发明名称 3D NON-AXISYMMETRIC COMBUSTOR LINER
摘要 A combustor liner with an input end and an output end includes an annular inner wall and an annular outer wall. At least one of the inner wall and outer wall is three-dimensionally contoured. The inner wall and the outer wall form a combustion chamber with the contours creating alternating expanding and constricting regions inside the chamber causing combustion gases to flow in the circumferential and axial directions.
申请公布号 US2011203286(A1) 申请公布日期 2011.08.25
申请号 US20100709951 申请日期 2010.02.22
申请人 UNITED TECHNOLOGIES CORPORATION 发明人 WAGNER JOEL H.;LUTJEN PAUL M.
分类号 F23R3/42 主分类号 F23R3/42
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