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公开(公告)号：US08979491B2
公开(公告)日：2015-03-17
申请号：US13289067
申请日：2011-11-04
CPC分类号： B64D27/26 , B64D27/20 , F01D25/162 , F01D25/28 , F02K3/06 , F05D2250/322 , Y02T50/671
摘要： A gas turbine engine has a rear mounting structure incorporating a mounting apparatus attached to a bypass duct wall with a link device of six rods for transferring core portion related inertia-induced loads, from an inner case of the core portion in a short circuit across an annular bypass air passage to the bypass duct wall.
摘要翻译： 一种燃气涡轮发动机具有后部安装结构，其包括安装在旁路管壁上的安装装置，其具有六个杆的连接装置，用于将芯部相关的惯性引起的负载从短路中的芯部的内壳跨越 环形旁路空气通道到旁路管道壁。
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公开(公告)号：US09068476B2
公开(公告)日：2015-06-30
申请号：US13334517
申请日：2011-12-22
申请人： Stephen Caulfeild , Bryan Olver
发明人： Stephen Caulfeild , Bryan Olver
CPC分类号： F01D25/28 , F01D25/26 , F05D2300/603 , F16C7/02 , Y02T50/672
摘要： The link rod can have a core portion supported inside an annular bypass duct with a bypass air passage extending radially therebetween, the link rod comprising a hot end fitting, a cold end, and an elongated and hollow strut body of composite material and having an aerodynamic cross-sectional shape, the strut body being secured to the hot end fitting and extending between the hot end fitting and the cold end, the hot end fitting having a metal body housing a spherical bearing mountable to the core portion, and the cold end housing a spherical bearing mountable to the bypass duct wall.
摘要翻译： 连杆可以具有支撑在环形旁路管道内的芯部分，旁路通道在其间径向延伸，所述连杆包括热端配件，冷端和细长且中空的复合材料支柱体，并且具有空气动力学 横截面形状，支柱体固定到热端配件并且在热端配件和冷端之间延伸，热端配件具有容纳可安装到芯部的球形轴承的金属体，并且冷端壳体 可安装到旁路管壁的球面轴承。
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公开(公告)号：US20130164126A1
公开(公告)日：2013-06-27
申请号：US13334517
申请日：2011-12-22
申请人： Stephen Caulfeild , Bryan Olver
发明人： Stephen Caulfeild , Bryan Olver
IPC分类号： F01D25/28
CPC分类号： F01D25/28 , F01D25/26 , F05D2300/603 , F16C7/02 , Y02T50/672
摘要： The link rod can have a core portion supported inside an annular bypass duct with a bypass air passage extending radially therebetween, the link rod comprising a hot end fitting, a cold end, and an elongated and hollow strut body of composite material and having an aerodynamic cross-sectional shape, the strut body being secured to the hot end fitting and extending between the hot end fitting and the cold end, the hot end fitting having a metal body housing a spherical bearing mountable to the core portion, and the cold end housing a spherical bearing mountable to the bypass duct wall.
摘要翻译： 连杆可以具有支撑在环形旁路管道内的芯部分，旁路通道在其间径向延伸，所述连杆包括热端配件，冷端和细长且中空的复合材料支柱体，并且具有空气动力学 横截面形状，支柱体固定到热端配件并且在热端配件和冷端之间延伸，热端配件具有容纳可安装到芯部的球形轴承的金属体，并且冷端壳体 可安装到旁路管壁的球面轴承。
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公开(公告)号：US09194296B2
公开(公告)日：2015-11-24
申请号：US13557270
申请日：2012-07-25
申请人： Ljubisa Vrljes , Stephen Caulfeild
发明人： Ljubisa Vrljes , Stephen Caulfeild
CPC分类号： F02C7/20 , Y10T29/49245
摘要： A bypass duct of a gas turbine engine has an inner bypass duct wall having a front end portion which is rigidly mounted to an engine core case and a rear end portion which is flexibly mounted to the core case. The flexible mounting between the rear portion of the inner bypass duct wall and the core case allows hot engine areas of the core case to thermally grow and contract relative to the inner bypass duct wall without imposing additional loads on the inner bypass duct wall.
摘要翻译： 燃气涡轮发动机的旁通管具有内部旁通管壁，内侧旁通管壁具有刚性地安装在发动机芯壳体上的前端部分，以及柔性地安装在芯壳体上的后端部分。 内部旁通管道壁的后部和芯壳之间的柔性安装允许芯壳的热引擎区域相对于内部旁路管道壁热生长和收缩，而不会在内部旁路管道壁上施加额外的负载。
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公开(公告)号：US20130309070A1
公开(公告)日：2013-11-21
申请号：US13557270
申请日：2012-07-25
申请人： Ljubisa VRLJES , Stephen Caulfeild
发明人： Ljubisa VRLJES , Stephen Caulfeild
CPC分类号： F02C7/20 , Y10T29/49245
摘要： A bypass duct of a gas turbine engine has an inner bypass duct wall has a front end portion which is rigidly mounted to an engine core case and a rear end portion which is flexibly mounted to the core case. The flexible mounting between the rear portion of the inner bypass duct wall and the core case allows hot engine areas of the core case to thermally grow and contract relative to the inner bypass duct wall without imposing additional loads on the inner bypass duct wall.
摘要翻译： 燃气涡轮发动机的旁通管具有内旁通管壁，其具有刚性地安装到发动机芯壳的前端部和柔性地安装到芯壳的后端部。 内部旁通管道壁的后部和芯壳之间的柔性安装允许芯壳的热引擎区域相对于内部旁路管道壁热生长和收缩，而不会在内部旁路管道壁上施加额外的负载。
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