公开(公告)号：US20160256957A1

公开(公告)日：2016-09-08

申请号：US14635639

申请日：2015-03-02

Applicant: United Technologies Corporation

Inventor： Steven Ivory ,  Monika D. Kinstler ,  David A. Gaudreau

IPC: B23K26/21 ,  F23R3/00

CPC classification number: B23K26/21 ,  B23K10/027 ,  B23K26/144 ,  B23K26/342 ,  B23K2101/00 ,  B23K2101/001 ,  B23K2103/52 ,  B23P6/00 ,  B23P6/007 ,  B23P2700/13 ,  F01D5/005 ,  F01D5/284 ,  F01D5/288 ,  F02K1/822 ,  F05D2230/232 ,  F23R3/002 ,  F23R3/007 ,  F23R2900/00019 ,  Y02T50/675 ,  Y10T29/49721 ,  Y10T29/49726 ,  Y10T29/49728

Abstract: Aspects of the disclosure are directed to repairing or restoring a liner associated with a combustor of an aircraft engine. The liner is at least partially stripped of at least one detail. An automated welding operation is applied to the liner. A coating of the liner on a cold side of the liner is retained on the liner during the welding operation.

Abstract translation: 本公开的方面涉及修理或恢复与飞行器发动机的燃烧器相关联的衬管。 衬垫至少部分剥离至少一个细节。 自动焊接操作适用于衬管。 在焊接操作期间，在衬套的冷侧上的衬套的涂层保持在衬套上。

公开(公告)号：US20160312627A1

公开(公告)日：2016-10-27

申请号：US15103077

申请日：2014-12-03

Applicant: UNITED TECHNOLOGIES CORPORATION

Inventor： Lei Chen ,  Zhiwei Yang ,  William J. Brindley ,  Monika D. Kinstler ,  Bruce R. Saxton

IPC: F01D5/28 ,  F01D25/00 ,  C22C19/05 ,  C25D5/50 ,  C25D5/40 ,  C25D7/00 ,  F01D9/02 ,  C25D3/12

CPC classification number: F01D5/288 ,  C22C19/058 ,  C25D3/12 ,  C25D3/562 ,  C25D3/665 ,  C25D5/18 ,  C25D5/40 ,  C25D5/50 ,  C25D7/00 ,  F01D9/02 ,  F01D25/005 ,  F01D25/007 ,  F05D2220/30 ,  F05D2230/30 ,  F05D2230/80 ,  F05D2230/90 ,  F05D2300/132 ,  F05D2300/175 ,  F05D2300/177

Abstract: A nickel-chromium (Ni—Cr) alloy and a method for electrodepositing the Ni—Cr alloy on a turbine engine component for dimensionally restoring the engine component are described. The engine component is restored by re-building wall thickness with the Ni—Cr alloy including from 2 to 50 wt % chromium balanced with nickel. The turbine component coated with the Ni—Cr alloy is heat-treated at a high temperature to homogenize composition of the alloy to mimic the base alloy and to restore materials lost during repair of the turbine component.

Abstract translation: 描述了一种镍 - 铬（Ni-Cr）合金和用于将Ni-Cr合金电沉积在涡轮发动机部件上用于尺寸恢复发动机部件的方法。 发动机部件通过Ni-Cr合金重新构造壁厚恢复，包括与镍平衡的2至50重量％的铬。 涂覆有Ni-Cr合金的涡轮机部件在高温下进行热处理，以使合金的组成均匀化，以模拟基体合金，并恢复在涡轮部件修复期间损失的材料。

公开(公告)号：US09987708B2

公开(公告)日：2018-06-05

申请号：US14635639

申请日：2015-03-02

Applicant: United Technologies Corporation

Inventor： Steven Ivory ,  Monika D. Kinstler ,  David A. Gaudreau

IPC: B23K26/21 ,  B23K10/02 ,  B23P6/00 ,  F01D5/00 ,  F23R3/00 ,  B23K26/342 ,  B23K26/144 ,  F01D5/28 ,  F02K1/82 ,  B23K101/00 ,  B23K103/00

CPC classification number: B23K26/21 ,  B23K10/027 ,  B23K26/144 ,  B23K26/342 ,  B23K2101/00 ,  B23K2101/001 ,  B23K2103/52 ,  B23P6/00 ,  B23P6/007 ,  B23P2700/13 ,  F01D5/005 ,  F01D5/284 ,  F01D5/288 ,  F02K1/822 ,  F05D2230/232 ,  F23R3/002 ,  F23R3/007 ,  F23R2900/00019 ,  Y02T50/675 ,  Y10T29/49721 ,  Y10T29/49726 ,  Y10T29/49728

Abstract: Aspects of the disclosure are directed to repairing or restoring a liner associated with a combustor of an aircraft engine. The liner is at least partially stripped of at least one detail. An automated welding operation is applied to the liner. A coating of the liner on a cold side of the liner is retained on the liner during the welding operation.

公开(公告)号：US20160263712A1

公开(公告)日：2016-09-15

申请号：US15032576

申请日：2015-01-20

Applicant: UNITED TECHNOLOGIES CORPORATION

Inventor： Steven Ivory ,  John H. Finn ,  Monika D. Kinstler

IPC: B23P6/00 ,  F23R3/00

CPC classification number: B23P6/007 ,  B22F3/1055 ,  B22F5/009 ,  B22F2007/068 ,  B23P2700/13 ,  B33Y10/00 ,  F23R3/002 ,  F23R3/007 ,  F23R2900/00019 ,  Y02P10/295

Abstract: A method of additively repairing a combustor liner panel includes removing a combustor liner panel from a combustor, inspecting the combustor liner panel to identify a damaged portion, removing material from the combustor liner panel around the damaged portion to form a repair zone having a substantially flat platform, and adding repair material to the repair zone on a layer by layer basis using an additive repair process.

Abstract translation: 一种附加地修理燃烧器衬套面板的方法包括从燃烧器去除燃烧器衬套面板，检查燃烧器衬套面板以识别受损部分，从损坏部分周围的燃烧器衬板移除材料以形成具有基本平坦的修复区 平台，并使用添加剂修复过程逐层地将修补材料添加到修复区域。

公开(公告)号：US20140174091A1

公开(公告)日：2014-06-26

申请号：US13725138

申请日：2012-12-21

Applicant: UNITED TECHNOLOGIES CORPORATION

Inventor： Steven Ivory ,  Monika D. Kinstler ,  John H. Finn

IPC: F23R3/00

CPC classification number: F23R3/002 ,  F23R2900/00019 ,  F23R2900/03042 ,  F23R2900/03044 ,  Y02T50/675 ,  Y02T50/6765

Abstract: A liner panel for a gas turbine engine includes a cold side having a backside feature and a hot side with a variable polarity weld.

Abstract translation: 用于燃气涡轮发动机的衬板包括具有背面特征的冷侧和具有可变极性焊接的热侧。