公开(公告)号：US08197189B2

公开(公告)日：2012-06-12

申请号：US11945490

申请日：2007-11-27

申请人： Philippe Bonniere ,  Andreas Eleftheriou ,  Ignatius Theratil ,  Aldo Abate

发明人： Philippe Bonniere ,  Andreas Eleftheriou ,  Ignatius Theratil ,  Aldo Abate

IPC分类号： F01D5/10

CPC分类号： F01D5/10 ,  F01D25/24 ,  F05D2250/15 ,  F05D2260/96

摘要： A retaining ring is mounted in frictional engagement with a static gas turbine engine part, such as a compressor shroud, in order to provide frictional damping.

摘要翻译： 保持环安装成与诸如压缩机护罩的静态燃气涡轮发动机部件摩擦接合，以提供摩擦阻尼。

公开(公告)号：US20090136348A1

公开(公告)日：2009-05-28

申请号：US11945490

申请日：2007-11-27

申请人： Philippe Bonniere ,  Andreas Eleftheriou ,  Ignatius Theratil ,  Aido Abate

发明人： Philippe Bonniere ,  Andreas Eleftheriou ,  Ignatius Theratil ,  Aido Abate

IPC分类号： F01D5/10

CPC分类号： F01D5/10 ,  F01D25/24 ,  F05D2250/15 ,  F05D2260/96

摘要： A retaining ring is mounted in frictional engagement with a static gas turbine engine part, such as a compressor shroud, in order to provide frictional damping.

摘要翻译： 保持环安装成与诸如压缩机护罩的静态燃气涡轮发动机部件摩擦接合，以提供摩擦阻尼。

公开(公告)号：US09080461B2

公开(公告)日：2015-07-14

申请号：US13364379

申请日：2012-02-02

申请人： Richard Ivakitch ,  Andreas Eleftheriou ,  Philippe Bonniere

发明人： Richard Ivakitch ,  Andreas Eleftheriou ,  Philippe Bonniere

IPC分类号： F01D25/00 ,  F01D21/04 ,  F01D5/06

CPC分类号： F01D21/04 ,  F01D5/066 ,  F01D21/045 ,  F05D2220/36 ,  F05D2250/75 ,  Y10T29/49318

摘要： A gas turbine engine having at least one spool assembly, the at least one spool assembly including a fan rotor, a compressor disposed downstream of the fan rotor, a turbine and a shaft connecting the fan rotor, compressor and turbine, a joint affixed to an upstream end of the shaft, and including a first link connecting the fan rotor to the shaft and a second link connecting the compressor to the shaft, the second link being less rigid then the first link.

摘要翻译： 一种具有至少一个阀芯组件的燃气涡轮发动机，所述至少一个阀芯组件包括风扇转子，设置在所述风扇转子下游的压缩机，涡轮机和连接所述风扇转子，压缩机和涡轮机的轴， 并且包括将风扇转子连接到轴的第一连杆和将压缩机连接到轴的第二连杆，第二连杆比第一连杆刚性小。

公开(公告)号：US08708656B2

公开(公告)日：2014-04-29

申请号：US12786902

申请日：2010-05-25

申请人： Barry Barnett ,  Philippe Bonniere

发明人： Barry Barnett ,  Philippe Bonniere

IPC分类号： F01D5/30

CPC分类号： F01D5/3007 ,  F05D2260/30

摘要： The blade dovetails and associated dovetail slots of a gas turbine engine rotor assembly are shaped so that during windmilling the high stress regions of the blade dovetails are shielded from rubbing against the disk and vice versa. Bumper surfaces are provided in low stress regions of the dovetail assembly such that the windmilling contact points between the blade dovetails and the disk are in non-critical areas of the dovetail assembly.

摘要翻译： 燃气涡轮发动机转子组件的叶片燕尾榫和相关联的燕尾槽成形为使得在风车期间，叶片燕尾榫的高应力区域被遮蔽而不与盘摩擦，反之亦然。 缓冲表面设置在燕尾组件的低应力区域中，使得叶片燕尾榫和盘之间的风向接触点位于燕尾组件的非关键区域。

公开(公告)号：US20110293429A1

公开(公告)日：2011-12-01

申请号：US12786902

申请日：2010-05-25

申请人： Barry Barnett ,  Philippe Bonniere

发明人： Barry Barnett ,  Philippe Bonniere

IPC分类号： F01D5/30

CPC分类号： F01D5/3007 ,  F05D2260/30

摘要： The blade dovetails and associated dovetail slots of a gas turbine engine rotor assembly are shaped so that during windmilling the high stress regions of the blade dovetails are shielded from rubbing against the disk and vice versa. Bumper surfaces are provided in low stress regions of the dovetail assembly such that the windmilling contact points between the blade dovetails and the disk are in non-critical areas of the dovetail assembly.

摘要翻译： 燃气涡轮发动机转子组件的叶片燕尾榫和相关联的燕尾槽成形为使得在风车期间，叶片燕尾榫的高应力区域被遮蔽而不与盘摩擦，反之亦然。 缓冲表面设置在燕尾组件的低应力区域中，使得叶片燕尾榫和盘之间的风向接触点位于燕尾组件的非关键区域。