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1. 发明授权

US06412160B1 Swaged tube fitting collar and die 有权
标题翻译：模锻管接头和模具
公开(公告)号：US06412160B1
公开(公告)日：2002-07-02
申请号：US09668909
申请日：2000-09-22
申请人： John Carl Glessner , Norman Stanton Baylis
发明人： John Carl Glessner , Norman Stanton Baylis
IPC分类号： B23P1700
CPC分类号： B21D39/046 , Y10T29/4981 , Y10T29/49845 , Y10T29/49908 , Y10T29/53987 , Y10T29/53996
摘要： An assembly for retaining a work piece and fitting together for placement in a swage machine. The assembly includes a die and a collar to keep the work piece from moving during the swaging process. The collar includes two clamping sections that are connected together, such as by a hinge. The collar is placed about the work piece and then clamped in place by a retaining bolt at the opposing end of the clamping sections. The die includes a recess for holding the collar and a recess for the tube. The assembly includes an anti-rotation feature to minimize rotation of the collar within the recess. One example of an anti-rotation feature is the formation of the recess and the collar in corresponding hexagonal shapes. The die may also include a recess for retaining a fitting to be swaged to the work piece. The die and collar assembly eliminates the need for nylon inserts and eliminates work piece rotation and axial movement during the automated swaging process.
摘要翻译：用于保持工件并装配在一起以用于放置在挤压机中的组件。组件包括模具和套环，以在模锻过程中保持工件不移动。套环包括两个连接在一起的夹紧部分，例如通过铰链。将套环放置在工件周围，然后通过夹紧部分的相对端处的固定螺栓夹紧就位。模具包括用于保持套环的凹部和用于管的凹部。组件包括防旋转特征，以使套环在凹槽内的旋转最小化。防旋转特征的一个示例是形成相应六边形形状的凹部和套环。模具还可以包括用于保持要被锻压到工件上的配件的凹部。模具和轴环组件消除了尼龙插入件的需要，并消除了自动模锻过程中的工件旋转和轴向移动。

2. 发明授权

US08430202B1 Compact high-pressure exhaust muffling devices 有权
标题翻译：紧凑型高压排气消声器
公开(公告)号：US08430202B1
公开(公告)日：2013-04-30
申请号：US13347728
申请日：2012-01-11
申请人： Jeffrey Lee Mason , Daniel Alexander Sieg , Carlos Eduardo Gutierrez , John Carl Glessner , Charles Steve Lawless
发明人： Jeffrey Lee Mason , Daniel Alexander Sieg , Carlos Eduardo Gutierrez , John Carl Glessner , Charles Steve Lawless
IPC分类号： B64D33/04
CPC分类号： F01D17/105 , F01D25/30 , F02C6/08 , F02C7/24 , F05B2250/191 , Y02T50/672
摘要： Compact, high-pressure exhaust muffling devices are disclosed. Some example muffling devices may include an inner flow conditioner including an inlet configured to convey a pressurized fluid flow into an inner flow conditioner interior. The inner flow conditioner may include a plurality of inner flow conditioner holes. The muffling device may include an exhaust can disposed substantially around the inner flow conditioner and arranged to receive the pressurized fluid flow via the inner flow conditioner holes into an exhaust can interior. The exhaust can may include a plurality of exhaust screen holes arranged to discharge the pressurized fluid flow from the exhaust can interior. The exhaust can interior may be substantially devoid of flow obstructions between the plurality of inner flow conditioner holes and the exhaust screen holes.
摘要翻译：公开了紧凑型高压排气消声装置。一些示例性的消音装置可以包括内部流动调节器，其包括被构造成将加压流体流输送到内部流动调节器内部中的入口。内部流动调节器可以包括多个内部流动调节器孔。消音装置可以包括基本上围绕内部流动调节器设置的排气罐，并且布置成将经由内部流动调节器孔的加压流体流接收到排气罐内部。排气罐可以包括多个排气筛孔，布置成从排气罐内部排出加压流体流。排气罐内部可以在多个内部流动调节器孔和排气筛孔之间基本上没有流动障碍物。

3. 发明授权

US08549859B2 Combustor apparatus in a gas turbine engine 有权
标题翻译：燃气涡轮发动机中的燃烧器装置
公开(公告)号：US08549859B2
公开(公告)日：2013-10-08
申请号：US12233903
申请日：2008-09-19
申请人： Timothy A. Fox , David J. Wiebe , David M. Ritland , John Carl Glessner
发明人： Timothy A. Fox , David J. Wiebe , David M. Ritland , John Carl Glessner
IPC分类号： F02C7/22
CPC分类号： F23R3/16 , F23R3/283 , F23R3/346 , F23R2900/00005
摘要： A combustion apparatus in a gas turbine engine comprises a combustor shell for receiving air, a fuel injection system associated with the combustor shell, a first fuel supply structure, and a shield structure. The fuel supply structure is in fluid communication with a source of fuel for delivering fuel from the source of fuel to the fuel injection system and comprises a first fuel supply elements including a first section extending along a first path having a component in an axial direction and a second section extending from the first section along a second path having a component in a circumferential direction. The shield structure is associated with at least a portion of the second section of the first fuel supply element.
摘要翻译：燃气涡轮发动机中的燃烧装置包括用于接收空气的燃烧器壳体，与燃烧器壳体相关联的燃料喷射系统，第一燃料供应结构和屏蔽结构。燃料供应结构与燃料源流体连通，用于将燃料从燃料源输送到燃料喷射系统，并且包括第一燃料供应元件，其包括沿着沿轴向方向具有部件的第一路径延伸的第一部分，以及第二部分沿着沿圆周方向具有部件的第二路径从第一部分延伸。屏蔽结构与第一燃料供应元件的第二部分的至少一部分相关联。

4. 发明授权

US08307943B2 High pressure drop muffling system 有权
标题翻译：高压降消声系统
公开(公告)号：US08307943B2
公开(公告)日：2012-11-13
申请号：US13178159
申请日：2011-07-07
申请人： Kevin Samuel Klasing , Bradley Willis Fintel , John Carl Glessner , Jeffrey Lee Mason , Christopher Jon Potokar , Robert Proctor
发明人： Kevin Samuel Klasing , Bradley Willis Fintel , John Carl Glessner , Jeffrey Lee Mason , Christopher Jon Potokar , Robert Proctor
IPC分类号： F01N1/08 , F01N1/00
CPC分类号： F02C6/08 , F02K3/075 , F05D2260/96 , Y10T137/85938
摘要： A system for venting a high-pressure flow stream is disclosed, the system comprising a device having a plurality of orifice plates, each orifice plate having a plurality of orifices, wherein the plurality of orifice plates are oriented relative to each other such that the pressure of the flow stream substantially drops.
摘要翻译：公开了用于排放高压流动流的系统，该系统包括具有多个孔板的装置，每个孔板具有多个孔，其中多个孔板相对于彼此定向，使得压力的流动基本上下降。

5. 发明申请

US20120006615A1 HIGH PRESSURE DROP MUFFLING SYSTEM 有权
标题翻译：高压减速系统
公开(公告)号：US20120006615A1
公开(公告)日：2012-01-12
申请号：US13178159
申请日：2011-07-07
申请人： Kevin Samuel Klasing , Bradley Willis Fintel , John Carl Glessner , Jeffrey Lee Mason , Christopher Jon Potokar , Robert Proctor
发明人： Kevin Samuel Klasing , Bradley Willis Fintel , John Carl Glessner , Jeffrey Lee Mason , Christopher Jon Potokar , Robert Proctor
IPC分类号： E04F17/04
CPC分类号： F02C6/08 , F02K3/075 , F05D2260/96 , Y10T137/85938
摘要： A system for venting a high-pressure flow stream is disclosed, the system comprising a device having a plurality of orifice plates, each orifice plate having a plurality of orifices, wherein the plurality of orifice plates are oriented relative to each other such that the pressure of the flow stream substantially drops.
摘要翻译：公开了用于排放高压流动流的系统，该系统包括具有多个孔板的装置，每个孔板具有多个孔，其中多个孔板相对于彼此定向，使得压力的流动基本上下降。

6. 发明授权

US07080515B2 Gas turbine can annular combustor 有权
标题翻译：燃气轮机可以环形燃烧器
公开(公告)号：US07080515B2
公开(公告)日：2006-07-25
申请号：US10667263
申请日：2003-09-19
申请人： Samer P. Wasif , Udo Schmitz , Robert Bland , Karsten Jordan , John Carl Glessner , J. Scott Markovitz , Bernd Prade , David Kargetta , Stephen Ramier , Stefan Dahlk
发明人： Samer P. Wasif , Udo Schmitz , Robert Bland , Karsten Jordan , John Carl Glessner , J. Scott Markovitz , Bernd Prade , David Kargetta , Stephen Ramier , Stefan Dahlk
IPC分类号： F02C3/00 , F23R3/04 , F23R3/14
CPC分类号： F23R3/14 , F23R3/286 , F23R3/343 , F23R3/54 , F23R3/60 , F23R2900/00014 , F23R2900/03044
摘要： A gas turbine engine (120) includes a cylindrical basket (146) having an axis (14) and a single main burner assembly (12) disposed within the basket. A burner insert (34) is disposed in an annular space between the burner assembly and the basket. The insert includes a face perpendicular to the axis of the basket. A plurality of passageways (114) are formed in the basket, positioned proximate to and downstream of the burner insert for allowing passage of a portion of an oxidizer flow (42) into a combustion chamber (30). A fluid flow path (38), defined between a combustion chamber liner portion (32) of the basket and a casing (40) spaced radially outward from the combustion liner portion, discharges a fluid into a flow reversal region (118) proximate an inlet (20) of the burner assembly. A fuel outlet (44) is disposed in the flow reversal region.
摘要翻译：燃气涡轮发动机（120）包括具有轴线（14）的圆柱形篮（146）和设置在篮内的单个主燃烧器组件（12）。燃烧器插入件（34）设置在燃烧器组件和篮子之间的环形空间中。插入件包括垂直于筐轴线的面。多个通道（114）形成在篮中，其位于燃烧器插入件附近和下游，以允许一部分氧化剂流（42）通入燃烧室（30）。限定在筐的燃烧室衬套部分（32）和与燃烧衬套部分径向向外间隔开的壳体（40）之间的流体流动路径（38）将流体排放到靠近入口的流动反向区域（118）（20）。燃料出口（44）设置在流动反转区域中。

7. 发明申请

US20100018210A1 COMBUSTOR APPARATUS IN A GAS TURBINE ENGINE 有权
标题翻译：燃气涡轮发动机中的燃烧器装置
公开(公告)号：US20100018210A1
公开(公告)日：2010-01-28
申请号：US12233903
申请日：2008-09-19
申请人： Timothy A. Fox , David J. Wiebe , David M. Ritland , John Carl Glessner
发明人： Timothy A. Fox , David J. Wiebe , David M. Ritland , John Carl Glessner
IPC分类号： F02C7/22 , F23R3/28
CPC分类号： F23R3/16 , F23R3/283 , F23R3/346 , F23R2900/00005
摘要： A combustion apparatus in a gas turbine engine comprises a combustor shell for receiving air, a fuel injection system associated with the combustor shell, a first fuel supply structure, and a shield structure. The fuel supply structure is in fluid communication with a source of fuel for delivering fuel from the source of fuel to the fuel injection system and comprises a first fuel supply elements including a first section extending along a first path having a component in an axial direction and a second section extending from the first section along a second path having a component in a circumferential direction. The shield structure is associated with at least a portion of the second section of the first fuel supply element.
摘要翻译：燃气涡轮发动机中的燃烧装置包括用于接收空气的燃烧器壳体，与燃烧器壳体相关联的燃料喷射系统，第一燃料供应结构和屏蔽结构。燃料供应结构与燃料源流体连通，用于将燃料从燃料源输送到燃料喷射系统，并且包括第一燃料供应元件，其包括沿着沿轴向方向具有部件的第一路径延伸的第一部分，以及第二部分沿着沿圆周方向具有部件的第二路径从第一部分延伸。屏蔽结构与第一燃料供应元件的第二部分的至少一部分相关联。

8. 发明授权

US06775989B2 Catalyst support plate assembly and related methods for catalytic combustion 有权
公开(公告)号：US06775989B2
公开(公告)日：2004-08-17
申请号：US10244064
申请日：2002-09-13
申请人： Ramarao V. Bandaru , John Carl Glessner
发明人： Ramarao V. Bandaru , John Carl Glessner
IPC分类号： F23R340
CPC分类号： F23R3/40 , B01J35/04 , F23C2900/13001
摘要： A catalytic combustor 30 includes a frame 32 and catalyst support plate assemblies 34 carried by the frame. A catalyst support plate assembly 34 includes a pair of opposing plates 36A, 36B, at least one having ridges 38A, 38B that define passageways 40 between the pair of opposing plates. A catalyst 44 is carried by the catalyst support plate assemblies 34. Both of the opposing plates 36A, 36B may have ridges 38A, 38B with valleys 42A, 42B between adjacent ridges. A pair of opposing plates 36A, 36B may be aligned and connected at opposing ridges 38A, 38B so that opposing valleys 42A, 42B define air passageways having predetermined shapes. The catalyst support plate assemblies 34 may be arranged in back-to-back relation so that adjacent pairs of catalyst support plate assemblies 34 define fuel/air passageways 46. Adjacent pairs of catalyst support plate assemblies 34 may be offset from one another to define a nested configuration.

9. 发明申请

US20140367925A1 HOT GAS SEAL 审中-公开
标题翻译：热气密封
公开(公告)号：US20140367925A1
公开(公告)日：2014-12-18
申请号：US14184063
申请日：2014-02-19
申请人： Stefan Dahlke , Jesse Eng , John Carl Glessner , Daniel Hofmann , Kenneth Michael Tamaddoni-Jahromi
发明人： Stefan Dahlke , Jesse Eng , John Carl Glessner , Daniel Hofmann , Roland Liebe , Kenneth Michael Tamaddoni-Jahromi
IPC分类号： F16J15/02
CPC分类号： F16J15/028 , F23M5/02 , F23M2900/05005 , F23R3/002 , F23R2900/00012
摘要： A hot gas seal for sealing an opening in a heat shield element or between heat shield elements of a heat shield includes a resilient portion for providing a force which is designed such that the hot gas seal can be held in the opening by the force and/or that the sealing efficiency of the hot gas seal is increased by the force. Further, a hot gas seal assembly for sealing an opening in a heat shield element or between heat shield elements of a heat shield against a hot gas is provided, the assembly including a sealing body and a further sealing element which is in a solid state at room temperature and in a high viscosity liquid state at a temperature of the hot gas.
摘要翻译：用于密封隔热元件中的开口或隔热罩的隔热元件之间的热气体密封件包括用于提供力的弹性部分，其被设计成使得热气体密封件能够通过该力保持在开口中和/ 或者通过力增加热气密封的密封效率。此外，提供了一种用于密封隔热元件中的开口或隔热件的热屏蔽元件与热气体的热气密封组件，该组件包括密封体和另一密封元件，该密封体和固定状态处于固态室温下，在热气体的温度下处于高粘度液体状态。

10. 发明授权

US08695989B2 Hot gas seal 失效
标题翻译：热气密封
公开(公告)号：US08695989B2
公开(公告)日：2014-04-15
申请号：US10837006
申请日：2004-04-30
申请人： Stefan Dahlke , Jesse Eng , John Carl Glessner , Daniel Hofmann , Roland Liebe , Kenneth Michael Tamaddoni-Jahromi
发明人： Stefan Dahlke , Jesse Eng , John Carl Glessner , Daniel Hofmann , Roland Liebe , Kenneth Michael Tamaddoni-Jahromi
IPC分类号： F16J15/02
CPC分类号： F16J15/028 , F23M5/02 , F23M2900/05005 , F23R3/002 , F23R2900/00012
摘要： An inventive hot gas seal for sealing an opening, e.g. a gap or hole, in a heat shield element or between heat shield elements of a heat shield or a liner comprises at least one resilient portion for providing a force which is designed such that the hot gas seal can be held in said opening by said force and/or that the sealing efficiency of the hot gas seal is increased by said force. Thus, further means for holding the seal in place and/or for increasing the sealing efficiency are not necessary. The invention is particularly useful if the design of said resilient portion is such that the force provides a holding action and increases the sealing efficiency, at the same time.
摘要翻译：用于密封开口的本发明的热气密封，例如，隔热元件中的间隙或孔，或隔热罩或衬套的隔热元件之间的间隙或孔包括至少一个用于提供力的弹性部分，该弹性部分被设计成使得热气体密封件能够通过所述力保持在所述开口中和/或通过所述力增加热气密封的密封效率。因此，不需要用于将密封件保持在适当位置和/或用于提高密封效率的另外的装置。如果所述弹性部分的设计使得力同时提供保持作用并提高密封效率，则本发明是特别有用的。

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