公开(公告)号：EP3062952A1

公开(公告)日：2016-09-07

申请号：EP14857676.2

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

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：EP2900416A1

公开(公告)日：2015-08-05

申请号：EP13841068.3

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.

公开(公告)号：EP3034651B1

公开(公告)日：2019-07-24

申请号：EP15199318.5

申请日：2015-12-10

Applicant: United Technologies Corporation

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

IPC: C23C24/10 ,  B23K9/04 ,  C23C28/02 ,  F01D5/28

公开(公告)号：EP3309264A1

公开(公告)日：2018-04-18

申请号：EP17185404.5

申请日：2017-08-08

Applicant: United Technologies Corporation

Inventor： BOCHIECHIO, Mario P. ,  LIN, Wangen ,  STOLZ, D. Slade ,  RAGHAVAN, Ashwin

IPC: C21D9/00 ,  B23P15/00 ,  B23K20/12 ,  C21D9/34 ,  C21D9/50

CPC classification number: C22F1/10 ,  B23K20/12 ,  B23K20/1275 ,  B23K33/00 ,  B23P15/006 ,  B32B15/01 ,  B32B15/043 ,  C21D9/0068 ,  C21D9/34 ,  C21D9/50 ,  C21D2261/00 ,  F01D9/02 ,  F05D2230/239

Abstract: A method of forming a hybrid component having an axis of rotation includes forming a first substrate having a first interface surface and a first average grain size, forming a second substrate having a second interface surface and a second average grain size different from the first average grain size, and inertia welding the first and second substrates at a junction of the first and second interface surfaces to form a solid-state joint between the first and second substrates.

Abstract translation: 形成具有旋转轴的混合部件的方法包括形成具有第一界面和第一平均粒度的第一基板，形成具有第二界面和不同于第一平均粒度的第二平均粒度的第二基板 尺寸和惯性将第一和第二基板焊接在第一和第二界面表面的接合处，以在第一和第二基板之间形成固态接合。

公开(公告)号：EP3308900A1

公开(公告)日：2018-04-18

申请号：EP17186219.6

申请日：2017-08-14

Applicant: United Technologies Corporation

Inventor： BOCHIECHIO, Mario P. ,  LIN, Wangen ,  SZELA, Edward R.

IPC: B23K35/30 ,  B23P15/00 ,  B23K20/16 ,  B23K35/00 ,  F01D5/34 ,  B23K101/00

CPC classification number: B23K20/16 ,  B23K20/026 ,  B23K20/233 ,  B23K35/001 ,  B23K35/004 ,  B23K35/304 ,  B23K2101/001 ,  B23P15/006 ,  F01D5/34 ,  F05D2230/232

Abstract: A method of forming a hybrid component (10) having an axis of rotation (18) includes forming a first substrate (20) having a first average grain size, forming a second substrate (22) having a second average grain size different from the first average grain size, positioning an interlayer (24) on one of the first and second substrates (20, 22), positioning a portion of the first substrate (20) adjacent a portion of the second substrate (22) such that the interlayer (24) extends between the portion of the first substrate (20) and the portion of the second substrate (22), heating the first and second substrates (20, 22) and the interlayer (24) at a temperature below the melting points of the first and second substrates (20, 22) to melt the interlayer (24), and isothermally solidifying the interlayer (24) to form a solid-state joint (26) between the portions of the first and second substrates (20, 22).

Abstract translation: 一种形成具有旋转轴线（18）的混合部件（10）的方法包括形成具有第一平均颗粒尺寸的第一基板（20），形成具有不同于第一平均颗粒尺寸的第二平均颗粒尺寸的第二基板（22） 平均晶粒尺寸，将中间层（24）定位在第一和第二衬底（20,22）中的一个上，将第一衬底（20）的一部分定位在第二衬底（22）的一部分附近，使得中间层 ）在第一衬底（20）的该部分和第二衬底（22）的该部分之间延伸，在低于第一衬底（22）的熔点的温度下加热第一和第二衬底（20,22）和中间层 和第二衬底（20,22）以熔化中间层（24），并且等温固化中间层（24）以在第一和第二衬底（20,22）的部分之间形成固态接头（26）。

公开(公告)号：EP3062954A1

公开(公告)日：2016-09-07

申请号：EP14857589.7

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: 一种再加工或修理部件的方法包括从由不可熔焊接的基础合金制造的部件去除铸造缺陷以形成导致通孔的空腔; 用背衬密封通孔; 并且用多个激光粉末沉积点的多个层来至少部分地填充所述空腔，所述多个激光粉末沉积点中的每一个由填充合金形成，所述多个层中的第一层包括所述多个 激光粉末沉积斑点与腔体的壁和背衬重叠。

公开(公告)号：EP3034651A1

公开(公告)日：2016-06-22

申请号：EP15199318.5

申请日：2015-12-10

Applicant: United Technologies Corporation

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

IPC: C23C24/10 ,  B23K9/04 ,  C23C28/02 ,  F01D5/28

CPC classification number: B23P6/007 ,  B22F1/025 ,  C23C24/106 ,  C23C28/022

Abstract: A method for coating a part according to an aspect of the disclosure includes the step binding a metallic powder (100) to a section (98) of the part. The metallic powder (100) is then energized which at least partially melts and resolidifies the metallic powder (100) to form a first metallic coating (102). After the first layer of metallic coating (102) is formed a second layer of metallic coating (110) is deposited on substantially all of the part.

Abstract translation: 根据本公开的一个方面的用于涂覆部件的方法包括将金属粉末（100）与部件的部分（98）结合的步骤。 金属粉末（100）然后通电，其至少部分地熔化并重新固化金属粉末（100）以形成第一金属涂层（102）。 在第一层金属涂层（102）形成之后，第二层金属涂层（110）沉积在基本上全部的部分上。