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公开(公告)号：US08961132B2
公开(公告)日：2015-02-24
申请号：US13459474
申请日：2012-04-30
申请人： Gabriel L. Suciu , Christopher M. Dye , William K. Ackermann , Stephen P. Muron , Ioannis Alvanos , Brian D. Merry , Arthur M. Salve , James W. Norris
发明人： Gabriel L. Suciu , Christopher M. Dye , William K. Ackermann , Stephen P. Muron , Ioannis Alvanos , Brian D. Merry , Arthur M. Salve , James W. Norris
CPC分类号： F01D11/006 , F01D5/066
摘要： A rotor for a gas turbine engine includes a plurality of blades which extend from a rotor disk and at least one spacer adjacent to the plurality of blades. A flow passage is defined between the rotor disk and the blades and spacer. A plurality of inlets are formed within the spacer to pump air into the flow passage.
摘要翻译： 用于燃气涡轮发动机的转子包括从转子盘和与多个叶片相邻的至少一个间隔件延伸的多个叶片。 流动通道限定在转子盘和叶片和间隔件之间。 在间隔件内形成多个入口以将空气泵送到流动通道中。
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公开(公告)号：US09938831B2
公开(公告)日：2018-04-10
申请号：US13283689
申请日：2011-10-28
申请人： Gabriel L. Suciu , Stephen P. Muron , Ioannis Alvanos , Christopher M. Dye , Brian D. Merry , Arthur M. Salve , James W. Norris
发明人： Gabriel L. Suciu , Stephen P. Muron , Ioannis Alvanos , Christopher M. Dye , Brian D. Merry , Arthur M. Salve , James W. Norris
摘要： A rotor for a gas turbine engine includes a plurality of blades which extend from a rotor disk, each of the plurality of blades extend from the rotor disk at an interface, the interface defined along a spoke.
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公开(公告)号：US20130108445A1
公开(公告)日：2013-05-02
申请号：US13283689
申请日：2011-10-28
申请人： Gabriel L. Suciu , Stephen P. Muron , Ioannis Alvanos , Christopher M. Dye , Brian D. Merry , Arthur M. Salve , James W. Norris
发明人： Gabriel L. Suciu , Stephen P. Muron , Ioannis Alvanos , Christopher M. Dye , Brian D. Merry , Arthur M. Salve , James W. Norris
摘要： A rotor for a gas turbine engine includes a plurality of blades which extend from a rotor disk, each of the plurality of blades extend from the rotor disk at an interface, the interface defined along a spoke.
摘要翻译： 用于燃气涡轮发动机的转子包括从转子盘延伸的多个叶片，所述多个叶片中的每一个叶片在接合处从转子盘延伸，所述界面沿辐条限定。
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公开(公告)号：US20130108413A1
公开(公告)日：2013-05-02
申请号：US13459474
申请日：2012-04-30
申请人： Gabriel L. Suciu , Christopher M. Dye , William K. Ackermann , Stephen P. Muron , loannis Alvanos , Brian D. Merry , Arthur M. Salve , James W. Norris
发明人： Gabriel L. Suciu , Christopher M. Dye , William K. Ackermann , Stephen P. Muron , loannis Alvanos , Brian D. Merry , Arthur M. Salve , James W. Norris
IPC分类号： F01D5/08
CPC分类号： F01D11/006 , F01D5/066
摘要： A rotor for a gas turbine engine includes a plurality of blades which extend from a rotor disk and at least one spacer adjacent to the plurality of blades. A flow passage is defined between the rotor disk and the blades and spacer. A plurality of inlets are formed within the spacer to pump air into the flow passage.
摘要翻译： 用于燃气涡轮发动机的转子包括从转子盘和与多个叶片相邻的至少一个间隔件延伸的多个叶片。 流动通道限定在转子盘和叶片和间隔件之间。 在间隔件内形成多个入口以将空气泵送到流动通道中。
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公开(公告)号：US08784062B2
公开(公告)日：2014-07-22
申请号：US13283710
申请日：2011-10-28
CPC分类号： F01D5/02 , F01D5/022 , F01D5/025 , F01D5/027 , F01D5/066 , F01D5/14 , F01D5/147 , F01D11/006 , F05D2240/20 , F05D2260/15 , Y10T29/49316 , Y10T29/4932
摘要： A spacer for a gas turbine engine includes a rotor ring defined along an axis of rotation, the rotor ring defines a forward circumferential flange which defines a first thickness and an aft circumferential flange which defines a second thickness, the first thickness different than the second thickness. A plurality of core gas path seals which extend from the rotor ring opposite the ramped interface.
摘要翻译： 用于燃气涡轮发动机的间隔件包括沿着旋转轴线限定的转子环，转子环限定限定第一厚度的前周向凸缘和限定第二厚度的后周向凸缘，第一厚度不同于第二厚度 。 多个核心气体路径密封件，其从转子环延伸，与斜坡界面相对。
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公开(公告)号：US20130108466A1
公开(公告)日：2013-05-02
申请号：US13283710
申请日：2011-10-28
CPC分类号： F01D5/02 , F01D5/022 , F01D5/025 , F01D5/027 , F01D5/066 , F01D5/14 , F01D5/147 , F01D11/006 , F05D2240/20 , F05D2260/15 , Y10T29/49316 , Y10T29/4932
摘要： A spacer for a gas turbine engine includes a rotor ring defined along an axis of rotation, the rotor ring defines a forward circumferential flange which defines a first thickness and an aft circumferential flange which defines a second thickness, the first thickness different than the second thickness. A plurality of core gas path seals which extend from the rotor ring opposite the ramped interface.
摘要翻译： 用于燃气涡轮发动机的间隔件包括沿着旋转轴线限定的转子环，转子环限定限定第一厚度的前周向凸缘和限定第二厚度的后周向凸缘，第一厚度不同于第二厚度 。 多个核心气体路径密封件，其从转子环延伸，与斜坡界面相对。
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公开(公告)号：US08944762B2
公开(公告)日：2015-02-03
申请号：US13283733
申请日：2011-10-28
CPC分类号： F01D11/005 , F01D5/066 , F05D2240/55
摘要： A spacer for a gas turbine engine includes a rotor ring defined along an axis of rotation and a plurality of core gas path seals which extend from the rotor ring, each of the plurality of core gas path seals extend from the rotor ring at an interface, the interface defined along a spoke.
摘要翻译： 用于燃气涡轮发动机的间隔件包括沿着旋转轴线限定的转子环和从转子环延伸的多个芯气体通道密封件，多个芯气体通道密封件中的每一个在转子环的界面处延伸， 沿着辐条定义的界面。
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公开(公告)号：US20130108468A1
公开(公告)日：2013-05-02
申请号：US13283733
申请日：2011-10-28
IPC分类号： F01D5/08
CPC分类号： F01D11/005 , F01D5/066 , F05D2240/55
摘要： A spacer for a gas turbine engine includes a rotor ring defined along an axis of rotation and a plurality of core gas path seals which extend from the rotor ring, each of the plurality of core gas path seals extend from the rotor ring at an interface, the interface defined along a spoke.
摘要翻译： 用于燃气涡轮发动机的间隔件包括沿着旋转轴线限定的转子环和从转子环延伸的多个芯气体通道密封件，多个芯气体通道密封件中的每一个在转子环的界面处延伸， 沿着辐条定义的界面。
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公开(公告)号：US20130283820A1
公开(公告)日：2013-10-31
申请号：US13459676
申请日：2012-04-30
申请人： Stephen P. Muron , Larry Foster
发明人： Stephen P. Muron , Larry Foster
CPC分类号： F01D5/282 , F01D5/147 , F02K3/06 , F04D29/023 , F04D29/324 , F04D29/388 , F05D2220/36 , F05D2300/6012 , F05D2300/612 , F05D2300/614
摘要： A fan blade having a body with a dovetail and an airfoil extending radially outwardly. The airfoil includes a pair of skins spaced to form an internal core, which define a pressure side and a suction side, and extending from a radially inner end to a radially outer tip. The core receives a plurality of braided tubes, with the tubes extending with at least a component in a radially outward direction. A fan and an engine are also described.
摘要翻译： 一种风扇叶片，其具有燕尾形的主体和径向向外延伸的翼型。 翼型件包括一对间隔开以形成内部芯的外皮，其限定了压力侧和吸力侧，并且从径向内端延伸到径向外端。 芯部容纳多个编织管，管子至少沿径向向外的方向延伸。 还描述了风扇和发动机。
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公开(公告)号：US09416668B2
公开(公告)日：2016-08-16
申请号：US13459676
申请日：2012-04-30
申请人： Stephen P. Muron , Larry Foster
发明人： Stephen P. Muron , Larry Foster
CPC分类号： F01D5/282 , F01D5/147 , F02K3/06 , F04D29/023 , F04D29/324 , F04D29/388 , F05D2220/36 , F05D2300/6012 , F05D2300/612 , F05D2300/614
摘要： A fan blade having a body with a dovetail and an airfoil extending radially outwardly. The airfoil includes a pair of skins spaced to form an internal core, which define a pressure side and a suction side, and extending from a radially inner end to a radially outer tip. The core receives a plurality of braided tubes, with the tubes extending with at least a component in a radially outward direction. A fan and an engine are also described.
摘要翻译： 一种风扇叶片，其具有燕尾形的主体和径向向外延伸的翼型。 翼型件包括一对间隔开以形成内部芯的外皮，其限定了压力侧和吸力侧，并且从径向内端延伸到径向外端。 芯部容纳多个编织管，管子至少沿径向向外的方向延伸。 还描述了风扇和发动机。
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