Methods and tooling assemblies for the manufacture of metallurgically-consolidated turbine engine components

Embodiments of a method (84) for manufacturing a turbine engine component (60) are provided, as are embodiments of a thermal growth constraint tool (118) for the manufacture of turbine engine components (60). In one embodiment, the method (84) includes the steps of obtaining (86) a plurality of arch...

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Bibliographic Details
Main Authors SMOKE, JASON, JAN, DAVID K, MITTENDORF, DON
Format Patent
LanguageEnglish
French
German
Published 09.03.2016
Subjects
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Summary:Embodiments of a method (84) for manufacturing a turbine engine component (60) are provided, as are embodiments of a thermal growth constraint tool (118) for the manufacture of turbine engine components (60). In one embodiment, the method (84) includes the steps of obtaining (86) a plurality of arched pieces (88), arranging (110) the plurality of arched pieces (88) in a ring formation (112), and bonding (116) the plurality of arched pieces (88) together to produce a monolithic ring (162) by heating the ring formation (112) to a predetermined bonding temperature while constraining the outward radial growth thereof. Bonding (116) comprises, in turn, positioning a thermal growth constraint ring (120, 122) around the ring formation (112), and heating the ring formation (112) to a predetermined bonding temperature at which the ring formation (112) grows into the thermal growth constraint ring (120, 122).
Bibliography:Application Number: EP20130153710