A turbomachine lubrication system uses gravity and pressurization to convey air and oil mixtures toward a central separator.
Segmented mandrels remove without tapers to maintain uniform wall thickness and prevent wrinkles in ceramic matrix composites.
An annular intermediate-temperature space reduces thermal stress on gas turbine inner platforms.
An arcuate flange with a deep pin-receiving bore distributes stress on ceramic matrix composite segments, extending lifespan in high-pressure gas turbines.