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公开(公告)号：US09038367B2
公开(公告)日：2015-05-26
申请号：US13234213
申请日：2011-09-16
Applicant: Gabriel L. Suciu , Brian D. Merry , Allan R. Penda , Christopher M. Dye , Jay Bhatt
Inventor： Gabriel L. Suciu , Brian D. Merry , Allan R. Penda , Christopher M. Dye , Jay Bhatt
CPC classification number: F02K1/70 , F01D17/162 , F02K1/12 , F02K1/1207 , F02K1/72 , F05D2220/36 , F05D2250/25
Abstract: A fan case of a gas turbine engine includes a fan blade containment section defined about an engine axis, a thrust reverser cascade section downstream of the blade containment section and a Fan Exit Guide Vane section downstream of the thrust reverser cascade section.
Abstract translation: 燃气涡轮发动机的风扇壳体包括围绕发动机轴线限定的风扇叶片容纳部分，叶片容纳部分下游的推力反向器级联部分和推力反向器级联部分下游的风扇出口引导叶片部分。
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公开(公告)号：US08695920B2
公开(公告)日：2014-04-15
申请号：US13340834
申请日：2011-12-30
Applicant: Gabriel L. Suciu , Brian D. Merry , Christopher M. Dye , Steven B. Johnson , Frederick M. Schwarz
Inventor： Gabriel L. Suciu , Brian D. Merry , Christopher M. Dye , Steven B. Johnson , Frederick M. Schwarz
IPC: B64D29/00
CPC classification number: B64D27/26 , B64D2027/264 , B64D2027/266 , F01D25/162 , F02C3/107 , F02C7/20 , F02K3/06 , F02K3/075 , F05D2260/4031 , F05D2260/40311
Abstract: 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.
Abstract translation: 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：US08672260B2
公开(公告)日：2014-03-18
申请号：US12629317
申请日：2009-12-02
Applicant: Allan R. Penda , Brian D. Merry , Gabriel L. Suciu , Christopher M. Dye
Inventor： Allan R. Penda , Brian D. Merry , Gabriel L. Suciu , Christopher M. Dye
IPC: B64D27/00
CPC classification number: B64D27/20 , B64D27/26 , B64D2027/268 , Y02T50/44
Abstract: A mounting system for a gas turbine engine assembly includes a plurality of mounting links attached the gas turbine engine along a single plane transverse to the engine centerline for separating the loads from the core engine.
Abstract translation: 用于燃气涡轮发动机组件的安装系统包括沿着与发动机中心线横向的单个平面连接燃气涡轮发动机的多个安装链路，用于将负载与核心发动机分离。
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公开(公告)号：US08596965B2
公开(公告)日：2013-12-03
申请号：US13294492
申请日：2011-11-11
Applicant: Brian D. Merry , Gabriel L. Suciu , Christopher M. Dye
Inventor： Brian D. Merry , Gabriel L. Suciu , Christopher M. Dye
IPC: F01D1/00
CPC classification number: F01D25/24 , F01D9/041 , F01D9/065 , F05D2240/12 , F05D2240/55
Abstract: A compressor case support arrangement for a gas turbine engine includes a fan section having a central axis and a compressor case for housing a compressor. An inlet case guides air to the compressor. The compressor case is positioned axially further from the fan section than the inlet case. A support member extends between the fan section and the compressor case. The support member restricts movement of the compressor case relative to the inlet case. The support member is positioned axially further from the fan section than the plumbing access area.
Abstract translation: 用于燃气涡轮发动机的压缩机壳体支撑装置包括具有中心轴线的风扇部分和用于容纳压缩机的压缩机壳体。 入口箱将空气引导到压缩机。 压缩机壳体比入口箱更远离风扇部分。 支撑构件在风扇部分和压缩机壳体之间延伸。 支撑构件限制压缩机壳体相对于入口壳体的移动。 支撑构件比管道通路区域更远离风扇部分。
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35.发明申请公开(公告)号：US20130239584A1
公开(公告)日：2013-09-19
申请号：US13419695
申请日：2012-03-14
Applicant: Gabriel L. Suciu , Jorn A. Glahn , Brian D. Merry , Christopher M. Dye
Inventor： Gabriel L. Suciu , Jorn A. Glahn , Brian D. Merry , Christopher M. Dye
CPC classification number: F02C6/08 , F01D15/08 , F02C7/32 , F02K3/06 , Y02T50/671
Abstract: A gas turbine engine has a spool, a towershaft connected to the spool, an impeller pump, and a speed control pump connected to the towershaft and to the impeller pump for driving the impeller pump at a constant speed.
Abstract translation: 燃气涡轮发动机具有阀芯，连接到阀芯的塔轴，叶轮泵和连接到塔轴和叶轮泵的速度控制泵，用于以恒定速度驱动叶轮泵。
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Patent Agency Ranking
36.发明申请COUNTER-ROTATING LOW PRESSURE TURBINE WITH GEAR SYSTEM MOUNTED TO TURBINE EXHAUST CASE 有权带齿轮系统的逆转低压涡轮机安装在涡轮机排气箱公开(公告)号：US20130223993A1
公开(公告)日：2013-08-29
申请号：US13408301
申请日：2012-02-29
Applicant: Brian D. Merry , Gabriel L. Suciu
Inventor： Brian D. Merry , Gabriel L. Suciu
CPC classification number: F01D15/12 , F01D1/24 , F01D25/162 , F01D25/30 , F02C3/107 , F02C7/32 , F02K3/072 , Y02T50/671
Abstract: A gas turbine engine includes a shaft defining an axis of rotation. An outer rotor directly drives the shaft and includes an outer set of blades. An inner rotor has an inner set of blades interspersed with the outer set of blades. The inner rotor is configured to rotate in an opposite direction about the axis of rotation from the outer rotor. A gear system couples the inner rotor to the shaft and is configured to rotate the inner set of blades at a faster speed than the outer set of blades.
Abstract translation: 燃气涡轮发动机包括限定旋转轴线的轴。 外转子直接驱动轴并且包括一组外部叶片。 内转子具有与外组叶片交替散布的内组叶片。 内转子构造成围绕与外转子的旋转轴线相反的方向旋转。 齿轮系统将内转子连接到轴，并且构造成以比外部组叶片更快的速度旋转内组叶片。
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公开(公告)号：US20130223991A1
公开(公告)日：2013-08-29
申请号：US13407836
申请日：2012-02-29
Applicant: Gabriel L. Suciu , Alan H. Epstein , Wesley K. Lord , Michael E. McCune , Brian D. Merry
Inventor： Gabriel L. Suciu , Alan H. Epstein , Wesley K. Lord , Michael E. McCune , Brian D. Merry
IPC: F01D15/12
CPC classification number: F02C7/36 , F01D15/12 , F02C3/06 , F02C3/107 , F05D2220/32 , F05D2220/36 , F05D2240/24 , F05D2240/35 , F05D2240/40 , F05D2240/60 , F05D2260/4031 , F05D2260/40311
Abstract: A gas turbine engine includes a core engine with a compressor section, a combustor and a turbine. The turbine drives an output shaft, and the output shaft drives at least four gears. Each of the at least four gears extends through a drive shaft to drive an associated fan rotor.
Abstract translation: 燃气涡轮发动机包括具有压缩机部分的核心发动机，燃烧器和涡轮机。 涡轮驱动输出轴，输出轴驱动至少四个齿轮。 所述至少四个齿轮中的每一个延伸穿过驱动轴以驱动相关联的风扇转子。
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公开(公告)号：US08511604B2
公开(公告)日：2013-08-20
申请号：US13484400
申请日：2012-05-31
Applicant: Gabriel L. Suciu , Brian D. Merry , Christopher M. Dye , Steven B. Johnson , Frederick M. Schwarz
Inventor： Gabriel L. Suciu , Brian D. Merry , Christopher M. Dye , Steven B. Johnson , Frederick M. Schwarz
IPC: B64D29/00
CPC classification number: B64D27/26 , B64D2027/264 , B64D2027/266
Abstract: A gas turbine engine includes a spool along an engine centerline axis which drives a gear train.
Abstract translation: 燃气涡轮发动机包括沿发动机中心线轴线驱动齿轮系的线轴。
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公开(公告)号：US08448895B2
公开(公告)日：2013-05-28
申请号：US13484361
申请日：2012-05-31
Applicant: Gabriel L. Suciu , Brian D. Merry , Christopher M. Dye , Steven B. Johnson , Frederick M. Schwarz
Inventor： Gabriel L. Suciu , Brian D. Merry , Christopher M. Dye , Steven B. Johnson , Frederick M. Schwarz
IPC: B64D29/00
CPC classification number: B64D27/26 , B64D2027/264 , B64D2027/266
Abstract: A gas turbine engine includes a fan section and a low spool that includes a low pressure compressor section. The low pressure compressor section includes eight (8) or less stages. A high spool includes a high pressure compressor section that has between eight to fifteen (8-15) stages. An overall compressor pressure ratio is provided by the combination of the low pressure compressor section and the high pressure compressor. A gear train is defined along an engine centerline axis. The low spool is operable to drive the fan section through the gear train.
Abstract translation: 燃气涡轮发动机包括风扇部分和包括低压压缩机部分的低阀芯。 低压压缩机部分包括八（8）个或更少的阶段。 高阀芯包括高压压缩机部分，其具有8至15（8-15）级。 整体压缩机压力比由低压压缩机部分和高压压缩机的组合提供。 齿轮系沿发动机中心线定义。 低阀芯可操作以通过齿轮系驱动风扇部分。
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公开(公告)号：US20130108466A1
公开(公告)日：2013-05-02
申请号：US13283710
申请日：2011-10-28
Applicant: Gabriel L. Suciu , Stephen P. Muron , Christopher M. Dye , Ioannis Alvanos , Brian D. Merry
Inventor： Gabriel L. Suciu , Stephen P. Muron , Christopher M. Dye , Ioannis Alvanos , Brian D. Merry
CPC classification number: F01D5/02 , F01D5/022 , F01D5/025 , F01D5/027 , F01D5/066 , F01D5/14 , F01D5/147 , F01D11/006 , F05D2240/20 , F05D2260/15 , Y10T29/49316 , Y10T29/4932
Abstract: A spacer for a gas turbine engine includes a rotor ring defined along an axis of rotation, the rotor ring defines a forward circumferential flange which defines a first thickness and an aft circumferential flange which defines a second thickness, the first thickness different than the second thickness. A plurality of core gas path seals which extend from the rotor ring opposite the ramped interface.
Abstract translation: 用于燃气涡轮发动机的间隔件包括沿着旋转轴线限定的转子环，转子环限定限定第一厚度的前周向凸缘和限定第二厚度的后周向凸缘，第一厚度不同于第二厚度 。 多个核心气体路径密封件，其从转子环延伸，与斜坡界面相对。
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