公开(公告)号：US06655146B2

公开(公告)日：2003-12-02

申请号：US09919028

申请日：2001-07-31

申请人： Ella Christine Kutter ,  Marwan Al-Roub ,  Thomas Anthony Leen ,  Daniel Dale Brown ,  Craig Douglas Young ,  Gilbert Farmer ,  Mohammad Ehteshami

发明人： Ella Christine Kutter ,  Marwan Al-Roub ,  Thomas Anthony Leen ,  Daniel Dale Brown ,  Craig Douglas Young ,  Gilbert Farmer ,  Mohammad Ehteshami

IPC分类号： F23R306

CPC分类号： F23M5/085 ,  F23R3/06 ,  F23R2900/03042 ,  Y02T50/675

摘要： A combustor liner has an annular shell which includes a first portion and a second portion. The first portion is provided with slot film cooling and the second portion is provided with multi-hole film cooling. The multi-hole cooling portion can be located either forward or aft of the slot film cooling portion, depending on the nature of the combustor that the liner is to be used in. In one possible embodiment, the liner includes a first annular panel, a second annular panel section joined at its forward end to the aft end of the first panel section, and a third annular panel section being joined at its forward end to the aft end of the second panel section. At least one of the panel sections has multi-hole film cooling and at least one other of the panel sections has slot film cooling.

摘要翻译： 燃烧器衬套具有包括第一部分和第二部分的环形壳体。 第一部分设置有槽膜冷却，第二部分设置有多孔膜冷却。 根据待使用的衬套的燃烧器的性质，多孔冷却部分可以位于狭缝膜冷却部分的前部或后部。在一个可能的实施例中，衬套包括第一环形板， 第二环形面板部分在其前端处连接到第一面板部分的后端，并且第三环形面板部分在其前端处连接到第二面板部分的后端。 所述面板部分中的至少一个具有多孔膜冷却，并且所述面板部分中的至少一个具有狭缝膜冷却。

公开(公告)号：US06543233B2

公开(公告)日：2003-04-08

申请号：US09783278

申请日：2001-02-09

申请人： Craig Douglas Young ,  Ella Christine Kutter

发明人： Craig Douglas Young ,  Ella Christine Kutter

IPC分类号： F23R306

CPC分类号： F23R3/50 ,  F23R3/08 ,  Y02T50/675

摘要： A combustor liner for use in a gas turbine engine includes a first annular panel section having a forward end, an aft end and a first cooling nugget located at the forward end thereof, and a second annular panel section having a forward end, an aft end and a second cooling nugget located at the forward end thereof. The second panel section is joined at its forward end to the aft end of the first panel section. A first row of cooling holes is located in the first cooling nugget, and a second row of cooling holes is located in the second cooling nugget. A group of dilution holes is located in the first panel section. The dilution holes are located at the aft end of the first panel section, immediately upstream of the second cooling nugget. Furthermore, each one of the dilution holes defines an aftmost edge, and all of the aftmost edges are axially aligned, even if the dilution holes have different hole diameters.

公开(公告)号：US20130081270A1

公开(公告)日：2013-04-04

申请号：US13249868

申请日：2011-09-30

申请人： David Bruce Patterson ,  Donald Michael Corsmeier ,  Craig Douglas Young ,  Donald Lee Gardner ,  James Edward Thompson ,  Daniel Dale Brown ,  Glenn Edward Wiehe

发明人： David Bruce Patterson ,  Donald Michael Corsmeier ,  Craig Douglas Young ,  Donald Lee Gardner ,  James Edward Thompson ,  Daniel Dale Brown ,  Glenn Edward Wiehe

IPC分类号： B23P17/00 ,  F02C3/14

CPC分类号： F23R3/50 ,  F23R3/002 ,  F23R3/60 ,  Y02E20/16 ,  Y10T29/49229 ,  Y10T29/4932

摘要： A method of assembling a combustion system for a gas turbine engine includes providing a combustion chamber frame, an inner casing structure, and an outer casing structure. The method also includes mounting the combustion chamber frame between the inner casing structure and the outer casing structure such that the combustion chamber frame is coupled to the inner casing structure and the outer casing structure.

摘要翻译： 一种组装燃气涡轮发动机的燃烧系统的方法包括提供燃烧室框架，内壳结构和外壳结构。 该方法还包括将燃烧室框架安装在内壳结构和外壳结构之间，使得燃烧室框架联接到内壳结构和外壳结构。

公开(公告)号：US08893382B2

公开(公告)日：2014-11-25

申请号：US13249868

申请日：2011-09-30

申请人： David Bruce Patterson ,  Donald Michael Corsmeier ,  Craig Douglas Young ,  Donald Lee Gardner ,  James Edward Thompson ,  Daniel Dale Brown ,  Glenn Edward Wiehe ,  Donald Scott Yeager ,  Mark Willard Marusko ,  Michael Joseph Zerbe

发明人： David Bruce Patterson ,  Donald Michael Corsmeier ,  Craig Douglas Young ,  Donald Lee Gardner ,  James Edward Thompson ,  Daniel Dale Brown ,  Glenn Edward Wiehe ,  Donald Scott Yeager ,  Mark Willard Marusko ,  Michael Joseph Zerbe

IPC分类号： B23P17/00 ,  F23R3/50 ,  F23R3/00 ,  F23R3/60

CPC分类号： F23R3/50 ,  F23R3/002 ,  F23R3/60 ,  Y02E20/16 ,  Y10T29/49229 ,  Y10T29/4932

摘要： A method of assembling a combustion system for a gas turbine engine includes providing a combustion chamber frame, an inner casing structure, and an outer casing structure. The method also includes mounting the combustion chamber frame between the inner casing structure and the outer casing structure such that the combustion chamber frame is coupled to the inner casing structure and the outer casing structure.

摘要翻译： 一种组装燃气涡轮发动机的燃烧系统的方法包括提供燃烧室框架，内壳结构和外壳结构。 该方法还包括将燃烧室框架安装在内壳结构和外壳结构之间，使得燃烧室框架联接到内壳结构和外壳结构。

公开(公告)号：US07222488B2

公开(公告)日：2007-05-29

申请号：US10238542

申请日：2002-09-10

申请人： Gilbert Farmer ,  Steven Clayton Vise ,  Walter Byron Houchens, III ,  Craig Douglas Young

发明人： Gilbert Farmer ,  Steven Clayton Vise ,  Walter Byron Houchens, III ,  Craig Douglas Young

IPC分类号： F02C3/06 ,  F02C1/00

CPC分类号： F23R3/10 ,  F23R3/50 ,  F23R2900/00005 ,  F23R2900/00017 ,  F23R2900/00018 ,  Y02T50/675

摘要： A fabricated cowl for a double annular combustor of a gas turbine engine having a longitudinal axis extending therethrough, including an outer annular portion, an inner annular portion, and a middle annular portion. A plurality of circumferentially spaced radial slots are formed in at least one of the annular portions. The outer annular portion includes a plurality of circumferentially spaced windows of desired size formed therein, wherein a plurality of outer radial members connecting the outer annular portion and the middle annular portion are provided between adjacent windows therein. Similarly, the inner annular portion includes a plurality of circumferentially spaced windows of desired size formed therein, wherein a plurality of inner radial members connecting the inner annular portion and the middle annular portion are provided between adjacent windows therein. The cowl further includes a plurality of circumferentially spaced stiffening ribs, where each stiffening rib includes: a middle portion including a rear edge configured to substantially conform to a forward surface of the middle annular portion so that an area extending between the forward and rear edges is upstream of the middle annular portion; an outer portion including a forward edge configured to conform to a rear surface of the outer annular portion; and, an inner portion including a forward edge configured to conform to a rear surface of inner annular portion. The middle rib portion further includes a forward edge configured to extend through the radial slots when positioned in the middle annular portion, whereas the inner and outer rib portions further include a rear edge configured to extend through the radial slots when positioned in the inner and outer annular portions. Each stiffening rib is then connected to the inner, outer and middle annular portions.

摘要翻译： 一种用于燃气涡轮发动机的双环形燃烧器的制造罩，其具有延伸穿过其中的纵向轴线，包括外部环形部分，内部环形部分和中间环形部分。 多个周向间隔开的径向槽形成在至少一个环形部分中。 外环形部分包括形成在其中的多个周向隔开的所需尺寸的窗口，其中连接外环形部分和中间环形部分的多个外径向构件设置在其中的相邻窗口之间。 类似地，内部环形部分包括形成在其中的多个周向间隔开的所需尺寸的窗口，其中连接内部环形部分和中间环形部分的多个内径向构件设置在其中的相邻窗口之间。 整流罩还包括多个周向间隔开的加强肋，其中每个加强肋包括：中间部分，其包括后边缘，该后边缘构造成基本上与中间环形部分的前表面相符，使得在前边缘和后边缘之间延伸的区域是 在中间环形部分的上游; 外部，包括构造成符合所述外环形部分的后表面的前边缘; 以及内部部分，其包括构造成符合内环形部分的后表面的前边缘。 中间肋部分还包括一个前边缘，其构造成当定位在中间环形部分中时延伸穿过径向狭槽，而内部和外侧肋部分还包括后部边缘，该后部边缘被配置为当定位在内部和外侧时延伸穿过径向槽 环形部分。 然后将每个加强肋连接到内，外和中间环形部分。

公开(公告)号：US20080115636A1

公开(公告)日：2008-05-22

申请号：US11560990

申请日：2006-11-17

申请人： Lynn Ann DeRose ,  Douglas Roy Forman ,  Craig Douglas Young ,  Michael Orlando Cimini ,  Gregory Alan Richardson ,  James Nelson Bratton ,  Lee Roy LaPierre

发明人： Lynn Ann DeRose ,  Douglas Roy Forman ,  Craig Douglas Young ,  Michael Orlando Cimini ,  Gregory Alan Richardson ,  James Nelson Bratton ,  Lee Roy LaPierre

IPC分类号： B25B23/144

CPC分类号： B25B23/1425

摘要： A radio identification enabled wrench system is disclosed. The system includes a template having multiple RFID tags. The template also corresponds to a part associated with a particular fastener that is associated with each of the multiple RFID tags. The system further includes a torque wrench having a RFID reader and a RFID antenna and a means for identifying what fastener the wrench is being used upon and whether the correct torque has been applied to the fastener and configured to provide a feedback for a user. The system includes a means for transferring data that may be either wired or wireless.

摘要翻译： 公开了一种无线识别功能的扳手系统。 该系统包括具有多个RFID标签的模板。 模板还对应于与多个RFID标签中的每一个相关联的特定紧固件相关联的部件。 该系统还包括具有RFID读取器和RFID天线的扭矩扳手和用于识别扳手正在使用的紧固件的装置，以及是否将正确的扭矩施加到紧固件并且被配置为向用户提供反馈。 该系统包括用于传送可能是有线或无线的数据的装置。

公开(公告)号：US08439299B2

公开(公告)日：2013-05-14

申请号：US11312410

申请日：2005-12-21

申请人： Huageng Luo ,  Craig Douglas Young

发明人： Huageng Luo ,  Craig Douglas Young

IPC分类号： B64D27/00

CPC分类号： F16F15/005 ,  B64C2220/00 ,  B64D27/00 ,  F16F15/02

摘要： An engine mount structure is provided with active vibration mechanisms which are attached in the vicinity of the engine mount to prevent engine vibrations from propagating into the engine mounting structure, for example, the wing or fuselage structure of an aircraft. Additionally, sensors are provided on the engine and/or wing/fuselage structure to provide control signals to the active vibration mechanisms so that the active vibration mechanism react to the sensed data to minimize the vibration transmissibility from the engine into the wing/fuselage.

摘要翻译： 发动机安装结构设置有主动振动机构，其附接在发动机底座附近，以防止发动机振动传播到发动机安装结构中，例如飞行器的机翼或机身结构。 此外，传感器设置在发动机和/或机翼/机身结构上以向主动振动机构提供控制信号，使得主动振动机构对所感测的数据作出反应，以使从发动机到机翼/机身的振动传递率最小化。

公开(公告)号：US07713021B2

公开(公告)日：2010-05-11

申请号：US11638053

申请日：2006-12-13

申请人： Scott Roger Finn ,  Craig Douglas Young ,  Peter Michael Finnigan

发明人： Scott Roger Finn ,  Craig Douglas Young ,  Peter Michael Finnigan

IPC分类号： F01D1/02 ,  B23P17/00

CPC分类号： F01D21/045 ,  B29C70/222 ,  B29C70/32 ,  B29L2031/3076 ,  B29L2031/7504 ,  F02K3/06 ,  F04D29/526 ,  F05D2300/603 ,  Y02T50/672 ,  Y10T29/49229 ,  Y10T29/49243

摘要： A fan containment casing includes a core comprising a number of tows. The core has a central region and two end regions. The tows are grouped into a number of bands and form a number of filament-wound radially disposed layers. The bands of tows are interleaved as a number of direct bands and indirect bands along at least a portion of one or more of the layers. A method of forming a fan containment casing includes winding a number of tows on a liner to form a number of radially disposed layers, where each of the layers is continuously connected to at least one adjacent one of the layers across one of the end regions via at least one of the tows.

摘要翻译： 风扇容纳壳体包括包括多个丝束的芯。 核心有一个中心区域和两个端部区域。 丝束被分组成多个带，并且形成许多缠绕在径向上的细丝层。 沿着一个或多个层的至少一部分，丝束的带被交织为多个直接带和间接带。 形成风扇容纳壳体的方法包括：在衬套上缠绕多个丝束以形成多个径向设置的层，其中每个层通过一个端部区域中的至少一个相邻层之间连续地连接到经过 至少一个丝束。

公开(公告)号：US06983599B2

公开(公告)日：2006-01-10

申请号：US10777567

申请日：2004-02-12

申请人： Craig Douglas Young ,  Bangalore Aswatha Nagaraj ,  Dane Anthony Elliott-Lewis ,  Joshua Leigh Miller ,  Kevin Swayne O'Hara

发明人： Craig Douglas Young ,  Bangalore Aswatha Nagaraj ,  Dane Anthony Elliott-Lewis ,  Joshua Leigh Miller ,  Kevin Swayne O'Hara

IPC分类号： F23R3/14

CPC分类号： C23C28/3215 ,  C23C4/00 ,  C23C4/02 ,  C23C28/325 ,  C23C28/3455 ,  F23M5/00 ,  F23M2900/05001 ,  F23M2900/05004 ,  F23R3/002 ,  Y02T50/67 ,  Y10T29/49346

摘要： A turbine engine combustor member, for example a deflector including an inner surface at a combustor interior and an outer surface away from such interior includes a body of a high temperature alloy having properties combining resistance to hot corrosion in March=1 flows and oxidation to avoid coating the outer surface. In one embodiment, the inner surface includes an environmental resistant coating comprising a ceramic-base thermal barrier coating. In some forms such coating includes an inner coating including Al under the ceramic-base coating. In another embodiment, the member includes air cooling passages and is substantially uncoated. Provision of such a member enables complete combustor assembly including a plurality of members and then coating all inner surfaces concurrently rather than individually before assembly.

摘要翻译： 涡轮发动机燃烧器构件，例如包括在燃烧器内部的内表面和远离这种内部的外表面的偏转器，包括具有在3月1日流动中抵抗热腐蚀和氧化以避免的性质的高温合金体 涂覆外表面。 在一个实施例中，内表面包括包含陶瓷基热障涂层的耐环境涂层。 在某些形式中，这种涂层包括在陶瓷基涂层下的包括Al的内涂层。 在另一个实施例中，构件包括空气冷却通道并且基本上未涂覆。 提供这种构件使得能够完成燃烧器组件，其包括多个构件，然后同时涂覆所有内表面，而不是在组装之前单独地涂覆。

公开(公告)号：US20090282805A1

公开(公告)日：2009-11-19

申请号：US12122263

申请日：2008-05-16

申请人： Herbert Kopecek ,  Johannes Eckstein ,  Craig Douglas Young

发明人： Herbert Kopecek ,  Johannes Eckstein ,  Craig Douglas Young

IPC分类号： F02C7/264 ,  F23Q7/06 ,  F02P23/04

CPC分类号： F02C7/264 ,  F02P23/04 ,  F23Q13/00 ,  F23R2900/00006

摘要： A gas turbine engine system comprising, a gas turbine engine including a combustion area, a laser, a fuel nozzle including a cavity operative to transmit a fuel into the combustion area, and an optical fiber engaging the cavity, operative to transmit light emitted from the laser to the combustion area, wherein the light is operative to ignite the fuel in the combustion area.

摘要翻译： 一种燃气涡轮发动机系统，包括：燃气涡轮发动机，其包括燃烧区域，激光器，包括用于将燃料输送到燃烧区域中的腔的燃料喷嘴;以及接合所述空腔的光纤， 激光到燃烧区域，其中光可操作地点燃燃烧区域中的燃料。