초록 ▼

A process for joining or coating carbon-carbon composite components. For joining such components, surfaces of two components are prepared so that they match. An interlayer comprised of a material having a melting point in excess of 2500°F. is sandwiched between the two surfaces and the assembly is h

A process for joining or coating carbon-carbon composite components. For joining such components, surfaces of two components are prepared so that they match. An interlayer comprised of a material having a melting point in excess of 2500°F. is sandwiched between the two surfaces and the assembly is held together under compression while it is heated to a temperature sufficient to melt the interlayer material or to a temperature sufficient to cause interdiffussion between the interlayer and the carbon-carbon composite material. In a preferred embodiment of this invention the interlayer material is a carbide former. For example, if zirconium is chosen as the interlayer material, a joint can be prepared at a temperature of 3400°F. which will retain its strength to temperatures in excess of 4350°F. If the second surface is a removable backing, the interlayer provides a coating of the surface of the carbon-carbon composite component.

대표청구항 ▼

A process for joining carbon-carbon composite component comprising the steps of: (a) preparing the surface of a first carbon-carbon composite component to be joined, (b) preparing a surface of a second carbon-carbon composite component so that the surface of said second component mates with said pre

A process for joining carbon-carbon composite component comprising the steps of: (a) preparing the surface of a first carbon-carbon composite component to be joined, (b) preparing a surface of a second carbon-carbon composite component so that the surface of said second component mates with said prepared surface of said first component, (c) preparing a thin interlayer having a thickness of between 0.001 inch and 0.004 inch and comprised of material having a melting point greater than 2500 F., (d) assembling said first component, said interlayer and said second component so that said mating surfaces are facing each other with said interlayer sandwiched between, and (e) while holding said assembly together under compression, heating for a time said assembly at a temperature not exceeding 36650 F. but sufficient to cause substantial mixing of the atoms of the interlayer with the atoms of the carbon-carbon composite.