发明名称 ASSEMBLY COMPRISING AN EXHAUST CASE AND A DOWNSTREAM ROTATIONALLY SYMMETRICAL PART
摘要 The invention relates to an assembly comprising: - a turbomachine exhaust case (110) that includes an external sleeve and an internal sleeve inside the former, both sleeves extending concentrically about a turbomachine axis, and also includes a plurality of arms extending radially between the sleeves; and - an annular part (130) that is centered about the axis, is mounted on one sleeve of the exhaust case, and is located downstream of the exhaust case in the direction in which the air flows inside the turbomachine; the assembly is characterized in that the annular part and the sleeve of the exhaust case on which the annular part is mounted each have a circumferential thread (131, 115), said threads cooperating with each other in order to allow the annular part to be screwed onto the sleeve of the exhaust case.
申请公布号 WO2016198806(A1) 申请公布日期 2016.12.15
申请号 WO2016FR51415 申请日期 2016.06.10
申请人 SAFRAN AIRCRAFT ENGINES 发明人 DE SOUSA, Mario, César;DEBRAY, Benoit, Argémiro, Matthieu;FOUQUET, Dominique, Michel;GHOSAROSSIAN-PRILLIEUX, Gregory;NOEL, Frédéric
分类号 F01D25/16;F02K1/04;F02K1/38;F02K1/48;F02K1/80 主分类号 F01D25/16
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