-
公开(公告)号：WO0187528A3
公开(公告)日：2002-02-28
申请号：PCT/US0140155
申请日：2001-02-21
Applicant: CHROMALLOY GAS TURBINE CORP
Inventor： FOSTER MICHAEL , UPDEGROVE KEVIN
IPC: F02C7/00 , B23K9/04 , B23K9/23 , B23K20/00 , B23K26/34 , B23K28/02 , B23K31/00 , B23K35/30 , B23K103/08 , B23K23/00
CPC classification number: B23K20/002 , B23K9/04 , B23K26/32 , B23K26/34 , B23K26/342 , B23K35/0244 , B23K35/3033 , B23K35/304 , B23K35/3046 , B23K2201/00 , B23K2201/001 , B23K2203/26
Abstract: A process is provided for welding a nickel or cobalt based superalloy article to minimize cracking by preheating the entire weld area to a maximum ductility temperature range, maintaining such temperature during welding and solidification of the weld, raising the temperature for stress relief of the superalloy, then cooling at a rate effective to minimize gamma prime precipitation.
Abstract translation: 提供了用于焊接镍或钴基超级合金制品以通过将整个焊接区域预热到最大延展性温度范围来最小化裂纹的过程，在焊接和固化焊接期间保持这种温度，提高超合金的应力消除温度， 然后以有效降低伽马质量降水的速率冷却。
-
公开(公告)号：JPH10183363A
公开(公告)日：1998-07-14
申请号：JP28390897
申请日：1997-10-16
Applicant: CHROMALLOY GAS TURBINE CORP
Inventor： KANG DAVID , UPDEGROVE KEVIN , GOODWATER FRANK
Abstract: PROBLEM TO BE SOLVED: To prevent the adhesion due to plating to cooling holes and to prevent a harmful affect to the flow of a cooling air by plating the outer surface of a component after pouring a masking material into the cooling path of the gas turbine engine component and charging plural cooling holes, and next removing the masking material. SOLUTION: The gas turbine engine component is pre-heated, the high temperature of molten masking material 5 is poured into cooling holes 4 under an effective pressure, and the masking material 5 is charged into the cooling path so as to be uniform with the surface of the component. Plating containing a noble metal of platinum or the like with a protective adhesive is applied on the outer surface of the component after aging and curing the masking material 5. The masking material 5 is removed after finishing plating. In the case of removing the masking material 5, the masking material 5 is removed by volatilizing with a high temperature added for an effective time. The masking material 5 is usually removed with the heat treatment of about 1,100-1,700 deg.F for 15-30 minutes and the surface of the super alloy being the component ins not harmfully affected with such temperature.
-
3.发明公开
公开(公告)号：EP1169495A4
公开(公告)日：2002-09-11
申请号：EP99967257
申请日：1999-12-10
Applicant: CHROMALLOY GAS TURBINE CORP
Inventor： UPDEGROVE KEVIN , GOODWATER FRANK , FAY WILLIAM
CPC classification number: C25F5/00
Abstract: A process is provided to strip a metallic coating from a turbine blade comprising attaching the blade to a positive lead from a power supply, submersing a portion of the blade with a metallic coating to be stripped into a bath of acidic electro stripping solution, said bath containing a negative lead from a power supply attached to a conductive grid; and providing a current to the blade in the bath for a period of time effective to remove the coating on the portion of the blade.
Abstract translation: 提供了一种从涡轮机叶片剥离金属涂层的方法，包括将叶片连接到来自电源的正极引线上，用金属涂层浸没叶片的一部分以剥离到酸性电剥离溶液浴中，所述浴 含有来自连接到导电栅格的电源的负极导线; 并向浴槽中的叶片提供电流一段时间，以有效去除叶片部分上的涂层。
-
公开(公告)号：EP1296796A4
公开(公告)日：2007-07-11
申请号：EP01964537
申请日：2001-02-21
Applicant: CHROMALLOY GAS TURBINE CORP
Inventor： FOSTER MICHAEL , UPDEGROVE KEVIN
IPC: F02C7/00 , B23K9/04 , B23K9/23 , B23K20/00 , B23K26/34 , B23K28/02 , B23K31/00 , B23K35/30 , B23K103/08 , B23K1/00
CPC classification number: B23K20/002 , B23K9/04 , B23K26/32 , B23K26/34 , B23K26/342 , B23K35/0244 , B23K35/3033 , B23K35/304 , B23K35/3046 , B23K2201/00 , B23K2201/001 , B23K2203/26
Abstract: A process is provided for welding a nickel or cobalt based superalloy article to minimize cracking by preheating the entire weld area to a maximum ductility temperature range, maintaining such temperature during welding and solidification of the weld, raising the temperature for stress relief of the superalloy, then cooling at a rate effective to minimize gamma prime precipitation.
-
公开(公告)号：EP1165281A4
公开(公告)日：2002-09-25
申请号：EP00902329
申请日：2000-01-04
Applicant: CHROMALLOY GAS TURBINE CORP
Inventor： FOSTER MICHAEL , KNOWLES THOMAS E , UPDEGROVE KEVIN , THURSTON CHRISTOPHER A
CPC classification number: B23K26/123 , B23K26/12 , B23K26/127 , B23K26/21 , B23K2201/001
Abstract: A protective gas shroud (1) for welding is provided by: positioning an article (2) into a chamber (4) having an opening at the top to permit welding of the article; introducing argon (8) into the body of the chamber to act as a protective gas shroud for the article during welding; introducing helium (10) into the open top of the chamber to assist in maintaining a protective gas shroud around the article during welding; and welding the article within the protective gas shroud.
-
Patent Agency Ranking
公开(公告)号：EP1385668A4
公开(公告)日：2007-09-12
申请号：EP02721107
申请日：2002-02-12
Applicant: CHROMALLOY GAS TURBINE CORP
Inventor： UPDEGROVE KEVIN , BADER PETER , FOSTER MICHAEL
CPC classification number: B23P6/005 , F01D5/005 , F01D5/20 , Y10T29/49318 , Y10T29/49336 , Y10T29/4973 , Y10T29/49737
Abstract: A blade tip cap of turbine blade is repaired by restoring the tip rail (4) and attaching a strengthening rib (5) across the blade tip cap connecting the concave wall to the convex wall of the tip rail.
-
公开(公告)号：AT511422T
公开(公告)日：2011-06-15
申请号：AT01964537
申请日：2001-02-21
Applicant: CHROMALLOY GAS TURBINE CORP
Inventor： FOSTER MICHAEL , UPDEGROVE KEVIN
IPC: B23K1/00 , F02C7/00 , B23K9/04 , B23K9/23 , B23K20/00 , B23K26/34 , B23K28/02 , B23K31/00 , B23K35/30 , B23K103/08
Abstract: A process is provided for welding a nickel or cobalt based superalloy article to minimize cracking by preheating the entire weld area to a maximum ductility temperature range, maintaining such temperature during welding and solidification of the weld, raising the temperature for stress relief of the superalloy, then cooling at a rate effective to minimize gamma prime precipitation.
-
公开(公告)号：CA2217843C
公开(公告)日：2006-07-11
申请号：CA2217843
申请日：1997-10-09
Applicant: CHROMALLOY GAS TURBINE CORP
Inventor： GOODWATER FRANK , UPDEGROVE KEVIN , KANG DAVID
Abstract: A process is provided for plating a coating onto a gas turbine engine component without detrimentally effecting air flow through cooling holes by injecting a maskant into the cooling passage to fill the cooling holes with the maskant, plating the external surface of the component with a coating, then removing the maskant from the component.
-
公开(公告)号：AT282139T
公开(公告)日：2004-11-15
申请号：AT01901747
申请日：2001-01-05
Applicant: SIEMENS WESTINGHOUSE POWER , CHROMALLOY GAS TURBINE CORP
Inventor： SINNOTT ZACHARY , SMITH KEVIN D , JUNKIN JOHN E , UPDEGROVE KEVIN , FOSTER MICHAEL F , LOVELACE DANIEL
IPC: F01D5/18 , B23K9/167 , B23K9/235 , B23K31/00 , B23P6/00 , F01D5/00 , F01D5/20 , F01D5/28 , F01D25/00 , F02C7/00
Abstract: A method for repairing a turbine blade (10) wherein the tip (16) of the blade is removed (41,43) and a replacement cap is attached by welding (49). The cap may consist of a plate (48) attached by welding and a squealer (54) formed by depositing weld material (52), as illustrated in FIG. 3. The plate and/or squealer may be formed from a material different from the material of the airfoil portion (42) of the blade in order to optimize the performance of the blade.
-
公开(公告)号：PT843026E
公开(公告)日：2001-12-28
申请号：PT97117725
申请日：1997-10-14
Applicant: CHROMALLOY GAS TURBINE CORP
Inventor： KANG DAVID , UPDEGROVE KEVIN , GOODWATER FRANK
Abstract: A process is provided for plating a coating onto a gas turbine engine component without detrimentally effecting air flow through cooling holes by injecting a maskant into the cooling passage to fill the cooling holes with the maskant, plating the external surface of the component with a coating, then removing the maskant from the component.
-
-
-
-
-
-
-
-
-
Search Results
48
records
(took 0.038 seconds)
