发明名称 Post-combustor for bypass gas turbine.
摘要 Postcombustion device including an outer casing (1), an exhaust casing (18) contained inside the outer casing and including outer (3) and inner (5) annular walls, the outer wall (3) being at a distance from the outer casing (1) and defining with it a main passage for secondary air (25), and connecting arms (6) joining the inner and outer walls, this postcombustion device also including an annular postcombustion wall (8) arranged inside the outer casing while being separated from it by a specific distance so as to provide a passage for coolant air (12) and defining a postcombustion chamber (9). According to the invention each connecting arm includes a casing (23) comprising an upper opening (24) communicating with the passage (25) and comprising a device with openings (26) passing through the downstream wall (27) of the arm (6) and communicating with the postcombustion chamber (9). One application is the production of a postcombustion device which has a high efficiency. <IMAGE>
申请公布号 EP0592305(A1) 申请公布日期 1994.04.13
申请号 EP19930402450 申请日期 1993.10.06
申请人 SOCIETE NATIONALE D'ETUDE ET DE CONSTRUCTION DE MOTEURS D'AVIATION, "S.N.E.C.M.A." 发明人 MAHIAS, OLIVIER MICHEL MARIE;PASQUALI, XAVIER JEAN-MARIE;ROCHE, JACQUES, ANDRE MICHEL;ROMERO, MIREILLE SIMONE NOELLE;VILFEU, ELISABETH
分类号 F02K3/04;F01D9/06;F02K3/10;F23R3/18;F23R3/20;(IPC1-7):F23R3/18 主分类号 F02K3/04
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