Gas ejection cone for aircraft turbojet engines

    公开(公告)号:US09611807B2

    公开(公告)日:2017-04-04

    申请号:US14484684

    申请日:2014-09-12

    Applicant: AIRCELLE

    CPC classification number: F02K1/36 B64C7/02 F02K1/04

    Abstract: 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.

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