Rotating ring structure for gas turbine engines and method for i

Powder metallurgy processes – Powder metallurgy processes with heating or sintering – Making porous product

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419 4, 419 5, 419 16, 419 36, 419 51, B22F 316

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055795323

ABSTRACT:
A composite jet engine compressor ring is made by casting a tape reinforced with ceramic fibers, winding the cast tape around a mandrel to form an unconsolidated ring, heating the ring to drive off binder, and pressing at a high temperature to form a unitary composite ring. Compression of the ring in an axial direction during hot pressing results in a desired axial spacing between adjacent fibers. The tape is preferably cast from a mixture of titanium base metal particles and a polyisobutylene binder dissolved in an organic solvent.

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