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1. 发明申请

US20150211380A1 TURBINE ENGINE COMPRISING A MEANS FOR MEASURING THE SPEED AND TORQUE OF A SHAFT OF THE TURBINE ENGINE AND METHOD FOR MONITORING SAID SHAFT 有权
标题翻译：涡轮发动机包括用于测量涡轮发动机轴的转速和扭矩的手段和用于监测上述轴的方法
公开(公告)号：US20150211380A1
公开(公告)日：2015-07-30
申请号：US14426147
申请日：2013-09-05
申请人： SNECMA
发明人： Augustin Curlier , Olivier Belmonte , Gilles Le Gouellec
IPC分类号： F01D21/00 , F01D1/18 , F01D25/24
CPC分类号： F01D21/003 , F01D1/18 , F01D25/24 , F02K3/025 , F05D2260/80 , F05D2270/304 , F05D2270/335 , F05D2270/809 , G01L3/105 , G01M15/14 , G01P3/488 , Y02T50/671
摘要： Turbine engine (1), in particular for an aircraft, comprising at least one axial shaft (2) rotatably mounted in a casing (3) of the turbine engine (1), the turbine engine (1) comprising an annular reference part (10) comprising short (11) and long (12) longitudinal reference teeth, first means for detecting the passage of the short (11) and long (12) reference teeth so as to measure the speed of the shaft (2) of the turbine engine (1) about its axis (X), an annular measurement part (20) comprising longitudinal measurement teeth (21); and second means for detecting the passage of the long reference teeth (12) and the measurement teeth (21) so as to measure the torque of the shaft (2, 102) of the turbine engine (1).
摘要翻译：涡轮发动机（1），特别是用于飞行器，包括可旋转地安装在涡轮发动机（1）的壳体（3）中的至少一个轴向轴（2），所述涡轮发动机（1）包括环形参考部分）包括短（11）和长（12）纵向参考齿，第一装置用于检测短（11）和长（12）基准齿的通过，以便测量涡轮发动机的轴（2）的速度（1）围绕其轴线（X），包括纵向测量齿（21）的环形测量部分（20）; 以及用于检测长参考齿（12）和测量齿（21）的通过以便测量涡轮发动机（1）的轴（2,102）的扭矩的第二装置。

2. 发明授权

US09347335B2 Tank having an inclined partition provided at its ends with through-holes for continuous supply of a supply liquid to a turbine engine 有权
标题翻译：具有倾斜隔板的罐在其端部设置有用于将供应液体连续地供应到涡轮发动机的通孔
公开(公告)号：US09347335B2
公开(公告)日：2016-05-24
申请号：US14472929
申请日：2014-08-29
申请人： SNECMA
发明人： Antoine Laigle , Gilles Le Gouellec , Bellal Waissi
IPC分类号： F01D25/20 , F16N17/06 , F01D25/18 , F01M11/00
CPC分类号： F01D25/20 , F01D25/18 , F01M2011/0095 , F16N17/06
摘要： The tank for a turbine engine comprises a partition separating a first compartment from a second compartment of the tank , the partition having a first end and a second end, the second end being closer to the bottom of the tank than the first end, the partition being inclined from the first end to the second end in the first direction and in the direction of the first outlet to the second outlet , the partition comprising at least one first Through-hole near the first end and at least one second through-hole closer to the second end than the first hole.
摘要翻译：用于涡轮发动机的罐包括将第一隔室与罐的第二隔室分开的隔板，隔板具有第一端和第二端，第二端比第一端更靠近罐的底部，隔板在第一方向和第一出口的方向上从第一端向第二端倾斜到第二出口，所述隔板包括在第一端附近的至少一个第一通孔和至少一个第二通孔密封件到第二个端头比第一个孔。

3. 发明授权

US09200525B2 Turbomachine blade incidence control system and turbomachine 有权
标题翻译：涡轮机叶片入口控制系统和涡轮机
公开(公告)号：US09200525B2
公开(公告)日：2015-12-01
申请号：US13654830
申请日：2012-10-18
申请人： SNECMA
发明人： Pascal Marly , Denis Louis Bocquet , Caroline Frantz , Gilles Le Gouellec
IPC分类号： F01D7/00 , B64C11/38
CPC分类号： F01D7/00 , B64C11/385
摘要： Turbomachine blade incidence control system including a fluidic cylinder with a first and a second chamber and having a pressurized fluid network adapted to selectively supply pressurized fluid to the first and/or the second chamber, the fluid network having one fluid routing device having a first normal position and a second protection position. The fluidic cylinder includes a fluid inlet positioned to be in fluid communication with the first chamber when the fluidic cylinder is in the blocked position, the routing device being adapted to set up a fluid communication between the inlet and the second chamber when it is in the protection position and to inhibit the fluid supply to the inlet when it is in the normal position.
摘要翻译：涡轮机叶片入口控制系统包括具有第一和第二室的流体气缸，并且具有适于选择性地将加压流体供应到第一和/或第二室的加压流体网络，流体网络具有一个具有第一正常流体的流体路径装置位置和第二个保护位置。流体气缸包括流体入口，该流体入口被定位成当流体气缸处于阻塞位置时与第一腔室流体连通，该路线装置适于在入口和第二腔室处于阻塞位置时建立流体连通保护位置，并且在入口处于正常位置时抑制流体供应。

4. 发明申请

US20150060206A1 TANK HAVING AN INCLINED PARTITION PROVIDED AT ITS ENDS WITH THROUGH-HOLES FOR CONTINUOUS SUPPLY OF A SUPPLY LIQUID TO A TURBINE ENGINE 有权
标题翻译：具有连续供应液体向涡轮发动机连续通孔的包含分段的油箱
公开(公告)号：US20150060206A1
公开(公告)日：2015-03-05
申请号：US14472929
申请日：2014-08-29
申请人： SNECMA
发明人： Antoine LAIGLE , Gilles Le Gouellec , Bellal Waissi
IPC分类号： F01D25/20 , F01D25/18
CPC分类号： F01D25/20 , F01D25/18 , F01M2011/0095 , F16N17/06
摘要： The tank for a turbine engine comprises a partition separating a first compartment from a second compartment of the tank , the partition having a first end and a second end, the second end being closer to the bottom of the tank than the first end, the partition being inclined from the first end to the second end in the first direction and in the direction of the first outlet to the second outlet , the partition comprising at least one first Through-hole near the first end and at least one second through-hole closer to the second end than the first hole.
摘要翻译：用于涡轮发动机的罐包括将第一隔室与罐的第二隔室分开的隔板，隔板具有第一端和第二端，第二端比第一端更靠近罐的底部，隔板在第一方向和第一出口的方向上从第一端向第二端倾斜到第二出口，所述隔板包括靠近第一端的至少一个第一通孔和至少一个第二通孔密封件到第二个端头比第一个孔。

5. 发明授权

US09708926B2 Turbine engine comprising a means for measuring the speed and torque of a shaft of the turbine engine and method for monitoring said shaft 有权
公开(公告)号：US09708926B2
公开(公告)日：2017-07-18
申请号：US14426147
申请日：2013-09-05
申请人： SNECMA
发明人： Augustin Curlier , Olivier Belmonte , Gilles Le Gouellec
IPC分类号： F01D21/00 , F01D1/18 , F01D25/24 , F02K3/02 , G01L3/10 , G01M15/14 , G01P3/488
CPC分类号： F01D21/003 , F01D1/18 , F01D25/24 , F02K3/025 , F05D2260/80 , F05D2270/304 , F05D2270/335 , F05D2270/809 , G01L3/105 , G01M15/14 , G01P3/488 , Y02T50/671
摘要： Turbine engine (1), in particular for an aircraft, comprising at least one axial shaft (2) rotatably mounted in a casing (3) of the turbine engine (1), the turbine engine (1) comprising an annular reference part (10) comprising short (11) and long (12) longitudinal reference teeth, first means for detecting the passage of the short (11) and long (12) reference teeth so as to measure the speed of the shaft (2) of the turbine engine (1) about its axis (X), an annular measurement part (20) comprising longitudinal measurement teeth (21); and second means for detecting the passage of the long reference teeth (12) and the measurement teeth (21) so as to measure the torque of the shaft (2, 102) of the turbine engine (1).

6. 发明申请

US20130101419A1 TURBOMACHINE BLADE INCIDENCE CONTROL SYSTEM AND TURBOMACHINE 有权
标题翻译：涡轮叶片入侵控制系统和涡轮机
公开(公告)号：US20130101419A1
公开(公告)日：2013-04-25
申请号：US13654830
申请日：2012-10-18
申请人： SNECMA
发明人： Pascal Marly , Denis Louis Bocquet , Caroline Frantz , Gilles Le Gouellec
IPC分类号： F01D7/00
CPC分类号： F01D7/00 , B64C11/385
摘要： Turbomachine blade incidence control system including a fluidic cylinder with a first and a second chamber and having a pressurized fluid network adapted to selectively supply pressurized fluid to the first and/or the second chamber, the fluid network having one fluid routing device having a first normal position and a second protection position. The fluidic cylinder includes a fluid inlet positioned to be in fluid communication with the first chamber when the fluidic cylinder is in the blocked position, the routing device being adapted to set up a fluid communication between the inlet and the second chamber when it is in the protection position and to inhibit the fluid supply to the inlet when it is in the normal position.
摘要翻译：涡轮机叶片入口控制系统包括具有第一和第二室的流体气缸，并具有适于选择性地将加压流体供应到第一和/或第二室的加压流体网络，流体网络具有一个具有第一正常的流体路径装置位置和第二个保护位置。流体气缸包括流体入口，该流体入口被定位成当流体气缸处于阻塞位置时与第一腔室流体连通，该路线装置适于在入口和第二腔室处于阻塞位置时建立流体连通保护位置，并且在入口处于正常位置时抑制流体供应。

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