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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：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：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：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：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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公开(公告)号：US09310072B2
公开(公告)日：2016-04-12
申请号：US13542808
申请日：2012-07-06
CPC分类号： F23C5/08 , F23R3/28 , F23R2900/00013 , F23R2900/00014
摘要： A fuel nozzle arrangement includes an annular combustor having four quadrants. Fuel injectors are located in the four quadrants and each fuel injector has either a first or second type nozzle attached to it. The first and second type fuel nozzles are located in an array so that at least two of one nozzle type are located together to allow for non-uniform injector spacing with uniform downstream temperatures.
摘要翻译： 燃料喷嘴装置包括具有四个象限的环形燃烧器。 燃料喷射器位于四个象限中，并且每个燃料喷射器具有连接到其上的第一或第二喷嘴。 第一和第二类型燃料喷嘴位于阵列中，使得一个喷嘴类型中的至少两个位于一起以允许具有均匀的下游温度的不均匀的喷射器间隔。
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公开(公告)号：US20130227959A1
公开(公告)日：2013-09-05
申请号：US13410752
申请日：2012-03-02
CPC分类号： F02C7/26 , F02C9/26 , F05D2220/50 , Y02T50/671
摘要： A method for controlling fuel flow to a gas turbine engine during starting includes monitoring acceleration of the gas turbine engine to determine actual acceleration value, and calculating a fuel flow rate for a setpoint acceleration using the actual acceleration value as a factor. The method further includes commanding the calculated fuel flow for the setpoint acceleration to the gas turbine engine.
摘要翻译： 用于控制在启动期间燃气涡轮发动机的燃料流量的方法包括监测燃气涡轮发动机的加速度以确定实际加速度值，并且使用实际加速度值作为因素来计算用于设定点加速度的燃料流量。 该方法还包括将计算出的燃料流量命令为燃气涡轮发动机的设定点加速度。
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公开(公告)号：US20140007579A1
公开(公告)日：2014-01-09
申请号：US13542808
申请日：2012-07-06
CPC分类号： F23C5/08 , F23R3/28 , F23R2900/00013 , F23R2900/00014
摘要： A fuel nozzle arrangement includes an annular combustor having four quadrants. Fuel injectors are located in the four quadrants and each fuel injector has either a first or second type nozzle attached to it. The first and second type fuel nozzles are located in an array so that at least two of one nozzle type are located together to allow for non-uniform injector spacing with uniform downstream temperatures.
摘要翻译： 燃料喷嘴装置包括具有四个象限的环形燃烧器。 燃料喷射器位于四个象限中，并且每个燃料喷射器具有连接到其上的第一或第二喷嘴。 第一和第二类型燃料喷嘴位于阵列中，使得一个喷嘴类型中的至少两个位于一起以允许具有均匀的下游温度的不均匀的喷射器间隔。
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