发明名称 CHAMBRE DE COMBUSTION AVEC DEFLECTEURS
摘要 <p>The chamber has an annular wall (15) with passages (20) ensuring cooling of the chamber by air circulation through the passages. An air inlet orifice is located in a plane of an external surface of the wall and defined in downstream by an external part of a downstream edge (25) of each passage. An air outlet orifice is defined by an internal part of the downstream edge and by a downstream edge (35) of a deflector (30). The deflector extends the wall towards interior of the chamber and downstream, and diverts air from exterior towards interior and downstream of the chamber. An independent claim is also included for a method for forming passages in an annular wall of a combustion chamber.</p>
申请公布号 FR2920221(B1) 申请公布日期 2015.04.24
申请号 FR20070057154 申请日期 2007.08.24
申请人 SOCIETE NATIONALE D'ETUDE ET DE CONSTRUCTION DE MOTEURS D'AVIATION SNECMA 发明人 PIEUSSERGUES CHRISTOPHE;SANDELIS DENIS
分类号 F23R3/06;F23R3/50 主分类号 F23R3/06
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