A combustor cap is cooperable with an impingement plate in a turbine fuel nozzle and includes a plurality of cap segments independently securable to the impingement plate. The plurality of cap segments are radially and tangentially movable relative to the impingement plate.
申请公布号
US2010058766(A1)
申请公布日期
2010.03.11
申请号
US20080208906
申请日期
2008.09.11
申请人
MCMAHAN KEVIN WESTON;INTILE JOHN CHARLES;SRINIVASAN SHIVA;STRYAPUNIN SERGEY ALEXANDROVICH
发明人
MCMAHAN KEVIN WESTON;INTILE JOHN CHARLES;SRINIVASAN SHIVA;STRYAPUNIN SERGEY ALEXANDROVICH