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1. 发明授权

US06652226B2 Methods and apparatus for reducing seal teeth wear 有权
公开(公告)号：US06652226B2
公开(公告)日：2003-11-25
申请号：US09783277
申请日：2001-02-09
申请人： Richard William Albrecht, Jr. , Joseph Charles Kulesa , Robert Paul Czachor , Shesh Krishna Srivatsa , Daniel Edward Wines , Thomas Tracy Wallace
发明人： Richard William Albrecht, Jr. , Joseph Charles Kulesa , Robert Paul Czachor , Shesh Krishna Srivatsa , Daniel Edward Wines , Thomas Tracy Wallace
IPC分类号： F01D1112
CPC分类号： F01D11/127 , F01D5/225 , F16J15/444 , Y02T50/672
摘要： A gas turbine engine includes a non-rotatable member that includes a honeycomb seal that reduces wear to rotor seal teeth disposed within the gas turbine engine. The gas turbine engine also includes a rotatable annular member including a sealing assembly disposed between rotor and stator components. The rotatable annular member includes seal teeth that extend radially outward from the rotatable annular member. The stator components include a non-rotatable member that includes a honeycomb seal that extends radially inward. The honeycomb seal is fabricated from a material that has a melting temperature less than approximately 2000° F.

2. 发明申请

US20120051917A1 TAPERED COLLET CONNECTION OF ROTOR COMPONENTS 有权
标题翻译：转子组件的锥形接头连接
公开(公告)号：US20120051917A1
公开(公告)日：2012-03-01
申请号：US12872376
申请日：2010-08-31
申请人： Daniel Edward Wines , James Hamilton Grooms , Craig William Higgins
发明人： Daniel Edward Wines , James Hamilton Grooms , Craig William Higgins
IPC分类号： F01D5/22 , F01D5/30
CPC分类号： F01D5/3015 , F01D5/066 , F01D11/001 , F01D11/005 , F05D2230/64 , F05D2260/30
摘要： A connection between an annular sleeve on a gas turbine engine first rotor component includes an annular tapered conical slot extending axially inwardly into the sleeve from an annular opening and tapers axially into the sleeve from the opening. An annular rim of a second rotor component is received within the conical slot and includes a rim inner conical surface mating with and contacting a sleeve inner conical surface in part bounding the conical slot. A sleeve cylindrical outer surface in part bounds the conical slot in the sleeve and a rim outer cylindrical surface on the annular rim contacts the sleeve cylindrical outer surface. An annular lip may extend radially inwardly from the sleeve and sleeve inner conical surface at the annular opening to the conical slot. The connection may be used between a first stage disk and an interstage seal.
摘要翻译：燃气涡轮发动机第一转子部件上的环形套筒之间的连接包括从环形开口轴向向内延伸到套筒中的环形锥形锥形槽，并且从开口轴向地锥形地套入套筒。第二转子部件的环形边缘被容纳在锥形槽内，并且包括边缘内圆锥形表面，该边缘内锥形表面与限定锥形槽的部分的套筒内锥形表面配合并接触。套筒圆柱形外表面部分地限制在套筒中的锥形槽，并且环形边缘上的边缘外圆柱形表面接触套筒圆柱形外表面。环形唇缘可以从环形开口处的套筒和套筒内锥形表面径向向内延伸到锥形槽。连接可以在第一级盘和级间密封之间使用。

3. 发明授权

US08636195B2 Welding process and component formed thereby 有权
标题翻译：由此形成焊接工艺和部件
公开(公告)号：US08636195B2
公开(公告)日：2014-01-28
申请号：US12708650
申请日：2010-02-19
申请人： Douglas Gerard Konitzer , Eric Scott Huron , David Paul Mourer , Brian James Girvin , Glenn Charles Culbertson , Daniel Edward Wines , Daniel David Noe
发明人： Douglas Gerard Konitzer , Eric Scott Huron , David Paul Mourer , Brian James Girvin , Glenn Charles Culbertson , Daniel Edward Wines , Daniel David Noe
IPC分类号： B23K20/12 , B23P15/04
CPC分类号： B23K20/129 , B23K20/1205 , B23K2101/001 , F01D5/063 , F01D11/001 , F05D2230/232 , Y10T29/4932
摘要： A process of fabricating a rotating component and a rotating component formed thereby. The rotating component has a rotational axis, at least one rim member, at least one disk member, and at least one airfoil member. The rim and disk members are welded together to define a first solid-state weld joint lying in a first plane that is not parallel to the rotational axis of the rotating component. The airfoil member is welded to the rim member to define a second solid-state weld joint lying in a second plane that is not parallel to the rotational axis of the rotating component. The rim member is located in a radially outward direction from the disk member, and the airfoil member is located in a radially outward direction from the rim member.
摘要翻译：一种由此形成的旋转部件和旋转部件的制造方法。旋转部件具有旋转轴线，至少一个轮缘部件，至少一个盘部件和至少一个翼型部件。轮缘和圆盘部件被焊接在一起以限定位于不平行于旋转部件的旋转轴线的第一平面中的第一固态焊接接头。翼型件被焊接到轮辋构件上以限定位于不平行于旋转部件的旋转轴线的第二平面中的第二固态焊接接头。轮缘构件位于从盘构件的径向向外的方向上，并且翼型构件位于沿着轮缘构件的径向向外的方向上。

4. 发明授权

US08608436B2 Tapered collet connection of rotor components 有权
标题翻译：转子零件的锥形夹头连接
公开(公告)号：US08608436B2
公开(公告)日：2013-12-17
申请号：US12872376
申请日：2010-08-31
申请人： Daniel Edward Wines , James Hamilton Grooms , Craig William Higgins
发明人： Daniel Edward Wines , James Hamilton Grooms , Craig William Higgins
IPC分类号： F01D5/02 , F01D11/00
CPC分类号： F01D5/3015 , F01D5/066 , F01D11/001 , F01D11/005 , F05D2230/64 , F05D2260/30
摘要： A connection between an annular sleeve on a gas turbine engine first rotor component includes an annular tapered conical slot extending axially inwardly into the sleeve from an annular opening and tapers axially into the sleeve from the opening. An annular rim of a second rotor component is received within the conical slot and includes a rim inner conical surface mating with and contacting a sleeve inner conical surface in part bounding the conical slot. A sleeve cylindrical outer surface in part bounds the conical slot in the sleeve and a rim outer cylindrical surface on the annular rim contacts the sleeve cylindrical outer surface. An annular lip may extend radially inwardly from the sleeve and sleeve inner conical surface at the annular opening to the conical slot. The connection may be used between a first stage disk and an interstage seal.
摘要翻译：燃气涡轮发动机第一转子部件上的环形套筒之间的连接包括从环形开口轴向向内延伸到套筒中的环形锥形锥形槽，并且从开口轴向地锥形地套入套筒。第二转子部件的环形边缘被容纳在锥形槽内，并且包括边缘内圆锥形表面，该边缘内锥形表面与限定锥形槽的部分的套筒内锥形表面配合并接触。套筒圆柱形外表面部分地限制在套筒中的锥形槽，并且环形边缘上的边缘外圆柱形表面接触套筒圆柱形外表面。环形唇缘可以从环形开口处的套筒和套筒内锥形表面径向向内延伸到锥形槽。连接可以在第一级盘和级间密封之间使用。

5. 发明申请

US20110206523A1 WELDING PROCESS AND COMPONENT FORMED THEREBY 有权
标题翻译：焊接工艺及其组成
公开(公告)号：US20110206523A1
公开(公告)日：2011-08-25
申请号：US12708650
申请日：2010-02-19
申请人： Douglas Gerard Konitzer , Eric Scott Huron , David Paul Mourer , Brian James Girvin , Glenn Charles Culbertson , Daniel Edward Wines , Daniel David Noe
发明人： Douglas Gerard Konitzer , Eric Scott Huron , David Paul Mourer , Brian James Girvin , Glenn Charles Culbertson , Daniel Edward Wines , Daniel David Noe
IPC分类号： F04D29/34 , B23K20/12
CPC分类号： B23K20/129 , B23K20/1205 , B23K2101/001 , F01D5/063 , F01D11/001 , F05D2230/232 , Y10T29/4932
摘要： A process of fabricating a rotating component and a rotating component formed thereby. The rotating component has a rotational axis, at least one rim member, at least one disk member, and at least one airfoil member. The rim and disk members are welded together to define a first solid-state weld joint lying in a first plane that is not parallel to the rotational axis of the rotating component. The airfoil member is welded to the rim member to define a second solid-state weld joint lying in a second plane that is not parallel to the rotational axis of the rotating component. The rim member is located in a radially outward direction from the disk member, and the airfoil member is located in a radially outward direction from the rim member.
摘要翻译：一种由此形成的旋转部件和旋转部件的制造方法。旋转部件具有旋转轴线，至少一个轮缘部件，至少一个盘部件和至少一个翼型部件。轮缘和圆盘部件被焊接在一起以限定位于不平行于旋转部件的旋转轴线的第一平面中的第一固态焊接接头。翼型件被焊接到轮辋构件上以限定位于不平行于旋转部件的旋转轴线的第二平面中的第二固态焊接接头。轮缘构件位于从盘构件的径向向外的方向上，并且翼型构件位于沿着轮缘构件的径向向外的方向上。

6. 发明授权

US07891952B2 Rotary machine components and methods of fabricating such components 失效
标题翻译：旋转机器部件和制造这些部件的方法
公开(公告)号：US07891952B2
公开(公告)日：2011-02-22
申请号：US11564070
申请日：2006-11-28
申请人： Daniel Edward Wines , Randy Joseph Ketterer , Barbara Ann Link , Mark Dean Pezzutti , Charles William Carrier , Terrence Owen Dyer , Richard Gordon Menzies , Andrew John Lammas
发明人： Daniel Edward Wines , Randy Joseph Ketterer , Barbara Ann Link , Mark Dean Pezzutti , Charles William Carrier , Terrence Owen Dyer , Richard Gordon Menzies , Andrew John Lammas
IPC分类号： F01D5/06
CPC分类号： B23P15/006 , F01D5/06 , F01D5/066 , F04D29/053 , F04D29/054 , F05D2230/25 , F05D2250/312 , F05D2250/314 , F05D2300/502 , Y10T29/4932 , Y10T29/49321
摘要： A method for fabricating a rotor assembly for a turbine, the turbine including a central rotational axis is provided. The method includes forging a first rotor component from a first material, separately forging a second rotor component from a second material, and coupling the second rotor component to the first rotor component at a location radially inward of the first rotor component. The second rotor component is coupled to the first rotor component in at least one axial-circumferential plane that is at least one of substantially parallel and obliquely oriented with respect to the central rotational axis.
摘要翻译：提供了一种用于制造用于涡轮机的转子组件的方法，所述涡轮机包括中心旋转轴线。该方法包括从第一材料锻造第一转子部件，分别从第二材料锻造第二转子部件，以及在第一转子部件的径向内侧的位置将第二转子部件联接到第一转子部件。第二转子部件在至少一个轴向圆周平面中联接到第一转子部件，该至少一个轴向圆周平面中的至少一个相对于中心旋转轴线基本上平行且倾斜地定向。

7. 发明申请

US20080120842A1 ROTARY MACHINE COMPONENTS AND METHODS OF FABRICATING SUCH COMPONENTS 失效
标题翻译：旋转机组件及其制造方法
公开(公告)号：US20080120842A1
公开(公告)日：2008-05-29
申请号：US11564070
申请日：2006-11-28
申请人： Daniel Edward Wines , Randy Joseph Ketterer , Barbara Ann Link , Mark Dean Pezzutti , Charles William Carrier , Terrence Owen Dyer , Richard Gordon Menzies , Andrew John Lammas
发明人： Daniel Edward Wines , Randy Joseph Ketterer , Barbara Ann Link , Mark Dean Pezzutti , Charles William Carrier , Terrence Owen Dyer , Richard Gordon Menzies , Andrew John Lammas
IPC分类号： B23P15/04 , F04D29/18
CPC分类号： B23P15/006 , F01D5/06 , F01D5/066 , F04D29/053 , F04D29/054 , F05D2230/25 , F05D2250/312 , F05D2250/314 , F05D2300/502 , Y10T29/4932 , Y10T29/49321
摘要： A method for fabricating a rotor assembly for a turbine, the turbine including a central rotational axis is provided. The method includes forging a first rotor component from a first material, separately forging a second rotor component from a second material, and coupling the second rotor component to the first rotor component at a location radially inward of the first rotor component. The second rotor component is coupled to the first rotor component in at least one axial-circumferential plane that is at least one of substantially parallel and obliquely oriented with respect to the central rotational axis.
摘要翻译：提供了一种用于制造用于涡轮机的转子组件的方法，所述涡轮机包括中心旋转轴线。该方法包括从第一材料锻造第一转子部件，分别从第二材料锻造第二转子部件，以及在第一转子部件的径向内侧的位置将第二转子部件联接到第一转子部件。第二转子部件在至少一个轴向圆周平面中联接到第一转子部件，该至少一个轴向圆周平面中的至少一个相对于中心旋转轴线基本上平行且倾斜地定向。

8. 发明授权

US07464577B2 Method for fabricating rotary machines 有权
标题翻译：旋转机械的制造方法
公开(公告)号：US07464577B2
公开(公告)日：2008-12-16
申请号：US10882367
申请日：2004-07-01
申请人： Mark Steven Habedank , Daniel Edward Wines , Mark Wesley Johnson , Gregory Stephen Bechtel , Charles William Carrier
发明人： Mark Steven Habedank , Daniel Edward Wines , Mark Wesley Johnson , Gregory Stephen Bechtel , Charles William Carrier
IPC分类号： B21D41/02
CPC分类号： F01D5/286 , B21K1/32 , B23P15/006 , C21D7/12 , F01D5/02 , F05D2230/00 , Y10T29/4932 , Y10T29/49536
摘要： A method and apparatus for fabricating a workpiece is provided. The method includes applying a predetermined axial force to a tool, translating the axial force into a radial force in the workpiece using the tool, and generating a hoop stress in the work piece sufficient to relieve residual stress in the workpiece.
摘要翻译：提供了一种用于制造工件的方法和装置。该方法包括对工具施加预定的轴向力，使用该工具将轴向力平移到工件中的径向力，并且在工件中产生足以减轻工件中的残余应力的环向应力。

9. 发明授权

US07344354B2 Methods and apparatus for operating gas turbine engines 有权
标题翻译：运行燃气轮机的方法和装置
公开(公告)号：US07344354B2
公开(公告)日：2008-03-18
申请号：US11222101
申请日：2005-09-08
申请人： Andrew John Lammas , Steven Mark Ballman , Daniel Edward Wines , David Lawrence Bedel , Sean Patrick McGowan
发明人： Andrew John Lammas , Steven Mark Ballman , Daniel Edward Wines , David Lawrence Bedel , Sean Patrick McGowan
IPC分类号： F01D9/06
CPC分类号： F01D5/081 , F04D27/023 , F04D29/321 , F05D2230/60 , F05D2260/602 , Y10T29/4932
摘要： A method of assembling a gas turbine engine that includes providing a rotor assembly including a rotor shaft, an air duct, and a rotor disk that includes a mounting arm, wherein the mounting arm extends radially inward from the rotor disk towards the rotor shaft and coupling a rotor impeller assembly to the mounting arm, wherein the rotor impeller assembly includes a carrier and a plurality of bleed tubes that each extend outwardly from the carrier and are configured to receive bleed air.
摘要翻译：一种组装燃气涡轮发动机的方法，其包括提供包括转子轴，风道和包括安装臂的转子盘的转子组件，其中所述安装臂从所述转子盘朝向所述转子轴径向向内延伸并且联接转子叶轮组件到安装臂，其中转子叶轮组件包括载体和多个排放管，每个排放管从载体向外延伸并且构造成接收放气。

10. 发明授权

US06899520B2 Methods and apparatus to reduce seal rubbing within gas turbine engines 有权
标题翻译：减少燃气涡轮发动机内密封摩擦的方法和装置
公开(公告)号：US06899520B2
公开(公告)日：2005-05-31
申请号：US10653337
申请日：2003-09-02
申请人： Mark Steven Habedank , Daniel Edward Wines , Christopher James League , Aaron Michael Dziech , George Edwin Whitaker
发明人： Mark Steven Habedank , Daniel Edward Wines , Christopher James League , Aaron Michael Dziech , George Edwin Whitaker
IPC分类号： F01D5/06 , F01D11/00 , F01D25/00 , F02C7/28 , F16J15/54 , F01D11/02
CPC分类号： F01D11/001 , F01D5/06
摘要： A method facilitates assembling a seal assembly for a gas turbine engine rotor assembly. The method comprises coupling a disk retainer to a first stage disk, and coupling an interstage seal assembly including an outer shell within the rotor assembly such that a downstream arm extending from the outer shell engages a second stage disk while an upstream arm extending from the outer shell engages the disk retainer.
摘要翻译：一种方法便于组装用于燃气涡轮发动机转子组件的密封组件。该方法包括将盘保持器联接到第一级盘，以及将包括外壳的级间密封组件联接在转子组件内，使得从外壳延伸的下游臂接合第二级盘，而从外部延伸的上游臂外壳接合盘保持器。

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