公开(公告)号：US20120210719A1

公开(公告)日：2012-08-23

申请号：US13463062

申请日：2012-05-03

Applicant: James A. Dierberger ,  Kevin W. Schlichting ,  Melvin Freling

Inventor： James A. Dierberger ,  Kevin W. Schlichting ,  Melvin Freling

IPC: F23R3/42 ,  B23P15/00

CPC classification number: F23R3/007 ,  F23R3/60 ,  F23R2900/00017 ,  F23R2900/00018 ,  Y10T29/49348

Abstract: A combustor assembly includes a support structure and at least one combustor liner panel selectively attached to the support structure. The combustor liner panel includes an uncooled ceramic portion, a cooled ceramic portion and a support that receives the cooled ceramic portion.

公开(公告)号：US08220314B2

公开(公告)日：2012-07-17

申请号：US12754474

申请日：2010-04-05

Applicant: James M. McDonough ,  Ronald J. Meister ,  Michael W. Johnson

Inventor： James M. McDonough ,  Ronald J. Meister ,  Michael W. Johnson

IPC: G01M3/02 ,  G01F25/00 ,  G01P21/00

CPC classification number: F23Q2/163 ,  F23Q2/162 ,  F23Q23/08 ,  Y10T29/49348

Abstract: A lighter device having a flow restrictor and associated methods for manufacturing and testing such lighter device and flow restrictor are described. The flow restrictor may be formed of a porous member to achieve a substantially fixed or varying flame height. The flow restrictor may be tested before or after assembly into a lighter housing by receiving a non-combustible fluid therethrough. The flow rate of the non-combustible fluid may be correlated to the flow rate of a combustible fluid through the flow restrictor to approximate the resultant flame height of a lighter incorporating the tested flow restrictor. The flow restrictor may also be tested by receiving a combustible fluid therethrough prior to assembling the flow restrictor into the lighter housing. In this manner, flow restrictors and corresponding lighter devices may be tested without introducing combustible fluids into such lighter devices prior to shipment. Also, a vacuum may be drawn on a fuel tank of the lighter prior to shipment.

Abstract translation: 描述了一种具有流量限制器的打火机装置和用于制造和测试这种较轻装置和限流器的相关方法。 限流器可以由多孔构件形成，以实现基本固定或变化的火焰高度。 流量限制器可以在组装到更轻的壳体中之前或之后通过从其中接收不可燃流体来测试。 不可燃流体的流速可以与通过限流器的可燃流体的流量相关，以接近结合了测试流量限制器的打火机的合成火焰高度。 在将限流器组装到打​​火机壳体之前，也可以通过接收通过其中的可燃流体来测试流量限制器。 以这种方式，可以测试流量限制器和对应的较轻的装置，而不会在装运前将可燃流体引入这种较轻的装置中。 此外，在装运前可以在打火机的燃料箱上抽真空。

公开(公告)号：US20120152231A1

公开(公告)日：2012-06-21

申请号：US13375871

申请日：2010-06-09

Applicant: Martin Johan Van Der Sluis ,  Paul Van Der Kooi

Inventor： Martin Johan Van Der Sluis ,  Paul Van Der Kooi

IPC: F24C3/08 ,  B23P11/00 ,  F24C15/10

CPC classification number: F24C15/107 ,  F24C3/085 ,  Y10T29/49348 ,  Y10T29/49826

Abstract: The present invention relates to a burner module for a cooker and a cooker and a method for such a burner module. The burner module according to the invention comprises: a carrier with which the burner module can be placed as a unit on a worktop; an outlet for gas provided on the carrier; an inlet provided on the carrier for supplying gas; and control means provided between an inlet and the outlet for realizing a gas flame.

Abstract translation: 本发明涉及一种用于炊具和炊具的燃烧器模块以及这种燃烧器模块的方法。 根据本发明的燃烧器模块包括：载体，燃烧器模块可以作为一个单元放置在工作台上; 提供在载体上的气体出口; 设置在载体上用于供应气体的入口; 以及设置在入口和出口之间用于实现气体火焰的控制装置。

公开(公告)号：US08147240B2

公开(公告)日：2012-04-03

申请号：US12405842

申请日：2009-03-17

Applicant: David C. Lyons ,  Travis P. Betcher ,  Louis L. Mead

Inventor： David C. Lyons ,  Travis P. Betcher ,  Louis L. Mead

IPC: F23Q2/32 ,  F23D14/46 ,  F23D14/62 ,  F23C7/00 ,  F24B1/18

CPC classification number: F23D14/84 ,  F23D14/586 ,  F23D2203/108 ,  F23D2212/00 ,  F23D2212/10 ,  F23D2213/00 ,  F23D2900/21004 ,  F24C3/082 ,  F24C15/004 ,  Y10T29/49348 ,  Y10T29/53

Abstract: A gas burner assembly includes a first sheet, a second sheet, and a conduit. The first sheet has an inner face, an outer face, an upper portion, and a lower portion. The second sheet also has an inner face, an outer face, an upper portion and a lower portion. The first and second sheets are secured relative to one another such that the first and second sheets are separated by a gap that defines a manifold between the inner faces of the first and second sheets with an elongate opening between the upper portions of the first and second sheets, the opening forming an outlet from the manifold. The conduit is in communication with the manifold, the conduit being adapted for connection to a source of gas.

Abstract translation: 气体燃烧器组件包括第一片，第二片和导管。 第一片具有内表面，外表面，上部和下部。 第二片也具有内表面，外表面，上部和下部。 第一和第二片相对于彼此固定，使得第一和第二片由在第一和第二片的内表面之间限定歧管的间隙分开，在第一和第二片的上部之间具有细长的开口 片材，该开口形成从歧管的出口。 导管与歧管连通，导管适于与气源连接。

公开(公告)号：US20110185572A1

公开(公告)日：2011-08-04

申请号：US12697005

申请日：2010-01-29

Applicant: Bin Wei ,  Jon Conrad Schaeffer ,  Ronald Scott Bunker ,  Wenwu Zhang ,  Kathleen Blanche Morey ,  Jane Marie Lipkin ,  Benjamin Paul Lacy ,  Wilbur Douglas Scheidt

Inventor： Bin Wei ,  Jon Conrad Schaeffer ,  Ronald Scott Bunker ,  Wenwu Zhang ,  Kathleen Blanche Morey ,  Jane Marie Lipkin ,  Benjamin Paul Lacy ,  Wilbur Douglas Scheidt

IPC: B21D53/00 ,  B23P17/00 ,  B23K26/00

CPC classification number: F02C7/18 ,  B23K26/0624 ,  B23K26/082 ,  B23K26/384 ,  B23K26/389 ,  B23K26/60 ,  B23K26/702 ,  B23K2101/001 ,  B23K2101/34 ,  F01D25/12 ,  F05D2230/00 ,  F05D2230/13 ,  Y10T29/49316 ,  Y10T29/4932 ,  Y10T29/49336 ,  Y10T29/49339 ,  Y10T29/49341 ,  Y10T29/49348 ,  Y10T29/49799

Abstract: A process and system are provided for forming shaped air holes, such as for use in turbine blades. Aspects of the disclosure relate to forming shaped portions of air holes using a short pulse laser, forming a metered hole corresponding to each shaped portion, and separately finishing the shaped portion using a short-pulse laser. In other embodiments, the order of these operations may be varied, such as to form the shaped portions and to finish the shaped portions using the short-pulse laser prior to forming the corresponding metered holes.

Abstract translation: 提供了用于形成诸如用于涡轮叶片的成形气孔的过程和系统。 本公开的方面涉及使用短脉冲激光器形成空气孔的成形部分，形成与每个成形部分相对应的计量孔，并且使用短脉冲激光单独精加工成形部分。 在其他实施例中，可以改变这些操作的顺序，诸如形成成形部分，并且在形成相应的计量孔之前使用短脉冲激光来完成成形部分。

公开(公告)号：US20110174299A1

公开(公告)日：2011-07-21

申请号：US12834145

申请日：2010-07-12

Applicant: Donald N. Zimmer

Inventor： Donald N. Zimmer

IPC: F24C3/00 ,  F28F7/00 ,  B21D53/02

CPC classification number: B23P15/00 ,  B29C45/18 ,  B29L2031/18 ,  F23D14/34 ,  F23D14/58 ,  F23D2900/14481 ,  F24H3/087 ,  F24H8/006 ,  F24H9/2035 ,  F25D21/14 ,  Y02B30/106 ,  Y10T29/49 ,  Y10T29/49348 ,  Y10T29/4935 ,  Y10T29/49389 ,  Y10T29/49826 ,  Y10T137/4463

Abstract: One aspect of this disclosure provides a heat exchanger that comprises a first panel half coupled to a corresponding second panel half that form a passageway having at least a first chamber adjacent an inlet end of the passageway and a second chamber and overlapping interference patterns formed in each of the first and second panel halves that extend along at least a portion of the length of the passageway and located between at least the first and second chambers.

Abstract translation: 本公开的一个方面提供一种热交换器，其包括联接到相应的第二面板半部的第一面板半部，所述第二面板半部形成通道，所述通道具有邻近通道的入口端的至少第一室，以及形成在每个中的第二室和重叠的干涉图案 所述第一和第二面板半部沿所述通道的至少一部分长度延伸并位于至少所述第一和第二腔室之间。

公开(公告)号：US20100266225A1

公开(公告)日：2010-10-21

申请号：US12827014

申请日：2010-06-30

Applicant: Nobuyoshi Yamashita ,  Natsuhiko Mori ,  Toshiyuki Mizutani ,  Takeshi Shimazaki ,  Koji Yamagata

Inventor： Nobuyoshi Yamashita ,  Natsuhiko Mori ,  Toshiyuki Mizutani ,  Takeshi Shimazaki ,  Koji Yamagata

IPC: F16C32/06

CPC classification number: B24B5/01 ,  B21K1/12 ,  B24B7/16 ,  F16C3/02 ,  F16C17/107 ,  F16C33/107 ,  F16C33/14 ,  F16C35/02 ,  F16C2220/46 ,  F16C2220/70 ,  F16C2226/12 ,  F16C2226/60 ,  Y10T29/49348

Abstract: A shaft member for hydrodynamic bearing apparatuses which can restore the pressure balance in a thrust bearing gap formed on both axial sides of the flange portion in an early stage is provided at low costs.A shaft material 10 integrally having a shaft portion 11 and a flange portion 12 is formed as a through-hole 19 opening to its both end faces 12a, 12b on the flange portion 12 of the shaft material 10 is formed in a common forging step. As a result, the through-hole 29 is formed to open to the inner diameter side of these bearing gap W1, W2 avoiding thrust bearing gaps W1, W2 formed on both end faces of the flange portion 22 of the shaft member 2 as a finished product.

Abstract translation: 能够以低成本提供用于流体动力轴承装置的轴构件，其能够在早期阶段恢复形成在凸缘部的两个轴向侧上的推力轴承间隙中的压力平衡。 形成有轴部11和凸缘部12一体地形成的轴材10，在通常的锻造工序中形成有贯通孔19，该贯通孔19在轴材10的凸缘部12上的两端面12a，12b开口。 结果，通孔29形成为向这些轴承间隙W1，W2的内径侧开口，避免形成在轴构件2的凸缘部22的两个端面上的推力轴承间隙W1，W2作为成品 产品。

公开(公告)号：US07716931B2

公开(公告)日：2010-05-18

申请号：US11364914

申请日：2006-03-01

Applicant: Alfred A. Mancini ,  David L. Burrus ,  Steven J. Lohmueller

Inventor： Alfred A. Mancini ,  David L. Burrus ,  Steven J. Lohmueller

IPC: F02C1/00

CPC classification number: F23R3/286 ,  F23R3/14 ,  F23R3/343 ,  F23R3/50 ,  F23R3/52 ,  Y02T50/675 ,  Y10T29/49348

Abstract: A method for assembling a gas turbine engine is provided. The method includes providing a combustor having a combustor liner assembly defining a combustion chamber. An outer combustor liner includes a radially extending first end that defines a combustion chamber input opening. An axially extending second end of the outer combustor liner defines a combustion chamber output opening. The first end transitions into the second end to form an arcuate cross-sectional shape of the outer combustor liner. A dome assembly is coupled to the first end of the combustor liner that extends downstream from the dome assembly. A fuel nozzle is positioned within a cyclone formed on the dome assembly and configured in a radial configuration.

Abstract translation: 提供一种用于组装燃气涡轮发动机的方法。 该方法包括提供具有限定燃烧室的燃烧器衬套组件的燃烧器。 外部燃烧器衬套包括限定燃烧室输入开口的径向延伸的第一端。 外燃烧器衬套的轴向延伸的第二端限定燃烧室输出开口。 第一端过渡到第二端以形成外部燃烧器衬套的弓形横截面形状。 圆顶组件联接到从圆顶组件的下游延伸的燃烧器衬套的第一端。 燃料喷嘴定位在形成在圆顶组件上的旋风分离器中并且被配置成径向构型。

公开(公告)号：US20100081100A1

公开(公告)日：2010-04-01

申请号：US12243916

申请日：2008-10-01

Applicant: John W. Olver ,  Jason Andrew Simmons

Inventor： John W. Olver ,  Jason Andrew Simmons

IPC: F23D11/00 ,  B21D53/00

CPC classification number: F23D1/00 ,  F23D2201/10 ,  F23D2201/20 ,  F23D2201/30 ,  Y10T29/49348

Abstract: A burner tip, and method of manufacture, has a support layer with an external surface and an internal surface defining at least one opening therethrough defining a passage therethrough to deliver fuel and combustion gasses, and a thermal protective layer disposed on at least one surface of the burner tip support layer. The thermal protective layer 22 has from about 5% to about 40% of an inorganic adhesive, from about 45% to about 92% of a filler, and from about 1% to about 20% of one or more emissivity agents.

Abstract translation: 燃烧器尖端和制造方法具有支撑层，其具有外表面和内表面，该内表面限定穿过其中的至少一个开口，其中穿过其中的通道以输送燃料和燃烧气体，以及设置在至少一个表面上的热保护层 燃烧器尖端支撑层。 热保护层22具有约5％至约40％的无机粘合剂，约45％至约92％的填料和约1％至约20％的一种或多种发射剂。

公开(公告)号：US20100078408A1

公开(公告)日：2010-04-01

申请号：US12241922

申请日：2008-09-30

Applicant: Stephen M. Liebold ,  Brian J. Currier

Inventor： Stephen M. Liebold ,  Brian J. Currier

IPC: B23K9/00 ,  B21D53/00

CPC classification number: H05H1/28 ,  H05H1/34 ,  Y10T29/49348

Abstract: A nozzle for a plasma torch can include a body that has an inner surface, an outer surface, a proximal end, and an exit orifice at a distal end. The nozzle can also include a liner surrounded by the inner surface of the body. The liner can include a proximal end and an exit orifice at a distal end adjacent the exit orifice of the body. The nozzle can include at least one vent passage formed in the body. The vent passage can have an inlet formed in the inner surface of the body and an outlet formed in the outer surface of the body. The vent passage can be disposed between the proximal end of the body and the proximal end of the liner. The plasma arc torch can include a configuration that allows for increased electrode life and nozzle life for a vented high current plasma process.

Abstract translation: 用于等离子体焰炬的喷嘴可以包括在远端具有内表面，外表面，近端和出口的主体。 喷嘴还可以包括由主体的内表面包围的衬里。 衬垫可以包括在靠近身体的出口的远端处的近端和出口孔。 喷嘴可以包括形成在主体中的至少一个排气通道。 排气通道可以具有形成在主体的内表面中的入口和形成在主体的外表面中的出口。 排气通道可以设置在主体的近端和衬套的近端之间。 等离子弧焊炬可以包括允许通气的高电流等离子体工艺增加电极寿命和喷嘴寿命的构造。