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41. 发明授权

US08234871B2 Method and apparatus for delivery of a fuel and combustion air mixture to a gas turbine engine using fuel distribution grooves in a manifold disk with discrete air passages 有权
标题翻译：用于使用具有离散空气通道的歧管盘中的燃料分配槽将燃料和燃烧空气混合物输送到燃气涡轮发动机的方法和装置
公开(公告)号：US08234871B2
公开(公告)日：2012-08-07
申请号：US12406216
申请日：2009-03-18
申请人： Lewis Berkley Davis, Jr. , Thomas Edward Johnson , Jason Thurman Stewart
发明人： Lewis Berkley Davis, Jr. , Thomas Edward Johnson , Jason Thurman Stewart
IPC分类号： F02C7/22
CPC分类号： F23R3/286 , F23R3/12
摘要： A nozzle has combustion air passages extending from a first, upstream end to a second, downstream end. A fuel distribution manifold is associated with the first, upstream end of the nozzle. Combustion air passages correspond to, and align with the air passages in the nozzle. Fuel distribution grooves are formed in one end of the fuel distribution manifold disk and extend from a central opening to the air passages. A fuel circuit cover closes the fuel distribution grooves to define fuel passages that extend from the central opening to the combustion air passages. A fuel supply conduit communicates with the central opening and the fuel passages for delivery of fuel to the combustion air in the air passages.
摘要翻译：喷嘴具有从第一上游端延伸到第二下游端的燃烧空气通道。燃料分配歧管与喷嘴的第一上游端相关联。燃烧空气通道对应于喷嘴中的空气通道并对齐。燃料分配槽形成在燃料分配歧管盘的一端并从中心开口延伸到空气通道。燃料回路盖封闭燃料分配槽以限定从中心开口延伸到燃烧空气通道的燃料通道。燃料供应管道与中心开口和燃料通道连通，用于将燃料输送到空气通道中的燃烧空气。

42. 发明授权

US08209986B2 Multi-tube thermal fuse for nozzle protection from a flame holding or flashback event 有权
标题翻译：多管式热保险丝，用于喷嘴保护，防止火焰持续或闪回事件
公开(公告)号：US08209986B2
公开(公告)日：2012-07-03
申请号：US12260451
申请日：2008-10-29
申请人： Benjamin Paul Lacy , Lewis Berkley Davis, Jr. , Thomas Edward Johnson , William David York
发明人： Benjamin Paul Lacy , Lewis Berkley Davis, Jr. , Thomas Edward Johnson , William David York
IPC分类号： F02C1/00
CPC分类号： F23R3/286 , F23D14/82 , F23D2900/00018 , Y10T29/49433
摘要： A protection system for a pre-mixing apparatus for a turbine engine, includes: a main body having an inlet portion, an outlet portion and an exterior wall that collectively establish a fuel delivery plenum; and a plurality of fuel mixing tubes that extend through at least a portion of the fuel delivery plenum, each of the plurality of fuel mixing tubes including at least one fuel feed opening fluidly connected to the fuel delivery plenum; at least one thermal fuse disposed on an exterior surface of at least one tube, the at least one thermal fuse including a material that will melt upon ignition of fuel within the at least one tube and cause a diversion of fuel from the fuel feed opening to at least one bypass opening. A method and a turbine engine in accordance with the protection system are also provided.
摘要翻译：一种用于涡轮发动机的预混合装置的保护系统，包括：主体，其具有共同建立燃料输送增压室的入口部分，出口部分和外壁; 以及多个燃料混合管，其延伸穿过所述燃料输送室的至少一部分，所述多个燃料混合管中的每一个包括流体连接到所述燃料输送室的至少一个燃料供给开口; 至少一个热熔丝设置在至少一个管的外表面上，所述至少一个热熔丝包括将在所述至少一个管内的燃料点燃时熔化的材料，并导致燃料从所述燃料供给口转向至少一个旁路开口。还提供了根据保护系统的方法和涡轮发动机。

43. 发明申请

US20120006033A1 Combustor and Combustor Screech Mitigation Methods 有权
标题翻译：燃烧器和燃烧器铲风缓解方法
公开(公告)号：US20120006033A1
公开(公告)日：2012-01-12
申请号：US12833237
申请日：2010-07-09
申请人： Kwanwoo Kim , Thomas Edward Johnson , Jong Ho Uhm , Gilbert Otto Kraemer
发明人： Kwanwoo Kim , Thomas Edward Johnson , Jong Ho Uhm , Gilbert Otto Kraemer
IPC分类号： F02C7/22
CPC分类号： F23R3/28 , F23C5/08 , F23R2900/00014
摘要： The present application provides for a combustor for use with a gas turbine engine. The combustor may include a cap member and a number of fuel nozzles extending through the cap member. One or more of the fuel nozzles may be provided in a non-flush position with respect to the cap member.
摘要翻译：本申请提供了一种与燃气涡轮发动机一起使用的燃烧器。燃烧器可以包括盖构件和延伸穿过帽构件的多个燃料喷嘴。一个或多个燃料喷嘴可以相对于盖构件设置在非冲洗位置。

44. 发明申请

US20110225947A1 SYSTEM AND METHODS FOR ALTERING AIR FLOW IN A COMBUSTOR 审中-公开
标题翻译：用于改变燃烧器中的空气流的系统和方法
公开(公告)号：US20110225947A1
公开(公告)日：2011-09-22
申请号：US12725602
申请日：2010-03-17
申请人： Benjamin Paul Lacy , Roy Marshall Washam , Thomas Edward Johnson
发明人： Benjamin Paul Lacy , Roy Marshall Washam , Thomas Edward Johnson
IPC分类号： F23R3/26 , F02C3/14 , F02C7/22
CPC分类号： F23R3/26 , F23R3/286
摘要： A combustor assembly of a turbine engine is provided with a mechanical air regulation unit which selectively varies the amount of air being delivered into a combustion zone of the combustor based upon a pressure of a fuel being supplied to the combustor. A first type of air regulation unit would act to increase the amount of air entering the combustion zone when greater amounts of a high heat value fuel are being delivered to the fuel nozzles of the combustor. A second type of air regulation unit could act to decrease the amount of air entering the combustion zone when greater amounts of a low heat value fuel are being delivered into the combustor through fuel nozzles.
摘要翻译：涡轮发动机的燃烧器组件设置有机械空气调节单元，其基于供应到燃烧器的燃料的压力选择性地改变被输送到燃烧器的燃烧区域中的空气量。当更大量的高热值燃料被输送到燃烧器的燃料喷嘴时，第一类型的空气调节单元将用于增加进入燃烧区域的空气量。当较大量的低热值燃料通过燃料喷嘴输送到燃烧器中时，第二类型的空气调节单元可以起到减少进入燃烧区域的空气量的作用。

45. 发明申请

US20110179795A1 INJECTOR WITH INTEGRATED RESONATOR 有权
标题翻译：具有集成谐振器的注射器
公开(公告)号：US20110179795A1
公开(公告)日：2011-07-28
申请号：US12499777
申请日：2009-07-08
申请人： Thomas Edward Johnson , Willy Steve Ziminsky , William David York , Christian Xavier Stevenson
发明人： Thomas Edward Johnson , Willy Steve Ziminsky , William David York , Christian Xavier Stevenson
IPC分类号： F02C7/24
CPC分类号： F23R3/28 , F23R2900/00014
摘要： The system may include a turbine engine. The turbine engine may include a fuel nozzle. The fuel nozzle may include an air path. The fuel nozzle may also include a fuel path such that the fuel nozzle is in communication with a combustion zone of the turbine engine. Furthermore, the fuel nozzle may include a resonator. The resonator may be disposed in the fuel nozzle directly adjacent to the combustion zone.
摘要翻译：该系统可以包括涡轮发动机。涡轮发动机可以包括燃料喷嘴。燃料喷嘴可以包括空气路径。燃料喷嘴还可以包括燃料路径，使得燃料喷嘴与涡轮发动机的燃烧区域连通。此外，燃料喷嘴可以包括谐振器。谐振器可以直接邻近燃烧区设置在燃料喷嘴中。

46. 发明申请

US20100263386A1 TURBINE ENGINE HAVING A LINER 审中-公开
标题翻译：具有内衬的涡轮发动机
公开(公告)号：US20100263386A1
公开(公告)日：2010-10-21
申请号：US12425229
申请日：2009-04-16
申请人： Kara Johnston Edwards , Thomas Edward Johnson
发明人： Kara Johnston Edwards , Thomas Edward Johnson
IPC分类号： F02C7/20 , F02C1/00
CPC分类号： F23R3/60 , F23R3/002
摘要： In one embodiment, a combustor of a turbine system may include a liner disposed inside the combustor. The lining element may include a heat shield having a mounting stud extending along an axis and a shell having an inner surface oriented towards the heat shield. The shell may include a passage configured to receive the mounting stud, and the mounting stud may include a structure configured to hold the heat shield apart from the inner surface of the shell along the axis of the mounting stud.
摘要翻译：在一个实施例中，涡轮机系统的燃烧器可以包括设置在燃烧器内部的衬套。衬里元件可以包括具有沿轴线延伸的安装螺柱的隔热罩和具有朝向隔热罩定向的内表面的外壳。外壳可以包括构造成接收安装螺柱的通道，并且安装螺柱可以包括构造成沿着安装螺柱的轴线将隔热罩与壳体的内表面隔开的结构。

47. 发明申请

US20100154436A1 Forward sleeve retainer plate and method 失效
标题翻译：前套保持板和方法
公开(公告)号：US20100154436A1
公开(公告)日：2010-06-24
申请号：US12656951
申请日：2010-02-22
申请人： Thomas Edward Johnson , James Thomas Brown
发明人： Thomas Edward Johnson , James Thomas Brown
IPC分类号： F02C7/20
CPC分类号： F01D9/023 , F05D2230/232
摘要： In a combustor section, wherein a forward sleeve is disposed to encircle a leading end of an impingement sleeve comprised of first and second impingement sleeve parts abutted along a longitudinal junction thereof, a retainer member disposed to overlie the longitudinal junction. The retainer member is welded to at least one of said forward sleeve and the impingement sleeve. The retainer member has first and second axial end edges disposed transverse to the longitudinal junction, and at least one of the axial end edges has a cutout defined therein and disposed to overlie the longitudinal junction.
摘要翻译：在燃烧器部分中，其中前套筒设置成环绕冲击套筒的前端，所述冲击套筒包括沿其纵向接合部邻接的第一和第二冲击套筒部件，设置成覆盖在纵向连接部上的保持器部件。保持器构件焊接到所述前部套筒和冲击套筒中的至少一个上。保持器构件具有横向于纵向接合部设置的第一和第二轴向端边缘，并且轴向端部边缘中的至少一个具有限定在其中的切口并且设置成覆盖纵向接合部。

48. 发明申请

US20100139280A1 MULTI-TUBE THERMAL FUSE FOR NOZZLE PROTECTION FROM A FLAME HOLDING OR FLASHBACK EVENT 有权
标题翻译：多管式保险丝，用于从火焰保持或闪回事件中进行喷嘴保护
公开(公告)号：US20100139280A1
公开(公告)日：2010-06-10
申请号：US12260451
申请日：2008-10-29
申请人： Benjamin Paul Lacy , Lewis Berkley Davis, JR. , Thomas Edward Johnson , William David York
发明人： Benjamin Paul Lacy , Lewis Berkley Davis, JR. , Thomas Edward Johnson , William David York
IPC分类号： F02C7/00 , B23P15/16
CPC分类号： F23R3/286 , F23D14/82 , F23D2900/00018 , Y10T29/49433
摘要： A protection system for a pre-mixing apparatus for a turbine engine, includes: a main body having an inlet portion, an outlet portion and an exterior wall that collectively establish a fuel delivery plenum; and a plurality of fuel mixing tubes that extend through at least a portion of the fuel delivery plenum, each of the plurality of fuel mixing tubes including at least one fuel feed opening fluidly connected to the fuel delivery plenum; at least one thermal fuse disposed on an exterior surface of at least one tube, the at least one thermal fuse including a material that will melt upon ignition of fuel within the at least one tube and cause a diversion of fuel from the fuel feed opening to at least one bypass opening. A method and a turbine engine in accordance with the protection system are also provided.
摘要翻译：一种用于涡轮发动机的预混合装置的保护系统，包括：主体，其具有共同建立燃料输送增压室的入口部分，出口部分和外壁; 以及多个燃料混合管，其延伸穿过所述燃料输送室的至少一部分，所述多个燃料混合管中的每一个包括流体连接到所述燃料输送室的至少一个燃料供给开口; 至少一个热熔丝设置在至少一个管的外表面上，所述至少一个热熔丝包括将在所述至少一个管内的燃料点燃时熔化的材料，并导致燃料从所述燃料供给口转向至少一个旁路开口。还提供了根据保护系统的方法和涡轮发动机。

49. 发明授权

US09010083B2 Apparatus for mixing fuel in a gas turbine 有权
标题翻译：用于在燃气轮机中混合燃料的装置
公开(公告)号：US09010083B2
公开(公告)日：2015-04-21
申请号：US13020156
申请日：2011-02-03
申请人： Jong Ho Uhm , Thomas Edward Johnson
发明人： Jong Ho Uhm , Thomas Edward Johnson
IPC分类号： F23R3/16 , F23R3/28 , F23D14/62
CPC分类号： F23R3/286 , F23D14/62 , F23R3/16 , F23R2900/00004 , F23R2900/00005
摘要： A combustor nozzle includes an inlet surface and an outlet surface downstream from the inlet surface, wherein the outlet surface has an indented central portion. A plurality of fuel channels are arranged radially outward of the indented central portion, wherein the plurality of fuel channels extend through the outlet surface.
摘要翻译：燃烧器喷嘴包括从入口表面下游的入口表面和出口表面，其中出口表面具有凹入的中心部分。多个燃料通道布置在凹陷中心部分的径向外侧，其中多个燃料通道延伸穿过出口表面。

50. 发明授权

US08984888B2 Fuel injection assembly for use in turbine engines and method of assembling same 有权
标题翻译：用于涡轮发动机的燃油喷射组件及其组装方法
公开(公告)号：US08984888B2
公开(公告)日：2015-03-24
申请号：US13281679
申请日：2011-10-26
申请人： Jong Ho Uhm , Thomas Edward Johnson
发明人： Jong Ho Uhm , Thomas Edward Johnson
IPC分类号： F02C1/00 , F02G3/00 , F23R3/28 , F23R3/10 , F23R3/34
CPC分类号： F23R3/283 , F23R3/10 , F23R3/34 , F23R3/346 , Y10T29/49231
摘要： A fuel injection assembly for use in a turbine engine is provided. The fuel injection assembly includes a plurality of tube assemblies, wherein each of the tube assemblies includes an upstream portion and a downstream portion. Each tube assembly includes a plurality of tubes that extend from the upstream portion to the downstream portion or from the upstream portion through the downstream portion. At least one injection system is coupled to at least one tube assembly of the plurality of tube assemblies. The injection system includes a fluid supply member that extends from a fluid source to the downstream portion of the tube assembly. The fluid supply member includes a first end portion located in the downstream portion of the tube assembly, wherein the first end portion has at least one first opening for channeling fluid through the tube assembly to facilitate reducing a temperature therein.
摘要翻译：提供了一种用于涡轮发动机的燃料喷射组件。燃料喷射组件包括多个管组件，其中每个管组件包括上游部分和下游部分。每个管组件包括从上游部分延伸到下游部分或从上游部分穿过下游部分延伸的多个管。至少一个注射系统联接到多个管组件的至少一个管组件。注射系统包括从流体源延伸到管组件的下游部分的流体供应构件。流体供应构件包括位于管组件的下游部分中的第一端部，其中第一端部具有至少一个第一开口，用于将流体引导通过管组件，以有助于降低其中的温度。

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