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1. 发明授权

US07591594B2 Turbomachine with a compact roller bearing 有权
标题翻译：涡轮机与紧凑型滚子轴承
公开(公告)号：US07591594B2
公开(公告)日：2009-09-22
申请号：US11072260
申请日：2005-03-07
申请人： Gilles Charier , Guy Dusserre-Telmon , Marc Marchi , Jean-Pierre Mourlan , Patrice Rosset , Zoltan Zsiga
发明人： Gilles Charier , Guy Dusserre-Telmon , Marc Marchi , Jean-Pierre Mourlan , Patrice Rosset , Zoltan Zsiga
IPC分类号： F16C43/04 , F16C33/58 , F01D25/16
CPC分类号： F01D5/026 , F01D25/166 , F16C2360/23
摘要： A turbomachine roller bearing that supports a shaft constituted by a trunnion of a shaft line of a high-pressure spool of a turbomachine to rotate relative to a stationary support that is connected to a casing of the turbomachine, said bearing comprising rollers inserted between an outer ring disposed adjacent to the stationary support and an inner ring disposed adjacent to the high-pressure trunnion, the inner ring extending along the axis beyond a downstream end of the high-pressure trunnion to which it is secured by clamping means, and being provided with anti-rotation means for preventing said inner ring from rotating relative to the high-pressure trunnion.
摘要翻译：一种涡轮机滚子轴承，其支撑由涡轮机的高压线轴的轴线的耳轴构成的轴，以相对于连接到涡轮机的壳体的固定支撑件旋转，所述轴承包括插入在外部环设置成邻近固定支撑件和邻近高压耳轴设置的内环，内环沿着轴线延伸超过高压耳轴的下游端，其通过夹紧装置固定到该下端，并且设置有用于防止所述内圈相对于高压耳轴旋转的防旋转装置。

2. 发明授权

US08714905B2 Method and a device for balancing pressure in a turbojet bearing enclosure 有权
标题翻译：方法和用于平衡涡轮喷气轴承外壳中的压力的装置
公开(公告)号：US08714905B2
公开(公告)日：2014-05-06
申请号：US12934784
申请日：2009-03-24
申请人： Ion Fintescu , Laurent Gille , Jean-Pierre Mourlan
发明人： Ion Fintescu , Laurent Gille , Jean-Pierre Mourlan
IPC分类号： F04D27/02
CPC分类号： F01D25/16 , F01D25/183 , F02C7/06 , F05D2240/63
摘要： A pressure-balancing device for balancing pressure in at least one bearing enclosure of a turbojet, the enclosure including a mechanism feeding the bearing with lubricating liquid, an air intake, at least one sealing system placed between the stator and the rotor in front of and/or behind the bearing, a recovery mechanism recovering the lubricating liquid, and a removal mechanism removing the mixture of air and of traces of lubricating liquid towards a venting circuit. Downstream from the bearing enclosure and in the venting circuit, the balancing device includes a regulator system regulating the air removal flow rate, thereby enabling the flow rate to be variable as a function of the speed of the engine, to remain non-zero, and, at high speeds, to be lower than when the regulator system is not included.
摘要翻译：一种用于平衡涡轮喷气发动机的至少一个轴承罩中的压力的压力平衡装置，所述外壳包括将所述轴承与润滑液体一起供给的机构，进气口，置于所述定子和所述转子之前的至少一个密封系统， /或在轴承后面，回收润滑液的回收机构，以及去除空气和痕量润滑液体的混合物朝向排气回路的去除机构。在轴承箱和通气回路下游，平衡装置包括调节排气流量的调节器系统，从而使流量可根据发动机的速度而变化，保持非零，以及，高速度，低于不包括调节器系统时。

3. 发明申请

US20110188992A1 METHOD AND A DEVICE FOR BALANCING PRESSURE IN A TURBOJET BEARING ENCLOSURE 有权
标题翻译：用于在涡轮轴承外壳中平衡压力的方法和装置
公开(公告)号：US20110188992A1
公开(公告)日：2011-08-04
申请号：US12934784
申请日：2009-03-24
申请人： Ion Fintescu , Laurent Gille , Jean-Pierre Mourlan
发明人： Ion Fintescu , Laurent Gille , Jean-Pierre Mourlan
IPC分类号： F01D3/04
CPC分类号： F01D25/16 , F01D25/183 , F02C7/06 , F05D2240/63
摘要： A pressure-balancing device for balancing pressure in at least one bearing enclosure of a turbojet, the enclosure including a mechanism feeding the bearing with lubricating liquid, an air intake, at least one sealing system placed between the stator and the rotor in front of and/or behind the bearing, a recovery mechanism recovering the lubricating liquid, and a removal mechanism removing the mixture of air and of traces of lubricating liquid towards a venting circuit. Downstream from the bearing enclosure and in the venting circuit, the balancing device includes a regulator system regulating the air removal flow rate, thereby enabling the flow rate to be variable as a function of the speed of the engine, to remain non-zero, and, at high speeds, to be lower than when the regulator system is not included.
摘要翻译：一种用于平衡涡轮喷气发动机的至少一个轴承罩中的压力的压力平衡装置，所述外壳包括将所述轴承与润滑液体一起供给的机构，进气口，置于所述定子和所述转子之前的至少一个密封系统， /或在轴承后面，回收润滑液的回收机构，以及去除空气和痕量润滑液体的混合物朝向排气回路的去除机构。在轴承箱和通气回路下游，平衡装置包括调节排气流量的调节器系统，从而使流量可根据发动机的速度而变化，保持非零，以及，高速度，低于不包括调节器系统时。

4. 发明申请

US20060239812A1 A METHOD OF REGULATING THE FLOW RATE OF AIR IN A ROTARY SHAFT OF A TURBOMACHINE 有权
标题翻译：调节涡轮转子轴中空气流量的方法
公开(公告)号：US20060239812A1
公开(公告)日：2006-10-26
申请号：US11279812
申请日：2006-04-14
申请人： Jerome Friedel , Jean-Pierre Mourlan , Daniel Plona
发明人： Jerome Friedel , Jean-Pierre Mourlan , Daniel Plona
IPC分类号： F03B11/00
CPC分类号： F01D5/08 , F01D17/105 , F04D27/0215 , F04D27/023 , F16K31/56 , Y10T137/0971
摘要： A device applied to regulating the flow rate of air flowing in a rotary shaft of a turbomachine, the shaft including at least one through orifice for passing air. The device at least one shutter member for shutting the orifice and secured to a deformable blade presenting bi-linear behavior, the blade being secured to the shaft and being suitable for deforming under the effect of the centrifugal force that results from the shaft rotating such that the shutter member is suitable for taking up two different positions depending on the speed of rotation of the shaft: one position in which it shuts the orifice; and another position in which it releases the orifice to allow air to pass through.
摘要翻译：一种用于调节在涡轮机的旋转轴中流动的空气的流量的装置，所述轴包括用于使空气通过的至少一个通孔。该装置至少有一个活门构件，用于关闭孔口并固定到呈现双线性行为的可变形叶片上，该叶片固定在该轴上并且适于在由轴旋转的离心力的作用下变形，使得挡板构件适合于根据轴的旋转速度卷取两个不同的位置：其中其关闭孔的一个位置; 以及释放孔口以允许空气通过的另一位置。

5. 发明授权

US07690184B2 Method for treating oil waste in a gas turbine engine 有权
标题翻译：一种用于处理燃气涡轮发动机中的废油的方法
公开(公告)号：US07690184B2
公开(公告)日：2010-04-06
申请号：US11774336
申请日：2007-07-06
申请人： Gerard Philippe Gauthier , Jean-Pierre Mourlan
发明人： Gerard Philippe Gauthier , Jean-Pierre Mourlan
IPC分类号： F02C7/06
CPC分类号： F02C7/06 , F01D25/18 , F01D25/32 , F05D2260/602
摘要： A method for treating an airflow, laden with oil, flowing in a tube communicating with a rolling bearing enclosure of a gas turbine engine, wherein the airflow is made to travel into a coking box associated with a heating mechanism, in which the air is heated to a sufficient temperature to coke the oil particles contained in the airflow. Preferably, the solid residues produced by the coking are collected in the coking box.
摘要翻译：一种用于处理在与燃气涡轮发动机的滚动轴承外壳连通的管中流动的气流的方法，其中使气流进入与加热机构相关联的焦化箱，其中空气被加热达到足够的温度以焦化包含在气流中的油颗粒。优选地，通过焦化产生的固体残余物被收集在焦化器中。

6. 发明申请

US20080173002A1 METHOD FOR TREATING OIL WASTE IN A GAS TURBINE ENGINE 有权
标题翻译：用于处理气体涡轮发动机中的油污的方法
公开(公告)号：US20080173002A1
公开(公告)日：2008-07-24
申请号：US11774336
申请日：2007-07-06
申请人： Gerard Philippe Gauthier , Jean-Pierre Mourlan
发明人： Gerard Philippe Gauthier , Jean-Pierre Mourlan
IPC分类号： F02C7/06 , F01D25/18
CPC分类号： F02C7/06 , F01D25/18 , F01D25/32 , F05D2260/602
摘要： The present invention relates to a method for treating an airflow, laden with oil particles, flowing in a tube (9) communicating with a rolling bearing enclosure of a gas turbine engine, wherein said airflow is made to travel into a coking box (20) associated with a heating means, in which the air is heated to a sufficient temperature to coke the oil particles contained in the airflow. Preferably, the solid residues produced by the coking are collected in the coking box (20).
摘要翻译：本发明涉及一种用于处理在与燃气涡轮发动机的滚动轴承箱连通的管（9）中流动的油颗粒的气流的方法，其中所述气流进入焦化箱（20）与加热装置相关联，其中空气被加热到足够的温度以焦化包含在气流中的油颗粒。优选地，通过焦化产生的固体残留物被收集在焦化器（20）中。

7. 发明申请

US20050196088A1 Turbomachine with a compact roller bearing 有权
标题翻译：涡轮机与紧凑型滚子轴承
公开(公告)号：US20050196088A1
公开(公告)日：2005-09-08
申请号：US11072260
申请日：2005-03-07
申请人： Gilles Charier , Guy Dusserre-Telmon , Marc Marchi , Jean-Pierre Mourlan , Patrice Rosset , Zoltan Zsiga
发明人： Gilles Charier , Guy Dusserre-Telmon , Marc Marchi , Jean-Pierre Mourlan , Patrice Rosset , Zoltan Zsiga
IPC分类号： F01D5/02 , F01D25/16 , F02C7/06 , F16C33/58 , F16K25/00
CPC分类号： F01D5/026 , F01D25/166 , F16C2360/23
摘要： A turbomachine roller bearing that supports a shaft constituted by a trunnion of a shaft line of a high-pressure spool of a turbomachine to rotate relative to a stationary support that is connected to a casing of the turbomachine, said bearing comprising rollers inserted between an outer ring disposed adjacent to the stationary support and an inner ring disposed adjacent to the high-pressure trunnion, the inner ring extending along the axis beyond a downstream end of the high-pressure trunnion to which it is secured by clamping means, and being provided with anti-rotation means for preventing said inner ring from rotating relative to the high-pressure trunnion.
摘要翻译：一种涡轮机滚子轴承，其支撑由涡轮机的高压线轴的轴线的耳轴构成的轴，以相对于连接到涡轮机的壳体的固定支撑件旋转，所述轴承包括插入在外部环设置成邻近固定支撑件和邻近高压耳轴设置的内环，内环沿着轴线延伸超过高压耳轴的下游端，其通过夹紧装置固定到该下端，并且设置有用于防止所述内圈相对于高压耳轴旋转的防旋转装置。

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