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公开(公告)号：US20120233982A1
公开(公告)日：2012-09-20
申请号：US13484361
申请日：2012-05-31
申请人： Gabriel L. Suciu , Brian D. Merry , Christopher M. Dye , Steven B. Johnson , Frederick M. Schwarz
发明人： Gabriel L. Suciu , Brian D. Merry , Christopher M. Dye , Steven B. Johnson , Frederick M. Schwarz
CPC分类号： B64D27/26 , B64D2027/264 , B64D2027/266
摘要： A gas turbine engine includes a spool along an engine centerline axis which drives a gear train, said spool includes a low pressure compressor with four to eight (4-8) stages.
摘要翻译： 燃气涡轮发动机包括沿着驱动齿轮系的发动机中心轴线的阀芯，所述阀芯包括具有四至八（4-8）级的低压压缩机。
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公开(公告)号：US20120198815A1
公开(公告)日：2012-08-09
申请号：US13340834
申请日：2011-12-30
申请人： Gabriel L. Suciu , Brian D. Merry , Christopher M. Dye , Steven B. Johnson , Frederick M. Schwars
发明人： Gabriel L. Suciu , Brian D. Merry , Christopher M. Dye , Steven B. Johnson , Frederick M. Schwars
CPC分类号： B64D27/26 , B64D2027/264 , B64D2027/266 , F01D25/162 , F02C3/107 , F02C7/20 , F02K3/06 , F02K3/075 , F05D2260/4031 , F05D2260/40311
摘要： A gas turbine engine includes a spool along an engine centerline axis which drives a gear train, said spool includes a low stage count low pressure turbine.
摘要翻译： 燃气涡轮发动机包括沿着发动机中心线轴线驱动齿轮系的线轴，所述线轴包括低段数低压涡轮机。
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公开(公告)号：US08210800B2
公开(公告)日：2012-07-03
申请号：US12138370
申请日：2008-06-12
IPC分类号： F01D17/00
CPC分类号： F01D17/162 , F02C9/20 , F04D27/0215 , F04D29/563 , Y02T50/671
摘要： An actuator module for a gas turbine engine includes a multiple of actuators mounted within a common actuator housing.
摘要翻译： 用于燃气涡轮发动机的致动器模块包括安装在公共致动器壳体内的多个致动器。
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公开(公告)号：US08192143B2
公开(公告)日：2012-06-05
申请号：US12154200
申请日：2008-05-21
IPC分类号： F01D15/12
CPC分类号： F02C7/32 , F01D25/18 , F05D2260/403 , Y10T29/49464
摘要： An assembly for a gas turbine engine includes an intermediate case and a gearbox. The intermediate case defines an annular transition duct. The gearbox comprises a plurality of lobes and is integrally formed with the annular transition duct.
摘要翻译： 用于燃气涡轮发动机的组件包括中间壳体和变速箱。 中间壳体限定环形过渡管道。 齿轮箱包括多个叶片，并与环形过渡管道整体形成。
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公开(公告)号：US20120121390A1
公开(公告)日：2012-05-17
申请号：US13340940
申请日：2011-12-30
CPC分类号： B64D27/26 , B64D2027/264 , B64D2027/266
摘要： A gas turbine engine includes a spool along an engine centerline axis which drives a gear train, said spool includes a low pressure compressor with four (4) stages.
摘要翻译： 燃气涡轮发动机包括沿着发动机中心轴线驱动齿轮系的线轴，所述线轴包括具有四（4）级的低压压缩机。
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公开(公告)号：US08167237B2
公开(公告)日：2012-05-01
申请号：US12052769
申请日：2008-03-21
IPC分类号： B64D27/02
CPC分类号： B64D27/26 , B64D2027/266 , B64D2027/268
摘要： A mounting system for a gas turbine engine includes a mounting linkage assembly and a tangential link positioned generally transverse to the mounting linkage assembly. The mounting linkage assembly reacts at least a thrust load. The tangential link reacts at least a vertical load, a side load, and a torque load of the gas turbine engine.
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公开(公告)号：US20090183512A1
公开(公告)日：2009-07-23
申请号：US12016337
申请日：2008-01-18
摘要： A mounting system for a gas turbine engine includes a thrust ring and a linkage assembly. The linkage assembly is at least partially received by the thrust ring. The linkage assembly reacts at least a side load and a thrust load communicated from the thrust ring.
摘要翻译： 用于燃气涡轮发动机的安装系统包括推力环和连杆组件。 连杆组件至少部分地被推力环接收。 连杆组件至少反作用于从止推环传递的侧向载荷和推力载荷。
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公开(公告)号：US10145266B2
公开(公告)日：2018-12-04
申请号：US13362237
申请日：2012-01-31
申请人： Brian D. Merry , Gabriel L. Suciu
发明人： Brian D. Merry , Gabriel L. Suciu
IPC分类号： F01D25/16
摘要： A gas turbine engine includes a shaft supported by first and second bearings for rotation relative to an inlet case. The first and second bearings are positioned within a common bearing compartment.
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公开(公告)号：US09957918B2
公开(公告)日：2018-05-01
申请号：US11846095
申请日：2007-08-28
摘要： A turbine engine is disclosed that includes a fan case surrounding a fan. A core is supported relative to the fan case by support structure, such as flow exit guide vanes, which are arranged downstream from the fan. The core includes a core housing having an inlet case arranged to receive airflow from the fan. A compressor case is arranged axially adjacent to the inlet case and surrounds a compressor stage. In one example, the example turbine engine includes a gear train arranged between the fan and a spool. The gear train is axially aligned and supported by the inlet case. An intermediate case is arranged axially adjacent to the compressor case. The support structure is arranged axially forward of the intermediate case. In one example, the support structure is axially aligned with the compressor case.
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公开(公告)号：US09915154B2
公开(公告)日：2018-03-13
申请号：US13116093
申请日：2011-05-26
CPC分类号： F01D5/282 , C04B37/00 , C04B2235/5244 , C04B2237/365 , C04B2237/38 , C04B2237/76 , F01D5/147 , F01D5/284 , F01D9/041 , F01D25/246 , F05D2240/12 , F05D2300/6033 , Y10T29/49321
摘要： A Ceramic Matrix Composite (CMC) airfoil segment for a gas turbine engine includes a box-shape fiber geometry which defines a rectilinear pressure side bond line and a rectilinear suction side bond line.
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