US3677835A - Homogeneous nickel-base superalloy castings - Google Patents

Homogeneous nickel-base superalloy castings Download PDF

Info

Publication number
US3677835A
US3677835A US81229A US3677835DA US3677835A US 3677835 A US3677835 A US 3677835A US 81229 A US81229 A US 81229A US 3677835D A US3677835D A US 3677835DA US 3677835 A US3677835 A US 3677835A
Authority
US
United States
Prior art keywords
dendritic
cellular
castings
homogeneous
nickel
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.)
Expired - Lifetime
Application number
US81229A
Inventor
John K Tien
Robert P Gamble
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.)
Raytheon Technologies Corp
Original Assignee
United Aircraft Corp
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
Application filed by United Aircraft Corp filed Critical United Aircraft Corp
Application granted granted Critical
Publication of US3677835A publication Critical patent/US3677835A/en
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Images

Classifications

    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22CALLOYS
    • C22C19/00Alloys based on nickel or cobalt
    • C22C19/03Alloys based on nickel or cobalt based on nickel
    • C22C19/05Alloys based on nickel or cobalt based on nickel with chromium
    • C22C19/051Alloys based on nickel or cobalt based on nickel with chromium and Mo or W
    • C22C19/055Alloys based on nickel or cobalt based on nickel with chromium and Mo or W with the maximum Cr content being at least 20% but less than 30%
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B22CASTING; POWDER METALLURGY
    • B22DCASTING OF METALS; CASTING OF OTHER SUBSTANCES BY THE SAME PROCESSES OR DEVICES
    • B22D27/00Treating the metal in the mould while it is molten or ductile ; Pressure or vacuum casting
    • B22D27/04Influencing the temperature of the metal, e.g. by heating or cooling the mould
    • B22D27/045Directionally solidified castings
    • CCHEMISTRY; METALLURGY
    • C30CRYSTAL GROWTH
    • C30BSINGLE-CRYSTAL GROWTH; UNIDIRECTIONAL SOLIDIFICATION OF EUTECTIC MATERIAL OR UNIDIRECTIONAL DEMIXING OF EUTECTOID MATERIAL; REFINING BY ZONE-MELTING OF MATERIAL; PRODUCTION OF A HOMOGENEOUS POLYCRYSTALLINE MATERIAL WITH DEFINED STRUCTURE; SINGLE CRYSTALS OR HOMOGENEOUS POLYCRYSTALLINE MATERIAL WITH DEFINED STRUCTURE; AFTER-TREATMENT OF SINGLE CRYSTALS OR A HOMOGENEOUS POLYCRYSTALLINE MATERIAL WITH DEFINED STRUCTURE; APPARATUS THEREFOR
    • C30B15/00Single-crystal growth by pulling from a melt, e.g. Czochralski method
    • CCHEMISTRY; METALLURGY
    • C30CRYSTAL GROWTH
    • C30BSINGLE-CRYSTAL GROWTH; UNIDIRECTIONAL SOLIDIFICATION OF EUTECTIC MATERIAL OR UNIDIRECTIONAL DEMIXING OF EUTECTOID MATERIAL; REFINING BY ZONE-MELTING OF MATERIAL; PRODUCTION OF A HOMOGENEOUS POLYCRYSTALLINE MATERIAL WITH DEFINED STRUCTURE; SINGLE CRYSTALS OR HOMOGENEOUS POLYCRYSTALLINE MATERIAL WITH DEFINED STRUCTURE; AFTER-TREATMENT OF SINGLE CRYSTALS OR A HOMOGENEOUS POLYCRYSTALLINE MATERIAL WITH DEFINED STRUCTURE; APPARATUS THEREFOR
    • C30B29/00Single crystals or homogeneous polycrystalline material with defined structure characterised by the material or by their shape
    • C30B29/10Inorganic compounds or compositions
    • C30B29/52Alloys

Definitions

  • the present invention relates in general to the nickelbase superalloy iield and, more particularly, to such alloys as processed to provide castings characterized by a cellular or plane front cast microstructure and the substantial absence of dendritic segregation.
  • the nickel-base superalloys are, of course, recognized as those alloys particularly adapted to high temperature operation in demanding environments such as those associated with the operation of gas turbine engines.
  • they consist of a nickel chromium solid solution matrix ('y phase) strengthened by aluminum and titanium in the form of a precipitate usually represented by the formula Ni3(Al,Ti) ('y' phase).
  • nickel chromium solid solution matrix 'y phase
  • they also normally include cobalt and the refractory metals for solution strengthening and often carbon, boron and zirconium.
  • This invention contemplates the achievement of homogeniety of structure in the constitutionally complex alloys, such as the nickel-base superalloys, by the suppression of dendritic growth, and manifested in the achievement o cellular and plane front cast microstructures.
  • FIG. l is a graphic representation of the degree of tungsten segregation normal to the growth direction in dendrictic crystals of MAR-M200.
  • FIG. 2 is a similar graphic representation for cellular/ plane front crystals in the same alloy system.
  • FIG. 3 depicts the high cycle fatigue limit of dendritic material with and without carbides as contrasted with plane front material without carbides.
  • FIG. 4 is a graph comparing the tensile yield strength and ductility of MAR-M200 single crystals, contrasting the properties of dendritic and cellular/ plane front structures.
  • the MAR-M200 alloy was selected as representative of one of the more constitutionally complex nickel-base superalloys and, inasmuch as it has been extensively investigated in columnar grained and monocrystal form, properties are readily available for the purposes of comparison. Accordingly, castings to the MAR-M200 chemistry were unidirectionally solidified according to the present invention in a vertical crystal grower of the type described in the aforementioned Ver Snyder patent, modified to provide positively controlled motion of the soliditication front. This was accomplished through the programmed movement of a single turn induction coil upward of the casting mold. As a matter of practice the coil was utilized to provide localized heating with portions of the ingot above and below the localized heating zone in a solidified state. With effective zone melting of this nature better casting constitutional homogeniety was felt possible. However, solidication upward from the melt is also perfectly feasible.
  • the homogeneous castings of the present invention have been provided by severely curtailing the depth of the mushy zone to inhibit the dendritic growth occurring therein.
  • the single turn induction coil is utilized to establish a high thermal gradient, typically 300-900 F. at the solid/melt interface, limiting the mushy zone to a maximum of about 1/2 inch in depth in this apparatus.
  • a programmed upward movement of the coil at a rate of about 0.2 inch/hour, with a corresponding upward velocity of the interface, has been formed to provide the cellular and plane front structures sought.
  • the mushy zone In a slow solidication rate process, it has been established, as previously mentioned, that the mushy zone must not exceed about 1A. inch in depth. Typically, the aim depth will be 1 centimeter or less and it has been conclusively established that at a Adepth of l centimeter a cellular structure is provided and at a mushy zone depth of 1 millimeter a plane front structure is achieved.
  • the unique cast structures Idescribed exhibit significantly improved physical properties even when compared to the advanced columnar-grained and monocrystalline articles obtained as taught by Ver Snyder and Piearcey.
  • these improvements include a substantial enhancement of ductility, significant improvement in fatigue properties, higher incipient melting temperature and elimination of surface defects (freckles) from single crystals.
  • FIGS. 1 and 2 show the degree of tungsten segregation normal to the growth direction in dendritic and cellular/ plane front crystals of MAR-M200 as ascertained by a microprobe scan.
  • the scan data are normalized relative to the tungsten concentration in the center of the dendrites or cells, respectively.
  • the tungsten distribution is nearly homogeneous throughout the section.
  • all other alloy additions must also be hornogeneously distributed since tungsten, with its low diiusivity, is the most ditlicult element to homogenize.
  • the dendritic material has a nonuni- 4 form 'y' size and distribution with finer 'y' precipitates occurring in the dendrites (high tungsten, low aluminum and titanium) and large 'y' precipitates in the interdendritic regions (low tungsten, high aluminum and titanium).
  • the cellular/ plane front structures exhibit a uniform fy' size and distribution.
  • One benefit of a uniform 'y' size is an expected improved creep resistance resulting from the increased phase stability associated with precipitates of uniform spatial morphology. This is of extreme importance in high volume fraction 'y' alloys such as NX-188 (8 Al, 18 Mo, balance Ni) wherein the 'y' morphology is typically extremely heterogeneous because of dendritic segregation.
  • the low melting Fy' phase (also often referred to as eutectic or massive 7') normally associated with the interdendritic regions is not present in the cellular/plane front castings.
  • this elimination of the low density melting phases raises the incipient melting point of the alloy at least 75 F., from 2265 iF. to 23400 F.
  • Carbides forming during casting are not nonequilibrium phases and are present even in homogeneous cast structures.
  • the deleterious eli'ects thereof, when present, are greatly reduced in the cellular/plane front crystals, the ⁇ MC carbides exhibiting precracldng in the dendritic structure but not in the castings of the present invention.
  • FIGS. 3 and 4 compare the properties of the old and new structures. There is a four-fold improvement in the ductility of cellular MAR-M200 single crystals over that of dendritic crystals between room temperature and 1400 F.
  • Unidirectionally solidified castings composed of an alloy consisting essentially of, by weight, up to about 25 percent chromium, 4-10 percent selected from the group consisting of aluminum, titanium and columbium, up to A3-0 percent cobalt, 3-20 percent selected from the group consisting of molybdenum, tantalum and tungsten, up to about 5 percent selected from the group consisting of boron, zirconium, hafnium and carbon, and at least 45 percent nickel, exhibiting a cellular/plane front microstructure and characterized by the substantial absence of dendrites.
  • Castings according to claim 1 further characterized by a monocrystalline microstructure.

Abstract

D R A W I N G
HOMOGENEOUS CASTING ARE ACHIEVED IN THE NICKEL-BASE SUPERALLOY SYSTEMS BY THE SUPPRESSION OF DENDRITIC SEGREGATION IN CONTROLLED UNIDIRECTIONAL SOLIDIFICATION, THE CASTING BEING CHARACTERIZED BY CELLULAR AND PLANE FRONT MICROSTRUCTURES.

Description

July 18, 1972 J, K. TIEN ETAL 3,671,835
HOMOGENEOUS NICKEL-BASESUPERALLOY CASTINGS Filed Oct. 16, 1970 2 Sheets-Sheet 1 W6. Z ZV O-Ooooda g l 0 au 5am/099V o /00 20a @'00 42630 5&0
ST/Q/r/ff ffm/R554 /f/fa/VJ July 18, 1972 J. K. TIEN ETAL HOMOGENEOUS NICKEL-BASE SUPERALLOY CASTINGS 2 Sheets-Sheet 2 Filed Oct. 16, 1970 z Q l.. llll I l l l l l ll W l\l\\l\\l\l\. KN l UI a @l UKQQ. l n MAYYMQ n ww wwmklw //Y 332729Z@ @7.5% ZZ@ United States Patent O 3,677,835 HOMOGENEOUS NICKEL-BASE SUPERALLOY CASTINGS John K. Tien, Rocky Hill, and Robert P. Gamble, Killing- Worth, Conn., assignors to United Aircraft Corporation, East Hartford, Conn.
Filed Oct. 16, 1970, Ser. No. 81,229 Int. Cl. C22c 19/00 U.S. Cl. 14S-32.5 4 Claims ABSTRACT OF THE DISCLOSURE Homogeneous castings are achieved in the nickel-base superalloy systems by the suppression of dendritic segregation. in controlled unidirectional solidication, the castings being characterized by cellular and plane front microstructures.
BACKGROUND OF THE INVENTION The present invention relates in general to the nickelbase superalloy iield and, more particularly, to such alloys as processed to provide castings characterized by a cellular or plane front cast microstructure and the substantial absence of dendritic segregation.
The nickel-base superalloys are, of course, recognized as those alloys particularly adapted to high temperature operation in demanding environments such as those associated with the operation of gas turbine engines. Typically, they consist of a nickel chromium solid solution matrix ('y phase) strengthened by aluminum and titanium in the form of a precipitate usually represented by the formula Ni3(Al,Ti) ('y' phase). In addition they also normally include cobalt and the refractory metals for solution strengthening and often carbon, boron and zirconium.
Representative of such alloys are the following:
Description: Composition (by weight) Udimet 700 15% Cr, 18.5% Co, 3.25% Ti, 4.25% Al, 5%- Mo, .1% C,
.03% B, balance Ni. B-l900 3% Cr, 10% Co, 1% Ti, 6% Al, 6% Mo, .11% C, 4.3% Ta, .07% Zr, .15% B, balance Ni. 9% Cr, 10% Co, 2% Ti, 5% Al, 12.5% W, .15% C, 1% Cb, 0.15% B, .05% Zr, balance Ni.
A common feature of all current nickel-base superalloy cast structures is the presence of dendritic segregation. Recently, through controlled unidirectional solidiiication techniques, the extent of constitutional inhomogeniety and other deleterious structural manifestations of dendritic segregation has been significantly reduced, or controlled, resulting in more homogeneous cast structures. Thus, the ancient art of structural manipulation of metals has received new impetus through these recent advances in certain casting processes. One of these recent advances in directional solidication is disclosed by Ver Snyder in U.S. Pat. No. 3,260,505 providing aligned grain boundaries in superalloy castings, and by Piearcey in U.S. Pat. No. 3,494,709 -wherein grain boundaries are eliminated.
While the ensuing columnar grained and monocrystalline castings possess near optimum grain morphology and superior overall properties for elevated temperature applications, complete elimination of dendritic segregation would be additionally advantageous. Depending on the particular superalloy chemistry such segregation can result in the formation of low melting or brittle phases, nonuniform distribution of the strengthening precipitates, interdendritic porosity and, surface freckles. In a specic application, one or more of these structural manifestations of dendritic segregation can be undesirable.
MAR-M200 Cil 3,677,835 Patented July 18, 1972 ICC In a number of alloy systems the means for eliminating or minimizing dendritic segregation are traditionally dependent upon either a solid state diffusion or mechanical working of the casting. However, the nickel-base superalloys, and other constitutionally complex alloys, strongly resist solid state homogenization, and under no circumstances is porosity eliminated by heat treatment. Furthermore, mechanical working negates the advantages of shape casting and oriented grain structures, either columnar or single crystal.
SUMMARY OF THE INVENTION This invention contemplates the achievement of homogeniety of structure in the constitutionally complex alloys, such as the nickel-base superalloys, by the suppression of dendritic growth, and manifested in the achievement o cellular and plane front cast microstructures.
BRIEF DESCRIPTION OF THE DRAWINGS FIG. l is a graphic representation of the degree of tungsten segregation normal to the growth direction in dendrictic crystals of MAR-M200.
FIG. 2 is a similar graphic representation for cellular/ plane front crystals in the same alloy system.
FIG. 3 depicts the high cycle fatigue limit of dendritic material with and without carbides as contrasted with plane front material without carbides.
FIG. 4 is a graph comparing the tensile yield strength and ductility of MAR-M200 single crystals, contrasting the properties of dendritic and cellular/ plane front structures.
DESCRIPTION O-F THE PREFERREDy EMBODIMENTS The approach utilized herein contemplates the suppression of dendritic :growth during solidiiication to provide unique cast nickel-base superalloy structures displaying significant improvements in physical properties. The resulting cellular and plane front cast structures have never before been achieved in these alloys to the best of the inventors knowledge.
The MAR-M200 alloy was selected as representative of one of the more constitutionally complex nickel-base superalloys and, inasmuch as it has been extensively investigated in columnar grained and monocrystal form, properties are readily available for the purposes of comparison. Accordingly, castings to the MAR-M200 chemistry were unidirectionally solidified according to the present invention in a vertical crystal grower of the type described in the aforementioned Ver Snyder patent, modified to provide positively controlled motion of the soliditication front. This was accomplished through the programmed movement of a single turn induction coil upward of the casting mold. As a matter of practice the coil was utilized to provide localized heating with portions of the ingot above and below the localized heating zone in a solidified state. With effective zone melting of this nature better casting constitutional homogeniety was felt possible. However, solidication upward from the melt is also perfectly feasible.
In the Ver Snyder process, as disclosed in the patent, columnar grain growth is achieved by removing heat from the melt through a water-cooled chill plate at the bottom of the mold while the power to the heating coils is o. This is, of course, unidirectional solidilication. In the Ver Snyder process dendrites are formed by upward growth in a so-called mushy zone which precedes the advancing solid/melt interface and is perhaps 3-9 inches in depth, depending upon the system parameters.
The homogeneous castings of the present invention have been provided by severely curtailing the depth of the mushy zone to inhibit the dendritic growth occurring therein. For this purpose, the single turn induction coil is utilized to establish a high thermal gradient, typically 300-900 F. at the solid/melt interface, limiting the mushy zone to a maximum of about 1/2 inch in depth in this apparatus. A programmed upward movement of the coil at a rate of about 0.2 inch/hour, with a corresponding upward velocity of the interface, has been formed to provide the cellular and plane front structures sought.
In general, in the solidcation process categorized by slow soliditication rates, the higher the thermal gradient the higher the soliditication rate achievable, particularly in the apparatus described. This is true since the high gradient, of course, limits the extent of dendritic growth, if any, by providing a temperature in excess of the liquidus temperature of the alloy at or very close to the interface. It will also be recognized that the dendritic segregation problem may also be regulated by limiting the time available for dendritic growth.
In a slow solidication rate process, it has been established, as previously mentioned, that the mushy zone must not exceed about 1A. inch in depth. Typically, the aim depth will be 1 centimeter or less and it has been conclusively established that at a Adepth of l centimeter a cellular structure is provided and at a mushy zone depth of 1 millimeter a plane front structure is achieved.
There appears to be no size limitations on the castings attainable and columnar grain and single cnystal articles up to 1 foot in length have been fabricated, normally for convenience in molds 1/2-1 inch in diameter.
The unique cast structures Idescribed exhibit significantly improved physical properties even when compared to the advanced columnar-grained and monocrystalline articles obtained as taught by Ver Snyder and Piearcey. In the MAR-M200 system, these improvements include a substantial enhancement of ductility, significant improvement in fatigue properties, higher incipient melting temperature and elimination of surface defects (freckles) from single crystals.
The marked difference between the normal dendritic cast structure and the more homogeneous cellular and plane front cast structures is readily ascertained by differential etching and this technique has been utilized in the examination of transverse sections of MAR-M200 single crystals. In the ydendritic cast structure, pronounced segregation is revealed as an array of light colored dendrite crosses surrounded by a large amount of darker interdendritic material. The cellular structure is essentially homogeneous except for narrow regions at the intercellular boundaries which act as traps for dispersed phases which form in the melt during solidtication, in this case approximately 1 volume percent MC-type carbides. In contrast the plane front structure achieved with MAR- M200 with very low carbon concentration is entirely homogeneous. Thus, it will be recognized that impurities as well as certain constituents such as carbon are important in determining whether a given homogeneous cast structure will be cellular or plane front.
FIGS. 1 and 2 show the degree of tungsten segregation normal to the growth direction in dendritic and cellular/ plane front crystals of MAR-M200 as ascertained by a microprobe scan. The scan data are normalized relative to the tungsten concentration in the center of the dendrites or cells, respectively. In the dendritic structure, there is a 50 percent difference in tungsten content between dendritic and interdendritic regions, reilecting dendritic segregation. On the other hand, in the cellular/plane front structures, the tungsten distribution is nearly homogeneous throughout the section. Obviously, all other alloy additions must also be hornogeneously distributed since tungsten, with its low diiusivity, is the most ditlicult element to homogenize.
There is also an ascertainable difference in the fy precipitate morphology in the dendritic and cellular/plane front single crystals. The dendritic material has a nonuni- 4 form 'y' size and distribution with finer 'y' precipitates occurring in the dendrites (high tungsten, low aluminum and titanium) and large 'y' precipitates in the interdendritic regions (low tungsten, high aluminum and titanium). The cellular/ plane front structures, however, exhibit a uniform fy' size and distribution.
One benefit of a uniform 'y' size is an expected improved creep resistance resulting from the increased phase stability associated with precipitates of uniform spatial morphology. This is of extreme importance in high volume fraction 'y' alloys such as NX-188 (8 Al, 18 Mo, balance Ni) wherein the 'y' morphology is typically extremely heterogeneous because of dendritic segregation.
Still another :advantage of the homogeneous cast structures provided hereby is that the low melting Fy' phase (also often referred to as eutectic or massive 7') normally associated with the interdendritic regions is not present in the cellular/plane front castings. The elimination of the low melting 7', a nonequilibrium phase, is the inherent result of the more uniform distribution of the 'y' forming elements in the cellular/plane front cast structures. In MAR-M200 this elimination of the low density melting phases raises the incipient melting point of the alloy at least 75 F., from 2265 iF. to 23400 F.
Carbides forming during casting are not nonequilibrium phases and are present even in homogeneous cast structures. However, the deleterious eli'ects thereof, when present, are greatly reduced in the cellular/plane front crystals, the `MC carbides exhibiting precracldng in the dendritic structure but not in the castings of the present invention.
Normally associated with dendritic solidiiication is the entrapment of evolved gases at the solid-liquid interface. Since the homogeneous castings are evolved with an essentially unperturbed solid-liquid interface during growth there are no dendrites and therefore, no resulting gaseous porosity. And the suppression of gaseous porosity in homogeneous cast structures is proving as significant in contributing to fatigue resistance as the elimination of precracked carbides.
The tensile strength, ductility and fatigue data presented in FIGS. 3 and 4 compare the properties of the old and new structures. There is a four-fold improvement in the ductility of cellular MAR-M200 single crystals over that of dendritic crystals between room temperature and 1400 F.
In view of the foregoing it is believed that the foregoing clearly establishes the significant advance in the superalloy art provided by the unique materials and techniques herein described. While it has been convenient to describe the invention in detail in connection with certain preferred embodiments and examples, these will be runderstood to be illustrative only and no limitation is intended thereby. Numerous modifications and improvements will be evident to those skilled in the art from the teachings herein and the invention in its true spirit and scope will be measured in accordance with the claims hereinafter set forth.
What is claimed is:
1. Unidirectionally solidified castings composed of an alloy consisting essentially of, by weight, up to about 25 percent chromium, 4-10 percent selected from the group consisting of aluminum, titanium and columbium, up to A3-0 percent cobalt, 3-20 percent selected from the group consisting of molybdenum, tantalum and tungsten, up to about 5 percent selected from the group consisting of boron, zirconium, hafnium and carbon, and at least 45 percent nickel, exhibiting a cellular/plane front microstructure and characterized by the substantial absence of dendrites.
2. `Castings according to claim 1 further characterized by a columnar grained microstructure.
3. Castings according to claim 1 further characterized by a monocrystalline microstructure.
4. In the production of columnar grained and monocrystalline castings from the nickel-base superalloys consisting essentially of, by weight, -up to about 25 percent chromium, 4-10 percent selected from the group consisting of aluminum, titanium and columbium, up to about 30 percent cobalt, 3-20 percent selected from the group consisting of molybdenum, tantalum and tungsten, up to vabout 5 percent selected from the group consisting of boron, zirconium, hafnium and carbon, and at least 45 percent nickel, the improvement which comprises unidirectionally solidfying the superalloys from the melt in a cellular/plane front solidication mechanism limiting the depth of the mushy zone preceding the advance of the 7/1966 Ver Snyder 75-171 -2/ 1970 Piearcey 75--171 RICHARD O. DEAN, Primary Examiner U.S. Cl. X.R.
US81229A 1970-10-16 1970-10-16 Homogeneous nickel-base superalloy castings Expired - Lifetime US3677835A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US8122970A 1970-10-16 1970-10-16

Publications (1)

Publication Number Publication Date
US3677835A true US3677835A (en) 1972-07-18

Family

ID=22162885

Family Applications (1)

Application Number Title Priority Date Filing Date
US81229A Expired - Lifetime US3677835A (en) 1970-10-16 1970-10-16 Homogeneous nickel-base superalloy castings

Country Status (1)

Country Link
US (1) US3677835A (en)

Cited By (25)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3767479A (en) * 1972-02-14 1973-10-23 Gen Electric Multicomponent eutectics for high temperature applications
US3772090A (en) * 1971-07-22 1973-11-13 Gen Electric Alloy microstructure control
US3793012A (en) * 1971-06-14 1974-02-19 Gen Electric Nickel-base tantalum carbide eutectic alloys
US3844845A (en) * 1973-11-15 1974-10-29 Gen Electric Directional composites by solid-state up-transformation
US3847679A (en) * 1973-11-15 1974-11-12 Gen Electric Directional eutectoid composites by solid-state up-transformation
US3902900A (en) * 1971-05-26 1975-09-02 Nat Res Dev Intermetallic compound materials
US3915761A (en) * 1971-09-15 1975-10-28 United Technologies Corp Unidirectionally solidified alloy articles
US4043841A (en) * 1974-09-13 1977-08-23 O.N.E.R.A. - Office National D'etudes Et De Recherches Aerospatiales Metal-refractory composite material
DE2801157A1 (en) * 1977-01-13 1978-07-20 Inco Europ Ltd NICKEL-CHROME SUPER ALLOY
DE2821524A1 (en) * 1977-05-25 1978-12-07 United Technologies Corp HEAT TREATED NICKEL-BASED SUPER ALLOY ARTICLE AND THE METHOD AND INTERSINGLE CRYSTAL ARTICLE OF ITS MANUFACTURING
DE2830396A1 (en) * 1978-07-11 1980-01-24 Inco Europ Ltd Cast nickel-chromium-superalloy - with addn. of hafnium increasing creep strength; esp. for use in gas turbine components with columnar cast structure
US4190094A (en) * 1978-10-25 1980-02-26 United Technologies Corporation Rate controlled directional solidification method
DE3109293A1 (en) * 1980-03-13 1982-02-04 Rolls-Royce Ltd., London ALLOY FOR SINGLE CRYSTAL CASTING
US4372789A (en) * 1980-08-07 1983-02-08 General Electric Company Directionally strengthened copper alloy parts for a gas turbine
US4492672A (en) * 1982-04-19 1985-01-08 The United States Of America As Represented By The Secretary Of The Navy Enhanced microstructural stability of nickel alloys
DE3502639C1 (en) * 1983-08-26 1986-02-27 Hitachi Zosen Corp., Osaka Alloy for exhaust valves
US4610736A (en) * 1983-03-23 1986-09-09 The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration Nickel base coating alloy
US4932974A (en) * 1989-07-06 1990-06-12 Pappas Michael J Prosthetic device with predetermined crystal orientation
US4969905A (en) * 1984-05-21 1990-11-13 Pappas Michael J Method for facilitating bone healing
US5077004A (en) * 1986-05-07 1991-12-31 Allied-Signal Inc. Single crystal nickel-base superalloy for turbine components
US5611389A (en) * 1980-12-30 1997-03-18 Societe Nationale D'etude Et De Construction De Moterus D'aviation S.N.E.C.M.A. Procedure for the fabrication of crystalline blades
EP0967036A2 (en) * 1998-06-26 1999-12-29 General Electric Company Unidirectionally solidified cast article and method of making
US20030145977A1 (en) * 2000-01-19 2003-08-07 Smashey Russell W. Directionally solidified superalloy weld wire
US20110076181A1 (en) * 2009-09-30 2011-03-31 General Electric Company Nickel-Based Superalloys and Articles
US20110076180A1 (en) * 2009-09-30 2011-03-31 General Electric Company Nickel-Based Superalloys and Articles

Cited By (29)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3902900A (en) * 1971-05-26 1975-09-02 Nat Res Dev Intermetallic compound materials
US3793012A (en) * 1971-06-14 1974-02-19 Gen Electric Nickel-base tantalum carbide eutectic alloys
US3772090A (en) * 1971-07-22 1973-11-13 Gen Electric Alloy microstructure control
US3915761A (en) * 1971-09-15 1975-10-28 United Technologies Corp Unidirectionally solidified alloy articles
US3767479A (en) * 1972-02-14 1973-10-23 Gen Electric Multicomponent eutectics for high temperature applications
US3844845A (en) * 1973-11-15 1974-10-29 Gen Electric Directional composites by solid-state up-transformation
US3847679A (en) * 1973-11-15 1974-11-12 Gen Electric Directional eutectoid composites by solid-state up-transformation
US4043841A (en) * 1974-09-13 1977-08-23 O.N.E.R.A. - Office National D'etudes Et De Recherches Aerospatiales Metal-refractory composite material
DE2801157A1 (en) * 1977-01-13 1978-07-20 Inco Europ Ltd NICKEL-CHROME SUPER ALLOY
DE2821524A1 (en) * 1977-05-25 1978-12-07 United Technologies Corp HEAT TREATED NICKEL-BASED SUPER ALLOY ARTICLE AND THE METHOD AND INTERSINGLE CRYSTAL ARTICLE OF ITS MANUFACTURING
DE2830396A1 (en) * 1978-07-11 1980-01-24 Inco Europ Ltd Cast nickel-chromium-superalloy - with addn. of hafnium increasing creep strength; esp. for use in gas turbine components with columnar cast structure
US4190094A (en) * 1978-10-25 1980-02-26 United Technologies Corporation Rate controlled directional solidification method
DE3109293A1 (en) * 1980-03-13 1982-02-04 Rolls-Royce Ltd., London ALLOY FOR SINGLE CRYSTAL CASTING
US4372789A (en) * 1980-08-07 1983-02-08 General Electric Company Directionally strengthened copper alloy parts for a gas turbine
US5611389A (en) * 1980-12-30 1997-03-18 Societe Nationale D'etude Et De Construction De Moterus D'aviation S.N.E.C.M.A. Procedure for the fabrication of crystalline blades
US4492672A (en) * 1982-04-19 1985-01-08 The United States Of America As Represented By The Secretary Of The Navy Enhanced microstructural stability of nickel alloys
US4610736A (en) * 1983-03-23 1986-09-09 The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration Nickel base coating alloy
DE3502639C1 (en) * 1983-08-26 1986-02-27 Hitachi Zosen Corp., Osaka Alloy for exhaust valves
US4969905A (en) * 1984-05-21 1990-11-13 Pappas Michael J Method for facilitating bone healing
US5077004A (en) * 1986-05-07 1991-12-31 Allied-Signal Inc. Single crystal nickel-base superalloy for turbine components
US4932974A (en) * 1989-07-06 1990-06-12 Pappas Michael J Prosthetic device with predetermined crystal orientation
EP0967036A3 (en) * 1998-06-26 2000-12-27 General Electric Company Unidirectionally solidified cast article and method of making
EP0967036A2 (en) * 1998-06-26 1999-12-29 General Electric Company Unidirectionally solidified cast article and method of making
US6217286B1 (en) 1998-06-26 2001-04-17 General Electric Company Unidirectionally solidified cast article and method of making
US20030145977A1 (en) * 2000-01-19 2003-08-07 Smashey Russell W. Directionally solidified superalloy weld wire
US8466389B2 (en) * 2000-01-19 2013-06-18 General Electric Company Directionally solidified superalloy weld wire
US20110076181A1 (en) * 2009-09-30 2011-03-31 General Electric Company Nickel-Based Superalloys and Articles
US20110076180A1 (en) * 2009-09-30 2011-03-31 General Electric Company Nickel-Based Superalloys and Articles
CN102031418A (en) * 2009-09-30 2011-04-27 通用电气公司 Nickel-based superalloys and articles

Similar Documents

Publication Publication Date Title
US3677835A (en) Homogeneous nickel-base superalloy castings
Ramsperger et al. Microstructure of the nickel-base superalloy CMSX-4 fabricated by selective electron beam melting
Zupanič et al. Structure of continuously cast Ni-based superalloy Inconel 713C
US3567526A (en) Limitation of carbon in single crystal or columnar-grained nickel base superalloys
Svetlov et al. Diffusional mechanism of gamma-prime-phase particle coalescence in single crystals of nickel-base superalloys
Kermanpur et al. Directional solidification of Ni base superalloy IN738LC to improve creep properties
JPH0239573B2 (en)
Fulin et al. Microstructure and segregation behavior of Rene88DT alloy prepared by ESR-CDS
CN109576532A (en) Third generation single crystal super alloy and the preparation of creep rupture strength height and oxidation resistant
Sani et al. Investigation on the homogenization treatment and element segregation on the microstructure of a γ/γ′-cobalt-based superalloy
Ye et al. Directional solidification of hypereutectic Nb-Si-Ti alloy: influence of drawing velocity change on microstructures
Cui et al. Preliminary investigation of directionally solidified NiAl–28Cr–5.5 Mo–0.5 Hf composite
Deyong et al. Microstructural and mechanical properties of rapidly solidified Cu Ni Sn alloys
US3929467A (en) Grain refining of metals and alloys
Huang et al. Solidification and segregation characteristics of Ni-based superalloy C700R-1 for ultra-supercritical steam turbine rotor
Li et al. Solidification characteristics and high temperature tensile properties of Ni-based superalloy IN713C
Yi et al. Effect of cooling rate on solidification microstructure and mechanical properties of TiB2-containing TiAl alloy
Al-Jarba et al. Carbon-containing single-crystal nickel-based superalloys: Segregation behavior and carbide formation
Sifeng et al. Influences of processing parameters on microstructure during investment casting of nickel-base single crystal superalloy DD3.
US4964453A (en) Directional solidification of superalloys
US3783032A (en) Method for producing directionally solidified nickel base alloy
Liu et al. A new method of fine grained casting for nickle-base superalloys
KR20180081313A (en) Directional solidification ni base superalloy and manufacturing method therefor
ZUPANIČ et al. Solidification of Be-free Ni-based dental alloy
US3782928A (en) Composite alloy for high temperature applications