FIELD OF THE INVENTION
[0001] The present invention relates to a method and composition for treating vanadium,
and more particularly to improving the oxidation resistance of the metal thereby enhancing
its utilization in fusion reactors.
BRIEF DESCRIPTION OF THE PRIOR ART
[0002] Fusion reactors typically include a number of concentric structural members for containing
a deuterium-tritium plasma within the center of the reactor. The first structural
member enclosing the plasma is referred to as the first wall which is backed up by
a thicker structure referred to as the blanket. The purpose of the blanket is to capture
neutrons which have permeated the first wall. Cooling pipes are embedded within the
blanket for maintaining an acceptable temperature within the reactor structure as
deuterium and tritium fuels are burned in the plasma.
[0003] Critical material problem areas for fusion reactors include two major considerations.
The first is the necessary compatibility of the first wall and blanket with coolants
such as helium, water or liquid metals. The second consideration is the minimization
of tritium fuel permeation through the first wall which would contaminate the coolant.
In order to satisfy these two major critical problem areas, the leading metals used
for the first wall and blanket are austenitic stainless steels, commercially known
as the Series 300 steels. These steels include a high chromium-iron-nickel alloy to
stabilize the high temperature phase of iron. The addition of chromium content in
the austenitic stainless steels is necessary to stabilize the non-magnetic phase of
the steel so that the iron component of the steel does not become magnetic, a condition
which would cause great stress on the structural material due to the presence of the
strong magnetic fields in the reactor which are employed to contain the plasma.
[0004] The most important advantage of the austenitic steels as reactor structural materials
resides in the fact that these steels offer good oxidation resistance and high temperature
strength. Unfortunately, these steels are not resistant to swelling at elevated temperatures
when exposed to a high flux of neutrons. Further, these steels have inferior thermal
physical properties due to their low thermal conductivity and high expansion coefficients
which accentuates thermal stress when installed in a high temperature reactor.
[0005] A further problem with the austenitic stainless steels is their propensity for induced
radioactivity which will result in these stainless steels becoming radioactive with
time.
[0006] The austenitic steels also suffer from poor corrosion resistance when exposed to
high temperature liquid metals that may be employed as a reactor coolant. This necessarily
restricts the choice of coolants available.
[0007] It has been recognized that vanadium alloys would offer major advantages when compared
to the austenitic stainless steels for fusion reactor applications. The major advantage
with respect to vanadium alloys includes greater strength and creep resistance at
elevated temperatures. In addition, vanadium alloys are not incompatible with liquid
metal coolants. They appear to further offer superior neutron irradiation damage resistance,
principally to swelling.
[0008] The vanadium alloys also provide superior thermophysical properties including lower
thermal expansion, greater thermal conductivity, and lower modulus.
[0009] It has also been determined that vanadium alloys offer significantly lower induced
radioactivity as compared with the steels.
[0010] Although these advantages present vanadium alloys as a highly desirable material
for fusion reactors, these alloys suffer from two major problems which have hitherto
prevented their use for first wall and blanket structures in a fusion reactor. These
major problem areas include greater reactivity with coolants containing oxygen which
results in oxygen embrittlement of the alloys and high tritium permeability, which
is unacceptable for the first wall which must contain the hydrogen isotope plasma
in the center of the reactor.
[0011] As a result of these severe problems, vanadium alloys (including chromium and titanium
constituents) have not found any significant application in commercial power reactors.
BRIEF DESCRIPTION OF THE PRESENT INVENTION
[0012] The primary purpose of the present invention is to render prior art vanadium alloys
compatible with gaseous and/or liquid coolants containing oxygen and/or water vapor
impurities for application to fusion reactor first wall or blanket structures at elevated
temperatures, customarily reaching up to 650°C.
[0013] Oxidation resistance of the vanadium alloys is achieved by diffusing a chromium and/or
aluminum constituent into a vanadium alloy substrate whereby the diffused chromium
or aluminum will be concentrated at the surface of the substrate while forming a rapidly
diminishing diffusion gradient through the remainder of the substrate.
[0014] A vanadium alloy treated in accordance with the present invention allows it to be
employed in a fusion reactor first wall and/or blanket structure so that the attendant
advantages of the vanadium alloy, as compared with the austenitic steels may be realized.
[0015] In utilizing this invention an oxide film is formed on the vanadium alloy which then
protects the alloy from further oxidation and embrittlement. The oxide film is also
useful as a tritium barrier.
BRIEF DESCRIPTION OF THE FIGURES
[0016] The above-mentioned objects and advantages of the present invention will be more
clearly understood when considered in conjunction with the accompanying drawings,
in which:
- figure 1 is a schematic view of a fusion reactor;
- figure 2 is a schematic representation of the present invention and illustrates
the enrichment of a vanadium alloy with a diffused chromium or aluminum surface layer;
- figure 3 is a schematic representation of means for treating a vanadium alloy panel
in accordance with the present invention to achieve the surface-enriched diffused
layer integral with a vanadium alloy, as shown in figure 2;
- figure 4 is a plot of weight grain by various vanadium materials, illustrating the
resistance to oxidation by an alloy of the present invention;
- figure 5 is a plot similar to that shown in figure 4 but with the ordinates normalized
as a function of weight per unit area squared and illustrates the oxidation kinetics
of-the present vanadium alloy with an enriched diffused layer.
DETAILED DESCRIPTION OF THE INVENTION
[0017] Figure 1 schematically illustrates a fusion reactor for which the present invention
has application. The reactor generally indicated in cross section by reference numeral
10 includes a central area where deuterium and tritium plasma are burned. A first
wall 13 confines plasma 12 and neutrons which are generated in the plasma will penetrate
the relatively thin first wall 13. In order to capture these neutrons, a relatively
thick blanket 14 concentrically backs up the first wall. The present improved vanadium
alloy has its greatest application as a structural material for the first wall 13
and blanket 14.
[0018] Radially outwardly from blanket 14 is shield 16, conventionally made of lead and
having as its primary purpose the confinement of neutrons which have passed through
the first wall and blanket. The electromagnets 18 are located around the shield 16
and are intended to generate a strong magnetic field which interacts with the plasma
and confines it to the center of the reactor. Deuterium and tritium fuels are provided
at inlets 20 and 22. Auxiliary heating means 24 and 26 preheat the fuel. At the outlet
30 of the reactor is a vacuum pump 28 which is employed to remove unburned fuel from
the reactor as well as to remove the helium ash from the burned fuel. Helium cryopumps
32 are provided for processing the helium and recovering fuel from the evacuated gas.
The recovered fuel is recycled at 36, and newly supplied fuel is introduced at 34.
The fuel is introduced at 38 and 40 to the auxiliary heaters 24 and 26.
[0019] The blanket 14 is provided with embedded coolant pipes 42 for maintaining the reactor
at an acceptable temperature level. Conventionally, the coolant undergoes tritium
extraction at 44. Primary and secondary heat exchangers 46, 48 generate steam for
the turbine 50, which is used to generate electricity.
[0020] Figure 2 schematically illustrates the surface-enriched vanadium alloy of the present
invention. Structurally speaking, a substrate 54 of a conventional vanadium alloy
is employed. Typically, such an alloy may include 15 percent chromium and 5 percent
titanium. Then, an enriching metal, preferably chromium and/or aluminum, is diffused
into the substrate 54 so as to form an enriched diffused layer 56. The diffused metal
will actually form a gradient through the entire thickness of the enriched alloy 52.
However, the greatest concentration of diffused metal atoms will reside immediately
adjacent the surface 57 of the enriched alloy 52.
[0021] It is to be stressed that the diffused layer 56 is not a coating but an actual diffusion
zone of chromium and/or aluminum into the substrate 54. In fact, a coating of the
material would be unsatisfactory because the high temperature environment would probably
cause delamination, flaking or the development of fissures in the coating leading
to loss of protection.
[0022] Figure 3 illustrates a simplified view of a setup for performing the method of the
present invention, namely, forming the diffused layer 56 (figure 2). As will be seen,
an evacuated vessel 58 has a vanadium alloy panel 60 suspended therein, the panel
being comprised totally of the vanadium alloy substrate 54 (figure 2). A chromium
and/or aluminum charge 62 is also included within the vessel 58 and the charge is
heated. As a result, chromium or aluminum vapors 64 evaporated from the charge and
diffuses into the substrate material of panel 60 forming a corresponding chromium
and/or aluminum diffused layer, such as 56 (figure 2). It is to be emphasized that
other conventional methods may be used for diffusing the chromium or aluminum into
the vanadium alloy substrate. For example, the chromium or aluminum might be deposited
onto the surface of the substrate via conventional means (i.e., sputtering) and subsequently
heated to effect diffusion of the chromium or aluminum into the substrate metal.
[0023] Although a particular vanadium alloy (15 percent chromium, 5 percent titanium) has
been disclosed, this is not to be construed as a limitation of the invention. Other
vanadium alloys may be employed as long as the alloy constituents enhance the oxidation
resistance property of the base metal and are soluble in the base metal so as to be
metallurgically compatible therewith. For example, it is conceivable that a nickel
constituent would be acceptable for a vanadium alloy substrate.
[0024] Further, metals other than chromium or aluminum could be used for enriching the surface
of the vanadium alloy. The depth and operating parameters of the diffusing material
may be determined by experimentation in accordance with the basic concepts of the
present invention, namely, enriching the surface of the vanadium alloy by diffusing
an appropriate metal onto the surface which will provide oxidation resistance in the
form of a protective oxide barrier in the presence of an oxidizing coolant as employed
in a fusion reactor operating at temperatures up to 650°C.
[0025] In order to visually compare the oxidation resistance of the surface-enriched vanadium
alloy with pure vanadium and the non-enriched vanadium alloy, reference is made to
figure 4. The left ordinate represents the oxygen weight gain (vs. time) of pure vanadium
and the known vanadium-chromium-titanium alloy. The right ordinate corresponds to
the oxygen pickup (vs. time) for the diffusion-enriched vanadium alloy of the present
invention, and stainless steel, the latter being the predominant structural material
for first walls and blankets, as previously discussed. As will be seen, the oxygen
pickup of stainless steel is the lowest over time. However, of the remaining vanadium
metals, the lowest plot, representing the chromium version of the present invention,
offers superior results.
[0026] Figure 5 compares the oxidation kinetics for pure vanadium, the non-enriched vanadium
alloy, and the chromium diffused surface-enriched alloy of the invention. Again, the
left ordinate corresponds to oxygen weight gain of the upper and middle plots, while
the right ordinate represents the weight gain for the chromium version of the present
invention. Inasmuch as the ordinate for these plots is normalized as the square of
micrograms per unit area, all of the plots illustrate that the oxidation rates in
fact follow parabolic curves which, in accordance with accepted metallurgical principles,
indicates a protective oxide layer. Again, it will be observed that the lowest weight
gain on a parabolic basis is the chromium surface diffused vanadium alloy. It is to
be understood that similar results would follow if the surface- diffused enrichment
was done with aluminum instead of chromium.
[0027] Accordingly, enriching vanadium alloy structural materials in accordance with the
present invention provides superior oxidation protection for first wall and blanket
structures of a fusion reactor.
[0028] It should be understood that the invention is not limited to the exact details of
construction shown and described herein for obvious modifications will occur to persons
skilled in the art.
1.- A method for improving the oxidation resistance of a structural member fabricated
from a vanadium alloy, the method comprising the steps:
- positioning the structural member in confronting relation to a charge having a metal
selected from the group including chromium and aluminum;
- heating the charge to form vapors;
- subjecting the member to the vapors for a period of time sufficient for the charge
metal to diffuse into a confronting surface of the member thus creating a gradient
of the charge metal through the member and defining an oxidation resistant enriched
surface layer.
2.- The method set forth in claim 1 wherein the vanadium alloy includes chromium and
titanium constituents.
3.- A method for improving the oxidation resistance of a structural member fabricated
from a vanadium alloy, the method comprising the steps of:
- coating at least one preselected surface of the member with a metal selected from
the group including chromium and aluminum;
- heating the coated metal until the coating diffuses into the member surface thus
creating a gradient of the metal through the member and defining an oxidation resistant
enriched surface layer.
. 4.- The method set forth in claim 3 wherein the vanadium alloy includes chromium
and titanium constituents.
5.- An oxidation resistant structural member comprising:
- a vanadium alloy substrate; and
- a metal, selected from the group including chromium and aluminum, diffused into
a surface of the substrate and forming anlenriched layer in which the concentration
of diffused metal decreases inwardly along a gradient.
6.- The member set forth in claim 5 wherein the alloy includes chromium and titanium
constituents.
7.- In a fusion reactor, at least one structural member pretreated for high temperature
oxidation resistance, said member comprising:
- a vanadium alloy substrate; and
- a metal selected from the group including chromium and aluminum diffused into a
surface of the substrate and forming an enriched layer in which the concentration
of the diffused metal decreases inwardly along a gradient.
8.- The structure set forth in claim 7 wherein the alloy includes chromium and titanium
constituents.