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1. 发明授权

US6098407A Premixing fuel injector with improved secondary fuel-air injection 失效
标题翻译：预燃燃油喷射器改进二次燃油喷射
公开(公告)号：US6098407A
公开(公告)日：2000-08-08
申请号：US93371
申请日：1998-06-08
申请人： John J. Korzendorfer , Jeffrey D. Melman , Alan J. Goetschius
发明人： John J. Korzendorfer , Jeffrey D. Melman , Alan J. Goetschius
IPC分类号： F23R3/30 , F23C7/00 , F23D14/02 , F23D14/22 , F23R3/28 , F02C7/22
CPC分类号： F23C7/002 , F23D14/02 , F23D14/22 , F23C2900/07002 , F23D2206/10 , F23D2211/00
摘要： A premixing, tangential entry fuel injector (10) for a gas turbine engine features a secondary fuel-air injection insert (40) positively secured to a centerbody shell (38) by a braze joint (98). A secondary fuel supply tube (42), positively secured to both a centerbody base (36) and to the insert (40), is curved in at least two dimensions. In an exemplary embodiment, the tube is coiled into a spiral shape covering a single 360.degree. cycle. During engine operation, the centerbody expands axially in response to elevated temperatures in the engine's interior, causing the insert (40) to be displaced away from the base (36). The curvature of the tube allows the tube to flex slightly to accommodate the displacement. Ideally the curvature of the tube is such that the tube's natural frequency is well above the maximum vibratory frequency that the tube will experience during engine operation.
摘要翻译：用于燃气涡轮发动机的预混合切向进入燃料喷射器（10）具有通过钎焊接头（98）主动固定到中心壳体（38）的二次燃料 - 空气注入插入件（40）。固定在中心体基座（36）和插入件（40）两者上的辅助燃料供给管（42）至少在两个维度上弯曲。在示例性实施例中，管被卷绕成覆盖单个360度循环的螺旋形状。在发动机运转期间，中心体响应于发动机内部的升高的温度而轴向膨胀，导致插入件（40）远离基座（36）移动。管的曲率允许管轻微弯曲以适应位移。理想地，管的曲率使得管的固有频率远高于管在引擎操作期间将经历的最大振动频率。

2. 发明授权

US09746381B2 Laser instrumentation bracket 有权
公开(公告)号：US09746381B2
公开(公告)日：2017-08-29
申请号：US13530208
申请日：2012-06-22
申请人： Witt C. Guinn , John J. Korzendorfer , David J. Sander , Kelly A. Vanston
发明人： Witt C. Guinn , John J. Korzendorfer , David J. Sander , Kelly A. Vanston
IPC分类号： G01K1/14 , F01D17/08 , G01K11/12 , G01K13/02
CPC分类号： G01K1/14 , F01D17/085 , F05D2270/80 , G01K11/12 , G01K13/02 , G01K2013/024 , Y10T29/49778
摘要： An exemplary laser instrumentation bracket includes a support structure providing a recess configured to receive a collar of a laser housing. The laser housing has a main body extending axially through an aperture of the support structure when the recess receives the collar.

3. 发明授权

US08985942B2 Turbine exhaust case duct 有权
标题翻译：涡轮排气箱管道
公开(公告)号：US08985942B2
公开(公告)日：2015-03-24
申请号：US13539610
申请日：2012-07-02
申请人： William A. Daniels , John J. Korzendorfer , David A. Debyah , Scott A. Ladd
发明人： William A. Daniels , John J. Korzendorfer , David A. Debyah , Scott A. Ladd
IPC分类号： F01D25/24
CPC分类号： F01D25/24 , Y02T50/671
摘要： An exhaust duct comprises a shroud body, a forward flange assembly, an aft flange assembly, an intermediate flange assembly, and a first plurality of bleed ports. The forward flange assembly extends radially inward from a forward shroud end for securing the forward shroud end downstream of a final turbine stage. The aft flange assembly extends circumferentially around and radially inward from an aft shroud end for securing the aft shroud end to an engine tail cone. The intermediate flange assembly is disposed forward of the aft flange assembly, and extends circumferentially around and radially inward from the shroud body for securing the shroud body to an engine bearing housing. The first plurality of bleed ports is disposed around the shroud body forward of a junction with the intermediate flange.
摘要翻译：排气管道包括护罩主体，前凸缘组件，后凸缘组件，中间凸缘组件和第一多个排气口。前法兰组件从前护罩端径向向内延伸，以将前护罩端固定在最终涡轮级的下游。后翼缘组件从后护罩端部周向地周向地径向向内延伸，以将后护罩端固定到发动机尾锥。中间凸缘组件设置在后凸缘组件的前方，并且从罩主体周向地周向地和径向向内延伸，以将罩体固定到发动机轴承壳体上。第一多个排出口设置在与中间凸缘的接合部的前方的护罩本体的周围。

4. 发明申请

US20140003922A1 TURBINE EXHAUST CASE DUCT 有权
标题翻译：涡轮排气箱
公开(公告)号：US20140003922A1
公开(公告)日：2014-01-02
申请号：US13539610
申请日：2012-07-02
申请人： William A. Daniels , John J. Korzendorfer , David A. Debyah , Scott A. Ladd
发明人： William A. Daniels , John J. Korzendorfer , David A. Debyah , Scott A. Ladd
IPC分类号： F01D25/24
CPC分类号： F01D25/24 , Y02T50/671
摘要： An exhaust duct comprises a shroud body, a forward flange assembly, an aft flange assembly, an intermediate flange assembly, and a first plurality of bleed ports. The forward flange assembly extends radially inward from a forward shroud end for securing the forward shroud end downstream of a final turbine stage. The aft flange assembly extends circumferentially around and radially inward from an aft shroud end for securing the aft shroud end to an engine tail cone. The intermediate flange assembly is disposed forward of the aft flange assembly, and extends circumferentially around and radially inward from the shroud body for securing the shroud body to an engine bearing housing. The first plurality of bleed ports is disposed around the shroud body forward of a junction with the intermediate flange.
摘要翻译：排气管道包括护罩主体，前凸缘组件，后凸缘组件，中间凸缘组件和第一多个排气口。前法兰组件从前护罩端径向向内延伸，以将前护罩端固定在最终涡轮级的下游。后翼缘组件从后护罩端部周向地周向地径向向内延伸，以将后护罩端固定到发动机尾锥。中间凸缘组件设置在后凸缘组件的前方，并且从罩主体周向地周向地和径向向内延伸，以将罩体固定到发动机轴承壳体上。第一多个排出口设置在与中间凸缘的接合部的前方的护罩本体的周围。

5. 发明申请

US20130343066A1 LASER INSTRUMENTATION BRACKET 有权
标题翻译：激光仪表支架
公开(公告)号：US20130343066A1
公开(公告)日：2013-12-26
申请号：US13530208
申请日：2012-06-22
申请人： Witt C. Guinn , John J. Korzendorfer , David J. Sander , Kelly A. Vanston
发明人： Witt C. Guinn , John J. Korzendorfer , David J. Sander , Kelly A. Vanston
IPC分类号： F21V21/00 , B23Q17/00
CPC分类号： G01K1/14 , F01D17/085 , F05D2270/80 , G01K11/12 , G01K13/02 , G01K2013/024 , Y10T29/49778
摘要： An exemplary laser instrumentation bracket includes a support structure providing a recess configured to receive a collar of a laser housing. The laser housing has a main body extending axially through an aperture of the support structure when the recess receives the collar.
摘要翻译：示例性的激光仪表支架包括提供凹部的支撑结构，所述凹部被构造成接收激光外壳的轴环。激光器壳体具有当凹部接收到轴环时轴向延伸穿过支撑结构的孔的主体。

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