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公开(公告)号：US09080461B2
公开(公告)日：2015-07-14
申请号：US13364379
申请日：2012-02-02
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。
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公开(公告)号：US08197189B2
公开(公告)日：2012-06-12
申请号：US11945490
申请日：2007-11-27
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。
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公开(公告)号：US20090136348A1
公开(公告)日：2009-05-28
申请号：US11945490
申请日：2007-11-27
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。
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公开(公告)号：US09140125B2
公开(公告)日：2015-09-22
申请号：US13364411
申请日：2012-02-02
CPC分类号： F01D5/025 , F05D2240/40 , F16B37/068 , Y10T29/49948
摘要： An apparatus and method for connecting a fan rotor to a shaft of a gas turbine engine includes a segmented clinch nut plate having a plurality of clinch nuts installed in pre-drilled holes in each segment. A plurality of mounting bolts extending through the holes in the rotor shaft and holes in a mounting device of the shaft threadedly engage the clinch nuts of the clinch nut plate. The segments of the clinch nut plate are disposed separately one from another.
摘要翻译： 用于将风扇转子连接到燃气涡轮发动机的轴的装置和方法包括分段夹紧螺母板，其具有安装在每个段中的预钻孔中的多个紧固螺母。 多个安装螺栓延伸穿过转子轴中的孔，并且轴的安装装置中的孔螺纹地接合夹紧螺母板的紧固螺母。 夹紧螺母板的段彼此分开地设置。
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公开(公告)号：US08632299B2
公开(公告)日：2014-01-21
申请号：US12956405
申请日：2010-11-30
IPC分类号： F01D25/26
CPC分类号： F01D25/002 , F01D25/24
摘要： A gas turbine engine includes a structure defining a circumferential passage in fluid communication with an internal passage in at least one strut radially extending into the engine, circumferential passage also in fluid communication with a plurality or nozzles or jets to provide a wash manifold integrated with the engine casing structure. One or more nozzles are provided in the manifold for directing a washing fluid injected into the duct.
摘要翻译： 燃气涡轮发动机包括限定在径向延伸到发动机中的至少一个支柱中的内部通道流体连通的圆周通道的结构，圆周通道也与多个喷嘴或喷嘴流体连通，以提供与 发动机套管结构。 在歧管中设置一个或多个喷嘴，用于引导注入到管道中的洗涤流体。
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公开(公告)号：US20130205800A1
公开(公告)日：2013-08-15
申请号：US13358889
申请日：2012-02-10
CPC分类号： F01D11/005 , F01D9/042 , F05D2240/55 , Y10T29/49245
摘要： Vane assemblies for gas turbine engines and methods for assembling vane assemblies are disclosed. The vane assemblies may include at least one shroud having at least one vane-receiving portion, at least one vane having at least one end portion received in the vane-receiving portion, and at least one sealing member having an uncompressed cross-section that is substantially circular. The sealing member(s) are disposed between and in contact with the end portion of the vane and the vane-receiving portion of the shroud.
摘要翻译： 公开了用于燃气涡轮发动机的叶片组件和组装叶片组件的方法。 叶片组件可以包括至少一个护罩，其具有至少一个叶片接收部分，至少一个叶片，其具有容纳在叶片容纳部分中的至少一个端部，以及至少一个具有未压缩横截面的密封构件， 大致圆形。 密封构件设置在叶片的端部和护罩的叶片接收部分之间并与之接触。
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公开(公告)号：US09951639B2
公开(公告)日：2018-04-24
申请号：US13358889
申请日：2012-02-10
CPC分类号： F01D11/005 , F01D9/042 , F05D2240/55 , Y10T29/49245
摘要： Vane assemblies for gas turbine engines and methods for assembling vane assemblies are disclosed. The vane assemblies may include at least one shroud having at least one vane-receiving portion, at least one vane having at least one end portion received in the vane-receiving portion, and at least one sealing member having an uncompressed cross-section that is substantially circular. The sealing member(s) are disposed between and in contact with the end portion of the vane and the vane-receiving portion of the shroud.
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公开(公告)号：US09353626B2
公开(公告)日：2016-05-31
申请号：US13614584
申请日：2012-09-13
CPC分类号： F01D5/025 , F02K3/06 , F04D29/266 , F05D2230/60 , F05D2250/292 , F05D2260/30 , F16D2001/0903 , Y10T29/49316
摘要： A rotor assembly for a gas turbine engine, with an annular sleeve having an inner member connected around the shaft to rotate together therewith and having an outer member with a first end connected to the inner member, the outer member defining an annular continuous frustoconical inner surface angled such as to extend closer to the central axis near the first end. A rotor disc includes an annular protuberance extending radially inwardly of the outer member and forced toward the first end, and having an annular continuous frustoconical outer surface complementary to the inner surface of the outer member and in torque-transmitting engagement therewith. The assembly includes means for axially pressing the sleeve and the disc against one another to maintain the complementary frustoconical surfaces in torque-transmitting engagement. A method of engaging a rotor disc to a driving shaft in a gas turbine engine is also provided.
摘要翻译： 一种用于燃气涡轮发动机的转子组件，其具有环形套筒，该内部构件围绕轴连接以与其一起旋转并具有外部构件，第一端连接到内部构件，外部构件限定环形连续的截头圆锥形内表面 成角度的，以便靠近第一端的中心轴线延伸。 转子盘包括沿着外部构件的径向向内延伸并被迫朝向第一端的环形突起，并且具有与外部构件的内表面互补的环形连续的截头圆锥形外表面和与其成扭矩传递接合。 组件包括用于将套筒和盘片彼此轴向按压以保持互补的截头圆锥形表面在扭矩传递接合中的装置。 还提供了一种将转子盘接合到燃气涡轮发动机中的驱动轴的方法。
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公开(公告)号：US08998574B2
公开(公告)日：2015-04-07
申请号：US13223701
申请日：2011-09-01
CPC分类号： F01D5/225 , F05D2260/30
摘要： A vane assembly of a gas turbine engine includes a plurality of circumferentially spaced vanes extending radially between an outer case and an inner case. A spring-tensioned stator restraining strap is provided around the outer case and surrounding outer ends of the respective vanes. The outer ends of the vanes are received in corresponding openings defined in the outer case and project radially outwardly from the outer case. The spring-tensioned strap compresses the respective vanes radially and inwardly in position.
摘要翻译： 燃气涡轮发动机的叶片组件包括在外壳和内壳之间径向延伸的多个周向隔开的叶片。 弹簧张紧的定子限制带设置在外壳周围并且围绕相应叶片的外端。 叶片的外端容纳在限定在外壳中的相应开口中，并从外壳径向向外突出。 弹簧张紧的带子将各个叶片径向和内向压缩在适当位置。
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公开(公告)号：US20130251517A1
公开(公告)日：2013-09-26
申请号：US13428720
申请日：2012-03-23
CPC分类号： F01D9/042
摘要： A vane assembly for a gas turbine engine includes an annular shroud having openings therein and a plurality of vanes extending radially from the shroud and each having an extremity received within one of the openings. A grommet is positioned within each opening for shielding the vane extremity from the annular shroud. The grommet includes an annular protrusion for providing sealing between the opening and the vane extremity, and an annular restraint element adjacent the protrusion for retaining the vane in place relative to the shroud.
摘要翻译： 用于燃气涡轮发动机的叶片组件包括其中具有开口的环形护罩和从护罩径向延伸的多个叶片，并且每个叶片具有容纳在一个开口内的末端。 护环位于每个开口内，用于屏蔽叶片末端与环形护罩。 索环包括用于在开口和叶片末端之间提供密封的环形突起，以及邻近突起的环形约束元件，用于相对于护罩保持叶片在适当位置。
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