公开(公告)号：SG137813A1

公开(公告)日：2007-12-28

申请号：SG2007037526

申请日：2007-05-24

Applicant: UNITED TECHNOLOGIES CORP

Inventor： MALLEY DAVID R

Abstract: A method for repairing a turbine engine component comprises the steps of providing a turbine engine component formed from a nickel-based superalloy, removing any defects from the turbine engine component, the removing step comprising subjecting the turbine engine component to a solutioning heat treatment using a heating rate in the range of from 29 degrees Fahrenheit/minute to approximately 40 degrees Fahrenheit/minute as the component passes through a temperature in the range of from 1100 degrees Fahrenheit to 1600 degrees Fahrenheit, and welding the turbine engine component to effect the repair. A deliberately slow post solution treatment cooling rate is used to substantially prevent weld cracks.

公开(公告)号：SG122036A1

公开(公告)日：2006-05-26

申请号：SG200508431

申请日：2005-10-26

Applicant: UNITED TECHNOLOGIES CORP

Inventor： IVORY STEVEN ,  ECHEVARRIA JOSE A ,  LOMASNEY GARY L ,  MALLEY DAVID R ,  MCMAHON KEVIN C ,  MOOR JAMES J ,  ROKICKI JOSEPH

Abstract: A method of repairing a braze joint (16) and the resulting joint includes removing an unsuitable portion (20) of a first joining material (18) in a joint (16) between a first member (12) and a second member (14) of an aerospace assembly (10) and cleaning the joint (16). A stripping solution is used to remove the unsuitable portion (20) of the first joining material (18). A first cleaning solution is used to clean the joint (16), and the joint (16) is further cleaned using a second cleaning solution. During a rebrazing step, a second joining material (60) moves into a void left by the removed unsuitable portion (20) from the removal step to form a new joint between the first member (12) and the second member (14) that includes the remaining first joining material (18) and the second joining material (60).

公开(公告)号：IT1181942B

公开(公告)日：1987-09-30

申请号：IT2426284

申请日：1984-12-27

Applicant: UNITED TECHNOLOGIES CORP

Inventor： PAULONIS DANIEL F ,  MALLEY DAVID R ,  BROWN EDGARD E

IPC: C22C19/05 ,  B21J1/06 ,  B21J5/00 ,  B21K1/32 ,  B21K1/36 ,  C22F1/10 ,  C22C

Abstract: Forging processes are described for cast superalloys. The forgeability of superalloy materials is improved by the development of overaged microstructure. The total forging process is usually performed in a series of steps with intervening heat treatments to reform the overaged microstructure.

公开(公告)号：GB2151951A

公开(公告)日：1985-07-31

申请号：GB8431277

申请日：1984-12-12

Applicant: UNITED TECHNOLOGIES CORP

Inventor： PAULONIS DANIEL F ,  MALLEY DAVID R ,  BROWN EDGAR E

IPC: C22C19/05 ,  B21J1/06 ,  B21J5/00 ,  B21K1/32 ,  B21K1/36 ,  C22F1/10 ,  B21K1/28

Abstract: Forging processes are described for cast superalloys. The forgeability of superalloy materials is improved by the development of overaged microstructure. The total forging process is usually performed in a series of steps with intervening heat treatments to reform the overaged microstructure.

公开(公告)号：NO845117L

公开(公告)日：1985-06-28

申请号：NO845117

申请日：1984-12-20

Applicant: UNITED TECHNOLOGIES CORP

Inventor： PAULONIS DANIEL F ,  MALLEY DAVID R ,  BROWN EDGAR E

IPC: B21J1/06 ,  C22C19/05 ,  B21J5/00 ,  B21K1/32 ,  B21K1/36 ,  C22F1/10 ,  C22F

Abstract: Forging processes are described for cast superalloys. The forgeability of superalloy materials is improved by the development of overaged microstructure. The total forging process is usually performed in a series of steps with intervening heat treatments to reform the overaged microstructure.

公开(公告)号：NO845117A

公开(公告)日：1985-06-28

申请号：NO845117

申请日：1984-12-20

Applicant: UNITED TECHNOLOGIES CORP

Inventor： PAULONIS DANIEL F ,  MALLEY DAVID R ,  BROWN EDGAR E

IPC: C22C19/05 ,  B21J1/06 ,  B21J5/00 ,  B21K1/32 ,  B21K1/36 ,  C22F1/10 ,  C22F

CPC classification number: C22F1/10 ,  B21J5/00 ,  B21K1/32

公开(公告)号：DK609584A

公开(公告)日：1985-06-28

申请号：DK609584

申请日：1984-12-19

Applicant: UNITED TECHNOLOGIES CORP

Inventor： BROWN EDGAR E ,  MALLEY DAVID R ,  PAULONIS DANIEL F

IPC: C22C19/05 ,  B21J1/06 ,  B21J5/00 ,  B21K1/32 ,  B21K1/36 ,  C22F1/10 ,  C22F

Abstract: Forging processes are described for cast superalloys. The forgeability of superalloy materials is improved by the development of overaged microstructure. The total forging process is usually performed in a series of steps with intervening heat treatments to reform the overaged microstructure.

公开(公告)号：DK609584D0

公开(公告)日：1984-12-19

申请号：DK609584

申请日：1984-12-19

Applicant: UNITED TECHNOLOGIES CORP

Inventor： BROWN EDGAR E ,  MALLEY DAVID R ,  PAULONIS DANIEL F

IPC: C22C19/05 ,  B21J1/06 ,  B21J5/00 ,  B21K1/32 ,  B21K1/36 ,  C22F1/10 ,  C22F

Abstract: Forging processes are described for cast superalloys. The forgeability of superalloy materials is improved by the development of overaged microstructure. The total forging process is usually performed in a series of steps with intervening heat treatments to reform the overaged microstructure.