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公开(公告)号：US06402469B1
公开(公告)日：2002-06-11
申请号：US09692947
申请日：2000-10-20
IPC分类号： F01D500
CPC分类号： F01D21/045 , F05B2260/3011 , F16C19/06 , F16C27/04 , F16C2360/23 , F16D9/06 , F16D9/08 , Y02T50/671
摘要： A fan decoupling fuse includes a ring having a row of fuse holes circumferentially spaced apart from each other by fuse ligaments sized to fail under shear when carrying abnormal radial loads from the fan.
摘要翻译： 风扇去耦保险丝包括一个具有一排保险丝孔的环，所述保险丝孔彼此间隔开，所述保险丝的尺寸在承受来自所述风扇的异常径向载荷时在剪切下失效。
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公开(公告)号：US06447248B1
公开(公告)日：2002-09-10
申请号：US09693449
申请日：2000-10-20
IPC分类号： F01B2516
CPC分类号： F01D21/045 , F01D25/162 , F05B2260/3011 , F05D2220/326 , F05D2220/327 , Y02T50/671
摘要： A bearing support includes a hollow cone diverging between a forward bearing seat and an aft mounting flange. The cone includes an integral annular fuse sized in thickness to fail in shear under abnormal imbalance load transfer between a gas turbine engine fan supported by a bearing in the forward seat and a fan frame mounted to the aft flange.
摘要翻译： 轴承支撑件包括在前轴承座和后安装凸缘之间分叉的中空锥。 锥体包括一个整体的环形保险丝，其厚度尺寸设计成在由前座中的轴承支撑的燃气涡轮发动机风扇和安装到后翼缘的风扇框架之间的异常不平衡负载传递下的剪切失效。
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公开(公告)号：US06491497B1
公开(公告)日：2002-12-10
申请号：US09668908
申请日：2000-09-22
申请人： Barry Lynn Allmon , Christopher Charles Glynn , Kenneth Lee Fisher , Daniel Edward Mollmann , Bala Corattiyil , Randy Marinus Vondrell , Morris Green Penn , Michael Joseph Gambone , Jan Christopher Schilling
发明人： Barry Lynn Allmon , Christopher Charles Glynn , Kenneth Lee Fisher , Daniel Edward Mollmann , Bala Corattiyil , Randy Marinus Vondrell , Morris Green Penn , Michael Joseph Gambone , Jan Christopher Schilling
IPC分类号： F01D2516
CPC分类号： F01D25/16 , F01D21/045 , F05B2260/3011 , F16C19/06 , F16C19/26 , F16C23/084 , F16C33/60 , F16C2360/23 , Y02T50/671 , Y10S416/50
摘要： A rotor assembly for a gas turbine engine includes a bearing assembly that reduces dynamic loads to a support frame and static bending to the rotor assembly during periods of rotor unbalance. The rotor assembly includes a rotor shaft coupled to a fan and supported longitudinally with a plurality of bearing assemblies on a support frame. A number two bearing assembly includes a paired race, a rolling element, and a mounting race. The mounting race includes a spherical face and is secured to the bearing assembly with a retainer that plastically fails at a pre-determined moment load.
摘要翻译： 用于燃气涡轮发动机的转子组件包括轴承组件，该轴承组件在转子不平衡期间减小对支撑框架的动态载荷和对转子组件的静态弯曲。 转子组件包括联接到风扇并且在支撑框架上纵向地支撑有多个轴承组件的转子轴。 第二轴承组件包括成对的座圈，滚动元件和安装座圈。 安装座圈包括一个球面，并用一个保持架固定在轴承组件上，保持器在预定的力矩载荷下塑性变形。
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公开(公告)号：US07353647B2
公开(公告)日：2008-04-08
申请号：US10845032
申请日：2004-05-13
申请人： Robert Joseph Orlando , Thomas Ory Moniz , John C. Brauer , John Leslie Henry , Raymond Felix Patt , Randy Marinus Vondrell , James Patrick Dolan , Erich Alois Krammer , David Cory Kirk
发明人： Robert Joseph Orlando , Thomas Ory Moniz , John C. Brauer , John Leslie Henry , Raymond Felix Patt , Randy Marinus Vondrell , James Patrick Dolan , Erich Alois Krammer , David Cory Kirk
CPC分类号： F02C3/13 , F02C3/04 , F05D2230/60
摘要： A method facilitates assembling a gas turbine engine including a compressor and a rotor assembly coupled in axial flow communication downstream from the compressor. The method comprises coupling a bypass system in flow communication with the compressor to channel a portion of flow discharged from the compressor towards the rotor assembly is channeled through the bypass system, and coupling a downstream end of the bypass system within the gas turbine engine such that the flow entering the bypass system flows past the rotor assembly and is discharged downstream from the rotor assembly.
摘要翻译： 一种方法有利于组装燃气涡轮发动机，该燃气涡轮发动机包括压缩机和在压缩机下游的轴向流动连通中联接的转子组件。 该方法包括将与压缩机流体连通的旁路系统联接以将从压缩机排出的一部分流向转子组件引导通过旁路系统，并将旁路系统的下游端连接在燃气涡轮发动机内，使得 进入旁路系统的流量流过转子组件，并从转子组件的下游排出。
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