发明名称 Aerodynamic shroud for the back of a combustion chamber of a turbomachine
摘要 An annular shroud (42), having an internal face intended to cover the back end wall (33) of an annular combustion chamber (12) of a turbomachine (14) fitted with a centrifugal compressor, together with an external face opposite said internal face, and where said shroud includes multiple apertures (54) intended to allow fuel injectors (38, 40) supported by said back end wall (33) to pass through, together with multiple bosses (56) which extend as projections on said external face radially towards the interior respectively from the respective radially internal edges (58) of said apertures (54), such that each of said bosses (56) delimits an extension (60) of the corresponding aperture (54) open radially towards the exterior so as to form an air intake scoop.
申请公布号 US8661829(B2) 申请公布日期 2014.03.04
申请号 US201113820763 申请日期 2011.09.13
申请人 BOURGOIS SEBASTIEN ALAIN CHRISTOPHE;HERNANDEZ DIDIER HIPPOLYTE;SNECMA 发明人 BOURGOIS SEBASTIEN ALAIN CHRISTOPHE;HERNANDEZ DIDIER HIPPOLYTE
分类号 F02C1/00 主分类号 F02C1/00
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