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公开(公告)号：US08961125B2
公开(公告)日：2015-02-24
申请号：US13324110
申请日：2011-12-13
申请人： Conway Chuong , Kurt P. Werner , Shelton O. Duelm
发明人： Conway Chuong , Kurt P. Werner , Shelton O. Duelm
IPC分类号： F01D25/24
CPC分类号： F01D25/243 , F01D9/042 , F05D2230/64
摘要： A gas turbine engine includes an engine casing structure and a retention block assembly. The engine casing structure includes a pocket which receives the retention block assembly. The retention block assembly includes a stop block and a pin that retains the stop block within the pocket. The stop block is loose relative to the pin.
摘要翻译： 燃气涡轮发动机包括发动机壳体结构和保持块组件。 发动机壳体结构包括容纳保持块组件的口袋。 保持块组件包括止动块和将止动块保持在口袋内的销。 止动块相对于销松动。
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公开(公告)号：US20140314547A1
公开(公告)日：2014-10-23
申请号：US13600781
申请日：2012-08-31
申请人： David J. Sander , Shelton O. Duelm
发明人： David J. Sander , Shelton O. Duelm
IPC分类号： F01D25/28
CPC分类号： F02C7/20 , F01D25/162 , F05D2300/6033 , Y02T50/672 , Y10T29/49947 , Y10T29/49948
摘要： A first ceramic matrix composite structure having a first flange with a first aperture, and a second structure having a second flange with a second aperture are clamped together by a fastener and spring assembly. The second flange is in contact with the first flange and the apertures of the first and second flanges align with each other. A threaded fastener having a thermal expansion rate that is different than the thermal expansion rate of at least one of the first ceramic matrix composite structure and second structure extends through the aligned apertures. The fastener includes a bolt, a nut, and a spring assembly that maintains a constant clamping pressure irrespective of the thermal expansion differences between the bolt and the first ceramic matrix composite structure and second structure.
摘要翻译： 具有第一凸缘和第二孔的第一陶瓷基体复合结构具有第一凸缘和具有第二孔的第二凸缘的第二结构由紧固件和弹簧组件夹紧在一起。 第二凸缘与第一凸缘接触并且第一和第二凸缘的孔彼此对准。 具有不同于第一陶瓷基体复合结构和第二结构中的至少一个的热膨胀率的热膨胀率的螺纹紧固件延伸穿过对准的孔。 紧固件包括螺栓，螺母和弹簧组件，其保持恒定的夹紧压力，而不管螺栓和第一陶瓷基体复合结构和第二结构之间的热膨胀差异如何。
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公开(公告)号：US09851008B2
公开(公告)日：2017-12-26
申请号：US13487721
申请日：2012-06-04
CPC分类号： F16J15/0887 , F01D9/02 , F01D11/005 , F01D11/08 , F02C7/28
摘要： A seal land for a gas turbine engine can include a seal body circumferentially extending about a longitudinal centerline axis. The seal body includes at least one sealing surface that extends in a plane that is transverse to the longitudinal centerline axis.
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4.发明授权Convergent-divergent gas turbine nozzle comprising movable flaps having a variable thickness in a lateral direction 有权收敛发散燃气轮机喷嘴包括在横向上具有可变厚度的可动翼片公开(公告)号：US09163582B2
公开(公告)日：2015-10-20
申请号：US13483499
申请日：2012-05-30
CPC分类号： F02K1/1223 , F02K1/12 , F05D2300/6033 , F23R3/16
摘要： A liner assembly includes a plurality of flaps arranged about a central axis and operable to move relative to the central axis. Each of the plurality of flaps defines a forward end and an aft end, lateral sides, and an inner surface and an outer surface relative to the central axis. Each of the plurality of flaps has a thickness between the inner surface and the outer surface, and thickness varies in a lateral direction between the lateral sides.
摘要翻译： 衬套组件包括围绕中心轴布置并可操作以相对于中心轴线移动的多个翼片。 多个翼片中的每一个限定了前端和后端，侧面以及相对于中心轴线的内表面和外表面。 多个翼片中的每一个在内表面和外表面之间具有厚度，并且厚度在横向方向之间在横向方向上变化。
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公开(公告)号：US20140010662A1
公开(公告)日：2014-01-09
申请号：US13540872
申请日：2012-07-03
IPC分类号： F01D5/14
CPC分类号： F01D5/147 , B29C70/30 , B29D99/0025 , B29L2031/082 , F01D5/14 , F01D5/28 , F01D5/282 , Y02T50/43 , Y10T29/49332
摘要： A method of forming an airfoil with an integrated platform includes: a) providing an airfoil core; b) wrapping a first overwrap ply around the airfoil core; c) darting a first end of the first overwrap ply to allow the overwrap ply to extend perpendicular to the airfoil core to form a first platform; d) filling the darted parts filler plies; e) wrapping a second overwrap ply around the first overwrap ply; f) darting a first end of the second overwrap ply to allow the second overwrap ply to extend adjacent to the first overwrap ply to form the first platform; g) filling the darted parts of the second overwrap ply with one or more filler plies; and h) placing a cap ply in the shape of the platform adjacent to at least one of the first and second overwrap plies. An airfoil with an integrated platform is also disclosed.
摘要翻译： 一种形成具有集成平台的翼型件的方法包括：a）提供翼型芯; b）围绕翼型芯缠绕第一外包裹层; c）打开第一外包裹层的第一端以允许外包裹层垂直于翼型芯延伸以形成第一平台; d）填充飞镖零件填充层; e）在第一外包裹层周围缠绕第二个外包裹层; f）打开第二外包裹层的第一端以允许第二外包裹层相邻于第一外包裹层延伸以形成第一平台; g）用一个或多个填料层填充第二外包装层的飞镖部分; 以及h）将帽层放置成与所述第一和第二外包裹层中的至少一个相邻的所述平台的形状。 还公开了具有集成平台的翼型件。
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公开(公告)号：US09328626B2
公开(公告)日：2016-05-03
申请号：US13590348
申请日：2012-08-21
CPC分类号： F01D25/08 , F01D11/00 , F01D11/02 , F02C7/24 , F02C7/28 , F05D2230/53 , F05D2240/15 , F05D2260/231 , Y02T50/675
摘要： An example annular turbomachine seal includes an attachment portion, a first leg radially inward of the attachment portion, and a second leg radially inward of the attachment portion and configured to block flow from directly contacting an attachment associated with a bearing compartment of a turbomachine.
摘要翻译： 示例性的环形涡轮机械密封件包括附接部分，附接部分径向向内的第一支腿和附接部分径向向内的第二支腿，并且构造成阻止与涡轮机的轴承室相关联的附件的直接接触的流动。
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公开(公告)号：US20130323045A1
公开(公告)日：2013-12-05
申请号：US13487721
申请日：2012-06-04
CPC分类号： F16J15/0887 , F01D9/02 , F01D11/005 , F01D11/08 , F02C7/28
摘要： A seal land for a gas turbine engine can include a seal body circumferentially extending about a longitudinal centerline axis. The seal body includes at least one sealing surface that extends in a plane that is transverse to the longitudinal centerline axis.
摘要翻译： 用于燃气涡轮发动机的密封面可以包括围绕纵向中心线轴向周向延伸的密封体。 密封体包括在垂直于纵向中心线轴线的平面中延伸的至少一个密封表面。
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公开(公告)号：US20130309078A1
公开(公告)日：2013-11-21
申请号：US13476062
申请日：2012-05-21
IPC分类号： F01D11/00
CPC分类号： F01D9/04 , F01D5/08 , F01D9/065 , F01D11/005 , F01D11/08 , F01D25/14 , F01D25/24 , F01D25/243 , F01D25/246 , F01D25/26 , F01D25/28 , F02C7/24 , F02C7/28 , F05D2240/14 , F05D2240/15 , F05D2260/231 , Y02T50/675 , Y02T50/676
摘要： A shield system for a gas turbine engine extends between an inner case structure and a vane pack.
摘要翻译： 用于燃气涡轮发动机的屏蔽系统在内壳结构和叶片组之间延伸。
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公开(公告)号：US09133723B2
公开(公告)日：2015-09-15
申请号：US13476062
申请日：2012-05-21
IPC分类号： F01D25/26 , F01D9/04 , F02C7/24 , F02C7/28 , F01D11/00 , F01D11/08 , F01D25/14 , F01D25/24 , F01D25/28
CPC分类号： F01D9/04 , F01D5/08 , F01D9/065 , F01D11/005 , F01D11/08 , F01D25/14 , F01D25/24 , F01D25/243 , F01D25/246 , F01D25/26 , F01D25/28 , F02C7/24 , F02C7/28 , F05D2240/14 , F05D2240/15 , F05D2260/231 , Y02T50/675 , Y02T50/676
摘要： A shield system for a gas turbine engine extends between an inner case structure and a vane pack.
摘要翻译： 用于燃气涡轮发动机的屏蔽系统在内壳结构和叶片组之间延伸。
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公开(公告)号：US20130149159A1
公开(公告)日：2013-06-13
申请号：US13324110
申请日：2011-12-13
申请人： Conway Chuong , Kurt P. Werner , Shelton O. Duelm
发明人： Conway Chuong , Kurt P. Werner , Shelton O. Duelm
IPC分类号： F01D5/32
CPC分类号： F01D25/243 , F01D9/042 , F05D2230/64
摘要： A gas turbine engine includes an engine casing structure and a retention block assembly. The engine casing structure includes a pocket which receives the retention block assembly. The retention block assembly includes a stop block and a pin that retains the stop block within the pocket. The stop block is loose relative to the pin.
摘要翻译： 燃气涡轮发动机包括发动机壳体结构和保持块组件。 发动机壳体结构包括容纳保持块组件的口袋。 保持块组件包括止动块和将止动块保持在口袋内的销。 止动块相对于销松动。
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