发明名称 MULTI-BORED COMBUSTION CHAMBER HAVING COUNTER-ROTATING TANGENTIAL FLOWS
摘要 The invention relates to a combustion chamber (100), in particular of a turboshaft engine, having an inner annular wall (102), an outer annular wall (104), and an annular chamber bottom (106) extending around an axis, the chamber bottom being provided with at least one opening (110) intended for receiving a fuel injector, said opening being substantially centred on a circular line (113) defining a first portion of the chamber bottom (106a) extending radially between the circular line and the inner annular wall, and a second portion of the chamber bottom (106b) extending radially between the circular line and the outer annular wall. The chamber bottom comprises first and second channels (114, 116) at an angle relative to a vector that is normal to the chamber bottom while extending tangentially, the first channels being arranged such as to allow air to flow in a first rotating direction (SG1), while the second channels are arranged such as to allow air to flow in a second rotating direction (SG2) opposite to the first rotating direction.
申请公布号 WO2011086320(A1) 申请公布日期 2011.07.21
申请号 WO2011FR50046 申请日期 2011.01.11
申请人 TURBOMECA;CARRERE, BERNARD, JOSEPH, JEAN-PIERRE;DUBOURDIEU-RAYROT, JEAN-MARC;HERNANDEZ, LORENZO, HUACAN;SERROT-GRACIE, ROBERT 发明人 CARRERE, BERNARD, JOSEPH, JEAN-PIERRE;DUBOURDIEU-RAYROT, JEAN-MARC;HERNANDEZ, LORENZO, HUACAN;SERROT-GRACIE, ROBERT
分类号 F23R3/00;F23R3/12;F23R3/14;F23R3/54 主分类号 F23R3/00
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