GB2208389A - A method of manufacturing components having portions of different wall thickness - Google Patents
A method of manufacturing components having portions of different wall thickness Download PDFInfo
- Publication number
- GB2208389A GB2208389A GB8818778A GB8818778A GB2208389A GB 2208389 A GB2208389 A GB 2208389A GB 8818778 A GB8818778 A GB 8818778A GB 8818778 A GB8818778 A GB 8818778A GB 2208389 A GB2208389 A GB 2208389A
- Authority
- GB
- United Kingdom
- Prior art keywords
- shell
- powder
- hollow
- filled
- mould
- 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
- 238000004519 manufacturing process Methods 0.000 title claims description 21
- 238000000034 method Methods 0.000 claims description 25
- 239000000843 powder Substances 0.000 claims description 15
- 239000000463 material Substances 0.000 claims description 9
- 238000003466 welding Methods 0.000 claims description 7
- 238000000462 isostatic pressing Methods 0.000 claims description 4
- 230000003014 reinforcing effect Effects 0.000 claims description 4
- 239000007787 solid Substances 0.000 claims description 3
- 239000011796 hollow space material Substances 0.000 claims 6
- 238000009792 diffusion process Methods 0.000 claims 4
- 239000000945 filler Substances 0.000 claims 4
- PXHVJJICTQNCMI-UHFFFAOYSA-N Nickel Chemical compound [Ni] PXHVJJICTQNCMI-UHFFFAOYSA-N 0.000 claims 3
- 239000007789 gas Substances 0.000 claims 3
- 229910045601 alloy Inorganic materials 0.000 claims 2
- 239000000956 alloy Substances 0.000 claims 2
- 150000001875 compounds Chemical class 0.000 claims 2
- 238000001513 hot isostatic pressing Methods 0.000 claims 2
- RTAQQCXQSZGOHL-UHFFFAOYSA-N Titanium Chemical compound [Ti] RTAQQCXQSZGOHL-UHFFFAOYSA-N 0.000 claims 1
- 239000004411 aluminium Substances 0.000 claims 1
- 229910052782 aluminium Inorganic materials 0.000 claims 1
- XAGFODPZIPBFFR-UHFFFAOYSA-N aluminium Chemical compound [Al] XAGFODPZIPBFFR-UHFFFAOYSA-N 0.000 claims 1
- 239000000919 ceramic Substances 0.000 claims 1
- 239000003795 chemical substances by application Substances 0.000 claims 1
- 239000002826 coolant Substances 0.000 claims 1
- 238000001816 cooling Methods 0.000 claims 1
- 238000005260 corrosion Methods 0.000 claims 1
- 230000007797 corrosion Effects 0.000 claims 1
- 238000010438 heat treatment Methods 0.000 claims 1
- 238000005304 joining Methods 0.000 claims 1
- 229910001092 metal group alloy Inorganic materials 0.000 claims 1
- 239000007769 metal material Substances 0.000 claims 1
- 229910052759 nickel Inorganic materials 0.000 claims 1
- 238000003825 pressing Methods 0.000 claims 1
- 230000001681 protective effect Effects 0.000 claims 1
- 239000012495 reaction gas Substances 0.000 claims 1
- 239000010936 titanium Substances 0.000 claims 1
- 229910052719 titanium Inorganic materials 0.000 claims 1
- 238000005266 casting Methods 0.000 description 3
- 230000007246 mechanism Effects 0.000 description 3
- 239000002699 waste material Substances 0.000 description 2
- 238000005520 cutting process Methods 0.000 description 1
- 238000011089 mechanical engineering Methods 0.000 description 1
- 239000002184 metal Substances 0.000 description 1
- 238000003908 quality control method Methods 0.000 description 1
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B22—CASTING; POWDER METALLURGY
- B22F—WORKING METALLIC POWDER; MANUFACTURE OF ARTICLES FROM METALLIC POWDER; MAKING METALLIC POWDER; APPARATUS OR DEVICES SPECIALLY ADAPTED FOR METALLIC POWDER
- B22F5/00—Manufacture of workpieces or articles from metallic powder characterised by the special shape of the product
- B22F5/04—Manufacture of workpieces or articles from metallic powder characterised by the special shape of the product of turbine blades
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B22—CASTING; POWDER METALLURGY
- B22F—WORKING METALLIC POWDER; MANUFACTURE OF ARTICLES FROM METALLIC POWDER; MAKING METALLIC POWDER; APPARATUS OR DEVICES SPECIALLY ADAPTED FOR METALLIC POWDER
- B22F3/00—Manufacture of workpieces or articles from metallic powder characterised by the manner of compacting or sintering; Apparatus specially adapted therefor ; Presses and furnaces
- B22F3/12—Both compacting and sintering
- B22F3/1208—Containers or coating used therefor
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B22—CASTING; POWDER METALLURGY
- B22F—WORKING METALLIC POWDER; MANUFACTURE OF ARTICLES FROM METALLIC POWDER; MAKING METALLIC POWDER; APPARATUS OR DEVICES SPECIALLY ADAPTED FOR METALLIC POWDER
- B22F7/00—Manufacture of composite layers, workpieces, or articles, comprising metallic powder, by sintering the powder, with or without compacting wherein at least one part is obtained by sintering or compression
- B22F7/06—Manufacture of composite layers, workpieces, or articles, comprising metallic powder, by sintering the powder, with or without compacting wherein at least one part is obtained by sintering or compression of composite workpieces or articles from parts, e.g. to form tipped tools
- B22F7/08—Manufacture of composite layers, workpieces, or articles, comprising metallic powder, by sintering the powder, with or without compacting wherein at least one part is obtained by sintering or compression of composite workpieces or articles from parts, e.g. to form tipped tools with one or more parts not made from powder
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B23—MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
- B23K—SOLDERING OR UNSOLDERING; WELDING; CLADDING OR PLATING BY SOLDERING OR WELDING; CUTTING BY APPLYING HEAT LOCALLY, e.g. FLAME CUTTING; WORKING BY LASER BEAM
- B23K20/00—Non-electric welding by applying impact or other pressure, with or without the application of heat, e.g. cladding or plating
- B23K20/04—Non-electric welding by applying impact or other pressure, with or without the application of heat, e.g. cladding or plating by means of a rolling mill
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B23—MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
- B23P—METAL-WORKING NOT OTHERWISE PROVIDED FOR; COMBINED OPERATIONS; UNIVERSAL MACHINE TOOLS
- B23P15/00—Making specific metal objects by operations not covered by a single other subclass or a group in this subclass
- B23P15/04—Making specific metal objects by operations not covered by a single other subclass or a group in this subclass turbine or like blades from several pieces
-
- 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
- F01D5/12—Blades
- F01D5/28—Selecting particular materials; Particular measures relating thereto; Measures against erosion or corrosion
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B22—CASTING; POWDER METALLURGY
- B22F—WORKING METALLIC POWDER; MANUFACTURE OF ARTICLES FROM METALLIC POWDER; MAKING METALLIC POWDER; APPARATUS OR DEVICES SPECIALLY ADAPTED FOR METALLIC POWDER
- B22F2202/00—Treatment under specific physical conditions
- B22F2202/06—Use of electric fields
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B22—CASTING; POWDER METALLURGY
- B22F—WORKING METALLIC POWDER; MANUFACTURE OF ARTICLES FROM METALLIC POWDER; MAKING METALLIC POWDER; APPARATUS OR DEVICES SPECIALLY ADAPTED FOR METALLIC POWDER
- B22F2998/00—Supplementary information concerning processes or compositions relating to powder metallurgy
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B22—CASTING; POWDER METALLURGY
- B22F—WORKING METALLIC POWDER; MANUFACTURE OF ARTICLES FROM METALLIC POWDER; MAKING METALLIC POWDER; APPARATUS OR DEVICES SPECIALLY ADAPTED FOR METALLIC POWDER
- B22F2998/00—Supplementary information concerning processes or compositions relating to powder metallurgy
- B22F2998/10—Processes characterised by the sequence of their steps
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Manufacturing & Machinery (AREA)
- Chemical & Material Sciences (AREA)
- Materials Engineering (AREA)
- Composite Materials (AREA)
- General Engineering & Computer Science (AREA)
- Powder Metallurgy (AREA)
- Pressure Welding/Diffusion-Bonding (AREA)
Description
2208389 M&C FOLIO: 230P56736 WANGDOC: 0816k A method of manufacturing
components having portions of different wall thickness The invention relates to a method of manufacturing components having portions of very different wall thickness. by means of isostatic pressing in a mould shell.
In many cases in mechanical engineering. components are used having portions with very different wall thicknesses, e.g. in housings for drive mechanisms a relatively thin metal shell is supported by solid reinforcing ribs. Usually there are also connecting flanges and bearing bosses, which also require thicker wall thicknesses.
Nowadays three alternative methods are mainly used for manufacturing such components:
1. A solid forged blank is machined by cutting off waste chips until the desired structure is obtained.
2. Sheets, castings and machined piece parts are fixedly assembled in a suitable way. e.g. by welding.
2 3. The required component is produced entirely by casting.
The above-mentioned manufacturing methods are accompanied by problems. The first method listed requires high manufacturing costs alongside large losses of material due to the resulting waste. In addition. for reasons of production efficiency. the wall thickness cannot fall below certain dimensions.
The second method listed is very 'costly because of the required preparatory work and the welding. Problems particularly arise because of thermal distortion during welding, so that quality control requirements are high.
Finally, the third method of complete casting is accompanied by appreciable size and wall thickness restrictions.
An object of the invention is to avoid the disadvantages of the known manufacturing methods and to provide a method of manufacturing components, which consist of metallic powders pressed in a mould shell and which have areas of very different wall thickness, e.g. housings for drive mechanisms and drive mechanism parts, the steps of the method operating accurately, efficiently, and in particular economically with a relatively low If 3 input of production means.
Claims (16)
1-1 . 1 i T 1 7 Claims 1. A method of manufacturing a structural component having portions of different wall thickness. by means of hot isostatic pressing of a mould shell, characterized by the following method steps:
a) at least two three dimensional shaped shell walls are superimposed on each other in such a way. that the adjacent surfaces thereof contact each other over a first partial area and are space& from each other to form one or more hollow spaces in a second partial area.
b) the adjacent surfaces of the shell walls are joined together over the first partial area, and in the second partial area are fitted together along the edges of the hollow spaces so as to be undetachable, C) the hollow spaces are filled with powder, which can be compressed metallurgically, and are degassed and sealed, d) the filled shell is isostatically pressed to form the finished component.
2. A method of manufacturing a component with areas of varying wall thicknesses. by means of isostatic pressing 8 of a mould shell, characterized by the following method steps:
a) at least two shell walls with congruent cavities are superimposed so that adjacent surfaces lie against each other. and, at least along the edges of one partial area, are joined so as to be gastight and undetachable, b) a hollow space is produced within the gas tight. joined edges by means of inflating.
C) the hollow spaces are filled with metallurgically compressible powder and degassed and sealed, 1 d) the filled shell is isostatically pressed to form the finished component
3. A method as claimed in claim 2. wherein the shell walls are initially flat plates.
4. A method as claimed in any one of claims 1 to 3. wherein. before the shell walls are joined. they are coated with a separating agent adjacent the hollow spaces of the component which are to be filled with powder.
-7 1 9
5. A method as claimed in any one of claims 1 to 4. wherein the joining of the edges of the hollow spaces of the component which are to be filled with powder is carried out by means of weld seams. in particular roll weld seams.
6. A method as claimed in any one of claims 2 to 5, wherein the inflating of the shell walls takes place against hollow moulds or mould dies which are appropriately formed or form the finished component.
7. A method as claimed in any one of claims 2 to 6. wherein the inflating of the shell walls takes place in several stages.
8. A method as claimed in any one of claims 1 to 7, wherein the shell walls consist of heat-resistant sheets. preferably of a Ni-based alloy.
9. A method as claimed in any one of claims 1 to 8, wherein in addition to the shell walls. formed solid elements made of a metallic or non- metallic material are used as components of the mould shell.
10. A method as claimed in any one of claims 1 to 9. wherein the material of the mould shell is of the same nature as the material of the powder to be compressed.
11. A method as claimed in any one of claims 1 to lo, wherein nonmetallic powder, particularly ceramic powder is used.
12. A method as claimed in any one of claims 1 to 11, wherein theindividual shell walls consist of different materials.
13. A method as claimed in any one of claims 1 to 12, wherein the individual shell walls consist of layers of different materials.
14. A method as claimed in any one of claims 1 to 13. for manufacturing a turbine blade with a central cooling channel, characterized by the following method steps:
a) four flat shell sheets with essentially the same contour are joined together along their edges e.g. by diffusion welding. so as to be undetachable and to lie on top of each other; b) by means of a tube opening into a gap between the two middle shell sheets. the shell join is inflated against a first two-sided hollow mould defining a central hollow space.
c) the central hollow space thus produced, is 1 i i 1 Q filled with an incompressible filler; d) the gaps between the shell sheets, lying against each other are, by means of filling tubes, inflated against a second two-sided hollow mould defining the outer shape of the turbine blade:
e) the incompressible filler is removed from the central hollow space; f) the hollow spaces between the first and the second shell sheets and between the third and the fourth shell sheets inflating are filled with powder and the finished turbine blade is produced by isostatic pressing of the shell at a suitable temperature.
15. A method of manufacturing a structural component substantially as herein described with reference to Figs. la and lb. or 2a to 2_q of the accompanying drawings.
16. Structural components manufactured by a method as claimed in any one of the preceding claims.
Published 1988 at The Patent Office. State House. 66 71 High Ho'born. London WClR 4TP. Further copies may be obtained frorn The Patent Office, Sales Branch, St Mary Cray. Orpington, Kent BR5 3RD Printed by Multiplex techniques ltd. St. Mary Cray, Kent. Con 1'8"7 t)aies zrancn, bT, zaary uray. urpingTon, Yenz zro o tij rTinwa Dy jawupitm ui"iiqutb i. o -j - ay. -- -- - -
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DE19873726056 DE3726056A1 (en) | 1987-08-06 | 1987-08-06 | METHOD FOR PRODUCING COMPONENTS WITH DIFFERENT WALL THICKNESSES |
Publications (3)
Publication Number | Publication Date |
---|---|
GB8818778D0 GB8818778D0 (en) | 1988-09-07 |
GB2208389A true GB2208389A (en) | 1989-03-30 |
GB2208389B GB2208389B (en) | 1991-05-29 |
Family
ID=6333147
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB8818778A Expired - Lifetime GB2208389B (en) | 1987-08-06 | 1988-08-08 | A method of manufacturing components having portions of different wall thickness |
Country Status (3)
Country | Link |
---|---|
DE (1) | DE3726056A1 (en) |
FR (1) | FR2619034B1 (en) |
GB (1) | GB2208389B (en) |
Cited By (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
EP0528720A1 (en) * | 1991-08-09 | 1993-02-24 | ACIERIES ET FORGES D'ANOR Société à Responsabilité Limitée | Process for co-laminating high speed steel on mild steel |
US7946035B2 (en) | 2006-04-11 | 2011-05-24 | Rolls-Royce Plc | Method of manufacturing a hollow article |
EP2384838A1 (en) * | 2010-05-06 | 2011-11-09 | Rolls-Royce plc | A mould assembly |
GB2549785A (en) * | 2016-04-29 | 2017-11-01 | Advanced Interactive Mat Science Ltd | Methods and apparatus for hot isostatic pressing |
EP3868493A1 (en) * | 2020-02-24 | 2021-08-25 | Rolls-Royce plc | Isostatic pressing |
Families Citing this family (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2868467B1 (en) | 2004-04-05 | 2006-06-02 | Snecma Moteurs Sa | TURBINE HOUSING WITH REFRACTORY HOOKS OBTAINED BY CDM PROCESS |
Citations (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB1443762A (en) * | 1972-12-05 | 1976-07-28 | Asea Ab | Container for manufacturing sintered products |
GB2002817A (en) * | 1977-08-18 | 1979-02-28 | Mtu Muenchen Gmbh | High-strength components of complex geometric shape and methods for their manufacture |
Family Cites Families (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2946681A (en) * | 1957-01-31 | 1960-07-26 | Federal Mogul Bower Bearings | Method of providing a body with a porous metal shell |
US4077109A (en) * | 1976-05-10 | 1978-03-07 | The International Nickel Company, Inc. | Hot working of metal powders |
US4137619A (en) * | 1977-10-03 | 1979-02-06 | General Electric Company | Method of fabricating composite structures for water cooled gas turbine components |
GB2073783B (en) * | 1980-04-10 | 1984-10-10 | Cameron Iron Works Inc | Lining valves by hot isotatic pressing |
JPS58223676A (en) * | 1982-03-05 | 1983-12-26 | ロ−ルス−ロイス・リミテツド | Composite product and manufacture |
JPS5966941A (en) * | 1982-10-07 | 1984-04-16 | Mitsubishi Heavy Ind Ltd | Manufacture of mold |
DE3241926A1 (en) * | 1982-11-12 | 1984-05-17 | MTU Motoren- und Turbinen-Union München GmbH, 8000 München | CONNECTION OF A CERAMIC ROTATION COMPONENT TO A METAL ROTATION COMPONENT FOR FLOW MACHINES, IN PARTICULAR GAS TURBINE ENGINES |
-
1987
- 1987-08-06 DE DE19873726056 patent/DE3726056A1/en active Granted
-
1988
- 1988-08-05 FR FR8810605A patent/FR2619034B1/en not_active Expired - Fee Related
- 1988-08-08 GB GB8818778A patent/GB2208389B/en not_active Expired - Lifetime
Patent Citations (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB1443762A (en) * | 1972-12-05 | 1976-07-28 | Asea Ab | Container for manufacturing sintered products |
GB2002817A (en) * | 1977-08-18 | 1979-02-28 | Mtu Muenchen Gmbh | High-strength components of complex geometric shape and methods for their manufacture |
Cited By (8)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
EP0528720A1 (en) * | 1991-08-09 | 1993-02-24 | ACIERIES ET FORGES D'ANOR Société à Responsabilité Limitée | Process for co-laminating high speed steel on mild steel |
US7946035B2 (en) | 2006-04-11 | 2011-05-24 | Rolls-Royce Plc | Method of manufacturing a hollow article |
EP2384838A1 (en) * | 2010-05-06 | 2011-11-09 | Rolls-Royce plc | A mould assembly |
US8425817B2 (en) | 2010-05-06 | 2013-04-23 | Rolls-Royce Plc | Mould assembly |
GB2549785A (en) * | 2016-04-29 | 2017-11-01 | Advanced Interactive Mat Science Ltd | Methods and apparatus for hot isostatic pressing |
US11278961B2 (en) | 2016-04-29 | 2022-03-22 | Sagittite Limited | Containment for hot isostatic pressing and vacuum degassing apparatus |
EP3868493A1 (en) * | 2020-02-24 | 2021-08-25 | Rolls-Royce plc | Isostatic pressing |
US12083600B2 (en) * | 2020-02-24 | 2024-09-10 | Rolls-Royce Plc | Isostatic pressing |
Also Published As
Publication number | Publication date |
---|---|
DE3726056C2 (en) | 1990-01-25 |
FR2619034B1 (en) | 1994-04-01 |
DE3726056A1 (en) | 1989-03-02 |
FR2619034A1 (en) | 1989-02-10 |
GB8818778D0 (en) | 1988-09-07 |
GB2208389B (en) | 1991-05-29 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
PCNP | Patent ceased through non-payment of renewal fee |
Effective date: 19950808 |