-
公开(公告)号：US10330111B2
公开(公告)日：2019-06-25
申请号：US15126371
申请日：2015-03-30
发明人： Scott C. Billings , Michael K. Gottschalk , William D. Owen , Edward J. Gallagher , Darryl Whitlow , Sue-Li Chuang , Mani Sadeghi
摘要： In one exemplary embodiment, an airfoil for a turbine engine includes an airfoil that has pressure and suction sides and extends in a radial direction from a 0% span position at an inner flow path location to a 100% span position at an airfoil tip. The airfoil has a curve that corresponds to a relationship between a leading edge dihedral and a span position. The leading edge dihedral has a portion of the curve with a change in dihedral in the range of 90% to 100% span position of greater than 10°. A positive dihedral corresponds to suction side-leaning. A negative dihedral corresponds to pressure side-leaning.
-
公开(公告)号：US10273816B2
公开(公告)日：2019-04-30
申请号：US14170985
申请日：2014-02-03
发明人： Jay T. Abraham , Ethan C. Drew , Scott C. Billings , Michael A. Weisse , James O. Hansen , Venkatarama K. Seetharaman
IPC分类号： F01D5/30
摘要： A fan blade of a gas turbine engine includes an airfoil, a root received in a slot of a hub, and a wear pad covering at least a portion of the root and made of an integrally bonded woven composite laminate.
-
公开(公告)号：US20160230572A1
公开(公告)日：2016-08-11
申请号：US14617614
申请日：2015-02-09
摘要： A dovetail root of a fan blade configured for operation within the fan assembly of a gas turbine engine. The dovetail root is imparted with a compressive residual stress layer along the outer faces of the dovetail root preventing crack formation within the dovetail root when the gas turbine engine is in operation. To further protect and structurally enhance the dovetail root, a wear covering is disposed on the dovetail root. The wear covering may consist of a composite laminate layer that is bonded to the metallic core of the dovetail root providing additional cracking protection of the dovetail root when the gas turbine engine is in operation.
摘要翻译： 风扇叶片的燕尾根被配置为在燃气涡轮发动机的风扇组件内操作。 燕尾根沿着燕尾根的外表面施加压缩残余应力层，防止在燃气轮机发动机运行时在燕尾根内形成裂纹。 为了进一步保护和结构地增强燕尾根，在燕尾根上设置磨损覆盖物。 磨损覆盖物可以由复合层压层组成，该复合层压层结合到燕尾榫根部的金属芯上，当燃气涡轮发动机运行时，它可以提供燕尾根的附加开裂保护。
-
公开(公告)号：US10570755B2
公开(公告)日：2020-02-25
申请号：US14617614
申请日：2015-02-09
摘要： A dovetail root of a fan blade configured for operation within the fan assembly of a gas turbine engine. The dovetail root is imparted with a compressive residual stress layer along the outer faces of the dovetail root preventing crack formation within the dovetail root when the gas turbine engine is in operation. To further protect and structurally enhance the dovetail root, a wear covering is disposed on the dovetail root. The wear covering may consist of a composite laminate layer that is bonded to the metallic core of the dovetail root providing additional cracking protection of the dovetail root when the gas turbine engine is in operation.
-
公开(公告)号：US09650902B2
公开(公告)日：2017-05-16
申请号：US13739218
申请日：2013-01-11
CPC分类号： F01D5/3007 , F01D5/3092 , F01D11/008 , F05D2220/36 , Y02T50/673
摘要： A fan section for a gas turbine engine includes a fan hub having a slot. A platform is supported by the fan hub. A fan blade has a root that is received in the slot. A wear pad is provided between the fan hub and the root and includes a flap integral with the wear pad to provide a seal relative to the platform. A fan blade for a gas turbine engine includes an airfoil extending from a root. A wear pad is secured to the root and has a free end providing a flap canted toward the root.
-
公开(公告)号：US20150110636A1
公开(公告)日：2015-04-23
申请号：US14170985
申请日：2014-02-03
发明人： Jay T. Abraham , Ethan C. Drew , Scott C. Billings , Michael A. Weisse , James O. Hansen , Venkatarama K. Seetharaman
CPC分类号： F01D5/3092 , F05D2220/36 , F05D2300/614 , F05D2300/701 , Y02T50/671
摘要： A fan blade of a gas turbine engine includes an airfoil, a root received in a slot of a hub, and a wear pad covering at least a portion of the root and made of an integrally bonded woven composite laminate.
摘要翻译： 燃气涡轮发动机的风扇叶片包括翼型件，容纳在轮毂的槽中的根部和覆盖根部的至少一部分并由整体结合的织造复合层压板制成的耐磨垫片。
-
公开(公告)号：US20170122336A1
公开(公告)日：2017-05-04
申请号：US15126371
申请日：2015-03-30
发明人： Scott C. Billings , Michael K. Gottschalk , William D. Owen , Edward J. Gallagher , Darryl Whitlow , Sue-Li Chuang , Mani Sadeghi
CPC分类号： F04D29/384 , F01D5/141 , F02C3/04 , F02C7/36 , F02K3/06 , F05D2220/36 , F05D2240/35 , F05D2250/70 , Y02T50/672 , Y02T50/673
摘要： In one exemplary embodiment, an airfoil for a turbine engine includes an airfoil that has pressure and suction sides and extends in a radial direction from a 0% span position at an inner flow path location to a 100% span position at an airfoil tip. The airfoil has a curve that corresponds to a relationship between a leading edge dihedral and a span position. The leading edge dihedral has a portion of the curve with a change in dihedral in the range of 90% to 100% span position of greater than 10°. A positive dihedral corresponds to suction side-leaning. A negative dihedral corresponds to pressure side-leaning.
-
公开(公告)号：US20140286781A1
公开(公告)日：2014-09-25
申请号：US13739218
申请日：2013-01-11
IPC分类号： F01D5/30
CPC分类号： F01D5/3007 , F01D5/3092 , F01D11/008 , F05D2220/36 , Y02T50/673
摘要： A fan section for a gas turbine engine includes a fan hub having a slot. A platform is supported by the fan hub. A fan blade has a root that is received in the slot. A wear pad is provided between the fan hub and the root and includes a flap integral with the wear pad to provide a seal relative to the platform. A fan blade for a gas turbine engine includes an airfoil extending from a root. A wear pad is secured to the root and has a free end providing a flap canted toward the root.
摘要翻译： 用于燃气涡轮发动机的风扇部分包括具有槽的风扇毂。 风扇集线器支持平台。 风扇叶片具有接收在槽中的根部。 在风扇轮毂和根部之间提供耐磨垫，并且包括与耐磨垫一体的翼片，以提供相对于平台的密封。 用于燃气涡轮发动机的风扇叶片包括从根部延伸的翼型件。 磨损垫固定到根部，并具有自由端，提供朝向根部倾斜的翼片。
-
-
-
-
-
-
-
搜索结果
8 条记录 (耗时 0.014 秒)
