GAS TURBINE COMPONENT AND METHOD OF FORMING

Components (100) are disclosed which include a first component section (102) and a second component section (104) joined to form a hollow structure (106) defining a plenum (108) having an interior surface (110), wherein the component sections (102, 104) each include mating ridges (120, 122, 124, 126...

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Bibliographic Details
Main Authors DIAO, Xiaoxue, THOMAS, Nicholas, LIN, Dechao, KOTTILINGAM, Srikanth Chandrudu
Format Patent
LanguageEnglish
French
German
Published 25.11.2020
Subjects
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