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 |