TURBINE AIRFOIL COMPONENTS CONTAINING CERAMIC-BASED MATERIALS

Hybrid turbine airfoil components (30,100) containing a ceramic material, in which detailed features of the components (30,100) are formed of materials other than ceramic materials. The components (30,100) include a first component (44,102) formed of a ceramic-based material and a second component (...

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Bibliographic Details
Main Authors Estill, Eric Alan, Marusko, Mark Willard, Darkins jr., Toby George, Heyward, John Peter, Deines, James Herbert, Hawkins, James Thomas, Jamison, Joshua Brian
Format Patent
LanguageEnglish
French
German
Published 31.03.2021
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Summary:Hybrid turbine airfoil components (30,100) containing a ceramic material, in which detailed features of the components (30,100) are formed of materials other than ceramic materials. The components (30,100) include a first component (44,102) formed of a ceramic-based material and a second component (46,104) formed of a metallic material. The first component (44,102) comprises an airfoil portion (38,102) and a nub (48,106), and the second component (46,104) is separately formed and attached to the first component (44,102) by casting the metallic material around the nub (48,106) of the first component (44,102). The second component (46,104) includes a platform portion (36,104) between the airfoil portion (38,102) and the nub (48,106) of the first component (44,102) and a dovetail portion (32,106) on the nub (48,106) of the first component (44,102). Each of the platform and dovetail portions (36,104;32,106) has at least one off-axis geometric feature (34,36,42,104) that results in the second component (46,104) having a more complex geometry than the first component (44,102).
Bibliography:Application Number: EP20110193396