxide.
- alkoxides where y is 2 are preferably combined with alkoxides having higher y values.
- M is any metal capable of forming a stable alkoxide, which can be purified by, for example, distillation or crystallization without decomposition; as y is defined above essentially all metals meet this requirement. It is preferred that the metal is selected from the group consisting of titanium, zirconium, silicon, nickel, iron and aluminum. It is especially preferred that M is aluminum.
- R can be any organic radical that can be distilled at temperatures below about 300°C. Since the alkoxide (-OR moiety) is not incorporated into the primer, the important criteria associated with it is that the resultant alcohol can be volatilized at temperatures that are not high enough to damage the primer or substrate. It is preferred that R is an alkane radical from C1 to C10.
- R is methyl, ethyl, propyl or sec-butyl as these radicals are volatilized as alcohols at relatively low temperatures.
- the alkoxides can be modified by incorporation of varying amounts of additives such as phosphate, silicate or magnesium oxide without affecting the sizing properties. Mixtures of the above metal alkoxides may also be used in the practice of this invention.
- partial hydrolyzates of the metal alkoxides can also be used as starting material, i.e., dimers, trimers, etc. of the monomeric alkoxides.
- the above metal alkoxides hydrolyze to amorphous hydrated metal oxides (sizing) when exposed to moisture such as atmospheric moisture or moisture on the fiber substrate surface and optionally heat as described below.
- An exemplary reaction believed to occur is that of aluminum alkoxide to alumina.
- the initial hydrolyzation reaction of aluminum alkoxides is empirically illustrated as Al(OR)3 + H2O Al(OR)2(OH) + R(OH) (1) This reaction proceeds rapidly with further hydrolyzation-polymerization to 2Al(OR)2(OH)+H2O >RO- -O- -OR+2 ROH, etc. (2) to incorporate n aluminum ions, i.e.
- the thickness of this primer layer can vary effectively from about 1.5 nanometers (nm) to about 1000 nm. Above about 1000 nm, the layer can be so thick as to create stress risers and to form a weak boundary layer. Below about 1.5 nm, the layer does not provide the properties such as crack propagation resistance and stress transfer at the levels typically required. In addition, it is preferable to apply the primer to the fiber surface with a plurality of layers of metal alkoxide as this facilitates removal of volatiles and solvent which can be more difficult to achieve from a single thick application.
- any fiber may be used in the practice of this invention that is useful for making composite articles.
- Examples include amide, carbon, metal, boron, glass, silicon carbide, alumina and KEVLAR TM fibers (DuPont DeNemours, E.I., Co., Wilmington, Delaware).
- graphite or glass fibers are used as these provide the properties most desired of composites such as strength and light weight. It is especially preferred to use graphite available from BASF as it resists environmental stresses and produces lightweight composites having good strength.
- any conventional resin matrix can be used for the practice of this invention that is useful for making composite articles.
- epoxides, bis-maleimides or polyimide resins are used as these provide the properties most desired such as good strength. It is especially preferred to use 3501-6 TM resin available from Hercules, Inc. (Wilmington, Delaware) 5208 resin available from Narmco,Arimide N TM resin (E.I. DuPont DeNemours) and LARC-TPI resin (Nasa) as they resist environmental stresses, are strong and are commercially readily available.
- a chopped fiber composite can be made by mixing chopped fibers coated with amorphous hydrated metal oxide and resin in a mold under pressure and optional heat.
- the metal alkoxide coated composite fibers are then maintained at a temperature of about 25°C to about 300°C as below 25°C the reaction kinetics are typically too slow and above 400°C loss of desirable fiber properties or crystallization of the coating may occur with an accompanying loss of mechanical strength.
- the reinforcing carbon fibers are dipped into the resin solution to form a tape prior to the molding step.
- the resin impregnated fibers are allowed to dry so that any solvent will evaporate.
- the graphite tape can then be cut into plies (layers of impregnated fibers) of the desired dimensions of the article to be fabricated.
- the plies are then stacked to create the desired thickness, typically in metal molds coated with mold release agent such as Micro Spray ⁇ (Micro-Spray Products Inc.).
- the assembled ply layup is then placed in a press and exposed to pressures and temperatures conventional for the resin system used and application desired.
- Inorganic primer was applied to unsized, surface treated, Celion 6000 graphite fiber available from BASF Corporation by drawing the fiber tow through a 1% toluene solution of Stauffer Chemical Company aluminum alkoxide, E-8385, and drum winding the coated tows.
- the resulting wound tape was heated at 200-325°C in an air oven to dry and thus produce the amorphous alumina coating.
- This primer may be used to advantage in a wide range of composites. For example, chopped fiber, filament wound and ordered fiber composites benefit from this primer. While this invention has been described in terms of a metal alkoxide, a mixture of various metal alkoxides can be used.
- This sizing coating provides improved oxidation resistance at elevated temperatures. At temperatures of about 100°C to about 975°C, this sizing results in more oxidatively stable fibers and hence composites. The resulting properties such as tensile and flexural strengths of composites made with the inorganic fiber sizing are believed at least equivalent or better than composites made using conventional organic fiber sizing. Yet the inorganic sizing agent can be utilized at thinner layers than the 1.0 wt. % loading of fibers typical of organic sizing. Thicker layers tend to set up stress risers and to form a weak boundary layer as the components segregate. Also, because of its oxidation resistance the inorganic sizing can be used equally as well with high temperature resins such as polyimides or with low temperature resins such as epoxy systems unlike organic sizing agents which are typically temperature specific.
- composites using the inorganic sized fibers will have improved wet strength retention, be less subject to microcracking and exhibit improved fracture toughness and impact strength properties. Also, the inorganic insulating sheath will have little, if any, deleterious effect on electrical equipment (e.g., cause shorting) should such a composite disintegrate.
- This invention provides an amorphous hydrated metal oxide sizing for fiber reinforced composites resulting in improved oxidation resistance. Thus, it makes a significant advance in the aerospace industry by providing new technology relating to composites.
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- Engineering & Computer Science (AREA)
- Textile Engineering (AREA)
- Chemical & Material Sciences (AREA)
- Inorganic Chemistry (AREA)
- Chemical Kinetics & Catalysis (AREA)
- General Chemical & Material Sciences (AREA)
- Surface Treatment Of Glass Fibres Or Filaments (AREA)
- Reinforced Plastic Materials (AREA)
- Treatments For Attaching Organic Compounds To Fibrous Goods (AREA)
- Chemical Or Physical Treatment Of Fibers (AREA)
- Compositions Of Macromolecular Compounds (AREA)
Abstract
A method of using a polymeric composite wherein the composite exhibits greater oxidative stability. The fiber reinforcement has a layer of amorphous hydrated metal alkoxide formed by deposition onto the fiber and subsequent hydrolysis of metal alkoxides. The improvement comprises exposing the composite to temperatures of about 100°C to about 975°C.
Description
- The field of art to which this invention pertains is methods for using composites.
- Weight saving and manufacturing cost benefits have led to the increase in use of organic matrix fiber reinforced composite structures in the aircraft and aerospace industries. In order to be a viable alternative to metal these composites should maintain the strength typical of conventional structural systems. In many applications composites are put under a variety of environmental and mechanical stresses. For example, frequently these composites are exposed over long periods of time to elevated temperatures which can result in a loss of composite properties. The loss of properties can result from heat induced microcracks that allow oxygen to attack the fibers. As a result of this deficiency, extensive research and development efforts have been undertaken to define methods and identify materials which improve composite performance in elevated temperatures. For example, it is known that surface preparation of fibers can be important in the formation of composites. Thus, the fiber can be coated with an organic primer or sizing agent to produce a surface which with improved handling (i.e., weaveability) and less subject to contamination when combined with the matrix resin develops the strengths which meet application requirements. A variety of sizing agents have been used to produce improved bondability including epoxy, polyimide and polyvinylacetate polymers. In particular, commonly assigned U.S. Patent No. 4,678,820 describes an amorphous hydrated metal oxide primer as a fiber size that provides improved wet strength to a fabricated composite. Although the above surface preparations have provided advantages, there is a need for new technology to aid in the advancement of lightweight aerospace-type composite structures.
- Accordingly, there is a constant search in this field of art for new methods of providing lightweight, structurally sound composites.
- The invention is directed to a method of using a polymeric composite wherein the composite exhibits greater oxidative stability. The fiber reinforcement has a layer of amorphous hydrated metal alkoxide formed by deposition onto the fiber and subsequent hydrolysis of metal alkoxides. The improvement comprises exposing the composite to temperatures of about 100°C to about 975°C.
- This amorphous hydrated metal oxide sizing for composite fibers provides improved oxidation resistance at elevated temperatures. Thus, this invention makes a significant advance to the aerospace industry by providing new technology relating to structural composites.
- The foregoing, and other features and advantages of the present invention will become more apparent from the following description, claims and accompanying drawings.
-
- The Figure graphically depicts the oxidation resistance of unsized graphite fiber and fibers having the sizing of this invention.
- Any metal alkoxide that hydrolyzes to give an amorphous hydrated metal oxide (i.e. a monohydroxy metal oxide) may be used in the practice of this invention. Metal alkoxides having the formula Mx(OR)y where x is 1 and y is 3 or 4 are preferred in forming the metal oxide primer of this disclosure, y being determined by the particular valence of the metal. Typically, a valence of at least 3 is preferable to form a monohydroxy metal oxide. However, alkoxides where y is 2 are preferably combined with alkoxides having higher y values. M is any metal capable of forming a stable alkoxide, which can be purified by, for example, distillation or crystallization without decomposition; as y is defined above essentially all metals meet this requirement. It is preferred that the metal is selected from the group consisting of titanium, zirconium, silicon, nickel, iron and aluminum. It is especially preferred that M is aluminum. Typically, R can be any organic radical that can be distilled at temperatures below about 300°C. Since the alkoxide (-OR moiety) is not incorporated into the primer, the important criteria associated with it is that the resultant alcohol can be volatilized at temperatures that are not high enough to damage the primer or substrate. It is preferred that R is an alkane radical from C₁ to C₁₀. It is especially preferred that R is methyl, ethyl, propyl or sec-butyl as these radicals are volatilized as alcohols at relatively low temperatures. In addition, the alkoxides can be modified by incorporation of varying amounts of additives such as phosphate, silicate or magnesium oxide without affecting the sizing properties. Mixtures of the above metal alkoxides may also be used in the practice of this invention. In addition, partial hydrolyzates of the metal alkoxides can also be used as starting material, i.e., dimers, trimers, etc. of the monomeric alkoxides.
- The above metal alkoxides hydrolyze to amorphous hydrated metal oxides (sizing) when exposed to moisture such as atmospheric moisture or moisture on the fiber substrate surface and optionally heat as described below. An exemplary reaction believed to occur is that of aluminum alkoxide to alumina. The initial hydrolyzation reaction of aluminum alkoxides is empirically illustrated as
Al(OR)₃ + H₂O Al(OR)₂(OH) + R(OH) (1)
This reaction proceeds rapidly with further hydrolyzation-polymerization to
2Al(OR)₂(OH)+H₂O >RO--O--OR+2 ROH, etc. (2)
to incorporate n aluminum ions, i.e. AlnOn-1(OH)(n+2)-x(OR)x assuming linear polymerization for simplicity. As the reaction proceeds the number of OR groups, i.e. x, relative to n decreases to a value depending on the hydrolysis temperature and available moisture concentration. Under normal application conditions, the ratio of residual OR groups as designated by x is less than 4 and n is 28 or greater. Such low levels of -OR do not impede the performance of the primer. In contrast, zirconium alkoxide is believed to hydrolyze to a hydrated oxide, i.e. ZrO₂ · 1.7 H₂O having no residual -OR or -OH groups. - The thickness of this primer layer can vary effectively from about 1.5 nanometers (nm) to about 1000 nm. Above about 1000 nm, the layer can be so thick as to create stress risers and to form a weak boundary layer. Below about 1.5 nm, the layer does not provide the properties such as crack propagation resistance and stress transfer at the levels typically required. In addition, it is preferable to apply the primer to the fiber surface with a plurality of layers of metal alkoxide as this facilitates removal of volatiles and solvent which can be more difficult to achieve from a single thick application.
- Any fiber may be used in the practice of this invention that is useful for making composite articles. Examples include amide, carbon, metal, boron, glass, silicon carbide, alumina and KEVLARTM fibers (DuPont DeNemours, E.I., Co., Wilmington, Delaware). Preferably graphite or glass fibers are used as these provide the properties most desired of composites such as strength and light weight. It is especially preferred to use graphite available from BASF as it resists environmental stresses and produces lightweight composites having good strength.
- Any conventional resin matrix can be used for the practice of this invention that is useful for making composite articles. Preferably epoxides, bis-maleimides or polyimide resins are used as these provide the properties most desired such as good strength. It is especially preferred to use 3501-6TM resin available from Hercules, Inc. (Wilmington, Delaware) 5208 resin available from Narmco,Arimide NTM resin (E.I. DuPont DeNemours) and LARC-TPI resin (Nasa) as they resist environmental stresses, are strong and are commercially readily available.
- Any method of making a composite may be used for the practice of this invention that provides composites having reinforcing amorphous hydrated metal oxide coated fibers. For example, a chopped fiber composite can be made by mixing chopped fibers coated with amorphous hydrated metal oxide and resin in a mold under pressure and optional heat. However, it is preferred to apply a coating of metal alkoxide to the carbon fibers by drawing the fiber through a solution of metal alkoxide. The metal alkoxide coated composite fibers are then maintained at a temperature of about 25°C to about 300°C as below 25°C the reaction kinetics are typically too slow and above 400°C loss of desirable fiber properties or crystallization of the coating may occur with an accompanying loss of mechanical strength. It is especially preferred to heat the aluminum alkoxide coated fibers to a temperature of about 100°C to about 200°C as the lower temperatures minimize the risk of mechanical property degradation of fibers and morphological transformation of the coatings leading to shrinkage and embrittlement. Surprisingly, an increase in temperature from room temperature (R.T.) to about 325°C does not affect an increase in metal alkoxide conversion to amorphous hydrated metal oxide.
- Once coated with amorphous hydrated metal oxide, the reinforcing carbon fibers (tows) are dipped into the resin solution to form a tape prior to the molding step. Typically, the resin impregnated fibers are allowed to dry so that any solvent will evaporate. The graphite tape can then be cut into plies (layers of impregnated fibers) of the desired dimensions of the article to be fabricated. The plies are then stacked to create the desired thickness, typically in metal molds coated with mold release agent such as Micro Spray♢ (Micro-Spray Products Inc.). The assembled ply layup is then placed in a press and exposed to pressures and temperatures conventional for the resin system used and application desired.
- Inorganic primer was applied to unsized, surface treated, Celion 6000 graphite fiber available from BASF Corporation by drawing the fiber tow through a 1% toluene solution of Stauffer Chemical Company aluminum alkoxide, E-8385, and drum winding the coated tows. The resulting wound tape was heated at 200-325°C in an air oven to dry and thus produce the amorphous alumina coating.
- The coated fibers and uncoated fibers as controls were tested for high temperature oxidation resistance using thermogravimetric analysis (TGA). The results are depicted in the Figure. In the Figure, percent weight loss (Y) is graphed against temperature in degrees centigrade (X). There is a significant difference in the thermal oxidative stability as shown by curve (A) (treated graphite) in comparison to curve (B) (untreated graphite).
- This primer may be used to advantage in a wide range of composites. For example, chopped fiber, filament wound and ordered fiber composites benefit from this primer. While this invention has been described in terms of a metal alkoxide, a mixture of various metal alkoxides can be used.
- This sizing coating provides improved oxidation resistance at elevated temperatures. At temperatures of about 100°C to about 975°C, this sizing results in more oxidatively stable fibers and hence composites. The resulting properties such as tensile and flexural strengths of composites made with the inorganic fiber sizing are believed at least equivalent or better than composites made using conventional organic fiber sizing. Yet the inorganic sizing agent can be utilized at thinner layers than the 1.0 wt. % loading of fibers typical of organic sizing. Thicker layers tend to set up stress risers and to form a weak boundary layer as the components segregate. Also, because of its oxidation resistance the inorganic sizing can be used equally as well with high temperature resins such as polyimides or with low temperature resins such as epoxy systems unlike organic sizing agents which are typically temperature specific.
- It is also believed that composites using the inorganic sized fibers will have improved wet strength retention, be less subject to microcracking and exhibit improved fracture toughness and impact strength properties. Also, the inorganic insulating sheath will have little, if any, deleterious effect on electrical equipment (e.g., cause shorting) should such a composite disintegrate.
- This invention provides an amorphous hydrated metal oxide sizing for fiber reinforced composites resulting in improved oxidation resistance. Thus, it makes a significant advance in the aerospace industry by providing new technology relating to composites.
- It should be understood that the invention is not limited to the particular embodiments shown and described herein, but that various changes and modifications may be made without departing from the spirit and scope of this novel concept as defined by the following claims.
Claims (5)
1. A method of using a fiber reinforced polymeric matrix composite material wherein the fiber reinforcement has a layer of amorphous hydrated metal alkoxide formed by deposition onto the fiber and subsequent hydrolysis of a layer of MxORy or combinations thereof where
a) x is 1;
b) y is 2, 3 or 4;
c) M has a valence of 2, 3 or 4; and
d) R is an organic radical;
wherein the improvement comprises: exposing the composite to temperatures of about 100°C to about 975°C wherein the composite has greater oxidative stability.
a) x is 1;
b) y is 2, 3 or 4;
c) M has a valence of 2, 3 or 4; and
d) R is an organic radical;
wherein the improvement comprises: exposing the composite to temperatures of about 100°C to about 975°C wherein the composite has greater oxidative stability.
2. The method as recited in claim 1 wherein M is selected from the group consisting of titanium, aluminum, and silicon and the fiber is selected from the group consisting of graphite, glass, silicon carbide, alulmina, boron and polyaramid.
3. The method as recited in claim 1 wherein the fiber is graphite and M is aluminum.
4. The method as recited in claim 1 wherein the composite is exposed to temperatures of about 500°C to about 975°C.
5. The method as recited in claim 1 wherein MxORy is partially hydrolyzed prior to application of the fiber.
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US28600088A | 1988-12-19 | 1988-12-19 | |
US286000 | 1988-12-19 |
Publications (2)
Publication Number | Publication Date |
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EP0387468A2 true EP0387468A2 (en) | 1990-09-19 |
EP0387468A3 EP0387468A3 (en) | 1991-06-05 |
Family
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Application Number | Title | Priority Date | Filing Date |
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EP19890630216 Withdrawn EP0387468A3 (en) | 1988-12-19 | 1989-12-08 | Stable amorphous hydrated metal oxide sizing for fibres in composites |
Country Status (3)
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EP (1) | EP0387468A3 (en) |
JP (1) | JPH02214748A (en) |
DE (1) | DE387468T1 (en) |
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US5227199A (en) * | 1992-01-14 | 1993-07-13 | General Atomics | Processes for applying metal oxide coatings from a liquid phase onto multifilament refractory fiber tows |
WO2008058924A1 (en) * | 2006-11-15 | 2008-05-22 | Herbert Costard | Method for the production of flameproofed fiber composite materials or prepregs |
Families Citing this family (1)
Publication number | Priority date | Publication date | Assignee | Title |
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CN113897776A (en) * | 2021-11-29 | 2022-01-07 | 中复神鹰碳纤维股份有限公司 | Silicon titanium based modified sizing agent and preparation method thereof |
Citations (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
LU61102A1 (en) * | 1969-06-12 | 1970-08-10 | Ici Ltd | PROCESS FOR THE PREPARATION OF COMPLEX ALUMINUM PHOSPHATE |
US3713865A (en) * | 1968-07-05 | 1973-01-30 | Ducommun Inc | Composite product and method of making same |
US4376803A (en) * | 1981-08-26 | 1983-03-15 | The Aerospace Corporation | Carbon-reinforced metal-matrix composites |
US4376804A (en) * | 1981-08-26 | 1983-03-15 | The Aerospace Corporation | Pyrolyzed pitch coatings for carbon fiber |
EP0074573A1 (en) * | 1981-09-03 | 1983-03-23 | Toyota Jidosha Kabushiki Kaisha | Method for making carbon/metal composite pretreating the carbon with tetraisopropyltitanate |
-
1989
- 1989-12-08 EP EP19890630216 patent/EP0387468A3/en not_active Withdrawn
- 1989-12-08 DE DE1989630216 patent/DE387468T1/en active Pending
- 1989-12-19 JP JP32940589A patent/JPH02214748A/en active Pending
Patent Citations (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3713865A (en) * | 1968-07-05 | 1973-01-30 | Ducommun Inc | Composite product and method of making same |
LU61102A1 (en) * | 1969-06-12 | 1970-08-10 | Ici Ltd | PROCESS FOR THE PREPARATION OF COMPLEX ALUMINUM PHOSPHATE |
US4376803A (en) * | 1981-08-26 | 1983-03-15 | The Aerospace Corporation | Carbon-reinforced metal-matrix composites |
US4376804A (en) * | 1981-08-26 | 1983-03-15 | The Aerospace Corporation | Pyrolyzed pitch coatings for carbon fiber |
EP0074573A1 (en) * | 1981-09-03 | 1983-03-23 | Toyota Jidosha Kabushiki Kaisha | Method for making carbon/metal composite pretreating the carbon with tetraisopropyltitanate |
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US5227199A (en) * | 1992-01-14 | 1993-07-13 | General Atomics | Processes for applying metal oxide coatings from a liquid phase onto multifilament refractory fiber tows |
WO2008058924A1 (en) * | 2006-11-15 | 2008-05-22 | Herbert Costard | Method for the production of flameproofed fiber composite materials or prepregs |
Also Published As
Publication number | Publication date |
---|---|
DE387468T1 (en) | 1991-06-13 |
JPH02214748A (en) | 1990-08-27 |
EP0387468A3 (en) | 1991-06-05 |
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