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1. 发明授权

US06739050B2 Methods for retaining gas turbine engine nozzle basesheets 有权
公开(公告)号：US06739050B2
公开(公告)日：2004-05-25
申请号：US10684275
申请日：2003-10-13
申请人： Darrell Senile , Bernard J. Renggli
发明人： Darrell Senile , Bernard J. Renggli
IPC分类号： B21D5300
CPC分类号： F02K1/12 , F02K1/1223 , Y10T29/49346
摘要： A method for assembling a flap and seal system for a gas turbine engine exhaust nozzle including a plurality of backbone assemblies facilitates attaching a basesheet to a backbone. The method includes attaching an attachment system including at least one strap to a basesheet, and coupling the basesheet to a backbone using the attachment system strap.

2. 发明授权

US06745570B2 Methods and apparatus for sealing gas turbine engine nozzles using a flap system 有权
标题翻译：使用翼片系统密封燃气涡轮发动机喷嘴的方法和装置
公开(公告)号：US06745570B2
公开(公告)日：2004-06-08
申请号：US10061618
申请日：2002-02-01
申请人： Bernard J. Renggli , Darrell Senile
发明人： Bernard J. Renggli , Darrell Senile
IPC分类号： F02K100
CPC分类号： F02K1/12 , F05D2230/60 , Y10S29/904 , Y10T29/49346 , Y10T29/494
摘要： A method for assembling a flap system for a gas turbine engine exhaust nozzle including a plurality of backbone assemblies facilitates extending a useful life of the exhaust nozzle. The method includes providing a flap basesheet having a width defined between a pair of side edges that are coupled together by a leading edge and a trailing edge, and including at least one stiffener that extends between the basesheet side edges and includes an intermediate portion that has a width that is smaller than that of the basesheet and is at least one of bonded to and formed integrally with the basesheet, and coupling the basesheet to the gas turbine engine with a backbone assembly.
摘要翻译：一种用于组装用于包括多个主干组件的燃气涡轮发动机排气喷嘴的翼片系统的方法有助于延长排气喷嘴的使用寿命。该方法包括提供一个翼片基片，其宽度限定在一对侧边缘之间，该对侧边缘通过前缘和后缘连接在一起，并且包括至少一个在基片侧边缘之间延伸的加强件，并包括中间部分，其宽度小于基片的宽度，并且是与基片结合并与基片一体形成的至少一个，并且将基片与骨架组件连接到燃气涡轮发动机。

3. 发明授权

US06658854B2 Methods and apparatus for retaining gas turbine engine nozzle basesheets 有权
公开(公告)号：US06658854B2
公开(公告)日：2003-12-09
申请号：US10061629
申请日：2002-02-01
申请人： Darrell Senile , Bernard J. Renggli
发明人： Darrell Senile , Bernard J. Renggli
IPC分类号： F02K112
CPC分类号： F02K1/12 , F02K1/1223 , Y10T29/49346
摘要： A method for assembling a flap and seal system for a gas turbine engine exhaust nozzle including a plurality of backbone assemblies facilitates attaching a basesheet to a backbone. The method includes attaching an attachment system including at least one strap to a basesheet, and coupling the basesheet to a backbone using the attachment system strap.

4. 发明申请

US20050235628A1 EJECTOR COOLED NOZZLE 有权
标题翻译：喷嘴冷却喷嘴
公开(公告)号：US20050235628A1
公开(公告)日：2005-10-27
申请号：US10828643
申请日：2004-04-21
申请人： Darrell Senile
发明人： Darrell Senile
IPC分类号： B64D33/04 , F02K1/00 , F02K1/12 , F02K1/36
CPC分类号： F02K1/1292 , B64D33/04 , F02K1/1223 , F02K1/36 , F05D2260/20 , F05D2260/601 , Y02T50/675
摘要： A gas turbine engine exhaust nozzle includes a divergent section located aft of a convergent section and a throat therebetween. An exterior fairing is spaced radially outwardly of the divergent section. An ejector cooling air flowpath leads from an ejector cooling air inlet in an aft portion of the fairing to a cooling air ejector in the nozzle. An annular nozzle plenum may be disposed between the divergent section of the nozzle and the external fairing and be part of the ejector cooling air flowpath between the ejector cooling air inlet and the ejector. A plurality of divergent flaps and divergent seals in the divergent section may employ cooling air passages, such as slots, to serve as the ejector. The fairing may include a plurality of circumferentially adjacent exterior flaps and exterior seals and employ truncated ends of or apertures in the exterior seals as the ejector cooling air inlet.
摘要翻译：燃气涡轮发动机排气喷嘴包括位于其间的收敛部分和喉部后方的发散部分。外部整流罩在发散部分的径向外侧间隔开。喷射器冷却空气流路从整流罩的后部的喷射器冷却空气入口引导到喷嘴中的冷却空气喷射器。环形喷嘴增压室可以设置在喷嘴的发散部分和外部整流罩之间，并且是喷射器冷却空气入口和喷射器之间的喷射器冷却空气流路的一部分。发散部分中的多个发散的翼片和发散的密封件可以使用诸如槽的冷却空气通道来用作喷射器。整流罩可以包括多个周向相邻的外部翼片和外部密封件，并且在外部密封件中使用截顶端或孔口作为喷射器冷却空气入口。

5. 发明申请

US20050091983A1 Methods and apparatus to reduce turbine engine nozzle basesheet stresses 有权
标题翻译：减少涡轮发动机喷嘴底板应力的方法和装置
公开(公告)号：US20050091983A1
公开(公告)日：2005-05-05
申请号：US10696319
申请日：2003-10-29
申请人： Darrell Senile , Christina Burke , Bernard Renggli , John Amneus
发明人： Darrell Senile , Christina Burke , Bernard Renggli , John Amneus
IPC分类号： F02K1/12 , F02K1/82
CPC分类号： F02K1/1223 , F02K1/82 , F05D2300/21 , F05D2300/603
摘要： A method facilitates assembling a flap system for a gas turbine engine exhaust nozzle including at least one backbone assembly. The method comprises providing a basesheet including a pair of circumferentially-spaced sides coupled together by an upstream side and a downstream side, forming at least one relief cut in the basesheet that extends at least partially across the basesheet from at least one of the circumferentially-spaced sides, and coupling the basesheet to the backbone assembly.
摘要翻译：一种方法便于组装用于包括至少一个主干组件的燃气涡轮发动机排气喷嘴的翼片系统。该方法包括提供一个底片，该底片包括一对周向间隔开的侧面，该侧面由上游侧和下游侧连接在一起，形成至少一个在底片中的一个凸出切口，其至少部分地穿过基片从至少一个圆周方向延伸，并且将基片连接到主体组件。

6. 发明授权

US08642170B2 Low thermal and radiation conductivity coating 有权
标题翻译：低热辐射导电涂层
公开(公告)号：US08642170B2
公开(公告)日：2014-02-04
申请号：US11967857
申请日：2007-12-31
申请人： Daniel P. Ivkovich , William Randolph Stowell , Darrell Senile , Thomas W. Rentz , John F. Ackerman
发明人： Daniel P. Ivkovich , William Randolph Stowell , Darrell Senile , Thomas W. Rentz , John F. Ackerman
IPC分类号： B32B5/16
CPC分类号： C03C14/004 , C23C28/042 , C23C28/048 , F02K1/825 , F05D2230/313 , F05D2230/90 , F05D2300/50211 , F05D2300/50212 , F05D2300/504 , F05D2300/603 , Y02T50/67 , Y10T428/25 , Y10T428/31612 , Y10T428/31663
摘要： A coating system that includes a plurality of portions, each portion comprising one or more layers. The coating system includes an outer portion, which is an infrared radiation (IR) interaction portion, that dissipates incident (IR). Underlying this outer portion is a performance portion. The performance portion comprises at least one layer that includes microspheres. Between the substrate and performance portion is a compliance portion. The compliance portion comprises at least one layer of high temperature material that has a coefficient of thermal expansion (CTE) intermediate the performance layer and the substrate. The compliance portion thus reduces any high temperature thermal mismatch between the substrate and the performance portion.
摘要翻译：一种涂覆系统，其包括多个部分，每个部分包括一个或多个层。涂层系统包括外部部分，其是消散入射（IR）的红外辐射（IR）相互作用部分。在该外部部分的下面是性能部分。性能部分包括至少一个包含微球的层。在基材和性能部分之间是柔顺部分。柔性部分包括至少一层高温材料层，其具有在性能层和衬底之间的热膨胀系数（CTE）。柔性部分因此降低了衬底和性能部分之间的任何高温热失配。

7. 发明申请

US20090169898A1 LOW THERMAL AND RADIATION CONDUCTIVITY COATING 有权
标题翻译：低热和辐射电导率涂层
公开(公告)号：US20090169898A1
公开(公告)日：2009-07-02
申请号：US11967857
申请日：2007-12-31
申请人： Daniel P. Ivkovich , William Randolph Stowell , Darrell Senile , Thomas W. Rentz , John F. Ackerman
发明人： Daniel P. Ivkovich , William Randolph Stowell , Darrell Senile , Thomas W. Rentz , John F. Ackerman
IPC分类号： B32B17/06
CPC分类号： C03C14/004 , C23C28/042 , C23C28/048 , F02K1/825 , F05D2230/313 , F05D2230/90 , F05D2300/50211 , F05D2300/50212 , F05D2300/504 , F05D2300/603 , Y02T50/67 , Y10T428/25 , Y10T428/31612 , Y10T428/31663
摘要： A coating system that includes a plurality of portions, each portion comprising one or more layers. The coating system includes an outer portion, which is an infrared radiation (IR) interaction portion, that dissipates incident (IR). Underlying this outer portion is a performance portion. The performance portion comprises at least one layer that includes microspheres. Between the substrate and performance portion is a compliance portion. The compliance portion comprises at least one layer of high temperature material that has a coefficient of thermal expansion (CTE) intermediate the performance layer and the substrate. The compliance portion thus reduces any high temperature thermal mismatch between the substrate and the performance portion.
摘要翻译：一种涂覆系统，其包括多个部分，每个部分包括一个或多个层。涂层系统包括外部部分，其是消散入射（IR）的红外辐射（IR）相互作用部分。在该外部部分的下面是性能部分。性能部分包括至少一个包含微球的层。在基材和性能部分之间是柔顺部分。柔性部分包括至少一层高温材料层，其具有在性能层和衬底之间的热膨胀系数（CTE）。柔性部分因此降低了衬底和性能部分之间的任何高温热失配。

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