NONGRAPHITIC IGNITION RESISTANT STRUCTURES

Abstract: A structure (20) which is particularly useful as a panel for the interior of airplanes comprises at least one polymeric matrix (24) having from 20 to 50 percent by weight nonlinear carbonaceous fibers and from 50 to 80 percent by weight organosilicone polymer incorporated therein. The structure is formed by heat and pressure application. On one surface of the structure, a polymeric film (22), preferably a polyester film, can be attached. The film advantageously can be provided with a decorative embossment (21). On the opposite surface of the matrix (24) there can be provided a reinforcement scrim (25). A layer of a wool-like fluff (26) of nonlinear and/or linear carbonaceous fibers can be provided on the opposite surface of the scrim (25) when thermal and sound insulation is desired. The opposite side of the fluff (26) is advantageously covered with a film or sheet (28) of a metal or polymeric material, or the like.

Description: NONGRAPHITIC IGNITION RESISTANT STRUCTURES The present invention relates to a means for synergistically improving the resistance to oxidation and to improve the thermal stability of carbonaceous materials made from polymeric precursor materials. The invention also relates to improving the ignition resistant properties of silicone polymers or silicone containing polymers. More particularly, the invention resides in a nongraphitic ignition resistant structure prepared from the combination of a nongraphitic carbonaceous material having a char formation greater than about 65 percent, an LOI value greater than 40, and a thermal conductivity of the material when in fiber form of less than 1 BTU(ft/hr)(ft 2 )(°F)[1.72 w/m 2 (K)], and an organosilicone polymer. The organosilicone polymer provides a synergistic improvement in the ignition resistant properties of the structure without any substantial alteration of the desirable characteristics of the carbonaceous material. On the other hand, the carbonaceous material can be used to enhance the ignition resistance of organosilicone polymer structures. Carbonaceous fibers and their method of preparation are known and are described in European Publication Serial No. 0199567, published October 29, 1986, to F. P. McCullough et al. and entitled, "Carbonaceous Fibers with Spring-Like Reversible Deflection and Method of Manufacture." The use of carbonaceous fibers for sound and thermal barriers is known from WIPO Publication No. 88/02695, published April 21, 1989, to McCullough et al. and entitled, "Sound and Thermal Insulation." These fibers in the form of battings and mats are now being proposed for use in areas subjected to high temperatures and degrading gases, especially oxidizing gases. The prior carbonaceous fibers or fiber structures have also been useful to provide a flame barrier. However, flame barriers in many cases are effective only against static or quiescent flames. There are occasions, however, when it is desirable to provide protection against dynamic flames which are produced as a result of rapid air flow and increased air pressure forces. Such dynamic flames can cause physical erosion of a flame barrier. U.S. Patent No. 4,308,471 (K. Tanaka et al.) granted December 29, 1981, and U.S. Patent No. 4,814,017 (B. E. Yoldas et al.) granted March 21, 1989, disclose organoalkoxysilanes which can be used in the structures of the present invention. U.S. Patent No. 3,811,997 (E. L. Yuan) granted May 21, 1974, discloses smoke and flame resistant structural articles for use in aircraft. The articles are constructed of a laminate or a honeycomb structure and are provided with a thin film of polyamine or polyamide to retard combustion of the underlying laminate and reduce smoke effusion from any burning that does occur. U.S. Patent No. 3,914,494 (I. K. Park) issued October 21, 1975, discloses a material for use, for example, as a facing sheet for a sandwich liner for noise suppression in a jet engine. The lightweight material includes woven carbon fibers in a resin matrix. The resin can be a phenolic or a polyimide. Burning phenolic resins, however, produce a highly irritating and toxic smoke. U.S. Patent No. 4,642,644 (Goldberg et al.) discloses polyaromatic precursor and carbonaceous materials which can be used *in the present invention. U.S. Patent No. 4,255,483 (N. R. Byrd et al.) issued March 10, 1981, discloses a firewall for use in environments such as an aircraft engine nacelle. The firewall includes a graphite fiber or glass cloth embedded in a silica containing polyimide resin. The presence of the silica is described as being necessary to provide the polyimide resin and the firewall with the desired stability in the presence of a fire and with low thermal conductivity. Carbonaceous materials, when in the form of fibers or fiber structures, are particularly well adapted for use in areas that are subjected to high temperatures and degrading gases, especially oxidizing gases. -2 -. The term "carbonaceous fibers" as used herein is intended to include linear or nonlinear carbonaceous fibers, or mixtures of such fibers. Such fibers having an aspect ratio (1/d) of greater than 10:1. The term "carbonaceous fiber structure" as used herein relates to polymeric fibers whose carbon content has been irreversibly increased as a result of a chemical reaction such as a heat treatment, as disclosed in European Publication No. 0199567, and is intended to include a multifilament tow composed of many filaments, a multiplicity of entangled carbonaceous fibers forming a wool-like fluff, a nonwoven batting, matting or felt, a woven web, scrim or fabric, a knitted cloth, for example a plain jersey knit, or the like. The structure when in the form of a batting or wool-like fluff may be prepared by conventional needle-punching means. The term "nongraphitic" as used herein relates to those carbonaceous materials having an elemental carbon content of less than 92 percent, which are substantially free of oriented carbon or graphite microcrystals of a three dimensional order, and as further defined in U.S. Patent No. 4,005,183. It should be understood that the term "particles" as used herein is intended to include powders, platelets, and the like. The term "ignition resistant" as used herein generally applies to any one of the characteristics that are referred to as flame arresting, flame retarding, fire shielding and fire barrier, as defined in 14 CFR 25.853(b). An article is considered to be "flame retarding" to the extent that once an igniting flame has ceased to contact unburned parts of a textile article, the article has the inherent ability to resist further propagation of the flame along its unburned portion, thereby stopping the internal burning process. Recognized tests to determine whether an article is flame retarding are, inter alia, the American Association of Textile Chemists and Colorists Test 0 Method 34-1966 and the National Bureau of Standards Test described in DOC FF 3-71. An article is considered to be "flame arresting" if it has the ability to block or prevent C - flames from contacting unburned parts of a flammable substance for at least five (5) minutes. An article is considered to be "fire shielding" if it is capable of deflecting flames and the radiation 0 therefrom in a similar manner as aluminum coated protective garments, which are known in the art. Fire barriers have the characteristic of being nonflammable and flame retarding and also provide 5 thermal insulation characteristics. The term "polymeric" or "polymeric resin" used herein includes natural polymers as well as other organic polymeric resins including organosilicone -, Q polymers. The term "carbonaceous" used herein refers to carbonaceous materials which have a carbon content of at least 65 percent and which have been prepared by the method described in the herein referenced EP Publication No. 0199567. The term "static flames" as used herein relates to flames which are subject to substantially little or no pressure such as, for example, the flame of a match, a candlestick or a butane lighter. The term "dynamic flames" as used herein relates to flames which are acting under a pressure such as disclosed in FAR 25.855 Appendix F. The term "silicone polymer" as used herein relates to the set or cured polymers which can be obtained from the silicone resins or the hydrolyzed partial condensation products of siloxanes such as manufactured by Dow Corning Corporation. The term "silicone resin" as herein disclosed relates to any precursor material which is capable of being polymerized to form the organosilicone polymers of the invention. The silicone resins include, but are not limited to, oligomers derived typically by the partial hydrolysis of a silane. The oligomers generally have a backbone of siloxane units and active sites which may be cured thermally and/or hydrolytically to form the organosilicone polymer. The silicone resins further include the precursor silane compounds which are capable of forming organosilicone polymers through a free radical condensation reaction or a heat condensation reaction. Typically the heat condensation and/or free radical condensation reactions are performed utilizing silanes having epoxy or vinyl moieties. The term "reinforcement scrim" relates to metallic, glass or fibrous structures which are woven, nonwoven, knitted or the like, and which are utilized to provide a mechanical or physical reinforcement to structures against dynamic forces. The term includes structures containing unidirectional fibers. The nonlinear carbonaceous fibers preferably used in the invention are resilient, shape reforming and have a reversible deflection greater than about 1.2:1. It should be understood that the reversible fiber deflection comprises two components, pseudoelongation and fiber elongation. Pseudoelongation results from the nonlinear configuration and/or false twist imposed on the fiber. Fiber elongation is the elongation to fiber break after the fiber has been made linear. All percentages referred to herein are in percentage by weight. The carbonaceous materials that are suitably employed in the present invention have a LOI value of greater than 40 as measured according to test method ASTM D 2863-77. The method is also known as the "oxygen index" or "limited oxygen index" (LOI) test. With this procedure the concentration of oxygen in 0 2 /N 2 mixtures is determined at which a vertically mounted specimen is ignited at its upper end and just continues to burn. The size of the specimen is 0.65 x 0.3 cm with a length of from 7 to 15 cm. The LOI values of different materials are calculated according to the following equation: -8- [0,] LOI = 100 [O, + N,] The carbonaceous materials of the invention are characterized as having a thermal conductivity of less than 1 BTU(ft/hr)(ft 2 )(°F)[w/m 2 (K)]. The percent char formation and thermal conductivity of various other materials are as follows: Thermal Conductivity BTU {ft/hr)(ft 2 )(°P) % Char [w/m 2 (K)] Carbonaceous particles of the invention: (18.6% N 2 ) >65 0.1 [0.172] (16.0% N 2 ) >65 0.2 [0.344] KEVLAR * * * 60 <1.0 [<1.72] KODEL™ 410 polyester 10 <1.0 [<1.72] Polyacrylonitrile 60 <1.0 [<1.72] Oxidized polyacrylonitrile 60 <1.0 [<1.72] THORNEL ® 300* >95 4.84 [8.33] Cotton >30 <1.0 [<1.72] Rayon <50 <1.0 [<1.72] Polycarbonate 22 <1.0 [<1.72] Polyethylene terephthalate 10 <1.0 [<1.72] Carbon particles >90 2.5 [4.3] THORNEL ® P758** >95 106.48 [183.1] - • Trademark of Amoco Corp., Danbury, CT, for graphite yarn **Trademark of Amoco Corp., Danbury, CT, for graphite yarn derived from pitch. The measurement of char formation as illustrated in the table and as discussed herein is made by using a standard thermogravimetric analysis apparatus that is adapted to perform the analysis in a nitrogen atmosphere. The apparatus is described in Encyclopedia of Polymer Science, Vol. 14, p. 21, John Wiley & Son, 1971. The measurement is performed by loading a sample onto a sample pan of the thermogravimetric analysis apparatus. The sample is then heated in an nitrogen atmosphere at a rate of 10°C/min. from ambient temperature to 900°C. The thermogravimetric apparatus records the sample weight remaining versus temperature. The percent of original weight remaining at 800°C is taken as the char percentage. More particularly, the present invention relates to an ignition resistant structure comprising a nonflammable, nongraphitic carbonaceous material having an LOI value of greater than 40, a char formation of greater than 65 percent, and a thermal conductivity of less than 1 BTU(ft/hr) (ft 2 ) (°F) [1.72 w/m 2 (K)], and an organosilicone polymer which is characterized by (Si-0-Si-0) n recurring units for imparting ignition resistance to the structure. The amount of organosilicone polymer utilized in the ignition resistant structure of the invention is at least an amount sufficient to provide ignition resistance. Preferably, the organosilicone polymer is present in an amount of from 0.5 to 90 percent by weight, depending on the characteristics of the structure desired. The organosilicone polymers utilized in the invention are prepared from precursor silicone resins by hydrolysis, heat condensation, or free radical condensation reaction. Preferred organosilicone polymers are those which can be prepared by heat setting or curing a compound selected from a hydrolyzed partial condensation product of R^SifOR 1 ) 4 - x or R χ Si(OOR' ) 4 - x , wherein R is an organic radical and R' is a lower alkyl or phenyl radical, and x is at least 1 but less than 4. Preferably, R is selected from lower alkyl, alkenyl, substituted alkyl and aryl. The preferred aryl is phenyl. These organosilicone polymers are obtained by thermosetting or curing a silicone resin by means of a catalyst. Other suitable silicone resins are mentioned in the Dow Corning Corp. publication entitled, "Information About High Technology Materials," 1986. Preferred silicone resins which can be polymerized by hydrolysis are the hydrolyzed partial condensation products of trimethoxymethylsilane, methoxytrime hyl- silane, dimethoxydimethylsilane, and the like. The organosilicone polymers when utilized in amounts of as little as 0.5 percent have resulted in enhancing the ignition resistance and resistance to oxidation of, for example, carbonaceous fiber structures and/or protection of the fibers while maintaining the favorable characteristics of the fiber structure. Amounts of from 0.5 to 20 percent have enhanced the ignition resistance, fire resistance and resistance to oxidation of most carbonaceous materials and/or protection of the materials, particularly fibers, while aintaining the favorable characteristics of the materials. The carbonaceous material improves the ignition resistance and stabilizes a structure which primarily comprises a cured or set organosilicone polymer. For example, a surface coating of the carbonaceous material in an amount of as little as 0.5 percent, when applied to a surface of the polymer, provides an effective flame barrier, while the distribution of the carbonaceous material throughout the organosilicone polymer improves the ignition resistance of the structure on the whole. Preferably the polymer structure contains the carbonaceous material along its surface as either fibers, particles, films, or the like. In accordance with another embodiment of the invention there is provided a flame barrier and fire resistant structure of the carbonaceous material and the organosilicone polymer for dynamic flames. More particularly, the invention provides a flame barrier and fire resistant structure comprising a compression formed thermoplastic or thermosetting polymeric matrix containing from 10 to 95 percent by weight of nonflammable nongraphitic carbonaceous fibers having an LOI value of greater than 40, a char formation of greater than 65 percent, and a thermal conductivity of less than 1 BTU(ft/hr)(ft 2 )(°F) [1.72 w/m 2 (K)], and an organosilicone polymer having (Si-0-Si-0) n recurring units for imparting ignition resistance to the structure. Advantageously, carbonaceous fibers and/or particles are intimately blended with the organosilicone -12- polymer at least at the surface of the organosilicone polymer. In accordance with another embodiment, the structure of the invention can comprise at least one structural panel of a compression formed composite of a thermoplastic or thermosetting resin matrix containing from 10 to 95 percent by weight of said nonflammable carbonaceous material and an organosilicone polymer to impart ignition resistance to the structure. The panel can be used in combination with a nonflammable reinforcement scrim comprising, for example, a woven, nonwoven, or knitted fabric, web, foam or a metallic screen or glass screen. Advantageously, the scrim is compressed between a pair of panels. Preferably, the carbonaceous fabric or web is also treated with said silicone resin. The structure, in combination with a reinforcement scrim, provides a flame barrier against a dynamic flame as described in FAR 25.855 Appendix F. The structure can be used to provide a flame barrier in aircraft, land or marine vehicles. The carbonaceous structures of the present invention provide an improvement over fiberglass structures which utilize phenolic binders. The improvement includes an advantage in weight as well as in smoke characteristics. In another embodiment, the carbonaceous fibers and/or particles and the organosilicone polymer can be blended with at least one other thermoplastic or thermosetting polymer. Various structures, including obvious modifications and adaptations thereof, will be apparent to those of ordinary skill in the art from the following drawings and further description of the preferred embodiments. Figure 1 is a perspective view partially in cross section of a structural panel of the invention, and Figure 2 is a perspective view of a structural panel of the invention with a sound absorbing and thermal barrier layer. In the broadest aspects of the invention, there is provided an improvement in the ignition resistance of carbonaceous materials and resistance to oxidation at high temperatures. There is further provided an improvement in thermal resistance of organosilicone polymer structures. > In accordance with another embodiment, the invention is directed to a composite which comprises a polymeric resin, such as a thermoplastic or thermosetting resin, which is compressed together with a batting of nonflammable carbonaceous fibers and/or particles. Prior to compression, the batting is treated with an organosilicone polymer in an amount sufficient to provide ignition resistance. Generally, there is utilized an amount of up to 20 percent, preferably about 10 percent, of a polymerizable silicone resin. The structure of this invention is particularly effective in forming a fire resistant or flame shielding structural panel for use in vehicles and installations, particularly airplanes. In an alternative embodiment, the structure of the present invention contains from 10 to 95 percent. preferably from 20 to 75 percent, by weight, non¬ flammable carbonaceous material, preferably fibers having an aspect ratio (1/d) of greater than 10:1. In a preferred embodiment, the carbonaceous fibers are nonlinear and possess a sinusoidal or coil¬ like configuration or a more complicated structural combination of the two. The polymeric resin used in the structure of the present invention can be selected from any of the conventional type resins such as thermoplastic resins and thermosetting resins. Thermoplastic resins, for example, can include polyethylene, ethylenevinyl acetate copolymers, polypropylene, polystyrene, polyvinyl chloride, polyvinyl acetate, polymethacrylate, acrylonitrile- butadiene-styrene copolymers (ABS), polyphenylene oxide (PPO), modified PPO, polycarbonate, polyacetal, polyamide, polysulfone, polyether sulfone, polyolefins, polyacrylonitrile, polyvinylidene chloride, polyvinyl acetate, polyvinyl alcohol, polyvinyl pyrrolidone, ethyl cellulose, polyvinyl chlorodivinyl acetate copolymer, polyacrylonitrile-styrene copolymer, polyacrylonitrile- vinyl chloride copolymer, carboxymethylcellulose, polyparaxylene, polyimide, polyamide-imide, polyester imide, polybenzimidazole, polyoxadiazole, and the like. Thermosetting resins, for example, may include phenolic resins, polysiloxanes, urea resin melamine resin, alkyl resin, vinyl ester resins, polyester resin, xylene resins, furanic resins, and the like. The thermosetting resins also include the organosilicones used to provide the improved fire resistant effect. Other suitable resinous materials are disclosed in Modern Plastics Encyclopedia, 1984-85, Vol. 61, No. 10A, McGraw-Hill, New York, New York. As shown in Figure 1, an exemplary structure of the invention in its simplest form comprises a heat cured panel 10 comprising a polymeric matrix 16 which contains the carbonaceous fibers and organosilicone polymer of the invention. A polymeric or metallic film 12 can additionally be provided on at least one surface of the panel to form a vapor barrier or decorative cover. The film 12 can be compressed onto the panel during a compression forming operation. Optionally, carbonaceous particles or platelets can be added. In Figure 2, there is shown a structure 20 which is particularly useful as a panel for the interior of airplanes. The structure 20 comprises at least one polymeric matrix 24 having from 20 to 50 percent by weight nonlinear carbonaceous fibers and from 50 to 80 percent by weight organosilicone polymer incorporated therein. The structure is formed by heat and pressure application. On one surface of the structure, a polymeric film 22, preferably a polyester film, can be attached. The film advantageously can be provided with a decorative embossment 21. On the opposite surface of the matrix 24 there can be provided a reinforcement scrim 25 as hereinbefore defined. A layer of a wool¬ like fluff 26 of nonlinear and/or linear carbonaceous fibers can be provided on the opposite surface of the scrim 25 when thermal and sound insulation is desired. The opposite side of the fluff 26 is advantageously covered with a film or sheet of a metal or polymeric material, or the like. The panel can be prepared by enclosing a wool¬ like fluff of carbonaceous fibers between sheets of a polymeric material, heating the polymeric sheets to the softening point and subjecting the sheets and fiber fluff to a compressive force. The compressive force is dependent upon the thickness of the panel desired and the use for which the panel is intended. The polymeric matrix as well as the thermal and sound insulating materials can contain biostabilizers such as tributyl tin and its derivatives, copper-bis(8- hydroxyquinoline), and the like. Preferred polymeric resins for forming panels for use in, for example, airplanes are the commercial polyesters such as, for example, polyester fibers sold by Eastmen Chemical Products under the trademark KODEL 410, 411, 432 and 435, and by E. I. du Pont De Nemours under the trademark DACRON 262 and 124W. The carbonaceous fibers of this invention are prepared by heat treating in an inert atmosphere a suitable stabilized or oxidized precursor polymeric fiber which can be made into an irreversibly heat set, fiber or filament without tension or stress. Preferably, the stabilized precursor material used in the present invention is derived from stabilized staple polyacrylonitrile (PAN) filaments. Polymeric precursor materials such as stabilized acrylic filaments which are advantageously utilized in preparing the carbonaceous fibers of the invention are selected from one or more of the following: acrylonitrile homopolymers, acrylonitrile copolymers and acrylonitrile terpolymers. The copolymers preferably contain at least about 85 mole percent of acrylonitrile units and up to 15 mole percent of one or more monovinyl units of styrene, methylacrylate, methyl methacrylate, vinyl chloride, vinylidene chloride, vinyl pyridine and the like copolymerized therewith. The acrylic filaments can also comprise terpolymers wherein the acrylonitrile units are at least about 85 mole percent. The preferred precursor materials are typically prepared by melt spinning, dry or wet spinning the precursor materials in a known manner to yield a monofilament or multifiber tow. The fibers or tow are then heated to a temperature and for a period of time as described in European Publication No. 0199567. In the case of polyacrylonitrile based fibers, the fibers can be formed by conventional methods such as by melt, dry or wet spinning a suitable liquid of the precursor material. The polyacrylonitrile (PAN) based fibers which have a normal nominal diameter of from 4 to 25 micrometers are collected as an assembly of a multiplicity of continuous filaments in tows. The fibers are then stabilized, for example by oxidation or any other conventional method of stabilization. The stabilized fibers or tows are thereafter heat treated according to the present invention, in a relaxed and unstressed condition, at elevated temperatures in an inert non-oxidizing atmosphere for a period of time to produce a heat induced thermoset reaction. A nitrogen content from 5 to 35 percent is maintained. At a temperature range of from 150°C to 525°C and above, the fibers are generally provided with a temporary to substantially permanent or irreversible heat set. It is to be understood that the fiber or tow can be initially heat treated at the higher range of temperatures so long as the heat treatment is conducted while the fiber is in a relaxed or unstressed state and under an inert, non-oxidizing atmosphere including under a reduced pressure atmosphere. As a result of the higher temperature treatment of 525°C and above, a substantially permanently or irreversible heat set is imparted to the fibers or tows. The resulting fibers or tows can be used per se or can be formed into a wool-like fluff. Such wool-like fluff has a bulk density of from 2.4 to 32 kg/m 3 . A number of methods known in the art can be used to create a fluff or batting-like body of considerable loft. The precursor stabilized linear polymeric fibers are prepared from well-known materials such as pitch (petroleum or coal tar), polyacetylene, acrylonitrile based materials, e.g., a polyacrylonitrile copolymer such as GRAFIL-01 ™ (trademark of E.I. du Pont de Nemours & Co.), polyphenylene, polyvinylidene chloride, polyaromatic amides (KEVLAR ™ , a trademark of E.I. du Pont de Nemours & Co.), polybenzimide resin, SARAN ™ (trademark of The Dow Chemical Company), and the like. The carbonaceous fibers derived from polyacrylonitrile based materials which can be utilized in the invention are classified into three groups. In a first group, the carbonaceous fibers have a carbon content of greater than 65 percent but less than 85 percent, are electrically noncσnductive and do not possess any electrostatic dissipating charac- teristics, i.e., they are not able to dissipate an electrostatic charge. The term electrically nonconductive as utilized in the present invention relates to a resistance of greater than 4 x 10 6 ohms-cm (10 7 ohms-in) when measured on a 6K (6000 filaments) tow of individual fibers having a diameter of from 4 to 20 microns. When the fiber is a stabilized and heat set polyacrylonitrile based fiber, it has been found that a nitrogen content of about 18 percent or higher results in an electrically nonconductive fiber. When linear carbonaceous fibers are being utilized in the invention it is preferably that the fibers having the electrical characteristics of the first group. In a second group, the carbonaceous fibers are classified as being partially electrically conductive (i.e., having a low conductivity) and having a carbon content of greater than 65 percent but less than 85 percent. The percent nitrogen content of such fibers is generally from 16 to 20 percent. Low conductivity means that a 6K tow of fibers in which the individual precursor fibers have a diameter of from 4 to 20 micrometer, has a resistance of from 4 x 10 6 to 4 x 10 3 ohms-cm (10 7 to 10 4 ohms-in). In a third group are fibers having a carbon content of at least 85 percent, but less than 92 percent, and a nitrogen content of at least 5 percent. These fibers are characterized as having a high electro- conductivity. That is, the fibers have an electrical -20- resistance when measured on a 6K tow of less than 4 x 10 3 ohms-cm (10 4 ohms-in). The carbonaceous fibers of the present invention may be blended with other synthetic or natural fibers. Examples of other reinforcing and/or conductive fibers that may be used include other carbonaceous or carbon fibers, cotton, wool, polyester, polyolefin, nylon, rayon, asbestos, glass fibers, fibers of silica, silica alumina, potassium titanate, silicone carbide, silicone nitride, boron nitride, boron, acrylic fibers, tetrafluoroethylene fibers, polyamide fibers, vinyl fibers, protein fibers, ceramic fibers such as aluminum silicate, and oxide fibers such as boron oxide, thoria and zirconia. A mat or batting of carbonaceous fibers can also be provided with platelets or particles of suitable silicates, such as the alkaline earth or alkaline metal silicates, to further improve their fire resistance performance. When two battings of carbonaceous fibers are provided that comprise a different denier size for each batting, the battings can be readily joined together by a phenomenon similar to the VELCRO™ "hook and eye" effect. Many different structures can be prepared from the synergistic composites of the invention. Structures prepared for a specific application, such as airplane panels, will depend on the mechanical properties desired by the end-user. Generally, a carbonaceous fiber and/or particle loading of from 10 to 75 percent by weight are preferably used for preparing flexible panels, in combination with other binder resins and/or organosilicone polymers. Exemplary of the structures of the present invention are those set forth in the following examples. Example 1 A. Battings were made by blending an appropriate percentage of each respective opened fiber in a blender/feed section of a sample size 30 cm Rando Webber Model B (manufactured by Rando Machine Corp.). The carbonaceous fibers had an LOI of greater than 40, a specific resistivity greater than 10 2 ohm-cm and a coefficient of emissivity of from 0.75 to 1. The battings thus produced typically were about 2.5 cm thick and had a bulk density in the range of from 6.4 to 96 kg/m 3 . The battings were thermally bonded by passing them on a conveyor belt through a thermal bonding oven at a temperature of about 300°C. B. To produce a flexible panel, the batting of part A was sprayed with Dow Corning 1-2577 conformal coating (a hydrolyzed partial condensation of trimethoxy methyl silane) until 10 percent of the total weight of the batting consisted of the coating. The coated batting was then compressed on a platen press between two vinyl sheets at a pressure of 25 lb/in 2 (172 kPa) at a temperature of 260°F (127°C). In lieu of the conformal coating, a silicone resin, which is polymerizable by either a heat condensation or a free radical condensation can be utilized. -22- Example 2 - Ignition Resistance Test The ignition resistance of the panels of the invention was determined following the test procedure set forth in 14 CFR 25.853 (b) . The test was performed as follows: A minimum of three battings having a dimension of 2.5 cm (thickness) x 15 cm x 30 cm and comprising 80 percent carbonaceous fibers and 20 percent polyester were prepared. The battings were sprayed with a solution of Dow Corning 1-2577 conformal coating (a hydrolyzed partial condensation of trimethoxy methyl silane) which cures by contact with moisture in air. The sprayed battings were compressed at a pressure of 25 lb/in 2 (172 kPa) at a temperature of 127°C to produce flexible panels. The silane coating consisted of 10 percent by weight based on the total weight of the panels. Standard vertical burn tests according to FAR 25.853b were conducted. The panels were conditioned by maintaining them in a conditioning room maintained at temperature of 21°C ± 5°C and at a relative humidity of 50 percent ± 5 percent for 24 hours preceding the test. Each specimen was supported vertically and exposed to a Bunsen or Turill burner with a nominal I.D. tube adjusted to give a flame of 3.8 cm in height. The minimum flame temperature measured by a calibrated thermocouple pyrometer in the center of the flame was 843°C. The lower edge of the specimen was 1.9 cm above the top edge of the burner. The flame was applied to the center line of the lower edge of the specimens for 12 seconds and then removed. Pursuant to the test, the material is said to pass if the material was self-extinguishing, the average burn length did not exceed 20 cm, the average after flame did not exceed 15 seconds, and there were no flame drippings. The panels of the invention passed the test. Example 3 A. A polyurethane foam billet having a dimension of 2.5 cm (thick) x 7.4 cm x 7.5 cm was covered with a panel from Example 1 except that the panel was free of any organosilicone polymer. The covered foam billet was subjected to the vertical burn test according to Example 2. At the conclusion of the test the polyurethane did not drip or burn. However, scorching and degradation of the polyurethane foam was observed where the flame was located. B. A test was run similar to Part A except that a panel of Example 1 was utilized which contained the organosilicone polymer. The polyurethane showed no signs of degradation and there was only a slight discoloration. Example 4 Following the procedure of FAR 25.855 Appendix F entitled, "Test Method to Determine Flame Penetration Resistance of Cargo Compartment Liners," a specimen was prepared which comprised a pair of panels prepared (according to Example 1) with a scrim of plain weave, woven fabric (26 g/m 2 ) of carbonaceous fibers compressed therebetween. The fabric was sprayed so as to contain 10 percent by weight, based on the total weight of the fabric, of Dow Corning 1-2577 conformal coating. A blend of a wool-like fluff of 77 percent -24- carbonaceous fibers and 23 percent polyester fibers was placed as the bottom layer against the panel which was then subjected to a flame with an air velocity before the onset of ignition to from about 16 to 32 km/h. 5 minutes after ignition, the thermocouple on the top side of the panel reached a maximum temperature of 49°C. There was erosion noted where the flames had impacted against the fluff. However, the specimen passed the test. The weight of the panels and scrim was 122 g and the fluff was 40 g. The panels and fluff measured 40 cm x 60 cm. Example 5 A. Following the procedure of Example 4, a specimen was prepared from a pair of panels, prepared by the procedure of Example 1, having a scrim of carbonaceous, plain weave, woven fabric (26 g/m 2 ) compressed therebetween, and a wool-like fluff of carbonaceous fibers on the top. The panels, scrim, and fluff measured 40 cm x 60 cm and had no organosilicone polymer. The total weight of the structure was 150 g. Tbe specimen when subjected to the flame treatment eroded and failed the test after 4.25 min. B. The experiment of Part A was repeated, except that the panels and scrim were treated with the Dow Corning conformal coating. The total weight of the structure was 154 g. The specimen when subjected to the flame treatment for 5 minutes passed the test. The final test temperature reached 113°C. It should be understood that the examples demonstrate that the structures of the invention at relatively low masses are capable of coming well within the temperature requirement of test procedure FAR 25.855. Moreover, a further reduction in mass of the structure is possible without exceeding the test temperature requirement of up to 240°C. Example 6 A specimen similar to that of Example 2 was prepared except that it contained 20 percent carbonaceous fiber, 10 percent conformal coating and 70 percent polyester. The specimen was placed in the National Bureau of Standards (NBS) smoke chamber and tested according to ASTM 662 with a radiant energy of 2.5 watts/cm 2 . For smoldering and flaming conditions the specific optical density, D s , defined by D s =132 log (100%T), where T is the light transmission at time t, was very low. At two minutes D s was less than 10 in the smoldering case and less than 15 in the flaming case. The smoke given off was basically from the polyester in the batting. The 0 2 , CO and C0 2 content of the smoke was analyzed by gas chromatography and the analysis is shown in the following table. Smoke Analysis in NBS Smoke Chamber as Percent Change From Standard Air Concentrations Smoldering Flaming Carbon Dioxide 0.010% 0.327% Oxygen -0.046% -0.451% Nitrogen 0.037% 0.125% A Drager gas detector tube was used to test for hydrogen cyanide in the smoke. None was detected down to a level of 2 ppm. Also investigated was the off-gas produced during heating of the carbonaceous fibers by thermogravimetry/mass spectrometry.. The heating was performed by increasing the temperature from 30°C to 1100°C at a rate of 20°C/min. in a helium atmosphere containing 5.6 percent oxygen. A first drop in weight which was noted was due to the evolution of physisorbed water. The fibers began to lose a large amount of weight at 550°C and were totally pyrolyzed at a temperature of 900°C. The major oxidative degradation product was C0 2 with substantial evolution observed between 375°C and 900°C. Lesser amounts of H 2 0 evolved between 30°C and 215°C and again above 350°C, and NO evolved between 500°C and 700°. There were indications of a little ammonia being evolved between 530°C and 890°C but this could not be confirmed. No HCN was detected by mass spectrometry, nor were any other of the standard gases of concern in the aircraft industry. Example 7 - Flame Barrier Test A test was performed on a 60 cm x 60 cm sample batting of approximately 14 oz/yd 2 (60.6 g/m 2 ) produced on a Rando Webber Model B. The sample was pressed at minimal pressure and was approximately 1.25 cm thick. The sample was placed on a 6.25 mm thick steel plate with a thermocouple (t χ ) adjacent the sample and a thermocouple (t 2 ) adjacent the backside of the plate. The sample was exposed to a large propane/air burner, 500,000 BtW/hr. The test requirements was that after 30 minutes t 2 is less than 450°F (232.2°C) . The results after 40 minutes are shown in the following table: _ fc l fc 2 Flame Temp. Steel Plate Near Front Temperature Time (min.) Surface °F (°C) op (o C ) 0 + 30 sec. 2180 (1176.1) 73 (22.8) 5 2230 (1204.0) 156 (68.9) 10 2235 (1206.8) 202 (94.4) 20 2238 (1208.4) 266 (130.0) 30 2235 (1206.8) 303 (151.6) 40 2240 (1208.6) 316 (154.7) The sample was composed of 81 percent carbonaceous nonlinear fibers heat treated at a 10 temperature of 650°C with a fiber diameter of about 10.8 microns, 9 percent KODEL™ 410 polyester binder fiber (8.5 denier, 1.5 in. staple) and 10 percent Dow Corning Silicone Resin No. 805. "•■* - * Example 8 Following the procedure set forth in U.S. Reissue Patent No. 27,794, a molten precursor polymer was cast into a film which was then heated in a nitrogen 20 atmosphere at rate of 5°C/min. to a temperature of 450°C to form a carbonaceous film. The carbonaceous film was then placed in contact with and laminated onto the surface of a polycarbonate sheet. The carbonaceous film was then sprayed with the 1-2577 Dow Corning conformal 25 resin until 10 percent of the total weight of the film consisted of the coating, thus providing the film with a thin coating of the silicone resin. The film, when subjected to a flame treatment for 5 minutes passed the 30 standard burn test. Example 9 Special acrylic fibers (SAF) manufactured by Courtaulds (U.K.) were dissolved in 10 to 15 percent sodium thiocyanate solution in an amount of 15 percent by weight. The resulting mixture was placed in a beaker and sufficient polymethylmethacrylate beads were added so that the final volume occupied by the beads of the resulting mixture was approximately 65 percent beads and 35 percent solution containing the solvated acrylic fibers. The resulting mixture was stirred and 20 percent by weight carbonaceous fibers added thereto and poured into a small mold. The water from the resulting mixture was allowed to evaporate in an oven at 60°C until a solid material was formed in the mold. This material was then carefully extracted with distilled deionized water to remove most of the sodium thiocyanate which had incorporated into the solid. The extracted solid was then allowed to dry at about 60°C in an oven and then allowed to rise at a temperature of 225°C for a period of 30 min. or longer in order to stabilize the acrylic polymer by oxidation and to drive off the beads in the form of raethylmethacrylate to produce an open cell structure. Most of the beads were driven off in a period of from 30 min. to 8 hours at a temperature of from 225°C to 280°C. The porous solid fiber containing foam material in its stabilized form was placed in a nitrogen purged oven and slowly heated up to a final temperature of 550°C. The resulting carbonaceous foam had a density of from 1 to 1.5 lb/ft 3 and a noticeable compressive resiliency. The resulting foam was sprayed with the 1-2577 Dow Corning conformal resin until 10 percent of the total weight of the foam consisted of the coating, thus providing the foam with a thin coating of the silicone resin. The foam, when subjected to a flame treatment for 5 minutes passed the standard burn test. Having described the invention in detail and by reference to the preferred embodiments thereof, it will be apparent that modifications and variations, such as may be readily apparent to persons skilled in the art, are intended to be included within the scope of the invention as herein defined in the appended claims.

Claims: AMENDED CLAIMS [received by the International Bureau on 4 September 1990 (04.09.90); original claims 4,6,9,16,18 and 19 amended; other claims unchanged (4 pages)] 1. An ignition resistant structure comprising a nongraphitic carbonaceous material having an LOI value of greater than 40, a char formation of greater than 65 percent, and a thermal conductivity of the carbonaceous material of less than 1 BTϋ(ft/hr)(ft 2 )(°F)[1.72 w/m 2 (K)], and an organosilicone polymer having (Si-0-Si-0) n recurring units for imparting ignition resistance to the structure. 2. The structure of Claim 1, comprising from 0.5 to 90 percent by weight of said organosilicone polymer in intimate admixture with said carbonaceous material. 3. The structure of Claim 1 or 2, including another polymeric resin in intimate admixture with said carbonaceous material and said organosilicone polymer. 4. The structure of Claim 1, wherein said carbonaceous material is derived from an oxidation stabilized acrylic material. 5. The structure of Claim 4, wherein said acrylic material is selected from homopolymers, copolymers and terpolymers of acrylonitrile. 6. The structure of Claim 1, wherein said carbonaceous material is in the form of fibers, particles, foam or a film and has a carbon content of greater than 65 percent and a nitrogen content of from 5 to 35 percent. 7. The structure of Claim 6, wherein said carbonaceous fibers are nonlinear carbonaceous fibers. 8. The structure of Claim 7, wherein said carbonaceous fibers are blended with other polymeric fibers. 9. The structure of Claim 1, wherein said organosilicone polymer is derived from a hydrolyzed partial condensation product of a compound selected from R χ Si(OR* ) 4 _ x and R x Si(OOR- ) 4 _ x , wherein R is an organic radical and R * is a lower alkyl or phenyl radical, and X is at least 1 but less than 4. 10. The structure of Claim 9, wherein R is selected from lower alkyl, alkenyl, substituted alkyl and aryl. 11. The structure of Claim 9, wherein said polymer is selected from trimethoxymethylsilane or trimethoxyphenylsilane. 12. A flame barrier and fire resistant structure comprising a compression formed thermoplastic or thermosetting polymeric matrix containing from 10 to 95 percent by weight of nonflammable nongraphitic carbonaceous fibers having an LOI value of greater than 40, a char formation of greater than 65 percent, and a thermal conductivity of less than 1 BTU(ft/hr) (ft 2 ) (°F) [1.72 w/m 2 (K)], and an organosilicone polymer having (Si-0-Si-0) n recurring units for imparting ignition resistance to the structure. 13. The structure of Claim 12, wherein said carbonaceous fibers are derived from an oxidation stabilized acrylic precursor material. 14. The structure of Claim 13, wherein said acrylic material is selected from acrylonitrile homopolymers, acrylonitrile copolymers and acrylonitrile terpolymers, wherein the copolymers contain at least about 85 mole percent of acrylonitrile units and up to 15 mole percent of one or more monovinyl units of styrene, methylacrylate, methyl methacrylate, vinyl chloride, vinylidene chloride, and vinyl pyridine copolymerized therewith. 15. The structure of Claim 12, 13 or 14, wherein said organosilicone polymer is derived from a hydrolyzed partial condensation product of a compound selected from R χ Si(0R') 4 _ χ and R χ Si(OOR' ) 4 _ x , wherein R is an organic radical and R' is a lower alkyl or phenyl radical, and X is at least 1 but less than 4. 16. The structure of Claim 12, including a carbonaceous fiber reinforcing scrim or fabric attached to at least one side of the structure. 17. The structure of Claim 16, wherein said structure is in the form of a panel, and wherein said scrim is compressed between a pair of said panels. 18. The structure of Claim 16, wherein said scrim contains said organosilicone polymer. 19. The structure of Claim 16, including a polymeric film positioned adjacent to the opposite side of the structure. 20. The structure of Claim 16, including a layer of a carbonaceous fiber fluff positioned adjacent to the opposite side of the scrim.

Inventors: HALL DAVID M, MCCULLOUGH FRANCIS P JR, SNELGROVE R VERNON, HALL, DAVID, M., MCCULLOUGH, FRANCIS, P., JR., SNELGROVE, R., VERNON
Applicants: DOW CHEMICAL CO, THE DOW CHEMICAL COMPANY
Application year: 1990
Main classification: B32B9
IPC codes: B32B5, E04B1