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1. 发明申请

US20100126018A1 METHOD OF MANUFACTURING A VANE WITH REDUCED STRESS 审中-公开
标题翻译：制造具有减少应力的VANE的方法
公开(公告)号：US20100126018A1
公开(公告)日：2010-05-27
申请号：US12277807
申请日：2008-11-25
申请人： Mitchell Jay Headley , Stephen Joseph Gruber
发明人： Mitchell Jay Headley , Stephen Joseph Gruber
IPC分类号： B23P11/00
CPC分类号： F01D9/044 , B23K1/0018 , B23K26/389 , B23K2101/001 , F05D2230/12 , F05D2230/237 , F05D2260/941 , Y10T29/49323
摘要： A method of manufacturing an airfoil assembly is described, the method comprising the steps of supplying an airfoil and a band, creating a support aperture in the band capable of receiving a portion of the airfoil, creating a slot in the band for reducing stress in the airfoil, and bonding the airfoil with the band.
摘要翻译：描述了一种制造翼型组件的方法，所述方法包括以下步骤：提供翼型和带状物，在所述带中产生能够接收所述翼型的一部分的支撑孔，在所述带中形成用于减小所述翼型件中的应力的槽翼型，并将翼型与带结合。

2. 发明授权

US07360990B2 Methods and apparatus for assembling gas turbine engines 有权
标题翻译：燃气轮机发动机组装方法及装置
公开(公告)号：US07360990B2
公开(公告)日：2008-04-22
申请号：US10964303
申请日：2004-10-13
申请人： Roger Owen Barbe , Mitchell Jay Headley , Scott Howard Pelletier , David N. Rosenow
发明人： Roger Owen Barbe , Mitchell Jay Headley , Scott Howard Pelletier , David N. Rosenow
IPC分类号： F04D29/56
CPC分类号： F01D17/162 , Y10S384/906
摘要： A method enables a variable vane assembly for a gas turbine engine including a casing and an inner shroud to be assembled. The method comprises providing at least one variable vane including a radially inner spindle that has a substantially circular cross-sectional shape, and coupling the variable vane radially between the casing and the inner shroud such that the radially inner spindle is rotatably coupled within an opening extending through the inner shroud, wherein the opening has a non-circular cross-sectional profile.
摘要翻译：一种方法使得能够组装用于包括壳体和内护罩的燃气涡轮发动机的可变叶片组件。该方法包括提供包括径向内心轴的至少一个可变叶片，其具有基本上圆形的横截面形状，并且将可变叶片径向地联接在壳体和内护罩之间，使得径向内心轴可旋转地联接在开口延伸通过内护罩，其中开口具有非圆形横截面轮廓。

3. 发明授权

US06821084B2 Torque tube bearing assembly 失效
标题翻译：扭矩管轴承总成
公开(公告)号：US06821084B2
公开(公告)日：2004-11-23
申请号：US10316778
申请日：2002-12-11
申请人： Julius Bathori , Sang Yeng Park , Mitchell Jay Headley
发明人： Julius Bathori , Sang Yeng Park , Mitchell Jay Headley
IPC分类号： F01D1108
CPC分类号： F16C23/045 , F01D25/16 , F04D29/563 , F16C35/02 , F16C2360/23
摘要： A bearing assembly for use in a gas turbine engine to rotatably mount a torque tube in an access hole extending through a fan duct. The torque tube connects a variable stator vane bell crank positioned inside the fan duct to an actuator positioned outside the fan duct. The bearing assembly includes a bearing having a spherical external engagement surface and a housing having a flange and an annular interior surface having an inner edge and an outer edge. The interior surface is sized and shaped for rotatably receiving the spherical external engagement surface of the bearing so the spherical engagement surface and the annular interior surface make contact along an annular contact area centered on a contact plane lying between the inner and outer edges. The contact plane is tilted with respect to the flange at an angle greater than five degrees.
摘要翻译：一种用于燃气涡轮发动机的轴承组件，用于将扭矩管可旋转地安装在延伸穿过风扇导管的进入孔中。扭矩管将位于风扇管道内部的可变定子叶片钟形曲柄连接到位于风扇导管外部的致动器。轴承组件包括具有球形外接合表面的轴承和具有凸缘的壳体和具有内边缘和外边缘的环形内表面。内表面的尺寸和形状适于可旋转地接收轴承的球形外部接合表面，使得球形接合表面和环形内表面沿着位于内边缘和外边缘之间的接触平面为中心的环形接触区域接触。接触平面以大于5度的角度相对于凸缘倾斜。

4. 发明授权

US08177502B2 Vane with reduced stress 失效
标题翻译：叶片减轻压力
公开(公告)号：US08177502B2
公开(公告)日：2012-05-15
申请号：US12277787
申请日：2008-11-25
申请人： Mitchell Jay Headley , Stephen Joseph Gruber
发明人： Mitchell Jay Headley , Stephen Joseph Gruber
IPC分类号： F01D9/04
CPC分类号： F01D9/044 , F01D9/041 , F04D29/542 , F04D29/644 , F05D2230/237 , F05D2240/122 , F05D2240/304 , F05D2260/941 , Y02T50/673
摘要： An airfoil assembly is described comprising an airfoil, a band coupled to the airfoil for providing at least a portion of support for the airfoil in the airfoil assembly and a slot capable reducing stress in the airfoil wherein the slot is located in the band near a portion of the airfoil. A compression system is described comprising a stator assembly comprising a plurality of arcuate vane sectors arranged circumferentially around a longitudinal axis, each vane sector comprising an airfoil, an arcuate inner band and an arcuate outer band coupled to the airfoil, and a slot capable of reducing stress in the airfoil, the slot being located in the vane sector near a portion of the airfoil.
摘要翻译：描述了一种翼型组件，其包括翼型件，连接到翼型件的带，用于为翼型组件中的翼型件提供至少一部分支撑件，以及能够减小翼型件中的应力的槽，其中，狭槽位于带内靠近部分的翼型。一种压缩系统被描述为包括定子组件，该定子组件包括围绕纵向轴线周向布置的多个弧形叶片扇区，每个叶片扇形部分包括翼型，弧形内带和耦合到翼型的弓形外带，以及能够减小在翼型中的应力，狭槽位于靠近翼型的一部分的叶片扇区中。

5. 发明授权

US07125222B2 Gas turbine engine variable vane assembly 有权
标题翻译：燃气涡轮发动机可变叶片总成
公开(公告)号：US07125222B2
公开(公告)日：2006-10-24
申请号：US10823933
申请日：2004-04-14
申请人： Nathan Gerard Cormier , Wayne Ray Bowen , James Edwin Rhoda , Mitchell Jay Headley
发明人： Nathan Gerard Cormier , Wayne Ray Bowen , James Edwin Rhoda , Mitchell Jay Headley
IPC分类号： F01D17/12
CPC分类号： F04D29/563 , F01D17/162 , Y10T403/587
摘要： A method facilitates assembling a variable vane assembly for a gas turbine engine including a casing and an inner shroud. The method comprises providing at least one variable vane including a radially inner spindle that includes a groove defined therein that has at least one machined face, and coupling the variable vane radially between the casing and the inner shroud such that at least a portion of the radially inner spindle is inserted at least partially through an opening extending radially through the inner shroud. The method also comprises securing the variable vane to the inner shroud by engaging the spindle machined face with a retainer coupled to the inner shroud.
摘要翻译：一种方法便于组装用于包括壳体和内护罩的燃气涡轮发动机的可变叶片组件。该方法包括提供包括径向内心轴的至少一个可变叶片，所述径向内心轴包括限定在其中的凹槽，其具有至少一个加工面，并且将可变叶片径向地联接在壳体和内护罩之间，使得至少一部分径向内心轴至少部分地穿过径向延伸穿过内护罩的开口。该方法还包括通过将主轴加工的面与与内护罩连接的保持器接合来将可变叶片固定到内护罩。

6. 发明授权

US06682299B2 Variable stator vane support arrangement 有权
标题翻译：可变定子叶片支撑装置
公开(公告)号：US06682299B2
公开(公告)日：2004-01-27
申请号：US09999275
申请日：2001-11-15
申请人： Wayne Ray Bowen , Jeffrey Clayton Potter , Mitchell Jay Headley
发明人： Wayne Ray Bowen , Jeffrey Clayton Potter , Mitchell Jay Headley
IPC分类号： F01D1716
CPC分类号： F16C17/10 , F01D9/02 , F01D11/001 , F01D17/162 , F04D29/563 , Y02T50/672
摘要： A trunnion support for a variable-position stator vane in a turbomachine. The stator vane includes an upper trunnion and a lower trunnion to allow the stator vane to be pivoted about a longitudinal axis. The lower trunnion is supported in a bushing that is carried in an opening provided in an annular stator vane carrier ring. The bushing is longitudinally split and is installed in the carrier ring while in a laterally compressed condition so that when installed in the carrier ring the bushing bears against the carrier ring opening in which it is positioned. When the carrier ring material expands with rising temperature, the pre-stress in the bushing will cause it to expand to maintain tight frictional engagement between the bushing and the opening and thereby prevent relative rotation between the bushing and the carrier ring to minimize wear of the carrier ring material.
摘要翻译：用于涡轮机中可变位置定子叶片的耳轴支撑。定子叶片包括上耳轴和下耳轴，以允许定子叶片围绕纵向轴线枢转。下耳轴支撑在被设置在环形定子叶片承载环中的开口中的衬套中。衬套纵向分开，并且在横向压缩状态下安装在承载环中，使得当安装在承载环中时，衬套抵靠在其定位的承载环开口上。当载体环材料随着温度升高而膨胀时，衬套中的预应力将使其膨胀以保持衬套和开口之间的紧密摩擦接合，从而防止衬套和承载环之间的相对旋转，以最小化载体环材料。

7. 发明申请

US20100129210A1 VANE WITH REDUCED STRESS 失效
标题翻译： VANE具有减少的应力
公开(公告)号：US20100129210A1
公开(公告)日：2010-05-27
申请号：US12277787
申请日：2008-11-25
申请人： Mitchell Jay Headley , Stephen Joseph Gruber
发明人： Mitchell Jay Headley , Stephen Joseph Gruber
IPC分类号： F01D9/04
CPC分类号： F01D9/044 , F01D9/041 , F04D29/542 , F04D29/644 , F05D2230/237 , F05D2240/122 , F05D2240/304 , F05D2260/941 , Y02T50/673
摘要： An airfoil assembly is described comprising an airfoil, a band coupled to the airfoil for providing at least a portion of support for the airfoil in the airfoil assembly and a slot capable reducing stress in the airfoil wherein the slot is located in the band near a portion of the airfoil. A compression system is described comprising a stator assembly comprising a plurality of arcuate vane sectors arranged circumferentially around a longitudinal axis, each vane sector comprising an airfoil, an arcuate inner band and an arcuate outer band coupled to the airfoil, and a slot capable of reducing stress in the airfoil, the slot being located in the vane sector near a portion of the airfoil.
摘要翻译：描述了一种翼型组件，其包括翼型件，连接到翼型件的带，用于为翼型组件中的翼型件提供至少一部分支撑件，以及能够减小翼型件中的应力的槽，其中，狭槽位于带内靠近部分的翼型。一种压缩系统被描述为包括定子组件，该定子组件包括围绕纵向轴线周向布置的多个弧形叶片扇区，每个叶片扇形部分包括翼型，弧形内带和耦合到翼型的弓形外带，以及能够减小在翼型中的应力，狭槽位于靠近翼型的一部分的叶片扇区中。

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