GB2239826A - Dual-alloy disk system - Google Patents
Dual-alloy disk systemInfo
- Publication number
- GB2239826A GB2239826A GB9001813A GB9001813A GB2239826A GB 2239826 A GB2239826 A GB 2239826A GB 9001813 A GB9001813 A GB 9001813A GB 9001813 A GB9001813 A GB 9001813A GB 2239826 A GB2239826 A GB 2239826A
- Authority
- GB
- United Kingdom
- Prior art keywords
- die
- metal
- vents
- bonded
- pieces
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Granted
Links
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B21—MECHANICAL METAL-WORKING WITHOUT ESSENTIALLY REMOVING MATERIAL; PUNCHING METAL
- B21K—MAKING FORGED OR PRESSED METAL PRODUCTS, e.g. HORSE-SHOES, RIVETS, BOLTS OR WHEELS
- B21K1/00—Making machine elements
- B21K1/28—Making machine elements wheels; discs
- B21K1/32—Making machine elements wheels; discs discs, e.g. disc wheels
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B21—MECHANICAL METAL-WORKING WITHOUT ESSENTIALLY REMOVING MATERIAL; PUNCHING METAL
- B21J—FORGING; HAMMERING; PRESSING METAL; RIVETING; FORGE FURNACES
- B21J5/00—Methods for forging, hammering, or pressing; Special equipment or accessories therefor
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
- F01D5/00—Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
- F01D5/02—Blade-carrying members, e.g. rotors
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Forging (AREA)
- Pressure Welding/Diffusion-Bonding (AREA)
- Supporting Of Heads In Record-Carrier Devices (AREA)
- Superconductors And Manufacturing Methods Therefor (AREA)
- External Artificial Organs (AREA)
- Laminated Bodies (AREA)
Abstract
Two pieces of metal are bonded together at a surface by placing the two pieces into contact at the surface and forging the two pieces in a die which causes substantial displacement of the metal originally at the surface in a direction parallel to and outwardly from the edges of the surface and into vents in the face of the die and within the die impressions. The strain and displacement fields are controlled by the die and vent geometry which is designed to concentrate the strain and displacement along the original bondline. In this way, up to 99.9 %+ of the defects which are potientially present at the original surface are efficiently displaced with moving metal away from the original contact between the two pieces of metal into sacrificial ribs that form in the vents and the remaining defects are subjected to significant strain. A portion of the displaced metal which contains many of the defects and which forms the sacrificial ribs is removed from the resulting bonded workpiece as the sacrificial ribs are removed from the workpiece. The result is a bond with superior properties and with a bond surface which can be located very precisely both in orientation and location (e.g., radial distance from the center of a disk). This system is particularly appropriate for forming dual-alloy high-pressure turbine disks for gas turbines in which an annular peripheral ring of a second superalloy is bonded to a central core of a first superalloy. The system is particularly effective if, prior to forging, surfaces to be bonded are closely shape-conforming, are very clean, and are diffusion-bonded using hot isostatic pressing while the surfaces are gas-free. The sacrificial ribs are formed by vents in the impressions of the forging dies. The vents are adjacent to the outer edges of the bond surface. The system may be accomplished by using one or more strikes in the same dies or same die geometry, or may include multiple strikes in which only one side of the bond is in proximity to a vent during each strike. Subsequent strikes would process the bondline resulting from the previous strikes, but with the rib removed. The die impressions would be so shaped that the resulting die cavity would closely conform to the original workpiece shape, except for the vents, so that metal displacement and strain would be concentrated at the bondline.
Applications Claiming Priority (3)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US07/225,907 US5106012A (en) | 1989-07-10 | 1988-07-29 | Dual-alloy disk system |
US37792589A | 1989-07-10 | 1989-07-10 | |
PCT/US1989/003292 WO1990002479A2 (en) | 1988-07-29 | 1989-07-28 | Dual-alloy disk system |
Publications (3)
Publication Number | Publication Date |
---|---|
GB9001813D0 GB9001813D0 (en) | 1990-09-05 |
GB2239826A true GB2239826A (en) | 1991-07-17 |
GB2239826B GB2239826B (en) | 1992-10-21 |
Family
ID=26920031
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB9001813A Expired - Fee Related GB2239826B (en) | 1988-07-29 | 1990-01-26 | Dual-alloy disk system |
Country Status (7)
Country | Link |
---|---|
EP (1) | EP0431019B1 (en) |
JP (1) | JP2721721B2 (en) |
AT (1) | ATE107558T1 (en) |
AU (2) | AU4180989A (en) |
DE (1) | DE68916432T2 (en) |
GB (1) | GB2239826B (en) |
WO (1) | WO1990002479A2 (en) |
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB2292534A (en) * | 1994-08-24 | 1996-02-28 | Snecma | Process for obtaining a bladed circular metallic article |
WO1997032112A1 (en) * | 1996-02-29 | 1997-09-04 | Siemens Aktiengesellschaft | Turbine shaft consisting of two alloys |
Families Citing this family (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US5100050A (en) * | 1989-10-04 | 1992-03-31 | General Electric Company | Method of manufacturing dual alloy turbine disks |
US5161950A (en) * | 1989-10-04 | 1992-11-10 | General Electric Company | Dual alloy turbine disk |
US8480368B2 (en) * | 2010-02-05 | 2013-07-09 | General Electric Company | Welding process and component produced therefrom |
US8956700B2 (en) | 2011-10-19 | 2015-02-17 | General Electric Company | Method for adhering a coating to a substrate structure |
KR101347034B1 (en) | 2012-11-20 | 2014-01-03 | 주식회사 노아닉스 | Coating apparatus for stents |
CN114453542B (en) * | 2022-02-10 | 2024-08-23 | 浙江申吉钛业股份有限公司 | Manufacturing method of titanium alloy bimetal for compressor disc of gas turbine engine |
Citations (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3046640A (en) * | 1957-12-04 | 1962-07-31 | Reynolds Metals Co | Process and product of zinc and aluminum lamination |
US3098022A (en) * | 1960-08-11 | 1963-07-16 | Anthony J Karnie | Covering a core by extrusion |
US3259969A (en) * | 1963-01-22 | 1966-07-12 | Central Cable Corp | Method of making butt welded joints |
US4094453A (en) * | 1976-08-02 | 1978-06-13 | Alforge Metals Corporation, Limited | Method for pressure welding metal workpieces |
Family Cites Families (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4529452A (en) * | 1984-07-30 | 1985-07-16 | United Technologies Corporation | Process for fabricating multi-alloy components |
-
1989
- 1989-07-28 EP EP89909656A patent/EP0431019B1/en not_active Expired - Lifetime
- 1989-07-28 JP JP1509044A patent/JP2721721B2/en not_active Expired - Lifetime
- 1989-07-28 AU AU41809/89A patent/AU4180989A/en not_active Abandoned
- 1989-07-28 WO PCT/US1989/003292 patent/WO1990002479A2/en active IP Right Grant
- 1989-07-28 DE DE68916432T patent/DE68916432T2/en not_active Expired - Fee Related
- 1989-07-28 AT AT89909656T patent/ATE107558T1/en not_active IP Right Cessation
-
1990
- 1990-01-26 GB GB9001813A patent/GB2239826B/en not_active Expired - Fee Related
-
1993
- 1993-06-28 AU AU41565/93A patent/AU4156593A/en not_active Abandoned
Patent Citations (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3046640A (en) * | 1957-12-04 | 1962-07-31 | Reynolds Metals Co | Process and product of zinc and aluminum lamination |
US3098022A (en) * | 1960-08-11 | 1963-07-16 | Anthony J Karnie | Covering a core by extrusion |
US3259969A (en) * | 1963-01-22 | 1966-07-12 | Central Cable Corp | Method of making butt welded joints |
US4094453A (en) * | 1976-08-02 | 1978-06-13 | Alforge Metals Corporation, Limited | Method for pressure welding metal workpieces |
Cited By (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB2292534A (en) * | 1994-08-24 | 1996-02-28 | Snecma | Process for obtaining a bladed circular metallic article |
GB2292534B (en) * | 1994-08-24 | 1998-03-11 | Snecma | Process for obtaining a bladed circular metallic article |
WO1997032112A1 (en) * | 1996-02-29 | 1997-09-04 | Siemens Aktiengesellschaft | Turbine shaft consisting of two alloys |
CN1083525C (en) * | 1996-02-29 | 2002-04-24 | 西门子公司 | Turbine shaft |
Also Published As
Publication number | Publication date |
---|---|
DE68916432T2 (en) | 1995-01-19 |
EP0431019A4 (en) | 1991-07-31 |
WO1990002479A2 (en) | 1990-03-22 |
JP2721721B2 (en) | 1998-03-04 |
EP0431019A1 (en) | 1991-06-12 |
DE68916432D1 (en) | 1994-07-28 |
GB9001813D0 (en) | 1990-09-05 |
JPH04500040A (en) | 1992-01-09 |
GB2239826B (en) | 1992-10-21 |
EP0431019B1 (en) | 1994-06-22 |
AU4156593A (en) | 1993-09-30 |
ATE107558T1 (en) | 1994-07-15 |
WO1990002479A3 (en) | 1990-05-31 |
AU4180989A (en) | 1990-04-02 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
713B | Proceeding under section 13(1) patents act 1977 | ||
713B | Proceeding under section 13(1) patents act 1977 | ||
PCNP | Patent ceased through non-payment of renewal fee |
Effective date: 19990728 |