发明名称 AIRCRAFT TURBOJET ENGINE EXHAUST CONE
摘要 <p>A gas ejection cone includes a cylindrical-shaped front cone portion, a conical-shaped rear cone portion, a ventilation tube and a support bearing of this drainage and/or ventilation tube. The ventilation tube extends inside the cylindrical-shaped front and conical-shaped rear cone portions and emerges at the end of the conical-shaped rear cone portion. In particular, the conical-shaped rear cone portion includes a front sub-portion connected to the cylindrical-shaped front cone portion, and a rear sub-portion removably secured to the front sub-portion. The rear sub-portion is further equipped with an outlet port of the ventilation tube.</p>
申请公布号 EP2828513(A1) 申请公布日期 2015.01.28
申请号 EP20130710474 申请日期 2013.02.18
申请人 AIRCELLE 发明人 SOULIER, PASCAL-MARIE PAUL MARCEL;GUILLON, JEAN-BERNARD;GUEGOU, JEAN-PIERRE
分类号 F02K1/04 主分类号 F02K1/04
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