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11. 发明申请

US20140061375A1 ASSEMBLY FOR MOUNTING A TURBINE ENGINE TO A PYLON 有权
标题翻译：用于安装涡轮发动机到PYLON的组件
公开(公告)号：US20140061375A1
公开(公告)日：2014-03-06
申请号：US13601395
申请日：2012-08-31
申请人： David F. Sandy , Zhijun Zheng , Stephen P. Dailey , Joseph P. Foster
发明人： David F. Sandy , Zhijun Zheng , Stephen P. Dailey , Joseph P. Foster
IPC分类号： B64D27/16
CPC分类号： B64D27/26 , B64D2027/266 , B64D2027/268 , F02C7/20 , F02K3/06
摘要： An assembly for mounting a turbine engine to a pylon includes a mounting beam, a plurality of fasteners, a first mounting linkage and a second mounting linkage. The mounting beam includes a mount beam fitting that extends axially between a first mount beam end and a second mount beam end, and a mount beam flange that extends radially out from the mount beam fitting at the first mount beam end. A first fastener aperture extends radially through the mount beam fitting, and a second fastener aperture extends axially through the mount beam flange. The fasteners connect the mounting beam to the pylon. A first of the fasteners is mated with the first fastener aperture, and a second of the fasteners is mated with the second fastener aperture. The first mounting linkage connects the first mount beam end to a first engine attachment. The second mounting linkage connects the second mount beam end to second engine attachments.
摘要翻译：用于将涡轮发动机安装到塔架的组件包括安装梁，多个紧固件，第一安装连杆和第二安装连杆。安装梁包括在第一安装梁端部和第二安装梁端部之间轴向延伸的安装梁配件以及从第一安装梁端部处的安装梁配件径向向外延伸的安装梁凸缘。第一紧固件孔口径向延伸穿过安装梁配件，并且第二紧固件孔口轴向延伸穿过安装梁凸缘。紧固件将安装梁连接到塔架。紧固件中的第一紧固件与第一紧固件孔口配合，并且第二紧固件与第二紧固件孔口配合。第一安装连杆将第一安装梁端连接到第一引擎附件。第二安装联动装置将第二安装梁端部连接到第二发动机附件。

12. 发明申请

US20130302157A1 ADJUSTABLE ENGINE MOUNT 有权
标题翻译：可调节发动机安装
公开(公告)号：US20130302157A1
公开(公告)日：2013-11-14
申请号：US13468072
申请日：2012-05-10
申请人： David F. Sandy , Zhijun Zheng
发明人： David F. Sandy , Zhijun Zheng
IPC分类号： F01D25/28 , F16M13/02
CPC分类号： F01D25/28 , B64D2027/262 , B64D2027/266 , B64D2027/268 , F02C7/20 , Y02T50/671
摘要： A forward engine mount assembly for a gas turbine engine includes a mount beam having a main body with a fore end and an aft end and a forward shackle assembly supported by the fore end of the mount beam. The forward shackle assembly comprises a first link configured to be connected to a first engine case structure and a second link configured to be connected to a second engine case structure. The first and second links are pivotally attached to each other.
摘要翻译：用于燃气涡轮发动机的前向发动机安装组件包括具有前端和后端的主体的安装梁和由安装梁的前端支撑的前向钩环组件。前向卸扣组件包括被配置为连接到第一发动机外壳结构的第一连杆和被配置为连接到第二发动机外壳结构的第二连杆。第一和第二连杆彼此枢转地连接。

13. 发明申请

US20120304811A1 GEARBOX MOUNT BRACKET 有权
标题翻译： GEARBOX安装支架
公开(公告)号：US20120304811A1
公开(公告)日：2012-12-06
申请号：US13149256
申请日：2011-05-31
申请人： Chris J. Niggemeier , Harvey C. Lee , Zhijun Zheng
发明人： Chris J. Niggemeier , Harvey C. Lee , Zhijun Zheng
IPC分类号： F16H57/02 , F16M13/02
CPC分类号： F02C7/32 , F05D2260/30 , F05D2260/36 , Y10T74/2186
摘要： A bracket for attaching a gearbox to an engine casing has a first portion having a first array of openings for receiving attachments therethrough, the first portion having, on a backside thereof, a first rail for engaging a slot in the engine casing, and a second portion having a second array of openings for receiving attachments therethrough. A hookup for attaching to the gearbox attaches to and in between the first portion and the second portion for diminishing effects of radial rotation between the casing and the gearbox.
摘要翻译：用于将齿轮箱附接到发动机壳体的支架具有第一部分，其具有用于接收穿过其的附件的第一开口阵列，其第一部分在其后侧具有用于接合发动机壳体中的狭槽的第一轨道，以及第二部分部分具有用于接收穿过其中的附件的第二开口阵列。用于附接到齿轮箱的连接件附接到第一部分和第二部分之间并且在第一部分和第二部分之间，以减小壳体和齿轮箱之间的径向旋转的影响。

14. 发明授权

US08561501B2 Gearbox mount bracket 有权
标题翻译：变速箱安装支架
公开(公告)号：US08561501B2
公开(公告)日：2013-10-22
申请号：US13149256
申请日：2011-05-31
申请人： Chris J. Niggemeier , Harvey C. Lee , Zhijun Zheng
发明人： Chris J. Niggemeier , Harvey C. Lee , Zhijun Zheng
IPC分类号： F16H57/02
CPC分类号： F02C7/32 , F05D2260/30 , F05D2260/36 , Y10T74/2186
摘要： A bracket for attaching a gearbox to an engine casing has a first portion having a first array of openings for receiving attachments therethrough, the first portion having, on a backside thereof, a first rail for engaging a slot in the engine casing, and a second portion having a second array of openings for receiving attachments therethrough. A hookup for attaching to the gearbox attaches to and in between the first portion and the second portion for diminishing effects of radial rotation between the casing and the gearbox.
摘要翻译：用于将齿轮箱附接到发动机壳体的支架具有第一部分，其具有用于接收穿过其的附件的第一开口阵列，其第一部分在其后侧具有用于接合发动机壳体中的狭槽的第一轨道，以及第二部分部分具有用于接收穿过其中的附件的第二开口阵列。用于附接到齿轮箱的连接件附接到第一部分和第二部分之间并且在第一部分和第二部分之间，以减小壳体和齿轮箱之间的径向旋转的影响。

15. 发明申请

US20130193298A1 GAS TURBINE ENGINE MOUNTING STRUCTURE WITH SECONDARY LOAD PATH 审中-公开
标题翻译：燃气涡轮发动机安装结构与二次负载路径
公开(公告)号：US20130193298A1
公开(公告)日：2013-08-01
申请号：US13360750
申请日：2012-01-29
申请人： David F. Sandy , Zhijun Zheng
发明人： David F. Sandy , Zhijun Zheng
IPC分类号： F16M13/02
CPC分类号： B64D27/26 , B64D2027/268
摘要： A connection for mounting an aircraft engine to an aircraft pylon has a plate to be bolted to a portion of an aircraft engine, and a body extending rearwardly from the plate. The body has a main pivot attachment to a balance beam, which has thrust links pivotally attached to the balance beam. A back-up connection is included between the balance beam and the body such that the back-up connection allows normal pivoting movement of the balance beam relative to the body without contact at the back-up connection.
摘要翻译：用于将飞机发动机安装到飞机挂架的连接件具有用于螺栓连接到飞行器发动机的一部分的板和从板向后延伸的主体。主体具有到平衡梁的主枢轴连接，其具有枢转地附接到平衡梁的推力连杆。在平衡梁和主体之间包括备用连接，使得备用连接允许平衡梁相对于主体的正常枢转运动而不在后备连接处接触。

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