초록 ▼

A method of forming a thermoactive binder composite product is performed by injecting a hot dry gas to activate the thermoactive binder. In the preferred embodiment, the hot dry gas is air. The method is particularly beneficial as applied to forming thermoplastic composite products and particularly

A method of forming a thermoactive binder composite product is performed by injecting a hot dry gas to activate the thermoactive binder. In the preferred embodiment, the hot dry gas is air. The method is particularly beneficial as applied to forming thermoplastic composite products and particularly thermoplastic/cellulose composites. Also part of the present invention is a two stage pressing process in which hot gas is injected during the first stage and the press charge is precompressed. The press charge is then placed in a second consolidation press where the hot gas is no longer injected and it is consolidated and cooled. Machinery for practicing the method includes a platen with a platen press which includes upper and lower platens with a plurality of hot air injection jets disposed on the surface of each platen. The platens are spaced apart and surrounded on the sides by an air-permeable containment shell structure to form a compression chamber to hold the base material to be pressed. Other machinery includes a consolidation press.

대표청구항 ▼

[ I claim:] [1.] A method of forming a thermoactive binder composite product comprising the steps of:choosing a base material including a thermoactive binder component;forming the base material into a mat having at least one surface expanse;providing jet structure for delivering a pressurized hot no

[ I claim:] [1.] A method of forming a thermoactive binder composite product comprising the steps of:choosing a base material including a thermoactive binder component;forming the base material into a mat having at least one surface expanse;providing jet structure for delivering a pressurized hot non-condensable gas toward and into the base material through the surface expanse, the jet structure including a plurality of jets adapted to be disposed in a predetermined distribution over the surface expanse with the plurality of jets having an average opening size and being spaced apart in the predetermined distribution by an average distance substantially greater than the average opening size;injecting, via the provided jet structure, the hot non-condensable gas into the base material, where the pressure of the gas is substantially dissipated in passage through the jets prior to entry into the base material at least during a portion of the step of injecting; andpressing the base material to compress it to a first density. [9.] A method of forming a thermoactive binder composite product comprising the steps of:supplying a base material including a thermoactive binder component;providing a platen press with a pair of opposed platens to compress a press change formed from the base material;choosing platens having an insulating inner face for contacting the press charge to thereby substantially limit conductive heat transfer between the platens and the press charge;injecting a hot dry gas into the press charge; andcompressing the press charge. The method of claim 9 further comprising the step of choosing hot air as the hot gas for the step of injecting. The method of claim 10 further comprising the step of heating the hot air to between 400.degree. and 600.degree. F. prior to the step of injecting. The method of claim 9 further comprising the step of choosing thermoplastic fluff as the thermoactive binder. A method of forming a thermoactive binder composite product comprising the steps of:selecting a gas permeable base material including a thermoactive binder component;forming the base material into a press charge having a pair of opposing sides; andinfusing a substantially dry hot gas into the base material through a first region on one of the opposing sides and through a second region on the other of the opposing sides simultaneously, with at least a substantial portion of the regions being opposed to each other across the press charge in a direction generally normal to the sides, where the temperature of the gas is greater than the activation temperature of the thermoactive binder component of the base material. The method of claim 13, further including the step of providing jet structure for infusing the substantially dry hot gas toward and into the base material through the opposing sides, the jet structure including a plurality of jets disposed over both opposing sides. The method of claim 14, further including the step of forcing an amount of gas through the jets sufficient to create a substantial pressure drop across the jets prior to entry of the gas into the base material. [16.] A method of forming a thermoplastic binder composite product comprising the steps of:selecting a gas permeable base material including a thermoplastic binder component, where the gas permeability of the base material varies upon activation of the thermoplastic binder;injecting a substantially dry hot gas into the base material from a plurality of discrete locations, where the temperature of the gas is greater than the activation temperature of the thermoplastic binder component of the base material;regulating the gas flow among the plurality of discrete locations so that variations in the permeability of the base material in the proximity of one or more of the plurality of discrete locations does not substantially affect gas flow into the base material from one of the one or more discrete locations relative to another of the plurality of discrete locations. The method of claim 16, further including the step of forming the base material into a press charge that includes opposing sides, and wherein the plurality of discrete locations includes locations on both opposing sides of the press charge. The method of claim 17, further comprising the step of compressing the base material into a substantially compact, solid product. The method of claim 18, further including the step of choosing a base material including thermoplastic material as the thermoactive binder. [23.] A method of forming a thermoactive binder and cellulosic composite product comprising the steps of:selecting a gas permeable base material including a thermoactive binder component and a cellulosic component;injecting a substantially dry hot gas into the base material where the temperature of the gas is greater than 400.degree. F., where the gas consists essentially of air; andlimiting the exposure of the base material to gas with a temperature greater than 400.degree. F. in step of injecting to avoid combustion.