[0001] This invention relates to the manufacture of hollow vessels such as fluid containers
and pressure vessels, by the superplastic expansion of a preform made of superplastically
deformable metal.
[0002] For convenience, the phrase «superplastic material» is used to describe material
capable of undergoing superplastic deformation.
[0003] It is known in the art to form hollow vessels by expanding preforms fabricated from
superplastic material in sheet form. In such methods, 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 the vessel. The applicants
have made vessels in this way and it is found that the local microstructures resulting
from tthe fusion welding do not exihibit super- plastic 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.
[0004] Most of the prior art examples of structures known to the applicants are formed from
a pre- form which is fabricated from sheet or plate material. The applicants themselves
previously thought it impossible, or at least highly undesireable, to use any material
other than sheet because the material to undergo superplastic forming should have
generally isotropic properties (which can be developed in sheet) rather than the unidirectional
properties of rod or bar material which arise as a consequence of its forming process.
[0005] In FR-A-22 445 428, however, it is proposed to make a hollow tubular preform by drawing
or extruding a metal disc, to subject the preform to a surface finishing process,
for example polishing or 'ironing' and then, after a pre-heating step, to superplastically
deform the preform to the shape of a container.
[0006] According to the invention, there is provided a method of making a hollow vessel,
for example a fluid container or pressure vessel, wherein a hollow pre-form made of
superplastically deformable metal is expanded to the required shape of the vessel
by applying pressure within the pre-form while maintaining it at a temperature permitting
superplastic deformation of the metal, characterised in that, to make the pre-form,
there is taken a length of solid superplastically deformable metal bar, and then the
central region extending along and around the central axis of the length of bar is
removed by machining so as to leave the pre-form with al wall having a grain structure
suitable for superplastic deformation.
[0007] Preferably, an axially extending hole is drilled in a length of solid hot-rolled
titanium alloy bar.
[0008] Advantageously, the pre-form is expanded within a mould by applying a controlled
pressure within the pre-form to achieve an initial expansion of the pre-form by superplastic
deformation and then, with a strain rate of the pre-form metal less than that during
the initial expansion and over a substantial period of time, further expansion of
the preform by a creep deformation process.
[0009] For a better understanding of the invention, reference will now be made by way of
example, to the accompanying drawings, in which:
Figure 1 is a schematic section view of a preform;
Figure 2 is a schematic section view of the pre- form located in a mould prior to
forming;
Figure 3 is a schematic section view of a pressure vessel formed by expansion of the
preform element; and,
Figure 4 is a sectioned view of another preform element located in its mould prior
to forming.
[0010] Referring to the drawings, the preform comprises a main body portion 1 which is formed
by cutting a length of bar and drilling or machining it to form a blind bore. The
bar is hot-rolled, centreless ground pickled and produced by normal metallurgical
methods from the alloy Ti 6A1 4V.
[0011] 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.
[0012] The preform is cleaned and degreased and then placed in a mould tool comprising mould
tool portions 5, 5
1. 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.
[0013] 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 °C ± 5 °C and allowed to stabilise.
[0014] 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 1.4-2.8 x 10
6 Pa (200-400 psi)) whereupon this pressure is maintained for a period to suit the
super-plastic forming strain rate, and then released (the whole process taking approximately
three (hours).
[0015] 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.
[0016] 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.
[0017] 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.
[0018] 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.
[0019] 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.
[0020] The bar from which the body portion 1, 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.
[0021] The hot rolling or forging will have been carried out so that, after the central
bore is formed in the bar, the body portion 1 is left with a cylindrical wall in which
the metallurgical grain dimensions are not too elongated in any one direction, i.e.
axially or circumferentially.
[0022] 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 occur by a super- plastic deformation
process while the remainder, i.e. the final expansion of the preform into the sharp
corners 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-
3 to 10-
4 S-
1, 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-
6 S-
1 for quite a large proportion (around one third say) of the overall deformation process
time to produce the final creep deformation stage.
[0023] Figure 4 illustrates the manufacture of another hollow article, namely a two-compartment
pressure vessel for use in the manufacture of cold dry air. The preform comprises
two cylindrical pieces of bar 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 simply 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.
1. A method of making a hollow vessel, for example a fluid container or pressure vessel,
wherein a hollow pre-form made of superplastically deformable metal is expanded to
the required shape of the vessel by applying pressure within the pre- form while maintaining
it at a temperature permitting superplastic deformation of the metal, characterised
in that, to make the pre-form (4), there is taken a length of solid superplastically
deformable metal bar, and then the central region extending along and around the central
axis of the length of bar is removed by machining so as to leave the pre-form (4)
with a wall having a grain structure suitable for superplastic deformation.
2. A method according to Claim 1, wherein an axially extending hole is drilled in
a length of solid hot-rolled Titanium alloy bar (1).
3. A method according to Claim 1 or Claim 2, wherein the pre-form is expanded within
a mould by applying a controlled pressure within the pre- form to achieve an initial
expansion of the pre- form by superplastic deformation and then, with a strain rate
of the pre-form metal less than that during the initial expansion and over a substantial
period of time, the pre-form is further expanded by a creep deformation process.
1. Verfahren zur Herstellung eines Hohlkörpers, beispielsweise eines Flüssigkeitsbehälters
oder eines Druckgefässes, bei welchem eine hohle Vorform aus superplastisch deformierbarem
Metall in die gewünschte Form des Hohlkörpers dadurch ausgedehnt wird, dass die Vorform
unter einen Innendruck gesetzt wird, wobei eine zur Durchführung der superplastischen
Deformation erforderliche Temperatur aufrechterhalten wird, dadurch gekennzeichnet,
dass zur Herstellung der Vorform (4) eine Länge einer massiven superplastisch verformbaren
Metallstange benutzt wird, bei der der Mittelbereich längs der Mittelachse der Stange
und um diese Achse herum durch spanabhebende Bearbeitung derart entfernt wird, dass
die Vorform (4) mit einer Wand verbleibt, die einen Kornaufbau besitzt, der für die
superplastische Deformation geeignet ist.
2. Verfahren nach Anspruch 1, bei welchem ein axial verlaufendes Loch in eine Länge
einer massiven heissgewalzten Stange (1 ) aus einer Titanlegierung ausgebohrt wird.
3. Verfahren nach den Ansprüchen 1 oder 2, bei welchem die Vorform in einer Form ausgedehnt
wird, indem ein gesteuerter Druck in die Vorform eingelassen wird um eine anfängliche
Ausdehnung der Vorform durch superplastische Deformation zu bewirken, und bei welchem
dann über eine beträchtliche Zeitdauer die Vorform weiter durch ein Kriechdeformationsverfahren
mit einer Beanspruchungsrate ausgedehnt wird, die kleiner ist als die Beanspruchungsrate
während der anfänglichen Ausdehnung.
1. Procédé de fabrication d'un récipient creux, par exemple d'un conteneur de fluide
ou d'un récipient sous pression, dans lequel une préforme creuse en métal déformable
de façon superplastique est soumise à expansion pour épouser la forme requise du récipient
en appliquant une pression à l'intérieur de la préforme tout en la maintenant à une
température permettant la déformation superplastique du métal, caractérisé en ce que,
pour fabriquer la préforme (4) on prélève un tronçon de barre métallique massive déformable
de façon superplastique, et on enlève alors par usinage la zone centrale s'étendant
le long et autour de l'axe du tronçon de barre de manière à conserver dans la préforme
(4) une paroi ayant une structure des grains qui convient à une déformation superplastique.
2. Procédé selon la revendication 1, dans lequel on perce un trou s'étendant axialement
dans un tronçon d'une barre massive d'alliage de titane laminé à chaud (1 ).
3. Procédé selon la revendication 1 ou la revendication 2, dans lequel on soumet à
expansion la préforme à l'intérieur d'un moule en appliquant une pression contrôlée
à l'intérieur de la préforme pour obtenir une expansion initiale de la préforme par
déformation superplastique et alors, avec une vitesse de déformation du métal de la
préforme intérieure à celle se produisant pendant l'expansion initiale et pendant
un laps de temps important, on soumet de nouveau la préforme à expansion par un procédé
de déformation par fluage.