发明名称 Gas ejection cone for aircraft turbojet engines
摘要 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.
申请公布号 US9611807(B2) 申请公布日期 2017.04.04
申请号 US201414484684 申请日期 2014.09.12
申请人 AIRCELLE 发明人 Soulier Pascal-Marie Paul Marcel;Guillon Jean-Bernard;Guegou Jean-Pierre
分类号 F02K1/36;F02K1/04;B64C7/02 主分类号 F02K1/36
代理机构 Burris Law, PLLC 代理人 Burris Law, PLLC
主权项 1. A gas ejection cone, comprising: a cylindrical-shaped front cone portion; a conical-shaped rear cone portion; a drainage and/or ventilation tube extending inside the cylindrical-shaped front cone portion and the conical-shaped rear cone portion, the drainage and/or ventilation tube emerging at an end of the conical-shaped rear cone portion; and a support bearing of the drainage and/or ventilation tube which is disposed inside the conical-shaped rear cone portion,wherein the conical-shaped rear cone portion is fixed and comprises a front sub-portion secured fixedly to the cylindrical-shaped front cone portion, and a rear sub-portion secured fixedly to the front sub-portion such that the front and rear sub-portions cannot rotate relative to the cylindrical-shaped front cone portion, the rear sub-portion being equipped with an outlet port of the drainage and/or ventilation tube and being removable from the front sub-portion in order to inspect an inside of the gas ejection cone.
地址 Gonfeville l'Orcher FR