公开(公告)号：US07340882B2

公开(公告)日：2008-03-11

申请号：US11149214

申请日：2005-06-10

申请人： Guy Lapergue ,  Regis Servant ,  Gael Bouchy ,  Alain Baum

发明人： Guy Lapergue ,  Regis Servant ,  Gael Bouchy ,  Alain Baum

IPC分类号： F02C7/06

CPC分类号： F01D21/045 ,  F01D25/16

摘要： The turbomachine of the invention extends longitudinally along an axis, and includes a rotor attached to drive shaft, arranged to rotate around an axis, supported by at least a first bearing, mounted on the fixed structure of the turbomachine by a bearing support element. The turbomachine is characterised by the fact that it includes a stop ring, mounted on the fixed structure of the turbomachine, to cooperate with the support element of the first bearing and, in the event of displacement of the rotor in relation to the fixed structure, to perform a function of axial retention of the rotor in an even manner, with no angle effect between the axis of the turbomachine and the axis of the drive shaft.

摘要翻译： 本发明的涡轮机器沿着轴线纵向延伸，并且包括附接到驱动轴的转子，该转子被布置为通过轴承支撑元件围绕安装在涡轮机的固定结构上的至少第一轴承支承的轴旋转。 涡轮机的特征在于它包括安装在涡轮机的固定结构上的止动环，以与第一轴承的支撑元件配合，并且在转子相对于固定结构移位的情况下， 以均匀的方式执行转子的轴向保持的功能，在涡轮机的轴线和驱动轴的轴线之间没有角度影响。

公开(公告)号：US07322180B2

公开(公告)日：2008-01-29

申请号：US11023601

申请日：2004-12-29

申请人： Guy Lapergue ,  Regis Servant ,  Gael Bouchy

发明人： Guy Lapergue ,  Regis Servant ,  Gael Bouchy

IPC分类号： F02K3/02

CPC分类号： F01D21/045

摘要： A turbo-jet engine including a fixed structure and a fan rotor mounted on a drive shaft supported by a first bearing and a second bearing. The engine further comprises an axial retaining device configured to form an emergency bearing and to cooperate with the fixed structure and mounted rigidly to the drive shaft. The engine includes a structural flange on which the second bearing is fixed, and the axial retaining device comprises a retaining disk mounted on the drive shaft and configured to cooperate with a stop disk of the flange to axially retain the fan and form an emergency bearing.

摘要翻译： 一种包括固定结构的涡轮喷气发动机和安装在由第一轴承和第二轴承支撑的驱动轴上的风扇转子。 发动机还包括轴向保持装置，该轴向保持装置构造成形成紧急轴承并与固定结构配合并刚性地安装到驱动轴上。 发动机包括结构凸缘，第二轴承固定在该结构凸缘上，并且轴向保持装置包括安装在驱动轴上的保持盘，并且构造成与凸缘的止动盘配合以轴向保持风扇并形成紧急轴承。

公开(公告)号：US20060087396A1

公开(公告)日：2006-04-27

申请号：US11256935

申请日：2005-10-25

申请人： Gael Bouchy ,  Regis Servant

发明人： Gael Bouchy ,  Regis Servant

IPC分类号： H01H61/00

CPC分类号： F16B31/021 ,  F01D21/045 ,  F05B2260/3011 ,  F16B33/002 ,  Y10S411/916

摘要： The turbine engine of the invention includes a rotor with at least one bearing, mounted on a bearing supporting part, said part being connected to the fixed structure by an uncoupling device, including at least one fusible screw passing through at least one bore, said screw comprising a head and a threaded portion, a fusible portion forming a preferential failure area, located between the head of the screw and its threaded portion. The screw comprises, between its threaded portion and its fusible portion, a portion for blocking the screw in rotation, cooperating with a complementary blocking portion provided in the bore. By means of the invention, the torsional torque related to the tightening of the screw is not transmitted to its fusible portion.

摘要翻译： 本发明的涡轮发动机包括具有安装在轴承支撑部分上的至少一个轴承的转子，所述部件通过非耦合装置连接到固定结构，所述非耦合装置包括至少一个穿过至少一个孔的可熔螺钉，所述螺钉 包括头部和螺纹部分，形成优先失效区域的可熔部分，位于螺钉头部及其螺纹部分之间。 螺杆在其螺纹部分和其可熔部分之间包括用于阻止螺杆旋转的部分，与设置在孔中的互补阻挡部分配合。 通过本发明，与拧紧螺钉相关的扭转扭矩不会传递到其可熔部分。

公开(公告)号：US20050276683A1

公开(公告)日：2005-12-15

申请号：US11149214

申请日：2005-06-10

申请人： Guy Lapergue ,  Regis Servant ,  Gael Bouchy ,  Alain Baum

发明人： Guy Lapergue ,  Regis Servant ,  Gael Bouchy ,  Alain Baum

IPC分类号： F01D21/04 ,  F01D25/16 ,  F01D21/00

CPC分类号： F01D21/045 ,  F01D25/16

摘要： The turbomachine of the invention extends longitudinally along an axis, and includes a rotor attached to drive shaft, arranged to rotate around an axis, supported by at least a first bearing, mounted on the fixed structure of the turbomachine by a bearing support element. The turbomachine is characterised by the fact that it includes a stop ring, mounted on the fixed structure of the turbomachine, to cooperate with the support element of the first bearing and, in the event of displacement of the rotor in relation to the fixed structure, to perform a function of axial retention of the rotor in an even manner, with no angle effect between the axis of the turbomachine and the axis of the drive shaft.

摘要翻译： 本发明的涡轮机器沿着轴线纵向延伸，并且包括附接到驱动轴的转子，该转子被布置为通过轴承支撑元件围绕安装在涡轮机的固定结构上的至少第一轴承支承的轴旋转。 涡轮机的特征在于它包括安装在涡轮机的固定结构上的止动环，以与第一轴承的支撑元件配合，并且在转子相对于固定结构移位的情况下， 以均匀的方式执行转子的轴向保持的功能，在涡轮机的轴线和驱动轴的轴线之间没有角度影响。

公开(公告)号：US20050241290A1

公开(公告)日：2005-11-03

申请号：US11041996

申请日：2005-01-26

申请人： Guy Lapergue ,  Regis Servant ,  Gael Bouchy

发明人： Guy Lapergue ,  Regis Servant ,  Gael Bouchy

IPC分类号： F01D21/04 ,  F01D25/16 ,  F02C7/06 ,  F02K3/06 ,  F16C19/36 ,  F16C23/08 ,  F16C33/58 ,  F02C3/04

CPC分类号： F01D21/04 ,  F01D25/16

摘要： The turbojet according to the invention comprises a fixed structure, a fan rotor fixed to a drive shaft (5) supported by a first bearing (6) and a second bearing (7), mounted on the said structure fixed through a bearing support part (11, 19), the first bearing (6) being mounted on the fixed structure of the turbojet through a device (13) enabling it to be decoupled (13) from the fixed structure, characterised by the fact that the second bearing (7) is mounted on the bearing support part (19) through a link acting as a ball joint (23, 24) and in that the turbojet also comprises means enabling axial displacements of the second bearing (7) with respect to the fixed structure of the turbojet if the first bearing (6) should be decoupled. The centring function of the second bearing (7) after decoupling of the first bearing (6) is thus provided without introducing excessive stresses in the bearing (7).

摘要翻译： 根据本发明的涡轮喷气发动机包括固定结构，固定到由第一轴承（6）支撑的驱动轴（5）的风扇转子和安装在通过轴承支撑部分固定的所述结构上的第二轴承（7） 第一轴承（6）通过装置（13）安装在涡轮喷气发动机的固定结构上，使得其能够与固定结构脱离（13），其特征在于，第二轴承（7） 通过用作球窝接头（23,24）的连杆安装在轴承支撑部分（19）上，并且涡轮喷气发动机还包括使第二轴承（7）相对于涡轮喷气发动机的固定结构能够轴向位移的装置 如果第一个轴承（6）应该去耦。 因此，在第一轴承（6）解耦之后，第二轴承（7）的定心功能不会在轴承（7）中引入过大的应力。

公开(公告)号：US20050172608A1

公开(公告)日：2005-08-11

申请号：US11023601

申请日：2004-12-29

申请人： Guy Lapergue ,  Regis Servant ,  Gael Bouchy

发明人： Guy Lapergue ,  Regis Servant ,  Gael Bouchy

IPC分类号： F01D25/00 ,  F01D21/04 ,  F02C7/06

CPC分类号： F01D21/045

摘要： The present invention pertains to a turbo-jet engine comprising a fixed structure, a fan rotor integral with a drive shaft supported by a first bearing and a second bearing. It is characterized in that it comprises means forming axial retaining means for the fan rotor and/or forming an emergency bearing, cooperating with means of the fixed structure and mounted integral with the drive shaft. In particular it comprises a structural flange on which the second bearing is fixed, and the means forming axial retaining means for the fan and/or forming an emergency bearing comprise a retaining disk mounted on the drive shaft and cooperating with a stop disk of flange for axially retaining fan and with a longitudinal sleeve of flange to form an emergency bearing.

摘要翻译： 本发明涉及一种涡轮喷气发动机，其包括固定结构，与由第一轴承和第二轴承支撑的驱动轴一体的风扇转子。 其特征在于，其包括形成用于风扇转子的轴向保持装置和/或形成紧急轴承的装置，其与固定结构的装置配合并与驱动轴一体地安装。 特别地，它包括结构法兰，第二轴承固定在该结构凸缘上，并且形成用于风扇的轴向保持装置和/或形成紧急轴承的装置包括安装在驱动轴上的保持盘，并与法兰的止动盘配合 轴向保持风扇和法兰的纵向套筒形成紧急轴承。

公开(公告)号：US07322181B2

公开(公告)日：2008-01-29

申请号：US11041996

申请日：2005-01-26

申请人： Guy Lapergue ,  Regis Servant ,  Gael Bouchy

发明人： Guy Lapergue ,  Regis Servant ,  Gael Bouchy

IPC分类号： F02K3/02

CPC分类号： F01D21/04 ,  F01D25/16

摘要： The turbojet includes a fixed structure, a fan rotor fixed to a drive shaft supported by a first bearing and a second bearing. The second bearing is mounted on the fixed structure through a bearing support part. The first bearing is mounted on the fixed structure of the turbojet through a device enabling it to be decoupled from the fixed structure. The second bearing is mounted on the bearing support part through a link acting as a ball joint. The turbojet also allows axial displacements of the second bearing with respect to the fixed structure of the turbojet if the first bearing should be decoupled. The centering function of the second bearing after decoupling of the first bearing is thus provided without introducing excessive stresses in the bearing.

摘要翻译： 涡轮喷气发动机包括固定结构，固定到由第一轴承和第二轴承支撑的驱动轴的风扇转子。 第二轴承通过轴承支撑部件安装在固定结构上。 第一轴承通过装置安装在涡轮喷气发动机的固定结构上，使其能够与固定结构分离。 第二轴承通过作为球窝接头的连杆安装在轴承支撑部件上。 涡轮喷气发动机还允许第二轴承相对于涡轮喷气发动机的固定结构的轴向位移，如果第一轴承应该被分离。 因此，在第一轴承解耦之后第二轴承的定中心功能不会在轴承中引入过大的应力。

公开(公告)号：US20050247526A1

公开(公告)日：2005-11-10

申请号：US11113049

申请日：2005-04-25

申请人： Regis Servant ,  Gael Bouchy ,  Guy Lapergue

发明人： Regis Servant ,  Gael Bouchy ,  Guy Lapergue

IPC分类号： F01D25/16 ,  F02C7/06 ,  F16N7/22 ,  F16C1/24

CPC分类号： F01D25/18 ,  F16C19/06 ,  F16C33/6659 ,  F16C33/6677 ,  F16C35/042 ,  F16C2360/23

摘要： A device for lubricating a component in an assembly of parts comprises a lubricant distribution chamber arranged in the vicinity of the component and formed by an annular setback in a ring mounted on a part of the assembly, said setback being closed automatically when the ring is mounted by means of a corresponding surface of the part into which there open out channels or ducts formed in the part and feeding the setback with lubricant and/or connecting the setback to means for taking lubricant to the component.

摘要翻译： 用于润滑部件组件中的部件的装置包括布置在部件附近并由安装在组件的一部分上的环中的环形挫折形成的润滑剂分配室，当安装环时，所述挫折被自动关闭 通过部件的对应表面，其中打开形成在部件中的通道或管道，并将润滑剂供给挫折和/或将挫折连接到用于将润滑剂用于部件的装置。