公开(公告)号：US10328526B2

公开(公告)日：2019-06-25

申请号：US15026410

申请日：2014-10-24

Applicant: United Technologies Corporation

Inventor： John T. Ols ,  Wangen Lin ,  Giovanni Whitman

IPC: B23K26/34 ,  B23K26/342 ,  B23K35/30 ,  B23K35/02 ,  B23P6/00 ,  F01D5/00 ,  B23K26/323 ,  B22F5/00 ,  B22F7/06 ,  B23K26/144 ,  F01D9/04 ,  F01D25/24 ,  C22F1/10 ,  B23K101/00 ,  B23K103/18

Abstract: A method is provided for reworking a component. The method includes at least partially filling a cavity in a non-fusion weldable base alloy with a multiple of layers of a multiple of laser powder deposition spots formed of a filler alloy. Each of the multiple of laser powder deposition spots at least partially overlaps at least one of another of the multiple of laser powder deposition spots. The filler alloy may be different than the non-fusion weldable base alloy.

公开(公告)号：US20160348519A1

公开(公告)日：2016-12-01

申请号：US15117626

申请日：2015-02-11

Applicant: UNITED TECHNOLOGIES CORPORATION

Inventor： Giovanni Whitman ,  Henry H. Thayer ,  Gary J. Larson ,  Wangen Lin ,  Donn Blankenship

IPC: F01D9/04 ,  C23C4/08 ,  C23C14/22 ,  C23C4/134

CPC classification number: F01D9/041 ,  C23C4/02 ,  C23C4/08 ,  C23C4/134 ,  C23C14/221 ,  F01D5/288 ,  F05D2220/32 ,  F05D2230/312 ,  F05D2230/313 ,  F05D2300/10 ,  Y02T50/672

Abstract: The present disclosure relates generally to a system and method for applying a metallic coating. A first metallic coating may be applied to a portion of a total surface of a part and a second metallic coating may be applied to substantially the total surface. The metallic coating may be applied to a vane cluster for use in a turbomachine.

Abstract translation: 本公开一般涉及用于施加金属涂层的系统和方法。 可以将第一金属涂层施加到部件的整个表面的一部分，并且可以将基本上全部表面施加第二金属涂层。 金属涂层可以施加到用于涡轮机中的叶片簇。

公开(公告)号：US11517981B2

公开(公告)日：2022-12-06

申请号：US16385539

申请日：2019-04-16

Applicant: United Technologies Corporation

Inventor： Wangen Lin ,  Gary J. Larson ,  Giovanni Whitman ,  Scott Poeppel ,  Joseph Wilson

IPC: B23K26/342 ,  F01D5/00 ,  F01D9/04 ,  B23P6/00 ,  B23K26/32 ,  B22F5/00 ,  B22F7/06 ,  B23K26/144 ,  F01D25/24 ,  B23K101/00 ,  C21D9/50 ,  B23K103/08 ,  C22C19/05

Abstract: A method of reworking an aerospace component includes removing a casting defect from a component manufactured of a non-fusion weldable base alloy to form a cavity. The cavity is then at least partially filled with a multiple of layers of discrete laser powder deposition spots of a filler alloy. A cast component for a gas turbine engine includes a cast component non-fusion weldable base alloy with a cavity filled with a multiple of layers of laser powder deposition spots of a filler alloy. The filler alloy may be different than the non-fusion weldable base alloy. A layer of non-fusion weldable base alloy is at least partially within the cavity and over the filler alloy.

公开(公告)号：US10569361B2

公开(公告)日：2020-02-25

申请号：US15032415

申请日：2014-09-16

Applicant: UNITED TECHNOLOGIES CORPORATION

Inventor： Wangen Lin

IPC: B23K26/342 ,  F01D5/00 ,  F01D9/04 ,  B23P6/00 ,  B23K26/32 ,  B22F5/00 ,  B22F7/06 ,  B23K26/144 ,  F01D25/24 ,  B23K101/00 ,  C21D9/50 ,  B23K103/08 ,  C22C19/05

Abstract: A method of reworking or repairing a component includes removing a casting defect from a component manufactured of a non-fusion weldable base alloy to form a cavity that results in a through hole; sealing the through hole with a backing; and at least partially filling the cavity with a multiple of layers of a multiple of laser powder deposition spots, each of the multiple of laser powder deposition spots formed of a filler alloy, a first layer of the multiple of layers includes a perimeter of the multiple of laser powder deposition spots that overlap a wall of the cavity and the backing.

公开(公告)号：US20190039191A1

公开(公告)日：2019-02-07

申请号：US15670775

申请日：2017-08-07

Applicant: UNITED TECHNOLOGIES CORPORATION

Inventor： David N. Potter ,  William J. Brindley ,  Wangen Lin

IPC: B23P6/00 ,  F04D29/38

Abstract: A weld clad layer having a substantially equiaxed grain microstructure may be formed by forming a repair area in a substrate, depositing a first layer of laser deposition spots in the repair area, and depositing a second layer of laser deposition spots over the first layer of laser deposition spots. The first layer of laser deposition spots may comprise a first laser deposition spot and a second laser deposition spot adjacent to the first laser deposition spot. The first laser deposition spot may solidify prior to deposition of the second laser deposition spot. The first layer of laser deposition spots may comprise titanium or titanium alloy.

公开(公告)号：US20180085867A1

公开(公告)日：2018-03-29

申请号：US15276021

申请日：2016-09-26

Applicant: United Technologies Corporation

Inventor： Wangen Lin ,  William J. Brindley ,  Bruce R. Saxton ,  Steven Ivory

IPC: B23P6/00 ,  B23K20/12 ,  B23K20/22 ,  B23P6/04 ,  C21D9/50 ,  C22F1/18 ,  C22F1/10 ,  C22F1/04 ,  B23K37/00

CPC classification number: B23P6/002 ,  B23K20/12 ,  B23K20/122 ,  B23K20/22 ,  B23K37/00 ,  B23K2101/001 ,  B23P6/005 ,  B23P6/045 ,  C21D9/50 ,  C22F1/04 ,  C22F1/10 ,  C22F1/183 ,  F01D5/005 ,  F01D25/243 ,  F05D2230/239 ,  F05D2230/80 ,  Y02T50/672

Abstract: A method is provided that involves a component including a first fastener aperture that extends through the component. During the method, the component is machined to enlarge the first fastener aperture to provide an enlarged aperture. The component is friction plug welded to plug the enlarged aperture with friction plug welded material. A second fastener aperture is machined in the friction plug welded material, where the second fastener aperture extends through the component.

公开(公告)号：US20160236298A1

公开(公告)日：2016-08-18

申请号：US15026410

申请日：2014-10-24

Applicant: UNITED TECHNOLOGIES CORPORATION

Inventor： John T. Ols ,  Wangen Lin ,  Giovanni Whitman

IPC: B23K26/342 ,  F01D9/04 ,  F01D25/24 ,  B23K26/00 ,  B23K26/144

CPC classification number: B23K26/342 ,  B22F5/009 ,  B22F7/062 ,  B22F2007/068 ,  B22F2999/00 ,  B23K26/144 ,  B23K26/323 ,  B23K35/0244 ,  B23K35/3033 ,  B23K2101/001 ,  B23K2103/26 ,  B23P6/007 ,  C22F1/10 ,  F01D5/005 ,  F01D9/041 ,  F01D25/246 ,  F05D2220/32 ,  F05D2230/234 ,  F05D2230/31 ,  F05D2230/42 ,  F05D2300/175 ,  F05D2300/177 ,  B22F3/105

Abstract: A method is provided for reworking a component. The method includes at least partially filling a cavity in a non-fusion weldable base alloy with a multiple of layers of a multiple of laser powder deposition spots formed of a filler alloy. Each of the multiple of laser powder deposition spots at least partially overlaps at least one of another of the multiple of laser powder deposition spots. The filler alloy may be different than the non-fusion weldable base alloy.

Abstract translation: 提供了一种用于重新组装组件的方法。 该方法包括至少部分地填充由非填充合金形成的多个激光粉末沉积点的多个层的不可焊接的基础合金中的空腔。 多个激光粉末沉积点中的每一个至少部分地与多个激光粉末沉积点中的至少一个重叠。 填充合金可以不同于不熔焊基体合金。

公开(公告)号：US20150190891A1

公开(公告)日：2015-07-09

申请号：US14418675

申请日：2013-07-19

Applicant: United Technologies Corporation

Inventor： Wangen Lin ,  Robert P. Schaefer ,  Chris Vargas

IPC: B23P6/04 ,  B23K1/20 ,  B23K31/02 ,  B23K1/00

CPC classification number: B23P6/04 ,  B23K1/0018 ,  B23K1/20 ,  B23K1/206 ,  B23K31/02 ,  B23P6/007 ,  B23P6/045 ,  F01D5/005 ,  F01D9/065 ,  F01D25/162

Abstract: A method of repairing defects in a casting formed from non-weldable or difficult-to-weld alloys is disclosed. The method includes removing the defect from the casting thereby forming a cavity in the casting, placing a filler material in the cavity and fusion welding the filler material in the cavity. The fusion welding produces surface cracks on the casting and sub-surface cracks in the casting. The method then includes brazing at least some of the surface cracks on the casting and processing the casting with a hot isostatic pressure (HIP) process to close at least some of the sub-surface cracks in the casting.

Abstract translation: 公开了一种修复由不可焊接或难焊接合金形成的铸件中的缺陷的方法。 该方法包括从铸造中去除缺陷，从而在铸件中形成空腔，将填充材料放置在空腔中并将填充材料熔合在空腔中。 熔焊在铸件中产生表面裂纹和铸件表面裂纹。 该方法然后包括在铸造上钎焊至少一些表面裂纹并用热等静压（HIP）工艺处理铸件，以关闭铸件中的至少一些次表面裂纹。

公开(公告)号：US11524363B2

公开(公告)日：2022-12-13

申请号：US16743431

申请日：2020-01-15

Applicant: United Technologies Corporation

Inventor： Wangen Lin

IPC: B23K26/342 ,  B22F5/00 ,  F01D5/00 ,  F01D9/04 ,  B23P6/00 ,  B23K26/32 ,  B22F7/06 ,  B23K26/144 ,  F01D25/24 ,  B23K101/00 ,  C21D9/50 ,  B23K103/08 ,  C22C19/05

Abstract: A method of reworking or repairing a component includes removing a casting defect from a component manufactured of a non-fusion weldable base alloy to form a cavity that results in a through hole; sealing the through hole with a backing; and at least partially filling the cavity with a multiple of layers of a multiple of laser powder deposition spots, each of the multiple of laser powder deposition spots formed of a filler alloy, a first layer of the multiple of layers includes a perimeter of the multiple of laser powder deposition spots that overlap a wall of the cavity and the backing.

公开(公告)号：US10265802B2

公开(公告)日：2019-04-23

申请号：US15026459

申请日：2014-10-24

Applicant: United Technologies Corporation

Inventor： Wangen Lin ,  Gary J. Larson ,  Giovanni Whitman ,  Scott Poeppel ,  Joseph Wilson

IPC: B23K26/342 ,  F01D5/00 ,  F01D9/04 ,  B23P6/00 ,  B23K26/32 ,  B22F5/00 ,  B22F7/06 ,  B23K26/144 ,  F01D25/24 ,  B23K101/00 ,  C21D9/50 ,  C22C19/05 ,  B23K103/08

Abstract: A method of reworking an aerospace component includes removing a casting defect from a component manufactured of a non-fusion weldable base alloy to form a cavity. The cavity is then at least partially filled with a multiple of layers of discrete laser powder deposition spots of a filler alloy. A cast component for a gas turbine engine includes a cast component non-fusion weldable base alloy with a cavity filled with a multiple of layers of laser powder deposition spots of a filler alloy. The filler alloy may be different than the non-fusion weldable base alloy. A layer of non-fusion weldable base alloy is at least partially within the cavity and over the filler alloy.