METHOD OF MANUFACTURING GAS TURBINE ENGINE COMPONENT FROM A MOLYBDENUM-RICH ALLOY

摘要

A method for manufacturing a gas turbine engine component from a molybdenum-rich alloy. The method includes the steps of providing a molybdenum powder of at least 50% molybdenum by weight, extruding the molybdenum powder to provide a first shape, forming the first shape to a second shape and forging the second shape to provide a third shape.