发明名称 Jet engine for airplane, has tube with one end mounted in exhaust opening by ball joint connection free in rotation and locked in translation, and another end mounted in jambs orifice by connection free in rotation and translation
摘要 <p>The engine has a jamb connected to an external case of a diffuser grid and an external shell (14) of the engine casing. A tube is placed between an orifice (22) of the jamb and an exhaust opening (23) of the shell. An end (61) of the tube is mounted in the opening by a ball joint connection free in rotation and locked in translation. An end (63) of the tube is mounted in the orifice by the connection free in rotation and translation.</p>
申请公布号 FR2860041(A1) 申请公布日期 2005.03.25
申请号 FR20030011064 申请日期 2003.09.22
申请人 SNECMA MOTEURS 发明人 LEPRETRE GILLES
分类号 F02K1/80;F01D9/06;F01D25/24;F02K1/00;(IPC1-7):F02C7/00 主分类号 F02K1/80
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