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公开(公告)号：US09097142B2
公开(公告)日：2015-08-04
申请号：US13488562
申请日：2012-06-05
申请人： David Ronald Adair , Pete Simpson
发明人： David Ronald Adair , Pete Simpson
IPC分类号： F01D25/28
CPC分类号： F01D25/28 , F05D2230/64 , Y10T29/49778
摘要： A first structural static component having an outer diameter is aligned with a second structural static component having an inner diameter to the centerline of a gas turbine engine rotating assembly. The first static component is centered inside the second static component leaving a gap between the outer diameter of the first component and the inner diameter of the second component to permit them to mate at operating temperatures. Tabs and slots are placed on the periphery of the static components to align the static components with the centerline at build temperature.
摘要翻译： 具有外径的第一结构静态部件与具有与燃气涡轮发动机旋转组件的中心线的内径的第二结构静态部件对准。 第一静态部件位于第二静态部件的中心，在第一部件的外径和第二部件的内径之间留有间隙，以允许它们在操作温度下配合。 标签和插槽位于静态组件的外围，以将静态组件与构建温度下的中心线对齐。
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公开(公告)号：US20130323037A1
公开(公告)日：2013-12-05
申请号：US13488562
申请日：2012-06-05
申请人： David Ronald Adair , Pete Simpson
发明人： David Ronald Adair , Pete Simpson
CPC分类号： F01D25/28 , F05D2230/64 , Y10T29/49778
摘要： A first structural static component having an outer diameter is aligned with a second structural static component having an inner diameter to the centerline of a gas turbine engine rotating assembly. The first static component is centered inside the second static component leaving a gap between the outer diameter of the first component and the inner diameter of the second component to permit them to mate at operating temperatures. Tabs and slots are placed on the periphery of the static components to align the static components with the centerline at build temperature.
摘要翻译： 具有外径的第一结构静态部件与具有与燃气涡轮发动机旋转组件的中心线的内径的第二结构静态部件对准。 第一静态部件位于第二静态部件的中心，在第一部件的外径和第二部件的内径之间留有间隙，以允许它们在操作温度下配合。 标签和插槽位于静态组件的外围，以将静态组件与构建温度下的中心线对齐。
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公开(公告)号：US20120242045A1
公开(公告)日：2012-09-27
申请号：US13463900
申请日：2012-05-04
申请人： David Ronald Adair , Walter Ernest Ainslie , Gordon F. Jewess , Anthony C. Jones , Eric J. Alexander
发明人： David Ronald Adair , Walter Ernest Ainslie , Gordon F. Jewess , Anthony C. Jones , Eric J. Alexander
IPC分类号： F02C7/28
CPC分类号： F01D9/023 , F01D11/003 , F01D11/005 , F16J15/0887 , F23R3/50 , F23R2900/00012
摘要： An example method of sealing an interface within a gas turbine engine includes holding a sealing ring arrangement relative to a turbine nozzle using a flange extending from a combustor liner. The method further includes urging the sealing ring arrangement toward a sealed relationship with the turbine nozzle.
摘要翻译： 密封燃气涡轮发动机内的界面的示例性方法包括使用从燃烧器衬套延伸的凸缘相对于涡轮喷嘴保持密封环装置。 该方法还包括将密封环装置推向与涡轮喷嘴的密封关系。
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公开(公告)号：US20110283491A1
公开(公告)日：2011-11-24
申请号：US12783678
申请日：2010-05-20
CPC分类号： F16B21/186 , Y10T24/44641 , Y10T29/49959
摘要： A retention assembly includes a retainer that attaches to a clip that snaps onto a shaft. The retainer includes a back plate with an opening for the shaft and at least one fastener for securement of the retainer to the clip.
摘要翻译： 保持组件包括附接到卡扣到轴上的夹子的保持器。 保持器包括具有用于轴的开口的后板和用于将保持器固定到夹子的至少一个紧固件。
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公开(公告)号：US09297266B2
公开(公告)日：2016-03-29
申请号：US13463900
申请日：2012-05-04
申请人： David Ronald Adair , Walter Ernest Ainslie , Gordon F. Jewess , Anthony C. Jones , Eric J. Alexander
发明人： David Ronald Adair , Walter Ernest Ainslie , Gordon F. Jewess , Anthony C. Jones , Eric J. Alexander
CPC分类号： F01D9/023 , F01D11/003 , F01D11/005 , F16J15/0887 , F23R3/50 , F23R2900/00012
摘要： An example method of sealing an interface within a gas turbine engine includes holding a sealing ring arrangement relative to a turbine nozzle using a flange extending from a combustor liner. The method further includes urging the sealing ring arrangement toward a sealed relationship with the turbine nozzle.
摘要翻译： 密封燃气涡轮发动机内的界面的示例性方法包括使用从燃烧器衬套延伸的凸缘相对于涡轮喷嘴保持密封环装置。 该方法还包括将密封环装置推向与涡轮喷嘴的密封关系。
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公开(公告)号：US08820045B2
公开(公告)日：2014-09-02
申请号：US12847359
申请日：2010-07-30
IPC分类号： F02G3/00
CPC分类号： F01D11/005 , F02C7/25 , F02C7/28 , F05D2220/50 , Y02T50/672
摘要： A drain assembly for an auxiliary power unit having a hot zone formed by a combustor case comprises a fire enclosure, a drain fitting, a discharge port and a piston seal. The fire enclosure encapsulates the hot zone of the combustor case. The drain fitting connects to the fire enclosure. The discharge port extends from the combustor case into the drain fitting. The piston seal is positioned between the drain fitting and the discharge port.
摘要翻译： 用于具有由燃烧器壳形成的热区的辅助动力单元的排水组件包括防火罩，排水配件，排放口和活塞密封件。 防火罩封装燃烧器外壳的热区。 排水配件连接到防火罩。 排放口从燃烧器壳体延伸到排水配件中。 活塞密封件位于排水接头和排放口之间。
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公开(公告)号：US09562569B2
公开(公告)日：2017-02-07
申请号：US13450612
申请日：2012-04-19
CPC分类号： F16D1/033 , F16B2200/50 , F16D1/076 , Y10T29/49947
摘要： A method of aligning flanges on two components to align and transfer torque from one component to the other uses a plurality of scallop regions on the periphery of a flange on one component; and a plurality of raised regions on the periphery of a flange on the other component, the raised regions being sized and shaped to engage the scallop regions on the flange when axially aligned to transfer torque there between.
摘要翻译： 在两个部件上对准凸缘对准和传递扭矩的方法使用一个部件上的凸缘的周边上的多个扇形区域; 以及在另一部件的凸缘的周边上的多个凸起区域，所述凸起区域的尺寸和形状适于与轴向对准的凸缘上的扇形区域接合以在其间传递扭矩。
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公开(公告)号：US20110072830A1
公开(公告)日：2011-03-31
申请号：US12568615
申请日：2009-09-28
申请人： David Ronald Adair , Walter Ernest Ainslie , Gordon F. Jewess , Anthony C. Jones , Eric J. Alexander
发明人： David Ronald Adair , Walter Ernest Ainslie , Gordon F. Jewess , Anthony C. Jones , Eric J. Alexander
CPC分类号： F01D9/023 , F01D11/003 , F01D11/005 , F16J15/0887 , F23R3/50 , F23R2900/00012
摘要： A gas turbine engine sealing arrangement which includes a combustor liner establishing a combustion area and a turbine nozzle configured to receive a portion of a combustor liner. A sealing ring arrangement is configured to seal with the turbine nozzle to control fluid flow from the combustion area and reduce leakage.
摘要翻译： 一种燃气涡轮发动机密封装置，其包括建立燃烧区域的燃烧器衬套和构造成容纳燃烧器衬套的一部分的涡轮喷嘴。 密封环装置构造成与涡轮喷嘴密封以控制来自燃烧区域的流体流动并减少泄漏。
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公开(公告)号：US20130276454A1
公开(公告)日：2013-10-24
申请号：US13450612
申请日：2012-04-19
CPC分类号： F16D1/033 , F16B2200/50 , F16D1/076 , Y10T29/49947
摘要： A method of aligning flanges on two components to align and transfer torque from one component to the other uses a plurality of scallop regions on the periphery of a flange on one component; and a plurality of raised regions on the periphery of a flange on the other component, the raised regions being sized and shaped to engage the scallop regions on the flange when axially aligned to transfer torque there between
摘要翻译： 在两个部件上对准凸缘对准和传递扭矩的方法使用一个部件上的凸缘的周边上的多个扇形区域; 以及在另一部件的凸缘的周边上的多个凸起区域，所述凸起区域的尺寸和形状被设计成与轴向对准的凸缘区域接合，以在其间传递扭矩
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公开(公告)号：US08215115B2
公开(公告)日：2012-07-10
申请号：US12568615
申请日：2009-09-28
申请人： David Ronald Adair , Walter Ernest Ainslie , Gordon F. Jewess , Anthony C. Jones , Eric J. Alexander
发明人： David Ronald Adair , Walter Ernest Ainslie , Gordon F. Jewess , Anthony C. Jones , Eric J. Alexander
IPC分类号： F02C1/00
CPC分类号： F01D9/023 , F01D11/003 , F01D11/005 , F16J15/0887 , F23R3/50 , F23R2900/00012
摘要： A gas turbine engine sealing arrangement which includes a combustor liner establishing a combustion area and a turbine nozzle configured to receive a portion of a combustor liner. A sealing ring arrangement is configured to seal with the turbine nozzle to control fluid flow from the combustion area and reduce leakage.
摘要翻译： 一种燃气涡轮发动机密封装置，其包括建立燃烧区域的燃烧器衬套和构造成容纳燃烧器衬套的一部分的涡轮喷嘴。 密封环装置构造成与涡轮喷嘴密封以控制来自燃烧区域的流体流动并减少泄漏。
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