GB2463304A - Manufacturing monocrystalline cast blades of cubic structure - Google Patents

Manufacturing monocrystalline cast blades of cubic structure Download PDF

Info

Publication number
GB2463304A
GB2463304A GB8227301A GB8227301A GB2463304A GB 2463304 A GB2463304 A GB 2463304A GB 8227301 A GB8227301 A GB 8227301A GB 8227301 A GB8227301 A GB 8227301A GB 2463304 A GB2463304 A GB 2463304A
Authority
GB
United Kingdom
Prior art keywords
vertical
grain
blades
mould
column
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
Application number
GB8227301A
Other versions
GB8227301D0 (en
GB2463304B (en
Inventor
Martial Gerard Alessandri
Jacques Leopold Emile Grammagnac
Jean-Marc Clement Francis Theret
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.)
Safran Aircraft Engines SAS
Original Assignee
Societe Nationale dEtude et de Construction de Moteurs dAviation SNECMA
SNECMA SAS
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 Societe Nationale dEtude et de Construction de Moteurs dAviation SNECMA, SNECMA SAS filed Critical Societe Nationale dEtude et de Construction de Moteurs dAviation SNECMA
Anticipated expiration legal-status Critical
Publication of GB8227301D0 publication Critical patent/GB8227301D0/en
Publication of GB2463304A publication Critical patent/GB2463304A/en
Application granted granted Critical
Publication of GB2463304B publication Critical patent/GB2463304B/en
Expired - Lifetime legal-status Critical Current

Links

Classifications

    • 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
    • C30B11/00Single-crystal growth by normal freezing or freezing under temperature gradient, e.g. Bridgman-Stockbarger method
    • C30B11/14Single-crystal growth by normal freezing or freezing under temperature gradient, e.g. Bridgman-Stockbarger method characterised by the seed, e.g. its crystallographic orientation
    • 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
    • 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
    • B22D27/20Measures not previously mentioned for influencing the grain structure or texture; Selection of compositions therefor
    • 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
    • C30B11/00Single-crystal growth by normal freezing or freezing under temperature gradient, e.g. Bridgman-Stockbarger 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

Landscapes

  • Chemical & Material Sciences (AREA)
  • Engineering & Computer Science (AREA)
  • Crystallography & Structural Chemistry (AREA)
  • Materials Engineering (AREA)
  • Metallurgy (AREA)
  • Organic Chemistry (AREA)
  • Mechanical Engineering (AREA)
  • Inorganic Chemistry (AREA)
  • Crystals, And After-Treatments Of Crystals (AREA)

Abstract

A method of manufacturing monocrystalline cast blades of cubic structure comprises effecting a directional solidification. A single grain crystal is selected by means of a selection device 1 at the outlet of which a single grain is to be found, of predetermined orientation and having an direction coincident with the vertical. It is arranged that the axis 12 of each portion 8 will be oriented in a direction of the selected crystal. The blades may be cast in a cluster by making a selected grain grow in a common vertical germination column 6, and the solidification front is made to progress continuously from the vertical column 6 up to the portions to be cast (18, fig 2) and along inclined branches 14 stemming from the germinating column 6.

Description

A METHOD FOR THE MANUFACTURE OF MONOCRYSTALLINE BLADES
This invention relates to a method of manufacturing in a shell mould monocrystalline cast blades or other parts of face-centred cubic structure.
In such methods the mould is fed with molten metal at its upper part, directional solidification is effected of which the front progresses vertically from the bottom to the top, a single columnar grain is selected by means of a selection device disposed in the lower part of the mould and at the outlet of which selection device a pre-determined single grain with a transverse orientation is produced. having a directionfOOlJ coincident with the vertical.
Methods for the manufacture of monocrystalline blades and parts are already known, in particular from French
Patent Specification No.1 481 366 and 2 037 187.
Furthermore, in British Application No.81.36625 filed 4th December, 1981, the Applicants proposed a method more particularly intended for the manufacture of fixed inlet guide blades of turbines.
According to. the present invention, there is provided a method of manufacturing in a shell mould, monocrystal-line cast blades with a face-centred cubic structure, the mould being supplied with molten metal at its upper part and directional solidification being effected of which the front progresses vertically from below to the top, a single columnar grain being selected by means of a selection device disposed at the lower part of the mould and at the outlet of which.a single grain is present..of.
predetermined transverse orientation and having a direc-tion [oOlj coincident with the vertical, the shells of the blades being so disposed that the axis of each por-tion will be orientated in the direction riii of the selected crystal.
An improvement in the creep properties of blades in accordance with the invention arises from the fact that it is advantageous that the structure of the monocrystalline parts should be oriented in the direction ElllJ along the principal axis of stress, that is to say, in the case where blades are cast without twist, the direction of the generating line of the blade. It is known that it is very difficult, in practice, impossible industrially, to cause a crystal to grow in this direction, but the method in accordance with the invention permits, by an ingenious arrangement, the production of monocrystalline parts orientated on the axis [111. S. -3-.
Preferably, a chicane device is used as the grain selection device, and in particular a device such as has been described in the above British Patent Application No.81.36625, that is to say, a device comprising a succession of rectilinear passages disposed in a common plane but perpendicular to one another.
The parts to be cast may be arranged as a cluster.
Preferably, the selected grain is caused to grow by the selection device as a common vertical germination column and the solidification front is caused to progress con-tinuously from the vertical column up to the parts to be cast along inclined branches stemming from the germina-tion column..
Advantageously, germination is initiated at each inclined branch, in a plurality of parts disposed parallel to the branch. More particularly, the parts are mounted in pairs at the ends of horizontal stems perpendicular to the inclined branches.
A plurality of selection devices and of vertical germina-tion columns may be arranged as a common cluster. As will be apparent from the following description, such a device enables simultaneous casting of a large number of blades (about forty).
One advantage of blades or other parts manufactured in accordance with the invention is that a micrographic examination in depth may reveal by the dentritic structure of the blade or other part examined that it has been produced in accordance with the claimed method.
The invention will now be described, by way of example, with reference to the accompanying diagrammatic drawings, in which; Figure 1 shows a front elevation of the cluster of parts to be moulded in accordance with the invention; Figure 2 is a plan view of the cluster of Figure 1; and Figure 3 shows, as a perspective view, a second arrange-ment of the cluster of test pieces' moulded in accordance with the invention.
In order to simplify the illustration, a common Figure (1 or 2), represents definitively the interface of the mould-part and the mould which are phus seen to be represented simultaneously, the same reference numerals being employed for the two corresponding parts of the one and of the other.
A grain selection device 1 is shown in Figure 1, similar to that described in British Patent Application No.81.36625 and is composed of two rectilinear passages perpendicular to one another; a vertical passage 2, a horizontal passage 3, and possibly another vertical passage 4 and another horizontal passage 5.
The selection device 1, parallel to the plane of Figure 1, discharges into a vertical column 6 for distribution of the grain.
The substantially horizontal solidification front 7, progresses from the bottom to the top in accordance with conventional techniques.
By the provision of the chicane device 1, it is ensured that one monocrystal of known orientation and defined by the said device is present in the vertical column 6; the axis 00lJ of the monocrystal is parallel to the vertical passage 2, and thus lies in the axis of the column 6, and the axis fl100j is ir the plane of the chicane.
It is also possible to develop a monocrystal of pre-determined orientation starting from a germ.
In accordance with the invention, the parts to be cast are disposed (there will be recognised here the corres-ponding form to the moulding of rotor blades 8, aerofoil 9, platform 10 and part of a root 11) in such a manner that the axis 12 of each blade will be orientated in a direction ill J of the selected crystal. The parts 8 thus form an angle = arc tg,[Twith the vertical (column 6) and an angle of 45 with the plane 13 of the chicane (Figure 2).
A rising, inclined branch 14 enables the continuous progression of the solidification front, from the vertical column 6 up to the lower part of each blade pOrtion 8.
The orientation of the branches 14 may be selected to be parallel or not to that of the blade portions 8. It is in effect the orientatIon of the part itself in a direction 11 111 which is the determining factor.
The method in accordance with the invention possesses in the sphere of metallurgy a very important advantage.
It may happen in practice that in the course of directional solidification, new grains are formed start-ing from a defect in the walls of the mould, owing to the S. -7-.
accidental presence on these walls of a grain which acts as a germinating factor.
In the proposed method, these parasitic grains of random orientation are rapidly extinguished by the growth of the main grain with directions [ 001 1 and [iO0.
The implantation of the branches 14 on the common column 6 responds to the minimal weight criterion in order to be able to dispose as many parts as possible as a common cluster. It is possible to arrange them, in the manner illustrated in Figure 1, somewhat like empty bottles on a drying rack, and distributed around the column 6 according to four directions Llll:i of the monocrystal.
In order to increase the number of parts per cluster, it is possible to mount a plurality of blades on each branch 14. Figure 2 shows the case where for each in-clined branch 14, a pair of parts 8 has been mounted at the ends of Stems 15 perpendicular to the axis 12 of the parts, which are indeed orientated in a direction E lii 1 of the crystal.
The metal supply, not shown in Figures 1 and 2, is effected at the upper part of the column 6. It is clear that it is possible to adopt any kind of arrangement other than that illustrated in Figures 1 and 2, it being understood that it is.essential to respect the orientation of each part in a direction [ ill of the monocrystal and to ensure the necessary conditions for the develop-ment in each part of the said monocrystal starting from the column 6 of the germination zone.
It is also possible to adopt an arrangement of the cluster in which a plurality of selection devices is utilised.
Thus, Figure 3 shows a group of forty parts, here cylin-drical test pieces. Five vertical columns 17 for the distribution of the grain are regularly distributed about a single metal supply arrangement 16 (only three columns are effectively illustrated) into which the upper ends of five grain selection devices 18 communicate (here, five chicanes).
At each of these five columns 17 there is a corresponding monocrystal of special orientation. For the distribu-tion of grain two vertical groups of four rough test pieces 19 and 20 (inclined branches 14 are not shown), are implanted on each column 17 at four levels the parts 19 and 20 of each col'umn being orieptated in two direc-tions [iiij of the selected monocrystal by the device 18 for the selection of the grain of the column. The outlines in a horizontal plane of the parts 19 and are perpendicular to one another, which is not, of course, readily apparent from the perspective view of Figure 3.
The supply with metal is effected from the inlet funnel 16 by inclined collectors 21 conducting the metal to the upper end of vertical supply column 22, which supplies the upper portion of each part 19, 20.
The grain selection devices 18, although they are independent one from the other, are regularly orientated with respect to the central supply 16 (for example in five planes at 720), in such a manner as to give to the cluster a symmetrical appearance about its vertical axis 23 (chain line) thus ensuring homogeneity and compactness. S.

Claims (11)

  1. CLAIMS1. A method of manufacturing in a shell mould, mono-crystalline cast blades with a face-centred cubic structure, the mould being supplied with molten metal at its upper part and directional solidification being effected of which the front progresses vertically from below to the top, a single columnar grain being selected by means of a selection device disposed at the lower part of the mould and at the outlet of which a single grain is present of predetermined transverse orientation and having a direction [0011 coincident with the vertical, the shells of the blades being so disposed that the axis of each portion will be orientated in the direction E11l of the selected crystal.
  2. 2. A method according to claim 1, wherein the selection device is a chicane device.
  3. 3. A method according to claim 2, wherein the chicane device is constituted by a succession of rectilinear passages disposed in a common vertical plane perpendicular to one another.
  4. 4. A method according to any one of claims 1 to 3, -11 -wherein the portions to. be moulded are arranged as a cluster.
  5. 5. A method according to claim 4, wherein the selected 5, grain is made, to grow by the selection device in a vertical single germination column and the solidification front is made to progress continuously from the vertical column up to the portions to be moulded along branches which are inclined and stemming from the germination column.
  6. 6. A method according to claim 5, wherein starting from each inclined branch, the, germination is caused to grow in a plurality of portions.
  7. 7. A method according to claim 6, wherein the said portions are mounted in pairs at the ends of horizontal stems perpendicular to the inclined branches.
  8. 8. A method according to any one of claims 5 to 7, wherein a plurality of selection devices and of vertical germination columns are disposed.in a common cluster.-12 - 9. A method of manufacturing monocrystalline cast parts in a shell mould comprising supplying the mould with molten metal, causing directional solidification from the bottom upwardly so that a single vertical grain has a direction rOOli and the individual shells of the blades are orientated with the direction [1111 10. A method of manufacturing monocrystalline cast blades or other parts substantially as hereinbefore described with respect to the accompanying drawings.11. A cast blade or other part.when made' by a method in accordance with any one of the preceding claims.Amendments to the claims have been filed as follows 1. A method of manufacturing in a shell mould, mono-crystalline cast blades with a face-centred cubic structure, the mould being supplied with. molten metal at its upper part and directional solidification being effected of which the front progresses vertically from below to the top, a single columnar grain being selected by means of a selection device disposed at the lower part of the mould and at the outlet of which a single grain is present of predetermined transverse orientation and having a direction [ooi coincident with the vertical, the shells of the blades being so disposed that the axis of each blade will be orientated in the direction rill] of the selected crystal.2. A method acrding to claim 1, wherein the selection device is a chicane device.3. A method according to claim 2, wherein the chicane device is constituted by a succession of rectilinear passages disposed in a coion vertical plane perpendicular to one another.4. A method according to any one of claims 1 to 3, ILt-wherein the portions to be tnoulded are arranged as a cluster.5. A method according to claim 4, wherein the selected grain is made to grow by the selection device in a vertical single germination column and the solidification front is made to progress continuously from the vertical column up to the portions to be moulded along branches which are inclined and stemming from the germination column.6. A method according to claim 5, wherein starting from each inclined branch, the germination is caused to grow in a plurality of portions.7. A method according to claim 6, wherein the said portions are mounted in pairs at the ends of horizontal stems perpendicular to the inclined branches.8. A method according to any one of claims 5 to 7, wherein a plurality of selection devices and of vertical germination columns are disposed in a common cluster.
  9. 9. A method of manufacturing rnonocrystalline cast elongate parts in a shell mould comprising supplying the mould with molten metal, causing directional solidi-fication from the bottom upwardly so that a single, selected, vertical grain has a direction [QO coincident with the vertical and the individual parts are orientated with their longitudinal axes in the direction of the selected crystal.
  10. 10. A method of manufacturing monocrystalline cast blades or other parts substantially as hereinbefore described with respect to the accompanying drawings.
  11. 11. A cast blade or other part when made by a method in accordance with any one of the preceding claims.
GB8227301A 1981-09-25 1982-09-24 A method for the manufacture of monocrystalline blades Expired - Lifetime GB2463304B (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR8118071A FR2734187A1 (en) 1981-09-25 1981-09-25 Casting and directional solidification. of a cluster of turbine rotor vanes

Publications (3)

Publication Number Publication Date
GB8227301D0 GB8227301D0 (en) 2009-09-16
GB2463304A true GB2463304A (en) 2010-03-17
GB2463304B GB2463304B (en) 2010-09-29

Family

ID=9262451

Family Applications (1)

Application Number Title Priority Date Filing Date
GB8227301A Expired - Lifetime GB2463304B (en) 1981-09-25 1982-09-24 A method for the manufacture of monocrystalline blades

Country Status (4)

Country Link
DE (1) DE3235359C1 (en)
FR (1) FR2734187A1 (en)
GB (1) GB2463304B (en)
IT (1) IT8223391A0 (en)

Families Citing this family (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2734189B1 (en) * 1989-05-24 1997-07-18 Snecma DEVICE FOR SELECTING A GRAIN OF CRYSTALLIZATION FOR SINGLE CRYSTAL PIECES IN FOUNDRY
CN1317095C (en) * 2004-02-25 2007-05-23 中国科学院金属研究所 Crystalloid laminae composited from single crystal and directional column crystal and preparing method
FR3004366B1 (en) * 2013-04-10 2021-04-30 Snecma MONOCRISTALLINE FOUNDRY MOLD
CN109648065B (en) * 2019-02-01 2020-08-21 中国科学院金属研究所 Method for evaluating recrystallization forming tendency of single crystal superalloy

Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB1263401A (en) * 1969-03-13 1972-02-09 United Aircraft Corp Double oriented single crystal castings
GB1280055A (en) * 1969-03-13 1972-07-05 United Aircraft Corp Double-oriented single crystal castings
GB2030069A (en) * 1978-09-18 1980-04-02 Howmet Turbine Components Mould for directional solidified single crystal castings and method for preparing same
GB2030233A (en) * 1978-09-16 1980-04-02 Rolls Royce Gas turbine engine blade
GB2037200A (en) * 1978-12-13 1980-07-09 United Technologies Corp Epitaxial solidification

Family Cites Families (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR1481366A (en) * 1965-05-27 1967-05-19 United Aircraft Corp Improvements to foundry parts and method and device for manufacturing these parts
US3625275A (en) * 1969-03-13 1971-12-07 United Aircraft Corp Apparatus and method for single-crystal casting
BE737493A (en) * 1969-08-14 1970-01-16 Monocrystalline turbine blade envelope mould
BE795953A (en) * 1973-02-26 1973-08-27 Petrov Dmitry A Monocrystalline metal products mfr - in a two cavity mould
US4292010A (en) * 1978-09-16 1981-09-29 Rolls-Royce Limited Cambered blade or vane for a gas turbine engine

Patent Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB1263401A (en) * 1969-03-13 1972-02-09 United Aircraft Corp Double oriented single crystal castings
GB1280055A (en) * 1969-03-13 1972-07-05 United Aircraft Corp Double-oriented single crystal castings
GB2030233A (en) * 1978-09-16 1980-04-02 Rolls Royce Gas turbine engine blade
GB2030069A (en) * 1978-09-18 1980-04-02 Howmet Turbine Components Mould for directional solidified single crystal castings and method for preparing same
GB2037200A (en) * 1978-12-13 1980-07-09 United Technologies Corp Epitaxial solidification

Also Published As

Publication number Publication date
GB8227301D0 (en) 2009-09-16
IT8223391A0 (en) 1982-09-23
GB2463304B (en) 2010-09-29
DE3235359C1 (en) 1997-01-30
FR2734187A1 (en) 1996-11-22

Similar Documents

Publication Publication Date Title
US5899257A (en) Process for the fabrication of monocrystalline castings
GB2463304A (en) Manufacturing monocrystalline cast blades of cubic structure
GB2301303A (en) Manufacture of monocrystalline aerodynamic blades
CN205567299U (en) A support for supporting fruit tree branch
US7250088B2 (en) Directionally solidified columnar grained article and apparatus for manufacture thereof
EP0126550A1 (en) Casting articles by directional solidification
EP0317315A3 (en) A method of making a casting mould
Bierhorst The apogamous life cycle of Trichomanes pinnatum—a confirmation of Klekowski's predictions on homoeologous pairing
CN105900607A (en) Position adjustment mechanism for line separator
Sekhar et al. Leaf development in the normal and solanifolia mutant of tomato (Lycopersicon esculentum)
CN208924814U (en) A kind of cultivating stand and fruit tree shaping system
CN206542751U (en) A kind of P. kingianum lodging-prevention device
CN207083615U (en) A kind of adjustable plant flower stand
SU1107820A2 (en) Apparatus for maturing sweets cast into starch molds
HUT60588A (en) Method for producing maize corn, maize plant and hybrid
DE2964298D1 (en) Device for the production of phosphoric acid
RU2392091C1 (en) Device for obtainment of heat-proof nickel alloy blade with monocrystalline structure
CN209002499U (en) A kind of interim stabilization device for going alone big tree planting for Palmae
CN221710677U (en) Wind-proof baffle for tree seedlings
CN216392391U (en) Other trees of road support of straightening
CN220493702U (en) Box-type Chinese yam cultivation device with clamping groove
CN215301973U (en) Arbor fixer
CN208783333U (en) Dendrobium nobile potting bracket
Frinken Progress in the Production of Heating Conductor Wires
RU2325971C1 (en) Device to produce monocrystal turbine blade casting

Legal Events

Date Code Title Description
PE20 Patent expired after termination of 20 years

Expiry date: 20020923