公开(公告)号：WO2015065606A1

公开(公告)日：2015-05-07

申请号：PCT/US2014/055742

申请日：2014-09-16

Applicant: UNITED TECHNOLOGIES CORPORATION

Inventor： LIN, Wangen

IPC: B23K26/342 ,  B22F5/00 ,  F01D25/00

CPC classification number: B23K26/342 ,  B22F5/009 ,  B22F7/062 ,  B22F2007/068 ,  B22F2999/00 ,  B23K26/144 ,  B23K26/32 ,  B23K2201/001 ,  B23K2203/08 ,  B23P6/007 ,  C21D9/50 ,  C22C19/057 ,  F01D5/005 ,  F01D9/041 ,  F01D25/24 ,  F05D2220/32 ,  F05D2230/10 ,  F05D2230/21 ,  F05D2230/31 ,  F05D2230/80 ,  F05D2300/17 ,  F05D2300/175 ,  F05D2300/177 ,  B22F3/105

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.

Abstract translation: 重新加工或修理部件的方法包括从由非熔接的可焊接的基础合金制成的部件去除铸造缺陷以形成导致通孔的腔; 用背衬密封通孔; 并且用多个激光粉末沉积点的多个层至少部分地填充所述腔，所述多个激光粉末沉积点中的每一个由填充合金形成，所述多个层的第一层包括所述多个 的激光粉末沉积点与空腔和背衬的壁重叠。

公开(公告)号：WO2015123268A1

公开(公告)日：2015-08-20

申请号：PCT/US2015/015374

申请日：2015-02-11

Applicant: UNITED TECHNOLOGIES CORPORATION

Inventor： WHITMAN, Giovanni ,  THAYER, Henry, H. ,  LARSON, Gary, J. ,  LIN, Wangen ,  BLANKENSHIP, Donn

IPC: B23H1/02 ,  B23K9/04 ,  B23H9/10

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涂覆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：WO2014051830A1

公开(公告)日：2014-04-03

申请号：PCT/US2013/051279

申请日：2013-07-19

Applicant: UNITED TECHNOLOGIES CORPORATION

Inventor： LIN, Wangen ,  SCHAEFER, Robert, P. ,  VARGAS, Chris

IPC: B23P6/04

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化在空腔中。 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：WO2015065847A1

公开(公告)日：2015-05-07

申请号：PCT/US2014/062194

申请日：2014-10-24

Applicant: UNITED TECHNOLOGIES CORPORATION

Inventor： OLS, John T. ,  LIN, Wangen ,  WHITMAN, Giovanni

IPC: B23K26/34

CPC classification number: B23K26/342 ,  B22F5/009 ,  B22F7/062 ,  B22F2007/068 ,  B22F2999/00 ,  B23K26/144 ,  B23K26/323 ,  B23K35/0244 ,  B23K35/3033 ,  B23K2201/001 ,  B23K2203/26 ,  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非熔化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：WO2015065846A1

公开(公告)日：2015-05-07

申请号：PCT/US2014/062183

申请日：2014-10-24

Applicant: UNITED TECHNOLOGIES CORPORATION

Inventor： LIN, Wangen ,  LARSON, Gary J. ,  WHITMAN, Giovanni ,  POEPPEL, Scott ,  WILSON, Joseph

IPC: B23K26/34

CPC classification number: B23K26/342 ,  B22F5/009 ,  B22F7/062 ,  B22F2007/068 ,  B22F2999/00 ,  B23K26/144 ,  B23K26/32 ,  B23K2201/001 ,  B23K2203/08 ,  B23P6/007 ,  C21D9/50 ,  C22C19/057 ,  F01D5/005 ,  F01D9/041 ,  F01D25/24 ,  F05D2220/32 ,  F05D2230/10 ,  F05D2230/21 ,  F05D2230/31 ,  F05D2230/80 ,  F05D2300/17 ,  F05D2300/175 ,  F05D2300/177 ,  B22F3/105

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.

Abstract translation: 对航空航天部件进行再加工的方法包括从由非熔接的可焊接的基体合金制成的部件去除铸造缺陷以形成空腔。 然后，空腔至少部分地填充有填充合金的多个分立的激光粉末沉积点的层。 用于燃气涡轮发动机的铸造部件包括具有填充有多个填充合金的激光粉末沉积点的多个腔的铸造部件不可焊接的基础合金。 填充合金可以不同于不熔焊的基体合金。 一层不熔焊接基体合金至少部分在腔内和填料合金之上。

公开(公告)号：EP3330038A1

公开(公告)日：2018-06-06

申请号：EP17203892.9

申请日：2017-11-27

Applicant: United Technologies Corporation

Inventor： LIN, Wangen ,  BOYNTON, Scott Lewis ,  BROWN, Alex Neese

IPC: B23K26/14 ,  B23K26/16 ,  B23K26/342 ,  B23K26/144 ,  B23K26/142 ,  B23K26/082

CPC classification number: B23K26/342 ,  B23K26/032 ,  B23K26/082 ,  B23K26/142 ,  B23K26/144 ,  B23K26/1476 ,  B23K26/1488 ,  B23K26/16

Abstract: A laser cladding head (12) comprises a protective housing (18), a focal array (26), a turning mirror (36), and a powder nozzle (34). The housing (18) extends along a primary axis (A P ) from a proximal end (20) to a distal end (22). The focal array (26) is situated at the proximal end (20) and oriented to receive and focus collimated light (28) in a beam (28) directed substantially along the primary axis (Ap). The turning mirror (30) is situated at the distal end (22) and disposed to redirect the beam (28) in an emission direction, towards a target point (P T ) separated from the turning mirror (30) by a working distance (D T ) of at most a tenth the focal length. The turning mirror (30) is a nonfocal reflective surface indexable to alter an impingement location (P I ) of the beam (28) on the turning mirror (30). The powder nozzle (34) is situated at the distal end (22) and receives and directs weld material towards the target point (P T ) for melting.

公开(公告)号：EP3450084A1

公开(公告)日：2019-03-06

申请号：EP18183020.9

申请日：2018-07-11

Applicant: United Technologies Corporation

Inventor： POTTER, David N. ,  BRINDLEY, William J. ,  LIN, Wangen

IPC: B23K26/342 ,  F01D5/00 ,  F01D5/12 ,  B23K26/60 ,  B23K101/00 ,  B23K103/14

Abstract: A weld clad layer having a substantially equiaxed grain microstructure may be formed by forming a repair area (304) in a substrate (201), by depositing a first layer of laser deposition spots (320) in the repair area (304), and depositing a second layer of laser deposition spots (320) over the first layer of laser deposition spots (320). The first layer of laser deposition spots (320) comprises a first laser deposition spot (320) and a second laser deposition spot (320) adjacent to the first laser deposition spot (320). The first laser deposition spot (320) solidifies prior to deposition of the second laser deposition spot (320). The first layer of laser deposition spots (320) comprises titanium or titanium alloy.

公开(公告)号：EP3330035A1

公开(公告)日：2018-06-06

申请号：EP17203838.2

申请日：2017-11-27

Applicant: United Technologies Corporation

Inventor： LIN, Wangen ,  BOYNTON, Scott Lewis ,  BROWN, Alex Neese

IPC: B23K26/03 ,  B23K26/14 ,  B23K26/16 ,  B23K26/342 ,  B23K26/144 ,  B23K26/142 ,  B23K26/082

CPC classification number: B23K26/342 ,  B23K26/032 ,  B23K26/142 ,  B23K26/144 ,  B23K26/1476 ,  B23K26/1488 ,  B23K26/16

Abstract: A laser cladding system (10) comprises a cladding head (12) and a gas system (50). The cladding head (12) extends along a primary axis (A P ), and comprises a mirror (30) and a powder nozzle (34) both situated at a distal end (22) of the head (40). The powder nozzle (34) directs weld material at a target point (P T ), and the mirror (30) directs a beam (28) of collimated light at the target point (P T ). The gas system (50) comprises a high-speed gas nozzle (304) and a gas knife (310). The high-speed gas nozzle (304) produces a gas sheath (302) coaxial with the beam (28) in a region between the mirror (30) and target point (P T ), shielding the mirror (30) from debris and backspatter. The gas knife (310) redirects the gas sheath (302) away from the target point (P T ) and redirects debris and molten backspatter away from an interior of the laser cladding head (12).

公开(公告)号：EP3299579A1

公开(公告)日：2018-03-28

申请号：EP17192394.9

申请日：2017-09-21

Applicant: United Technologies Corporation

Inventor： LIN, Wangen ,  BRINDLEY, William J. ,  SAXTON, Bruce R. ,  IVORY, Steven

IPC: F01D5/00 ,  B23K20/12 ,  B23P6/00

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 (20) including a first fastener aperture (36) that extends through the component (20). During the method, the component (20) is machined to enlarge the first fastener aperture (36) to provide an enlarged aperture (54). The component (20) is friction plug welded to plug the enlarged aperture (54) with friction plug welded material (56). A second fastener aperture (36B) is machined in the friction plug welded material (56), where the second fastener aperture (36B) extends through the component (20).

Abstract translation: 提供了一种方法，其涉及包括延伸穿过部件（20）的第一紧固件孔（36）的部件（20）。 在该方法期间，部件（20）被机械加工以扩大第一紧固件孔（36）以提供扩大的孔（54）。 部件（20）被摩擦塞焊接，以用摩擦塞焊接材料（56）塞住扩大的孔（54）。 在摩擦塞焊接材料（56）中加工第二紧固件孔（36B），其中第二紧固件孔（36B）延伸穿过部件（20）。

公开(公告)号：EP3062953A1

公开(公告)日：2016-09-07

申请号：EP14857767.9

申请日：2014-10-24

Applicant: United Technologies Corporation

Inventor： OLS, John T. ,  LIN, Wangen ,  WHITMAN, Giovanni

IPC: B23K26/34

CPC classification number: B23K26/342 ,  B22F5/009 ,  B22F7/062 ,  B22F2007/068 ,  B22F2999/00 ,  B23K26/144 ,  B23K26/323 ,  B23K35/0244 ,  B23K35/3033 ,  B23K2201/001 ,  B23K2203/26 ,  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: 提供了一个方法来修改组件。 该方法包括利用由填充合金形成的多个激光粉末沉积点的多个层来至少部分地填充非熔融可焊接基础合金中的空腔。 多个激光粉末沉积斑点中的每一个至少部分地与多个激光粉末沉积斑点中的另一个中的至少一个重叠。 填充合金可以与不可熔焊接的基础合金不同。