AU4180989A - Dual-alloy disk system - Google Patents

Dual-alloy disk system

Info

Publication number
AU4180989A
AU4180989A AU41809/89A AU4180989A AU4180989A AU 4180989 A AU4180989 A AU 4180989A AU 41809/89 A AU41809/89 A AU 41809/89A AU 4180989 A AU4180989 A AU 4180989A AU 4180989 A AU4180989 A AU 4180989A
Authority
AU
Australia
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.)
Abandoned
Application number
AU41809/89A
Inventor
Wilford H. Couts Jr.
Hugo E. Delgado
Thimoty E. Howson
John M. Hyzak
Steven H. Reichman
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Wyman Gordon Co
Original Assignee
Wyman Gordon Co
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Family has litigation
First worldwide family litigation filed litigation Critical https://patents.darts-ip.com/?family=26920031&utm_source=google_patent&utm_medium=platform_link&utm_campaign=public_patent_search&patent=AU4180989(A) "Global patent litigation dataset” by Darts-ip is licensed under a Creative Commons Attribution 4.0 International License.
Priority claimed from US07/225,907 external-priority patent/US5106012A/en
Application filed by Wyman Gordon Co filed Critical Wyman Gordon Co
Publication of AU4180989A publication Critical patent/AU4180989A/en
Abandoned legal-status Critical Current

Links

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B21MECHANICAL METAL-WORKING WITHOUT ESSENTIALLY REMOVING MATERIAL; PUNCHING METAL
    • B21KMAKING FORGED OR PRESSED METAL PRODUCTS, e.g. HORSE-SHOES, RIVETS, BOLTS OR WHEELS
    • B21K1/00Making machine elements
    • B21K1/28Making machine elements wheels; discs
    • B21K1/32Making machine elements wheels; discs discs, e.g. disc wheels
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B21MECHANICAL METAL-WORKING WITHOUT ESSENTIALLY REMOVING MATERIAL; PUNCHING METAL
    • B21JFORGING; HAMMERING; PRESSING METAL; RIVETING; FORGE FURNACES
    • B21J5/00Methods for forging, hammering, or pressing; Special equipment or accessories therefor
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01DNON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D5/00Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
    • F01D5/02Blade-carrying members, e.g. rotors

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.
AU41809/89A 1988-07-29 1989-07-28 Dual-alloy disk system Abandoned AU4180989A (en)

Applications Claiming Priority (4)

Application Number Priority Date Filing Date Title
US07/225,907 US5106012A (en) 1989-07-10 1988-07-29 Dual-alloy disk system
US225907 1988-07-29
US37792589A 1989-07-10 1989-07-10
US377925 1989-07-10

Related Child Applications (1)

Application Number Title Priority Date Filing Date
AU41565/93A Division AU4156593A (en) 1988-07-29 1993-06-28 Dual-alloy disk system

Publications (1)

Publication Number Publication Date
AU4180989A true AU4180989A (en) 1990-04-02

Family

ID=26920031

Family Applications (2)

Application Number Title Priority Date Filing Date
AU41809/89A Abandoned AU4180989A (en) 1988-07-29 1989-07-28 Dual-alloy disk system
AU41565/93A Abandoned AU4156593A (en) 1988-07-29 1993-06-28 Dual-alloy disk system

Family Applications After (1)

Application Number Title Priority Date Filing Date
AU41565/93A Abandoned AU4156593A (en) 1988-07-29 1993-06-28 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)

Families Citing this family (7)

* Cited by examiner, † Cited by third party
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
FR2723868B1 (en) * 1994-08-24 1996-09-20 Snecma PROCESS FOR OBTAINING A METAL CIRCULAR PIECE WITH BLADES
PL183445B1 (en) * 1996-02-29 2002-06-28 Siemens Ag Turbine shaft made of two different alloys
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

Family Cites Families (5)

* Cited by examiner, † Cited by third party
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
US4529452A (en) * 1984-07-30 1985-07-16 United Technologies Corporation Process for fabricating multi-alloy components

Also Published As

Publication number Publication date
JP2721721B2 (en) 1998-03-04
JPH04500040A (en) 1992-01-09
WO1990002479A3 (en) 1990-05-31
EP0431019B1 (en) 1994-06-22
GB9001813D0 (en) 1990-09-05
EP0431019A1 (en) 1991-06-12
GB2239826B (en) 1992-10-21
DE68916432T2 (en) 1995-01-19
DE68916432D1 (en) 1994-07-28
GB2239826A (en) 1991-07-17
WO1990002479A2 (en) 1990-03-22
ATE107558T1 (en) 1994-07-15
AU4156593A (en) 1993-09-30
EP0431019A4 (en) 1991-07-31

Similar Documents

Publication Publication Date Title
US3628226A (en) Method of making hollow compressor blades
US4883216A (en) Method for bonding an article projection
US4676843A (en) Process for joining component workpieces made of a superalloy employing the diffusion bonding process
US5099573A (en) Method of making hollow articles
US4934583A (en) Apparatus for bonding an article projection
IT9021627A1 (en) METHOD FOR MANUFACTURING DOUBLE ALLOY TURBINE DISCS
JPH04253532A (en) Manufacture of hollow metal product
JPS6137387A (en) Manufacture of integral multi-alloy part
US3588980A (en) Method for making a contoured article
US5072871A (en) Method of making hollow articles
GB2239826B (en) Dual-alloy disk system
US4527410A (en) Blade twisting apparatus
GB1119617A (en) Compressor blade for a gas turbine engine
ATE63709T1 (en) METHOD OF MAKING PROFILE PARTS BY GRINDING AND TURBO ENGINE BLADES MADE ACCORDINGLY.
EP0892173A1 (en) Process for manufacturing hydraulic turbine wheels and the wheels obtained thereby
JP2784686B2 (en) Manufacturing method of yoke member
IT1160151B (en) PROPELLER MANUFACTURING PROCEDURE
EP0360608A1 (en) Ion extraction grids
US11235395B2 (en) Controlled fracture machining method for producing through-holes
JPS6233039A (en) Forging method for discoid forging
US5217673A (en) Arrangement for the removal of an embedding body from the embedded component
SU956098A1 (en) Method of producing part with beaded hole
JPS6123528A (en) Method and tool for working ironing
JPS62267043A (en) Forging method for turbine blade
SU1174143A1 (en) Method of producing annular forgings having a hub and flange