초록 ▼

An apparatus may comprise a tool capable of holding a part during curing of the part, and a passive temperature control system. The passive temperature control system may have a phase change material selected as having a phase change temperature that may be capable of controlling heat generated by t

An apparatus may comprise a tool capable of holding a part during curing of the part, and a passive temperature control system. The passive temperature control system may have a phase change material selected as having a phase change temperature that may be capable of controlling heat generated by the part during curing of the part held by the tool.

대표청구항 ▼

1. A method for curing a part, the method comprising: providing a tool, the tool comprising: a material having a first surface substantially parallel to a second surface;a plurality of cavities completely inside the material and substantially parallel to the first surface and to the second surface;

1. A method for curing a part, the method comprising: providing a tool, the tool comprising: a material having a first surface substantially parallel to a second surface;a plurality of cavities completely inside the material and substantially parallel to the first surface and to the second surface; anda phase change material disposed within the plurality of cavities, the phase change material having a phase change temperature that is about a cure temperature for a composite laminate part, the phase change material further selected so that a change of phase of the phase change material absorbs heat during the change of phase at the phase change temperature,placing the composite laminate part on the first surface of the material;curing the composite laminate part, thereby generating heat; andtransferring the generated heat, during said curing, from the composite laminate part to the phase change material by inducing the change of phase in the phase change material in the plurality of cavities so as to maintain a third temperature of the part within a desired temperature range near the cure temperature,wherein the tool includes a first section in which the plurality of cavities are located and a second section in which there are none of the plurality of cavities, wherein the composite laminate part includes a thicker portion relative to a thinner portion of the composite laminate part, and wherein said placing the composite laminate part comprises placing the thicker portion of the composite laminate part over the first section and placing the thinner portion over the second section. 2. The method of claim 1, wherein the plurality of cavities is located a distance from the first surface of the material on which the composite laminate part is placed, and wherein the method further comprises: selecting the distance to allow the phase change material to absorb the heat from the part. 3. The method of claim 1, wherein said placing further comprises: laying up the composite laminate part on the tool. 4. The method of claim 1, wherein the cure temperature comprises about 250 degrees Fahrenheit plus or minus 10 degrees Fahrenheit. 5. The method of claim 1, wherein said placing includes placing the composite laminate part such that selected areas of the composite laminate part are in closer proximity to the phase change material than other areas of the composite laminate part. 6. The method of claim 1, wherein providing the tool includes providing the tool such that the cavities have a shape selected from the group consisting of: squares, rectangles, triangles, and hexagons. 7. The method of claim 1, wherein providing the tool includes providing air gaps within the plurality of cavities along with the phase change material. 8. The method of claim 7, wherein the air gaps have a size that takes into account different amounts of thermal expansion that occurs between the tool and the phase change material. 9. The method of claim 1, wherein providing the tool includes selecting the material from the group consisting of: steel, aluminum, reinforced silicon rubber, nickel, carbon fiber composite, and nickel-steel alloy. 10. The method of claim 1 further comprising: generating exothermic reactions in the composite laminate part during said curing.