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

IPC分类号： F02C3/04 ,  F02K3/04

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。

公开(公告)号：US07966806B2

公开(公告)日：2011-06-28

申请号：US11555097

申请日：2006-10-31

申请人： John Leslie Henry ,  Robert Joseph Orlando ,  Thomas Ory Moniz

发明人： John Leslie Henry ,  Robert Joseph Orlando ,  Thomas Ory Moniz

IPC分类号： F02K3/02 ,  F02K3/072

CPC分类号： F02C3/067 ,  F02C7/36 ,  F05D2260/40311

摘要： A turbofan engine assembly includes a core gas turbine engine including a high-pressure compressor, a combustor, and a high-pressure turbine, a low-pressure turbine coupled to said core gas turbine engine, a counter-rotating booster compressor comprising a first rotor section configured to rotate in a first direction and a second rotor section configured to rotate in an opposite second direction, and a gearbox comprising an input and an output, said gearbox output coupled to at least one of said first and second rotor sections, said gearbox input coupled to said low-pressure turbine. A method of assembling the turbofan engine assembly described herein is also provided.

摘要翻译： 涡轮风扇发动机组件包括：包括高压压缩机，燃烧器和高压涡轮机的核心燃气涡轮发动机，与所述核心燃气涡轮发动机相连的低压涡轮;反向旋转增压压缩机，包括第一转子 其构造成沿第一方向旋转，第二转子部分构造成沿相反的第二方向旋转;以及齿轮箱，包括输入和输出，所述齿轮箱输出联接到所述第一和第二转子部分中的至少一个，所述变速箱 输入端连接到所述低压涡轮。 还提供了一种组装本文所述涡轮风扇发动机组件的方法。

公开(公告)号：US20080098718A1

公开(公告)日：2008-05-01

申请号：US11555097

申请日：2006-10-31

申请人： John Leslie Henry ,  Robert Joseph Orlando ,  Thomas Ory Moniz

发明人： John Leslie Henry ,  Robert Joseph Orlando ,  Thomas Ory Moniz

IPC分类号： F02K3/02

CPC分类号： F02C3/067 ,  F02C7/36 ,  F05D2260/40311

摘要： A turbofan engine assembly includes a core gas turbine engine including a high-pressure compressor, a combustor, and a high-pressure turbine, a low-pressure turbine coupled to said core gas turbine engine, a counter-rotating booster compressor comprising a first rotor section configured to rotate in a first direction and a second rotor section configured to rotate in an opposite second direction, and a gearbox comprising an input and an output, said gearbox output coupled to at least one of said first and second rotor sections, said gearbox input coupled to said low-pressure turbine. A method of assembling the turbofan engine assembly described herein is also provided.

摘要翻译： 涡轮风扇发动机组件包括：包括高压压缩机，燃烧器和高压涡轮机的核心燃气涡轮发动机，与所述核心燃气涡轮发动机相连的低压涡轮;反向旋转增压压缩机，包括第一转子 其构造成沿第一方向旋转，第二转子部分构造成沿相反的第二方向旋转;以及齿轮箱，包括输入和输出，所述齿轮箱输出联接到所述第一和第二转子部分中的至少一个，所述变速箱 输入端连接到所述低压涡轮。 还提供了一种组装本文所述涡轮风扇发动机组件的方法。

公开(公告)号：US07228683B2

公开(公告)日：2007-06-12

申请号：US10895585

申请日：2004-07-21

申请人： John Leslie Henry

发明人： John Leslie Henry

IPC分类号： F02K3/11

CPC分类号： F02C5/12 ,  F02C5/02 ,  F02K3/11

摘要： Methods and apparatus for generating thrust from a gas turbine engine using a pulse detonation system is provided. The gas turbine engine includes a fan assembly, and a bypass duct channeling air to a core engine and the pulse detonation system. The method includes injecting a charge of fuel into a pulse detonation tube that is coupled radially outward from the core engine, and controlling a supply of air from the fan into the pulse detonation tube through an opening in the inlet end of the pulse detonation tube using a rotary valve that is positioned radially outward from the core engine.

摘要翻译： 提供了使用脉冲爆震系统从燃气涡轮发动机产生推力的方法和装置。 燃气涡轮发动机包括风扇组件和将空气引导到核心发动机和脉冲爆震系统的旁路管道。 该方法包括将燃料的燃料喷射到从核心发动机径向向外连接的脉冲爆管中，并通过脉冲爆管的入口端的开口控制从风扇进入脉冲爆管的空气供应，使用 从核心发动机径向向外定位的旋转阀。

公开(公告)号：US07409819B2

公开(公告)日：2008-08-12

申请号：US10976382

申请日：2004-10-29

申请人： John Leslie Henry

发明人： John Leslie Henry

IPC分类号： F02C3/20 ,  F02K3/072 ,  F02C3/067

CPC分类号： F02K3/062 ,  F01D1/24 ,  F01D25/16 ,  F02C3/067 ,  F05D2260/40311

摘要： A method of assembling a gas turbine engine that includes rotatably coupling a first low-pressure turbine rotor to a high-pressure turbine, rotatably coupling a second low pressure turbine rotor to the first low-pressure turbine rotor, and rotatably coupling the second low-pressure turbine rotor to a turbine rear-frame such that a weight of the high-pressure turbine is transmitted to the turbine rear-frame.

摘要翻译： 一种组装燃气涡轮发动机的方法，其包括将第一低压涡轮机转子可旋转地联接到高压涡轮机，将第二低压涡轮机转子可旋转地联接到第一低压涡轮机转子，以及将第二低压涡轮机转子 高压涡轮机转子到涡轮机后框架，使得高压涡轮机的重量被传递到涡轮机后框架。