公开(公告)号：US09677180B2

公开(公告)日：2017-06-13

申请号：US13336394

申请日：2011-12-23

Applicant: Subhash K. Naik ,  Charles J. Teague ,  James Carl Loebig

Inventor： Subhash K. Naik ,  Charles J. Teague ,  James Carl Loebig

IPC: C23C28/04 ,  C23C28/00 ,  F01D5/28

CPC classification number: C23C28/042 ,  C23C28/044 ,  C23C28/3215 ,  C23C28/345 ,  C23C28/3455 ,  F01D5/288 ,  F05D2220/3212 ,  F05D2300/504 ,  F05D2300/611 ,  Y02T50/67

Abstract: One embodiment of the present invention is a unique engine hot section component having a coating system operative to reduce heat transfer to the hot section component. Another embodiment is a unique method for making a gas turbine engine hot section component with a coating system. Other embodiments include apparatuses, systems, devices, hardware, methods, and combinations for gas turbine engines, hot section components and coating systems. Further embodiments, forms, features, aspects, benefits, and advantages of the present application shall become apparent from the description and figures provided herewith.

公开(公告)号：US20110299065A1

公开(公告)日：2011-12-08

申请号：US12981317

申请日：2010-12-29

Applicant: James Carl Loebig ,  Jefre H. Cockerham ,  Emil R. Dejulio ,  James E. McDonald

Inventor： James Carl Loebig ,  Jefre H. Cockerham ,  Emil R. Dejulio ,  James E. McDonald

IPC: G01J3/00 ,  G01J1/00

CPC classification number: G01J5/0088 ,  G01J5/048 ,  G01J5/0803 ,  G01J5/0806 ,  G01J5/0821

Abstract: One embodiment of the present invention is a unique system for measuring radiant energy in gas turbine engines, gas turbine engine components and gas turbine engine/component rigs. Another embodiment is a unique method for measuring radiant energy in gas turbine engines, gas turbine engine components and gas turbine engine/component rigs. Other embodiments include apparatuses, systems, devices, hardware, methods, and combinations for measuring radiant energy. Further embodiments, forms, features, aspects, benefits, and advantages of the present application shall become apparent from the description and figures provided herewith.

Abstract translation: 本发明的一个实施例是用于测量燃气涡轮发动机，燃气涡轮发动机部件和燃气涡轮发动机/部件钻机中的辐射能的独特系统。 另一个实施例是用于测量燃气涡轮发动机，燃气涡轮发动机部件和燃气涡轮发动机/部件钻机中的辐射能的独特方法。 其他实施例包括用于测量辐射能的装置，系统，装置，硬件，方法和组合。 本申请的其他实施例，形式，特征，方面，益处和优点将从本文提供的描述和图中变得显而易见。

公开(公告)号：US06606854B1

公开(公告)日：2003-08-19

申请号：US09551728

申请日：2000-04-18

Applicant: Robert G. Siefker ,  Baily Ramachandra Vittal ,  Von David Baker ,  Syed Arif Khalid ,  James Carl Loebig

Inventor： Robert G. Siefker ,  Baily Ramachandra Vittal ,  Von David Baker ,  Syed Arif Khalid ,  James Carl Loebig

IPC: F02K148

CPC classification number: F02K1/48 ,  B63G13/02 ,  B63H21/34 ,  F02K1/386 ,  F05D2250/25 ,  Y02T50/672

Abstract: Disclosed is an exhaust mixer (50) including a passage (54) extending from an inlet (56) to an outlet (58) that is coincident with a centerline axis of mixer (50). Several ridges (68) are circumferentially disposed about the axis and each flare away from the centerline axis relative to a direction along the centerline axis from inlet (56) toward outlet (58). Ridges (68) each define a corresponding one of several inner channels (74) radially disposed about passage (54) that each intersect passage (54) between inlet (56) and outlet (58). Several outer channels (84) are also radially disposed about passage(54) and are each positioned between a corresponding pair of inner channels (74). Ridges are each shaped to turn inner channels (74and outer channels (84) about the axis as ridges (68) extend along the indicated direction. Inner channels (74) diverge away from the axis and one another in this direction while outer channels (84) converge toward the axis and one another in this direction.

Abstract translation: 公开了一种排气混合器（50），其包括从入口（56）延伸到与混合器（50）的中心线轴线重合的出口（58）的通道（54）。 围绕轴线周向地布置有多个脊部68，并且每个脊部沿着中心线轴线相对于从入口（56）朝向出口（58）的中心线轴线的方向远离。 脊（68）各自限定围绕通道（54）径向设置的几个内通道（74）中的相应的一个，每个内通道（74）各自在入口（56）和出口（58）之间相交通道（54）。 几个外通道（84）也围绕通道（54）径向设置，并且分别位于相应的一对内通道（74）之间。 脊部各自被成形为当脊（68）沿着指示的方向延伸时围绕轴线转动内部通道（74和外部通道（84））。内部通道（74）在该方向上沿轴线彼此偏离，而外部通道 ）在这个方向上朝着轴线并且彼此会聚。

公开(公告)号：US20170342863A1

公开(公告)日：2017-11-30

申请号：US15073282

申请日：2016-03-17

Applicant: James C. Muskat ,  Todd S. Taylor ,  Mike Nesteroff ,  Eric Donovan ,  James Carl Loebig

Inventor： James C. Muskat ,  Todd S. Taylor ,  Mike Nesteroff ,  Eric Donovan ,  James Carl Loebig

IPC: F01D25/30 ,  F01D9/04 ,  F01D11/00

CPC classification number: F01D25/305 ,  F01D9/041 ,  F01D11/003 ,  F02K1/386 ,  F02K1/825 ,  F05D2220/323 ,  F05D2260/96

Abstract: Systems and methods for suppressing infrared radiation generated by a turbine engine. A system comprises a primary assembly having a center body, a plurality of vanes extending from the center body, an outer radial duct with the plurality of vanes extending therethrough, a structural baffle, and a mixer. The primary assembly is disposed in the exhaust flow path of a turbine engine and encased in ducting and/or an airfoil. An air flow path defined between the center body and outer radial duct is axially spit by an interface rim and flow segregator. The flow segregator segregates engine core flow from ambient air flow.

公开(公告)号：US08946635B2

公开(公告)日：2015-02-03

申请号：US12981317

申请日：2010-12-29

Applicant: James Carl Loebig ,  Jefre H. Cockerham ,  Emil R. Dejulio ,  James E. McDonald

Inventor： James Carl Loebig ,  Jefre H. Cockerham ,  Emil R. Dejulio ,  James E. McDonald

IPC: G01J5/00 ,  G01J5/04 ,  G01J5/08

CPC classification number: G01J5/0088 ,  G01J5/048 ,  G01J5/0803 ,  G01J5/0806 ,  G01J5/0821

Abstract: One embodiment of the present invention is a unique system for measuring radiant energy in gas turbine engines, gas turbine engine components and gas turbine engine/component rigs. Another embodiment is a unique method for measuring radiant energy in gas turbine engines, gas turbine engine components and gas turbine engine/component rigs. Other embodiments include apparatuses, systems, devices, hardware, methods, and combinations for measuring radiant energy. Further embodiments, forms, features, aspects, benefits, and advantages of the present application shall become apparent from the description and figures provided herewith.

Abstract translation: 本发明的一个实施例是用于测量燃气涡轮发动机，燃气涡轮发动机部件和燃气涡轮发动机/部件钻机中的辐射能的独特系统。 另一个实施例是用于测量燃气涡轮发动机，燃气涡轮发动机部件和燃气涡轮发动机/部件钻机中的辐射能的独特方法。 其他实施例包括用于测量辐射能的装置，系统，装置，硬件，方法和组合。 本申请的其他实施例，形式，特征，方面，益处和优点将从本文提供的描述和图中变得显而易见。

公开(公告)号：US20140246183A1

公开(公告)日：2014-09-04

申请号：US14195143

申请日：2014-03-03

Applicant: James Carl Loebig ,  Emil Dejulio

Inventor： James Carl Loebig ,  Emil Dejulio

IPC: F28D9/00 ,  F28D9/02 ,  B21D53/04 ,  F28F3/12

CPC classification number: F28D9/0068 ,  B21D53/04 ,  F28D9/0037 ,  F28D9/02 ,  F28F3/12 ,  F28F2260/02 ,  Y10T29/49366

Abstract: An apparatus includes a first flow panel and a second flow panel. The first flow panel includes a first flow portion and a second flow portion. The first flow portion defines a flow passageway within which a gas can flow in a first direction. The second flow portion defines a set of microchannels in fluid communication with the flow passageway and within which the gas can flow in a second direction, where the second direction is nonparallel to the first direction. The first flow panel is coupled to the second flow panel to define a heat transfer passageway within which a heat transfer medium can be conveyed in a third direction, where the third direction is opposite the first direction. In such embodiments, the heat transfer passageway is fluidically isolated from the flow passageway and the set of microchannels by a thermally conductive side wall.

Abstract translation: 一种装置包括第一流动面板和第二流动面板。 第一流动面板包括第一流动部分和第二流动部分。 第一流动部分限定了气体在第一方向上流动的流动通道。 第二流动部分限定与流动通道流体连通的一组微通道，其中气体可以在第二方向上流动，其中第二方向与第一方向不平行。 第一流动面板联接到第二流动面板以限定传热通道，传热介质可以在其中第三方向与第一方向相反的第三方向传送。 在这种实施例中，传热通道由导热侧壁与流动通道和该组件的微通道流体隔离。