公开(公告)号：US08402770B2

公开(公告)日：2013-03-26

申请号：US13375915

申请日：2010-06-08

申请人： Fabrice Marcel Noel Garin ,  Maurice Guy Judet ,  Patrick Claude Pasquis ,  Wilfried Lionel Schweblen

发明人： Fabrice Marcel Noel Garin ,  Maurice Guy Judet ,  Patrick Claude Pasquis ,  Wilfried Lionel Schweblen

IPC分类号： F02C7/12

CPC分类号： F01D25/12 ,  F01D5/082 ,  Y02T50/676

摘要： A turbine engine including a channel for injecting a cooling air flow of a high-pressure turbine disk, opening into a cavity that is substantially isolated, upstream, from a cavity in which an air flow sampled at the output of a high-pressure compressor circulates, by a first labyrinth seal, and downstream, from a cavity communicating with the primary flow of the turbine engine, by a second labyrinth seal. The turbine engine includes channels communicating with the injection channel and opening through a static part of the first labyrinth seal between two lips of that seal, so as to allow an air flow coming from the injection channel to be injected between the lips.

摘要翻译： 一种涡轮发动机，包括用于喷射高压涡轮盘的冷却空气流的通道，所述通道从高压压缩机的输出处采样的空气流循环的空腔开口到空腔中，空腔基本上隔离在空腔中， 通过第一迷宫式密封件，并且通过第二迷宫式密封件从与涡轮发动机的主流体连通的空腔下游。 涡轮发动机包括与喷射通道连通并且通过该密封件的两个唇缘之间的第一迷宫式密封件的静态部分打开的通道，以便允许来自注射通道的空气流注入嘴唇之间。

公开(公告)号：US20120085104A1

公开(公告)日：2012-04-12

申请号：US13375915

申请日：2010-06-08

申请人： Fabrice Marcel Noel Garin ,  Maurice Guy Judet ,  Patrick Claude Pasquis ,  Wilfried Lionel Schweblen

发明人： Fabrice Marcel Noel Garin ,  Maurice Guy Judet ,  Patrick Claude Pasquis ,  Wilfried Lionel Schweblen

IPC分类号： F02C7/12

CPC分类号： F01D25/12 ,  F01D5/082 ,  Y02T50/676

摘要： A turbine engine including a channel for injecting a cooling air flow of a high-pressure turbine disk, opening into a cavity that is substantially isolated, upstream, from a cavity in which an air flow sampled at the output of a high-pressure compressor circulates, by a first labyrinth seal, and downstream, from a cavity communicating with the primary flow of the turbine engine, by a second labyrinth seal. The turbine engine includes channels communicating with the injection channel and opening through a static part of the first labyrinth seal between two lips of that seal, so as to allow an air flow coming from the injection channel to be injected between the lips.

摘要翻译： 一种涡轮发动机，包括用于喷射高压涡轮盘的冷却空气流的通道，所述通道从高压压缩机的输出处采样的空气流循环的空腔向上游开口，所述空腔基本上隔离， 通过第一迷宫式密封件，并且通过第二迷宫式密封件从与涡轮发动机的主流体连通的空腔下游。 涡轮发动机包括与喷射通道连通并且通过该密封件的两个唇缘之间的第一迷宫式密封件的静态部分打开的通道，以便允许来自注射通道的空气流注入嘴唇之间。

公开(公告)号：US08336317B2

公开(公告)日：2012-12-25

申请号：US12889791

申请日：2010-09-24

申请人： Stéphane Pierre Guillaume Blanchard ,  Patrick Claude Pasquis ,  Wilfried Lionel Schweblen ,  Jean-Claude Christian Taillant

发明人： Stéphane Pierre Guillaume Blanchard ,  Patrick Claude Pasquis ,  Wilfried Lionel Schweblen ,  Jean-Claude Christian Taillant

IPC分类号： F02C7/12

CPC分类号： F01D5/082 ,  F01D11/001 ,  F01D25/12 ,  F02C7/18 ,  Y02T50/671 ,  Y02T50/676

摘要： A turbine engine, including a final centrifugal compressor stage associated with a diffuser for supplying air to a combustion chamber, and a ventilation element for ventilating a high-pressure turbine wheel, is disclosed. The ventilation element includes an injection element for injecting air onto the wheel and a take-up element for taking up a flow for cooling the impeller of the compressor, where the take-up element has a labyrinth seal mounted at the outlet of the injection element, and the air outlet orifices are installed between the injection element and the labyrinth seal and leading upstream of the turbine wheel.

摘要翻译： 公开了一种涡轮发动机，包括与用于向燃烧室供应空气的扩散器相关联的最终离心压缩机台，以及用于使高压涡轮机叶轮通风的通风元件。 通风元件包括用于将空气喷射到轮上的注射元件和用于吸收用于冷却压缩机叶轮的流动的卷取元件，其中卷取元件具有安装在注射元件出口处的迷宫式密封件 并且空气出口孔安装在注射元件和迷宫式密封件之间并引导到涡轮机叶轮的上游。