EP0194827A2 - Superplastic forming - Google Patents
Superplastic forming Download PDFInfo
- Publication number
- EP0194827A2 EP0194827A2 EP86301667A EP86301667A EP0194827A2 EP 0194827 A2 EP0194827 A2 EP 0194827A2 EP 86301667 A EP86301667 A EP 86301667A EP 86301667 A EP86301667 A EP 86301667A EP 0194827 A2 EP0194827 A2 EP 0194827A2
- Authority
- EP
- European Patent Office
- Prior art keywords
- preform
- pressure
- superplastically
- superplastic
- metal
- 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
- 239000002184 metal Substances 0.000 claims abstract description 8
- 229910052751 metal Inorganic materials 0.000 claims abstract description 8
- 239000007787 solid Substances 0.000 claims abstract description 8
- 238000003754 machining Methods 0.000 claims abstract description 5
- 239000011796 hollow space material Substances 0.000 claims abstract 3
- 238000000034 method Methods 0.000 claims description 24
- 239000012530 fluid Substances 0.000 claims description 7
- 238000004519 manufacturing process Methods 0.000 claims description 5
- 238000001125 extrusion Methods 0.000 claims description 3
- 238000003825 pressing Methods 0.000 claims description 3
- 239000007769 metal material Substances 0.000 claims description 2
- 239000000463 material Substances 0.000 description 13
- 238000003466 welding Methods 0.000 description 5
- 239000007789 gas Substances 0.000 description 4
- XKRFYHLGVUSROY-UHFFFAOYSA-N Argon Chemical compound [Ar] XKRFYHLGVUSROY-UHFFFAOYSA-N 0.000 description 2
- 229910001209 Low-carbon steel Inorganic materials 0.000 description 2
- 229910001069 Ti alloy Inorganic materials 0.000 description 2
- 238000005242 forging Methods 0.000 description 2
- 230000004927 fusion Effects 0.000 description 2
- 238000005098 hot rolling Methods 0.000 description 2
- 239000002904 solvent Substances 0.000 description 2
- 239000010935 stainless steel Substances 0.000 description 2
- 229910001220 stainless steel Inorganic materials 0.000 description 2
- 239000010936 titanium Substances 0.000 description 2
- 229910045601 alloy Inorganic materials 0.000 description 1
- 239000000956 alloy Substances 0.000 description 1
- 229910052786 argon Inorganic materials 0.000 description 1
- 239000003795 chemical substances by application Substances 0.000 description 1
- 238000005520 cutting process Methods 0.000 description 1
- 238000005553 drilling Methods 0.000 description 1
- 238000010894 electron beam technology Methods 0.000 description 1
- 238000003780 insertion Methods 0.000 description 1
- 230000037431 insertion Effects 0.000 description 1
- 230000002093 peripheral effect Effects 0.000 description 1
- 239000007921 spray Substances 0.000 description 1
- RUDFQVOCFDJEEF-UHFFFAOYSA-N yttrium(III) oxide Inorganic materials [O-2].[O-2].[O-2].[Y+3].[Y+3] RUDFQVOCFDJEEF-UHFFFAOYSA-N 0.000 description 1
Images
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B21—MECHANICAL METAL-WORKING WITHOUT ESSENTIALLY REMOVING MATERIAL; PUNCHING METAL
- B21D—WORKING OR PROCESSING OF SHEET METAL OR METAL TUBES, RODS OR PROFILES WITHOUT ESSENTIALLY REMOVING MATERIAL; PUNCHING METAL
- B21D26/00—Shaping without cutting otherwise than using rigid devices or tools or yieldable or resilient pads, i.e. applying fluid pressure or magnetic forces
- B21D26/02—Shaping without cutting otherwise than using rigid devices or tools or yieldable or resilient pads, i.e. applying fluid pressure or magnetic forces by applying fluid pressure
- B21D26/053—Shaping without cutting otherwise than using rigid devices or tools or yieldable or resilient pads, i.e. applying fluid pressure or magnetic forces by applying fluid pressure characterised by the material of the blanks
- B21D26/055—Blanks having super-plastic properties
Definitions
- This invention relates to the manufacture of hollow articles such as fluid containers and pressure vessels, by the superplastic expansion of a preform made of superplastically deformable metal.
- a method of making a hollow article for example a fluid container or pressure vessel which method includes making a pre-form by machining a hallow space within a solid piece of superglastically deformable metal and then superplastically expanding the pre-form to the required shape of said article by applying pressure within said hallow space while maintaining the pre-form at a temperature permitting superplastic deformation of said metal.
- a method of producing a container for fluid including the steps of:-
- said preform conprises a length of rod having a bore machined therein.
- said method further includes the steps of attaching a hollow plug to the mouth of said blind passage by welding, and the step of introducing pressurised fluid into said passage via said plug, thereby to expand said preform.
- said mould tool is of similar axial extent to said preform.
- the invention also extends to a pressure vessel whenever manufactured in accordance with the above method.
- the preform conprises a main body portion 1 which is formed by cutting a length of rod and drilling or machining it to form a blind bore.
- the rod is hot-rolled, centreless ground pickled and produced by normal metallurgical methods from the alloy Ti 6Al 4V.
- An end plug 2 is turned from the same rod material as the main body portion 1 and a spout 3 is formed of the same material.
- the main body portion 1, end plug 2 and spout 3 are thoroughly degreased and then electron beam welded together to form in combination a preform 4.
- the preform is cleaned and degreased and then placed in a mould tool conprising mould tool portions 5, 51.
- the mould is formed of mild steel and prior to insertion of the preform the interior of the mould is degreased, spray coated with Yttria release agent in a solvent base, and then baked in an oven to drive off the solvent.
- the assembled mould tool with the preform inside is placed in a stainless steel muffle box 6 which is subsequently sealed by welding, but having inlets for shielding gas and for forming gas.
- the muffle box and its contents are then placed in a cold press. Low pressure gas is allowed to flood the muffle box via inlet 7 and the cold press is then heated electrically to a temperature of 930°Ct5°C and allowed to stabilize.
- the superplastic forming temperature typically between 900°C and 950°C
- argon gas at pressure is admitted to the preform via spout 3.
- the pressure is controlled to increase gradually over a period from atmospheric to the forming pressure (typically 200-400 psi) whereupon this pressure is maintained for a period to suit the superplastic forming strain rate, and then released (the whole process taking approximately three hours).
- the mould is then allowed to cool to a temperature sufficiently low to allow handling and the muffle box and its contents are removed from the press and disassembled to allow removal of the formed component.
- Ti 6A1 4V is the material employed; however, it is believed that the above described method has applications with other superplastic material.
- the preform In design of an appropriate preform, it is the ratio of wall thickness to internal diameter that is the critical factor in determining the forming pressure cycle.
- the preform may be shaped internally and externally by conventional machining methods, to form, for example, external lugs or internal ribs.
- the mould tool comprises two portions of mild steel. It can however be formed of stainless steel and indeed this is preferred for it obviates the need for a muffle box.
- the rod from which the body portion l, plug 2 and spout 3 of the preform 4 are made can be produced by hot rolling as mentioned earlier or alternatively could be made by a forging process.
- the body portion 1 could be produced by extrusion as an open-ended hollow cylinder which is then fitted with plug 2 and spout 3 at one end while a solid blanking plug (not shown) is welded in place at its other end.
- the length of rod and/or the details of the process is or are selected so that the metallurgical grain dimensions of the wall of the preform are not too elongated in any one direction, ie axially or circumferentially.
- the article to be produced is to have one or more fairly sharp corners, such as the peripheral corners where the cylindrical part of the completed pressure vessel shown in figure 3 meets the domed end faces of the vessel, it may be preferred to so control the application of the pressure within the preform that the major part of the expansion of the preform occurs by a superplastic deformation process while the remainder, ie the final expansion of the preform into the sharp comers of the mould, occurs by a creep deformation process.
- the pressure applied within the preform can be controlled to maintain a strain rate within the preform material in or around the range 10 to 10 -4 , this giving the superplastic deformation stage of the process, and then the pressure is maintained constant, or very gradually increasing, at a value producing a strain rate of around 10 for quite a large proportion (around one third say) of the overall deformation process time to produce the final creep deformation stage.
- Figure 4 illustrates the manufacture of another hollow article, nameley a two-compartment pressure vessel for use in the manufacture of cold dry air.
- the preform comprises two cylindrical pieces of rod 41 and 42 each of which has been drilled from one end to form a blind hole therein. A radial hole is also drilled in each piece and the two are joined by a length of titanium alloy tube 43 fixed by welding into the respective radial holes.
- the open end of the hole in the piece 41 is closed by welding a solid titanium alloy plug 44 therein while the open end of the hole in piece 42 is fitted with a plug 2 and spout 3 of figure 1.
- Both pieces 41 and 42 are then superplastically expanded by the application of pressure to spout 46 so that they take up the shape of the mould 47. After expansion, plug and spout 45 and 46 are replaced by a solid plug or possibly the spout 46 is sinply sealed off and exit and entry holes (not shown) for the air to be processed are drilled in the originally closed ends of the pieces 41 and 42.
Landscapes
- Physics & Mathematics (AREA)
- Fluid Mechanics (AREA)
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Shaping Metal By Deep-Drawing, Or The Like (AREA)
- Blow-Moulding Or Thermoforming Of Plastics Or The Like (AREA)
- Forging (AREA)
- Powder Metallurgy (AREA)
Abstract
Description
- This invention relates to the manufacture of hollow articles such as fluid containers and pressure vessels, by the superplastic expansion of a preform made of superplastically deformable metal.
- It is known in the art to form hollow articles by expanding preforms fabricated Lsuperplastic material in sheet form. In such methods, one, two or more sheets of superplastic material are fusion welded together around their peripheries to form an envelope which is then superplastically expanded against a mould tool to form a structure. The applicants have made vessels in this way and it is found that the local microstructures resulting from the fusion welding do not exhibit superplastic properties to any great degree. In addition, the presence of a seam is thought to degrade the structural integrity of the container and moreover the finished product will have an external flange remaining adjacent the seam which will need to be machined away if the container is to have a smooth outer surface.
- According to one aspect of the invention, there is provided a method of making a hollow article, for example a fluid container or pressure vessel which method includes making a pre-form by machining a hallow space within a solid piece of superglastically deformable metal and then superplastically expanding the pre-form to the required shape of said article by applying pressure within said hallow space while maintaining the pre-form at a temperature permitting superplastic deformation of said metal.
- According to a second aspect, there is provided a method of producing a container for fluid, said method including the steps of:-
- (i) selecting a solid blank of a superplastic metal material,
- (ii) foinung an elongate blind passage in said blank thereby to create a preform element,
- (iii) introducing said preform into a mould tool,
- (iv) expanding said preform superplastically under selected conditions of temperature and pressure to conform to said mould tool.
- Preferably, said preform conprises a length of rod having a bore machined therein.
- Conveniently, said method further includes the steps of attaching a hollow plug to the mouth of said blind passage by welding, and the step of introducing pressurised fluid into said passage via said plug, thereby to expand said preform.
- Preferably said mould tool is of similar axial extent to said preform.
- The invention also extends to a pressure vessel whenever manufactured in accordance with the above method.
- All of the prior art examples of structures known to the applicants are formed from a preform which is fabricated from sheet or plate material. The Applicants themselves previously thought it inpossible, or at least highly undesireable, to use any material other than sheet because it was thought necessary that the material to undergo superplastic forming should have generally isotropic properties (which can be developed in sheet) rather than the unidirectional properties of bar which arise as a consequence of its forming process. For convenience, the phrase "superplastic material" is used to described material capable of undergoing superplastic deformation.
- By way of example only, an embodiment of pressure vessel manufactured in accordance with this invention will now be described in detail, reference being made to the accoupanying drawings, in which:
- Figure 1 is a schematic section view of a preform element,
- Figure 2 is a schematic section view of the preform element located in the mould tool prior to forming,
- Figure 3 is a schematic section view of the pressure vessel formed by expansion of the preform element, and
- Figure 4 is a sectioned view of another preform element located in its mould tool prior to forming.
- Referring to the drawings, the preform conprises a main body portion 1 which is formed by cutting a length of rod and drilling or machining it to form a blind bore. The rod is hot-rolled, centreless ground pickled and produced by normal metallurgical methods from the alloy Ti 6Al 4V.
- An end plug 2 is turned from the same rod material as the main body portion 1 and a
spout 3 is formed of the same material. The main body portion 1, end plug 2 andspout 3 are thoroughly degreased and then electron beam welded together to form in combination a preform 4. - The preform is cleaned and degreased and then placed in a mould tool conprising
mould tool portions 5, 51. The mould is formed of mild steel and prior to insertion of the preform the interior of the mould is degreased, spray coated with Yttria release agent in a solvent base, and then baked in an oven to drive off the solvent. - The assembled mould tool with the preform inside is placed in a stainless
steel muffle box 6 which is subsequently sealed by welding, but having inlets for shielding gas and for forming gas. The muffle box and its contents are then placed in a cold press. Low pressure gas is allowed to flood the muffle box via inlet 7 and the cold press is then heated electrically to a temperature of 930°Ct5°C and allowed to stabilize. - Once the temperature of the preform has reached the superplastic forming temperature (typically between 900°C and 950°C) argon gas at pressure is admitted to the preform via
spout 3. The pressure is controlled to increase gradually over a period from atmospheric to the forming pressure (typically 200-400 psi) whereupon this pressure is maintained for a period to suit the superplastic forming strain rate, and then released (the whole process taking approximately three hours). - The mould is then allowed to cool to a temperature sufficiently low to allow handling and the muffle box and its contents are removed from the press and disassembled to allow removal of the formed component.
- It is emphasised that in the above example the ranges of values of temperature and pressure are relevant only for the example under consideration. Appropriate parameters for other preforms can be calculated from knowledge of the flow stress of the superplastic material concerned and assessment of the internal pressure required to generate an approximately equivalent hoop stress.
- In the above example Ti 6A1 4V is the material employed; however, it is believed that the above described method has applications with other superplastic material.
- In design of an appropriate preform, it is the ratio of wall thickness to internal diameter that is the critical factor in determining the forming pressure cycle. The preform may be shaped internally and externally by conventional machining methods, to form, for example, external lugs or internal ribs.
- In the above example, the mould tool comprises two portions of mild steel. It can however be formed of stainless steel and indeed this is preferred for it obviates the need for a muffle box.
- The rod from which the body portion l, plug 2 and
spout 3 of the preform 4 are made can be produced by hot rolling as mentioned earlier or alternatively could be made by a forging process. As a further possibility, the body portion 1 could be produced by extrusion as an open-ended hollow cylinder which is then fitted with plug 2 andspout 3 at one end while a solid blanking plug (not shown) is welded in place at its other end. - For the best results, the length of rod and/or the details of the process (ie the particular parameters of the hot rolling, forging or extrusion process) is or are selected so that the metallurgical grain dimensions of the wall of the preform are not too elongated in any one direction, ie axially or circumferentially.
- Particularly where the article to be produced is to have one or more fairly sharp corners, such as the peripheral corners where the cylindrical part of the completed pressure vessel shown in figure 3 meets the domed end faces of the vessel, it may be preferred to so control the application of the pressure within the preform that the major part of the expansion of the preform occurs by a superplastic deformation process while the remainder, ie the final expansion of the preform into the sharp comers of the mould, occurs by a creep deformation process. For example, while maintaining the preform at its superplastic deformation temperature throughout the process, the pressure applied within the preform can be controlled to maintain a strain rate within the preform material in or around the range 10 to 10-4, this giving the superplastic deformation stage of the process, and then the pressure is maintained constant, or very gradually increasing, at a value producing a strain rate of around 10 for quite a large proportion (around one third say) of the overall deformation process time to produce the final creep deformation stage.
- Figure 4 illustrates the manufacture of another hollow article, nameley a two-compartment pressure vessel for use in the manufacture of cold dry air. The preform comprises two cylindrical pieces of
rod titanium alloy tube 43 fixed by welding into the respective radial holes. The open end of the hole in thepiece 41 is closed by welding a solidtitanium alloy plug 44 therein while the open end of the hole inpiece 42 is fitted with a plug 2 andspout 3 of figure 1. Bothpieces mould 47. After expansion, plug andspout spout 46 is sinply sealed off and exit and entry holes (not shown) for the air to be processed are drilled in the originally closed ends of thepieces
Claims (2)
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB858506157A GB8506157D0 (en) | 1985-03-09 | 1985-03-09 | Superplastic forming |
GB8506157 | 1985-03-09 |
Publications (3)
Publication Number | Publication Date |
---|---|
EP0194827A2 true EP0194827A2 (en) | 1986-09-17 |
EP0194827A3 EP0194827A3 (en) | 1987-08-19 |
EP0194827B1 EP0194827B1 (en) | 1989-05-24 |
Family
ID=10575741
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
EP19860301667 Expired EP0194827B1 (en) | 1985-03-09 | 1986-03-10 | Superplastic forming |
Country Status (7)
Country | Link |
---|---|
EP (1) | EP0194827B1 (en) |
JP (1) | JPH0790295B2 (en) |
DE (1) | DE3663458D1 (en) |
DK (1) | DK160000C (en) |
ES (1) | ES8702187A1 (en) |
GB (2) | GB8506157D0 (en) |
NO (1) | NO163598C (en) |
Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2591131A1 (en) * | 1985-12-10 | 1987-06-12 | Messerschmitt Boelkow Blohm | PROCESS FOR MANUFACTURING RESERVOIRS BY SUPERPLASTIC STATE DEFORMATION |
FR2772459A1 (en) * | 1998-05-14 | 1999-06-18 | Commissariat Energie Atomique | Process for fabricating a watertight envelope for a reservoir |
US8991683B2 (en) | 2006-03-30 | 2015-03-31 | The Boeing Company | Mark-off suppression in superplastic forming and diffusion bonding |
Families Citing this family (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US5407494A (en) * | 1993-12-21 | 1995-04-18 | Crs Holdings, Inc. | Method of fabricating a welded metallic duct assembly |
US6182487B1 (en) * | 1998-02-18 | 2001-02-06 | Nippon Sanso Corporation | Metal vessel and a fabrication method for the same |
CN103769482B (en) * | 2013-10-22 | 2016-08-24 | 北京航星机器制造有限公司 | A kind of integral forming method of titanium alloy air intake duct part |
Citations (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB1378421A (en) * | 1972-01-18 | 1974-12-27 | British Aircraft Corp Ltd | Forming articles from superplastic alloys |
FR2245428A1 (en) * | 1973-10-02 | 1975-04-25 | Alter Licensing Ets | |
GB2030480A (en) * | 1978-09-29 | 1980-04-10 | British Aerospace | Method of making a stiffened panel |
Family Cites Families (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB276247A (en) * | 1927-02-24 | 1927-08-25 | Ernst Asberger | Improved metal blowing process |
GB888461A (en) * | 1956-11-14 | 1962-01-31 | Thompson J Wolverhampton Ltd | Improvements relating to a method of and means for forming an inflated hollow body from sheet or plate metal |
JPS52130465A (en) * | 1976-04-26 | 1977-11-01 | Yamaha Motor Co Ltd | Bulge processing method |
FR2453693A1 (en) * | 1979-04-13 | 1980-11-07 | Aerospatiale | PROCESS FOR FORMING SUPERPLASTIC MATERIAL |
JPS5744431A (en) * | 1980-08-30 | 1982-03-12 | Nippon Koki Kk | Formation of hot bulge and pattern or the like for pipe to be worked using metallic bead as medium |
-
1985
- 1985-03-09 GB GB858506157A patent/GB8506157D0/en active Pending
-
1986
- 1986-03-07 NO NO860872A patent/NO163598C/en unknown
- 1986-03-07 DK DK104286A patent/DK160000C/en not_active IP Right Cessation
- 1986-03-08 ES ES552806A patent/ES8702187A1/en not_active Expired
- 1986-03-10 GB GB08605888A patent/GB2175235B/en not_active Expired
- 1986-03-10 DE DE8686301667T patent/DE3663458D1/en not_active Expired
- 1986-03-10 EP EP19860301667 patent/EP0194827B1/en not_active Expired
- 1986-03-10 JP JP61050712A patent/JPH0790295B2/en not_active Expired - Lifetime
Patent Citations (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB1378421A (en) * | 1972-01-18 | 1974-12-27 | British Aircraft Corp Ltd | Forming articles from superplastic alloys |
FR2245428A1 (en) * | 1973-10-02 | 1975-04-25 | Alter Licensing Ets | |
GB2030480A (en) * | 1978-09-29 | 1980-04-10 | British Aerospace | Method of making a stiffened panel |
Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2591131A1 (en) * | 1985-12-10 | 1987-06-12 | Messerschmitt Boelkow Blohm | PROCESS FOR MANUFACTURING RESERVOIRS BY SUPERPLASTIC STATE DEFORMATION |
FR2772459A1 (en) * | 1998-05-14 | 1999-06-18 | Commissariat Energie Atomique | Process for fabricating a watertight envelope for a reservoir |
US8991683B2 (en) | 2006-03-30 | 2015-03-31 | The Boeing Company | Mark-off suppression in superplastic forming and diffusion bonding |
Also Published As
Publication number | Publication date |
---|---|
GB8605888D0 (en) | 1986-04-16 |
JPH0790295B2 (en) | 1995-10-04 |
ES552806A0 (en) | 1987-01-01 |
GB2175235B (en) | 1988-12-21 |
DK104286A (en) | 1986-09-10 |
DE3663458D1 (en) | 1989-06-29 |
EP0194827A3 (en) | 1987-08-19 |
NO163598C (en) | 1990-06-27 |
DK160000C (en) | 1991-06-17 |
GB2175235A (en) | 1986-11-26 |
ES8702187A1 (en) | 1987-01-01 |
JPS61253130A (en) | 1986-11-11 |
NO860872L (en) | 1986-09-10 |
NO163598B (en) | 1990-03-19 |
DK104286D0 (en) | 1986-03-07 |
GB8506157D0 (en) | 1985-04-11 |
EP0194827B1 (en) | 1989-05-24 |
DK160000B (en) | 1991-01-14 |
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