公开(公告)号：US09015941B2

公开(公告)日：2015-04-28

申请号：US13663925

申请日：2012-10-30

Applicant: Bell Helicopter Trextron Inc.

Inventor： Ramesh Thiagarajan ,  Robert Mark Chris ,  John R. McCullough ,  Suvankar Mishra

IPC: B23P6/00 ,  B29C44/18 ,  B29C73/06 ,  B29C73/10 ,  B29C73/26 ,  B29L31/60 ,  B29L31/08

CPC classification number: B23P6/00 ,  B23P6/002 ,  B23P2700/00 ,  B29C44/18 ,  B29C73/063 ,  B29C73/10 ,  B29C2073/264 ,  B29L2031/082 ,  B29L2031/608 ,  Y10T29/49318 ,  Y10T29/49723 ,  Y10T29/49725 ,  Y10T29/49726 ,  Y10T29/49732 ,  Y10T29/49734 ,  Y10T29/49746 ,  Y10T428/24157

Abstract: A method of the present disclosure includes of repairing a core stiffened structure with structural foam. Another method includes splicing core members together using structural foam. Another method includes joining a core member to a structure using structural foam. Another method includes using structural foam to stabilize a core member during a machining process. Another method includes stabilizing a core member with structural foam to prevent the core member from crushing in autoclave pressure. The present disclosure further includes a core stiffened structure have a core member with structural foam therein.

Abstract translation: 本公开的方法包括用结构泡沫修复芯加固结构。 另一种方法包括使用结构泡沫将芯部件拼接在一起。 另一种方法包括使用结构泡沫将芯构件连接到结构上。 另一种方法包括在加工过程中使用结构泡沫来稳定芯构件。 另一种方法包括用结构泡沫稳定芯部件以防止芯件在高压釜压力下破碎。 本公开还包括具有在其中具有结构泡沫的芯构件的芯加强结构。

公开(公告)号：US20150060438A1

公开(公告)日：2015-03-05

申请号：US14537229

申请日：2014-11-10

Applicant: Gregory R. Gaul

Inventor： Gregory R. Gaul

IPC: B23P6/00 ,  B21D3/16

CPC classification number: B23P6/002 ,  B21D3/00 ,  B21D3/16 ,  Y10T29/37 ,  Y10T29/49318

Abstract: A gas turbine nozzle can be refurbished to reduce downstream deflection. The outer shroud of the gas turbine nozzle is held in a fixture, and then the nozzle is heated. The heated nozzle is then reshaped by a force exerted upon the inner shroud of the gas turbine, reducing the downstream deflection of the nozzle. After the deformation of the nozzle, an aft hook of the nozzle that has been adjusted by previous refurbishment efforts can be rebuilt to remove the previous adjustments.

Abstract translation: 燃气轮机喷嘴可以被翻新以减少下游偏转。 燃气轮机喷嘴的外护罩保持在固定装置中，然后加热喷嘴。 然后通过施加在燃气轮机的内护罩上的力将加热的喷嘴重新成形，从而减少喷嘴的下游偏转。 在喷嘴变形之后，可以重建已经通过先前的翻新工作调节的喷嘴的后钩，以消除先前的调整。

公开(公告)号：US20150052750A1

公开(公告)日：2015-02-26

申请号：US14391794

申请日：2013-04-12

Applicant: SNECMA

Inventor： Romain Rene Marcel Chardonnet ,  Patrick Gilbert Petit ,  Alain Martinez

IPC: F01D25/28 ,  F01D9/04 ,  B23P6/00

CPC classification number: F01D25/285 ,  B23K31/02 ,  B23K2101/001 ,  B23P6/002 ,  F01D9/04 ,  F01D9/044 ,  F05D2230/60 ,  F05D2230/64 ,  Y10T29/49323 ,  Y10T29/53913

Abstract: A method and tooling for assembling a guide vane stage that includes an inner shroud and an outer shroud that are coaxial and interconnected by radial airfoils, the method including holding plates pressed against an outer surface of the inner shroud so that the plates cover gaps formed between openings in the inner shroud and the airfoils at least in part and in a manner that is leaktight, and applying a sealing resin to the inner surface of the inner shroud so that the resin fills the gaps and so that radially inner ends of the airfoils are embedded in the resin.

Abstract translation: 一种用于组装导叶台的方法和工具，其包括通过径向翼型件共轴并且互连的内护罩和外护罩，所述方法和工具包括将板压在内护罩的外表面上，使得板覆盖形成在 至少部分地并且以密封的方式在内护罩和翼型件中的开口，并且将密封树脂施加到内护罩的内表面，使得树脂填充间隙，使得翼型件的径向内端为 嵌入树脂中。

公开(公告)号：US20150044041A1

公开(公告)日：2015-02-12

申请号：US14522648

申请日：2014-10-24

Applicant: Siemens Energy, Inc.

Inventor： Mrinal Munshi ,  Shivashankar Vinay Amatiganahally ,  Eric L. Roach ,  Todd F. Young

IPC: F01D9/02 ,  B23P6/00

CPC classification number: F01D9/041 ,  B23P6/002 ,  F01D5/005 ,  F01D5/18 ,  F01D5/186 ,  F01D5/187 ,  F01D5/20 ,  F01D11/14 ,  F05D2230/232 ,  Y10T29/49318

Abstract: A gas turbine vane containment cap is attached to an inboard surface of the vane inner shroud by penetrating flat weld filler, formed in a root gap between the cap and inner shroud. A semi-circular bead weld filler is formed outboard the penetrating weld filler closer to the vane exterior. Vane containment caps so welded are more resistant to in-service cracking along weldments.

Abstract translation: 燃气轮机叶片收容盖通过穿过扁平焊接填料而附接到叶片内护罩的内侧表面，形成在盖和内护罩之间的根部间隙中。 在靠近叶片外部的穿透焊接填料外侧形成半圆形焊缝填料。 如此焊接的叶片密封盖更能抵抗沿焊件的在役开裂。

公开(公告)号：US20150040395A1

公开(公告)日：2015-02-12

申请号：US14374282

申请日：2013-01-28

Applicant: SNECMA

Inventor： Michael Delapierre ,  Eric Gvozdenovic ,  Christian Manuel Planas ,  Patrick Jean-Louis Reghezza

IPC: F01D5/00 ,  B23P6/00 ,  F01D5/30

CPC classification number: F01D5/005 ,  B23P6/002 ,  B23P6/005 ,  F01D5/06 ,  F01D5/30 ,  F01D5/3007 ,  F01D5/3092 ,  F04D29/322 ,  F05D2260/941 ,  Y02T50/672 ,  Y10T29/49318

Abstract: A method for repairing a flange of a rotor, to a transverse surface of which a disk of a fan in an upstream turbo-fan engine is attached. The flange includes, in a form of a ring, openings for connecting to the disk and intermediate discharge openings. Wear marks are formed by friction of the fan blades on the flange. The method includes machining spot facings onto the flange, in areas with wear marks; placing anti-wear slugs in the discharge openings that can be covered by the blades during friction; and the spot facings extend between the connection openings and are circumferentially limited by clamping surfaces of the connection between the disk and the flange.

Abstract translation: 一种用于修理转子的凸缘的方法，其安装在上游涡轮风扇发动机的风扇的盘的横向表面上。 凸缘包括环形，用于连接到盘和中间排出口的开口。 磨损痕由风扇叶片在凸缘上的摩擦形成。 该方法包括在具有磨损痕迹的区域上加工法兰上的斑点; 将抗磨损块塞在可在摩擦过程中被叶片覆盖的排放口; 并且光斑贴面在连接开口之间延伸并且通过盘与凸缘之间的连接的夹紧表面周向地限制。

公开(公告)号：US20150030432A1

公开(公告)日：2015-01-29

申请号：US13951704

申请日：2013-07-26

Applicant: Bruce L. Smith

Inventor： Bruce L. Smith

IPC: F01D5/18 ,  B23P6/00 ,  F01D25/14

CPC classification number: B23P6/002 ,  F01D5/005 ,  F01D5/186 ,  F01D5/187 ,  F01D5/288 ,  F05D2230/80 ,  F05D2240/122 ,  Y10T29/49238

Abstract: An airfoil (112) including an internal cooling circuit (136) to direct cooling fluid (120) through an interior of the airfoil. The airfoil also includes a trailing edge (114′) defining plugged holes (115) and cooling holes (116) along a radial direction (117). A selective group (314) of the cooling and plugged holes are based on a reduced cooling fluid requirement at the trailing edge (114′) resulting from an improved thermal barrier coating (126). A process (200) is also provided including removing (202) an airfoil from service in a gas turbine engine and adding or improving (204) a thermal barrier coating on the airfoil. The process also includes selectively (206) plugging holes in the airfoil in response to a reduced cooling fluid required through the airfoil as a result of the added or improved thermal barrier coating.

Abstract translation: 包括内部冷却回路（136）的翼型件（112），以将冷却流体（120）引导通过翼型件的内部。 翼型件还包括沿着径向方向（117）限定堵塞孔（115）和冷却孔（116）的后缘（114'）。 冷却和堵塞孔的选择性组（314）基于由改进的热障涂层（126）产生的在后缘（114'）处减少的冷却流体需求。 还提供了一种方法（200），包括在燃气涡轮发动机中移除（202）翼型件并且增加或改进（204）翼型件上的热障涂层。 该方法还包括响应于由于增加或改进的热障涂层而通过翼型件所需的减少的冷却流体而选择性地（206）堵塞翼型件中的孔。

公开(公告)号：US08914975B2

公开(公告)日：2014-12-23

申请号：US12374519

申请日：2007-07-13

Applicant: Joachim Wulf

Inventor： Joachim Wulf

IPC: B23P6/00 ,  F01D5/00 ,  F01D9/04

CPC classification number: F01D5/005 ,  B23P6/002 ,  F01D9/041 ,  Y02T50/672 ,  Y10T29/49318 ,  Y10T29/49341 ,  Y10T29/49721 ,  Y10T29/4973

Abstract: A method for repairing a guide blade segment fashioned as a twin guide blade segment within a guide blade composite element, the guide blades being formed from a nose segment and a rear edge segment, the method having identification, within a guide blade segment, of a non-repairable guide blade to be separated from the guide blade composite structure; separation of a non-repairable guide blade from a one repairable guide blade in a first plane of division; division of at least one separated guide blade in a second plane of division between the nose segment and the rear edge segment; reconditioning of the at least one repairable nose segment and/or rear edge segment; joining of a reconditioned and/or new nose segment to a reconditioned and/or new rear edge segment to form at least one guide blade; and joining of at least two guide blades to form a guide blade segment.

Abstract translation: 一种用于修复在导向叶片复合元件内形成为双引导叶片段的导向叶片段的方法，所述引导叶片由鼻部段和后缘段形成，所述方法在引导叶片段内具有一个 不可修复的导向叶片与导向叶片复合结构分离; 在第一分割平面中将不可修复的导向叶片与一个可修复的导向叶片分离; 在鼻段和后缘段之间的第二分割平面中划分至少一个分离的引导叶片; 修复所述至少一个可修复的鼻部段和/或所述后缘部分; 将修复和/或新的鼻部段连接到修复和/或新的后缘部分以形成至少一个引导刀片; 以及连接至少两个导向叶片以形成导向叶片段。

公开(公告)号：US08893381B2

公开(公告)日：2014-11-25

申请号：US13334746

申请日：2011-12-22

Applicant: Daniel David Noe ,  Douglas Jerome Jones ,  Michael Alan Pierson

Inventor： Daniel David Noe ,  Douglas Jerome Jones ,  Michael Alan Pierson

IPC: B23P6/00 ,  F01D11/00 ,  F01D5/06 ,  F16J15/06 ,  B23P15/02 ,  F01D5/00 ,  F16J15/00 ,  F01D5/30

CPC classification number: F01D11/006 ,  B23P6/00 ,  B23P6/002 ,  B23P15/02 ,  F01D5/005 ,  F01D5/06 ,  F01D5/3038 ,  F01D11/00 ,  F01D11/005 ,  F05B2230/10 ,  F05B2230/90 ,  F05D2230/10 ,  F05D2230/90 ,  F16J15/00 ,  F16J15/062 ,  Y10T29/49316 ,  Y10T29/49318 ,  Y10T29/4932 ,  Y10T29/49325 ,  Y10T29/49726 ,  Y10T29/49728

Abstract: A method of repairing a seal wire groove is disclosed, the groove forming an annular structure having an outer surface and an inner surface and defining an original profile when new, comprising the steps of: removing a less-than-annular portion of the original profile of the groove to remove damaged portions of at least one of the inner and outer surfaces thereby forming a void; adding new material to the void; and shaping the new material to form a new profile of the groove.

Abstract translation: 公开了一种修复密封线槽的方法，所述凹槽形成具有外表面和内表面的环形结构，并且在新的情况下限定原始轮廓，包括以下步骤：移除原始轮廓的小于环形部分 以去除内表面和外表面中的至少一个的损坏部分，从而形成空隙; 向空白添加新材料; 并形成新材料，形成新的凹槽。

公开(公告)号：US20140259666A1

公开(公告)日：2014-09-18

申请号：US13797382

申请日：2013-03-12

Applicant: HONEYWELL INTERNATIONAL INC.

Inventor： Brian G. Baughman ,  Gary Winchester ,  William F. Hehmann ,  Donald G. Godfrey

IPC: B23P6/00

CPC classification number: B23P6/002 ,  B22F3/1055 ,  B22F5/04 ,  B22F7/062 ,  B22F2007/068 ,  B23K1/0018 ,  B23K2101/001 ,  B23P6/005 ,  F01D5/005 ,  Y02P10/295 ,  Y10T29/49318 ,  Y10T29/4973

Abstract: In accordance with an exemplary embodiment, a method for repairing a damaged metallic component using additive manufacturing techniques includes separating a damaged portion of the damaged metallic component from an undamaged portion of the damaged metallic component, measuring the undamaged portion to determine the dimensions of the removed damaged portion, fabricating a replacement portion using additive manufacturing techniques in accordance with the determined dimensions of the removed damaged portion, and joining the replacement portion with the undamaged portion of the damaged metallic component to form a repaired metallic component.

Abstract translation: 根据示例性实施例，使用添加剂制造技术来修复损坏的金属部件的方法包括将损坏的金属部件的损坏部分与损坏的金属部件的未损坏部分分开，测量未损坏的部分以确定被去除的尺寸 使用添加剂制造技术根据确定的去除的损坏部分的尺寸制造替换部分，并将替换部分与损坏的金属部件的未损坏部分接合以形成修复的金属部件。

公开(公告)号：US20140245607A1

公开(公告)日：2014-09-04

申请号：US14281338

申请日：2014-05-19

Applicant: MECHANICAL DYNAMICS AND ANALYSIS, LLC

Inventor： James Harvey COFFEY ,  Andrew Otto RUEHS

IPC: B23P6/00

CPC classification number: B23P6/002 ,  B23B27/04 ,  B23B29/043 ,  B23C5/12 ,  B23P6/007 ,  F01D5/005 ,  F05D2230/10 ,  F05D2230/232 ,  F05D2230/235 ,  Y10T29/37 ,  Y10T29/49318 ,  Y10T29/49728 ,  Y10T29/4973 ,  Y10T29/49734 ,  Y10T29/49737 ,  Y10T29/53983 ,  Y10T82/25

Abstract: A method for repairing a rotor of a turbine includes providing a rotor having a groove portion defined by a circumferential portion of the rotor. The circumferential portion of the rotor is removed to create an opening to provide access to the groove such that the opening, immediately adjacent the groove, is narrower than the groove. A guide block may be extended into a receiving slot separating a first protruding surface from a second protruding surface of the rotor such that a weld area slot of the guide block extends over at least a portion of the opening. The opening may be welded adjacent the guide block to close at least a portion of the opening.

Abstract translation: 一种用于修理涡轮机的转子的方法包括提供具有由转子的周向部分限定的凹槽部分的转子。 移除转子的圆周部分以产生开口以提供对凹槽的通路，使得紧邻凹槽的开口比凹槽更窄。 引导块可以延伸到将第一突出表面与转子的第二突出表面分开的接收槽中，使得引导块的焊接区域槽在开口的至少一部分上延伸。 开口可以被焊接在引导块附近以关闭开口的至少一部分。