GB2137666A - Heat treatment of Al-Li alloys - Google Patents
Heat treatment of Al-Li alloys Download PDFInfo
- Publication number
- GB2137666A GB2137666A GB08407904A GB8407904A GB2137666A GB 2137666 A GB2137666 A GB 2137666A GB 08407904 A GB08407904 A GB 08407904A GB 8407904 A GB8407904 A GB 8407904A GB 2137666 A GB2137666 A GB 2137666A
- Authority
- GB
- United Kingdom
- Prior art keywords
- atmosphere
- heat treatment
- torr
- dry
- alloys
- 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
- 238000010438 heat treatment Methods 0.000 title claims abstract description 25
- 229910001148 Al-Li alloy Inorganic materials 0.000 title description 9
- 239000001989 lithium alloy Substances 0.000 title description 7
- CURLTUGMZLYLDI-UHFFFAOYSA-N Carbon dioxide Chemical compound O=C=O CURLTUGMZLYLDI-UHFFFAOYSA-N 0.000 claims abstract description 62
- 239000012298 atmosphere Substances 0.000 claims abstract description 33
- 229910002092 carbon dioxide Inorganic materials 0.000 claims abstract description 31
- 229910001868 water Inorganic materials 0.000 claims abstract description 19
- 229910052744 lithium Inorganic materials 0.000 claims abstract description 15
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 claims abstract description 15
- 239000001569 carbon dioxide Substances 0.000 claims abstract description 13
- WHXSMMKQMYFTQS-UHFFFAOYSA-N Lithium Chemical compound [Li] WHXSMMKQMYFTQS-UHFFFAOYSA-N 0.000 claims abstract description 12
- 230000036961 partial effect Effects 0.000 claims abstract description 5
- 229910000838 Al alloy Inorganic materials 0.000 claims abstract description 4
- VUZPPFZMUPKLLV-UHFFFAOYSA-N methane;hydrate Chemical compound C.O VUZPPFZMUPKLLV-UHFFFAOYSA-N 0.000 claims abstract 2
- IJGRMHOSHXDMSA-UHFFFAOYSA-N Atomic nitrogen Chemical compound N#N IJGRMHOSHXDMSA-UHFFFAOYSA-N 0.000 claims description 12
- 238000000034 method Methods 0.000 claims description 11
- QVGXLLKOCUKJST-UHFFFAOYSA-N atomic oxygen Chemical compound [O] QVGXLLKOCUKJST-UHFFFAOYSA-N 0.000 claims description 7
- 239000001301 oxygen Substances 0.000 claims description 7
- 229910052760 oxygen Inorganic materials 0.000 claims description 7
- 229910052757 nitrogen Inorganic materials 0.000 claims description 6
- 230000003647 oxidation Effects 0.000 claims description 4
- 238000007254 oxidation reaction Methods 0.000 claims description 4
- 239000012535 impurity Substances 0.000 claims 1
- 208000021017 Weight Gain Diseases 0.000 description 16
- 230000004584 weight gain Effects 0.000 description 16
- 235000019786 weight gain Nutrition 0.000 description 16
- 229910045601 alloy Inorganic materials 0.000 description 14
- 239000000956 alloy Substances 0.000 description 14
- 229910052786 argon Inorganic materials 0.000 description 8
- XKRFYHLGVUSROY-UHFFFAOYSA-N Argon Chemical compound [Ar] XKRFYHLGVUSROY-UHFFFAOYSA-N 0.000 description 6
- 239000007795 chemical reaction product Substances 0.000 description 5
- 238000000265 homogenisation Methods 0.000 description 4
- 238000011282 treatment Methods 0.000 description 4
- 238000006243 chemical reaction Methods 0.000 description 3
- 230000003247 decreasing effect Effects 0.000 description 3
- 230000000694 effects Effects 0.000 description 3
- 230000015572 biosynthetic process Effects 0.000 description 2
- 230000002401 inhibitory effect Effects 0.000 description 2
- 238000012423 maintenance Methods 0.000 description 2
- 239000000463 material Substances 0.000 description 2
- 239000000203 mixture Substances 0.000 description 2
- 239000012299 nitrogen atmosphere Substances 0.000 description 2
- 239000000047 product Substances 0.000 description 2
- 229920006395 saturated elastomer Polymers 0.000 description 2
- 229910018134 Al-Mg Inorganic materials 0.000 description 1
- 229910018467 Al—Mg Inorganic materials 0.000 description 1
- 229910000881 Cu alloy Inorganic materials 0.000 description 1
- 229910000733 Li alloy Inorganic materials 0.000 description 1
- 229910010092 LiAlO2 Inorganic materials 0.000 description 1
- 229910006309 Li—Mg Inorganic materials 0.000 description 1
- 229910019086 Mg-Cu Inorganic materials 0.000 description 1
- 230000002411 adverse Effects 0.000 description 1
- 238000005275 alloying Methods 0.000 description 1
- XAGFODPZIPBFFR-UHFFFAOYSA-N aluminium Chemical compound [Al] XAGFODPZIPBFFR-UHFFFAOYSA-N 0.000 description 1
- 229910052782 aluminium Inorganic materials 0.000 description 1
- 239000004411 aluminium Substances 0.000 description 1
- 238000000137 annealing Methods 0.000 description 1
- 230000009286 beneficial effect Effects 0.000 description 1
- 239000000470 constituent Substances 0.000 description 1
- 230000002939 deleterious effect Effects 0.000 description 1
- 230000002349 favourable effect Effects 0.000 description 1
- 239000007789 gas Substances 0.000 description 1
- 238000011835 investigation Methods 0.000 description 1
- 239000011159 matrix material Substances 0.000 description 1
- 230000035515 penetration Effects 0.000 description 1
- 238000010926 purge Methods 0.000 description 1
- 230000009257 reactivity Effects 0.000 description 1
- 229910052596 spinel Inorganic materials 0.000 description 1
- 239000011029 spinel Substances 0.000 description 1
Classifications
-
- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22F—CHANGING THE PHYSICAL STRUCTURE OF NON-FERROUS METALS AND NON-FERROUS ALLOYS
- C22F1/00—Changing the physical structure of non-ferrous metals or alloys by heat treatment or by hot or cold working
- C22F1/02—Changing the physical structure of non-ferrous metals or alloys by heat treatment or by hot or cold working in inert or controlled atmosphere or vacuum
Landscapes
- Chemical & Material Sciences (AREA)
- Physics & Mathematics (AREA)
- Thermal Sciences (AREA)
- Crystallography & Structural Chemistry (AREA)
- Engineering & Computer Science (AREA)
- Materials Engineering (AREA)
- Mechanical Engineering (AREA)
- Metallurgy (AREA)
- Organic Chemistry (AREA)
- Battery Electrode And Active Subsutance (AREA)
Abstract
The heat treatment of aluminium alloys having a lithium content in excess of 0.5% is carried out in an atmosphere of carbon dioxide and water vapour, the partial pressure of water vapour being at least 4 torr and more usually 10-50 torr.
Description
SPECIFICATION
Heat treatment of aluminium alloys containing lithium
The present invention relates to the heat treatment of aluminium alloys having a substantial content of lithium, that is to say more than 0.5% and more usually more than 1% Li. Such alloys, which may also contain Mg and/or Cu as principal alloying constituents, are of very considerable interest by virtue of the possibility of producing structural components having a high strength/weight ratio.
Owing to the reactivity of lithium, particularly at elevated temperatures, the heat treatment, such as solution heat treatment homogenisation and annealing, of such alloys presents considerable difficulties. At the solution heat treatment temperature, typically carried out at a temperature in the range of 500 - 575"C almost total loss of the lithium content may occur, particularly with thin section material, within normal heat treatment times by reason of reaction of lithium with the furnace atmosphere.
It has, of course, been found possible to reduce the rate of such reaction by control of the composition of the furnace atmosphere. In any heat treatment process of Al-Li alloys the reaction between the lithium content and the furnace atmosphere has two consequences (a) loss of lithium from the alloy (b) formation of reaction products which penetrate the intergrain boundaries. In the latter case the adverse effect of reaction products (in relation to the weight of such products) increases in line with the increase of volume due to the formation of such products. In particular the penetration of the intergrain boundaries is exceptionally undesirable in thin alloy sheet (section) because of the severe loss of alloy integrity.
For a viable commercial heat treatment operation the process conditions must be such that they can be maintained within reasonable limits of variation in commercial practice. Thus in a commercial heat treatment furnace adapted to treat a substantial load of material it is necessary to operate substantially at atmospheric pressure. It is exceedingly difficult to operate a heat treatment furnace without some ingress of atmospheric air.
Studies have been made of the effects of reducing the moisture content of the furnace atmosphere since prior studies show it to be beneficial in reducing the rate of oxidation of Mg in the case of Al-Mg alloys. In order to eliminate the effects of other potentially reactive components, particularly N2 and CO2, present in air, we have carried out such studies in an atmosphere composed of 80% argon and 20% oxygen.
It was found that, as represented by an increase in the weight of the treated specimen, the rate of attack was greatly decreased as the moisture content of this synthetic "air" atmosphere was decreased. However it was found that at the lowest moisture levels, which couid be expected to be maintained in practical commercial operation, the rate of oxidation of Li was unacceptably high. On the other hand when the moisture content was held at 10-3 torr the rate of attack on the Li content was considered generally acceptable.
Since commercial gases at such low moisture level are available, further tests were carried out in the laboratory to determine the rate of attack on the Li content in nitrogen and dry carbon dioxide atmospheres. In these tests the results obtained with dry nitrogen were markedly superior to those with dry carbon dioxide. Not unexpectedly Li was attacked more rapidly in the dry carbon dioxide atmosphere. The rate of attack in a dry nitrogen atmosphere was equivalent to that achieved with the synthetic air (80% Ar, 2.0% 02) of the same moisture content. It was therefore concluded that under practical conditions it would not be possible to employ a nitrogen atmosphere because of the difficulty in avoiding ingress of normal atmospheric moisture into the dry moisture furnace atmosphere.It was however discovered that the rate of weight gain was somewhat less for undried atmospheric air that for the argon/oxygen mixture at the same rnoisture content.
It was concluded that some atmospheric component was exerting an inhibiting effect on the attack of Li by oxygen in the presence of water vapour. It was confirmed that this inhibiting effect was due to carbon dioxide by Ar 80%,0220% synthetic air, which showed a small, but significant, decrease in weight gain in the presence of water vapour. In further tests employing a carbon dioxide atmosphere it was found that the rate of attack on Li was sharply decreased when the carbon dioxide atmosphere had an increased moisture content (17.5 torr H20), (about 2.3% weight) equivalent to saturated air at 20"C as compared with the discouraging results achieved in an atmosphere of dry carbon dioxide.
It was concluded according to the present invention that an essentially CO2 atmosphere containing a definite moisture content, could be employed as an atmosphere in any heat treatment of Al-Li alloys, because ingress of small amounts of oxygen, nitrogen and water vapour from ambient atmosphere would not be specially deleterious in relation to the rate of attack on the Li content of the alloy.
According to the present invention a heat treatment of an Al-Li alloy is carried out in an atmosphere consisting essentially. of carbon dioxide having a water content controlled to be in the range of 4 to 250 torr or even higher (about 0.6 - 31% by weight). This treatment is particularly effective in reducing oxidation of lithium in heat treatments carried out at temperatures in excess of 450"C.
It is preferred to maintain the water vapour content of the CO2 at a value in the range of 10 50 torr, since this can be achieved very easily.
In the following Table 1 are given the weight gains recorded when holding an Al-2.7% Li (by weight) alloy at 520"C in different dry and wet atmospheres. The weight gains are recorded as milligrams/cm2.
Table 1
Atmosphere
Time Dry 20%0 Wet 20%0 Dry CO2 Wet CO2 Dry N2
Minutes 80% Ar 80% Ar
5 25 53.3 91.7 43.3 5.0
10 74 145.0 233.3 105.0 16.6
20 136.6 266.7 400 166.7 80.0
45 224.6 483.3 645.0 266.7 235.0
60 226.3 583.3 756.7 310 278.0
90 330.8 750 948.3 383.3 343.0 120 395.0 890 1100.0 445.0 401.0 180 494.0 1136.7 1375.0 550.0 500.0 240 583.3 1603.3 1596.4 638.3 586.0 300 648.0 2205 1785 715.0 666.0
Weight Gain g/cm2
Note: "Dry" = 10-3 torr H20 "Wet" = 17.5torrH20 The figures in the above Table show nearly equal actual weight gains in dry oxygen/argon, dry nitrogen and wet carbon dioxide atmospheres.It should be appreciated that the reaction products in different atmospheres include lithium spinel "-LiAlO2, Li2N and Li2CO2. Thus a particular weight gain cannot be directly quantified with Li loss from the alloy. Investigation of the surface deposits formed on the surface of the alloy after heating in various atmospheres has revealed that at treatment temperatures of the order of 500"C the principal reaction product formed in wet or dry air or dry carbon dioxide is y-LiAI02, whereas in wet CO2 it is LiAlsO8, sp that a given weight gain in a wet CO2 atmosphere represents a much lower Li loss than for tfre other atmospheres.
In the accompanying Figure 1 the Li loss resulting from the weight gains at treatment times different atmospheres given in the foregoing Table is shown, calculated on the basis that all the weight gain is due to the principal reaction product present in the surface deposit.
It will be seen that heat treatment at 520"C in CO2, having a moisture content of the order of 15-20 torr results in an Li loss of only about 25% of the loss in the next least unfavourable atmosphere tested, namely dry "air". It should be noted that the maintenance of so low a moisture content as the "dry" conditions employed in these tests, would be difficult in an industrial heat treatment furnace. On the other hand the maintenance of the "wet" CO2 atmosphere (17.5 torr H20) is extremely simple, since this can be achieved by supplying the furnace atmosphere with a stream of CO2, bubbled through water at 15-20"C with a contact time sufficient to saturate the CO2 with water vapour.
In the accompanying Fig. 2 are graphically illustrated the weight gains resulting from the heat treatment of Al-2.7%Li alloy in a carbon dioxide atmosphere saturated with water vapour at 0 C, 20"C and 70"C respectively.
The partial pressure of water vapour at these temperatures approximate to 4.6 torr, 1 7.5 torr and 234 torr respectively.
It will be seen that even under the least favourable conditions the weight gain results in an Li loss as LiAl508 no greater than that achieved in dry air at 10"-3 torr H20.
Further tests were carried out for the same alloy (Al, 2.7% Li) in the same atmospheres and same times as in Table 1, but at the higher temperature of 575"C.
The resulting weight gains are indicated in the following Table 2.
Table 2
Atmosphere
Time Dry 20%02 Wet 20%02 Dry CO2 Wet CO2 Dry N2 minutes 80% Ar 80% Ar
5 31.3 149.2 278.4 92.5 6.4
10 80.6 410.8 512.5 189.1 13.6
20 149.4 889.2 801.7 212.5 22.2
45 276.1 2549.2 1231.7 573.9 40.6
60 332.2 2962.5 1385.9 665.0 50.3
90 426.7 3018.4 1690.0 883.9 70.3 120 502.8 3052.5 1951.7 976.1 92.8 180 635.5 3064.2 2377.5 1181.7 135.0 240 749.5 1328.9 175.0 300 838.3 1376.7 193.0
It will be seen that at the higher temperature of 575"C, although the rate of weight gain in wet CO2 is considerably higher than at the lower temperature of 520"C, the weight gain figure, when translated into terms of Li loss, represent an approximately fourfold loss of Li in dry N2 as compared with the loss of Li in the wet CO2 atmosphere.When the test time was increased from 1 to 5 hours, the additional Li loss was between five and six times greater in dry N2 than in wet CO2.
The present invention is particularly applicable to the high temperature homogenisation process for Al-Li alloys containing Cu and/or Mg, described in our copending British Patent
Application No. 83.07829 and greatly reduces the Li loss involved in carrying out that very advantageous homogenisation process.
Heat treatment of Al-Li alloys, particularly such alloys containing Mg and/or Cu are however rarely if ever carried out at temperatures as high as 575"C.
Although the Li loss and weight gain involved in heat treatment, such as homogenisation heat treatment, of Al-Li alloys at temperatures somewhat below 500"C are lower for a given treatment time the employment of a wet CO2 atmosphere remains advantageous at such lower temperature.
The present procedure is tolerant of the presence of small quantities of air in the wet CO2 furnace atmosphere. Preferably the total nitrogen and oxygen content of the furnace atmosphere is held below 1%. That is readily achieved by standard purging techniques. It is preferred to adopt the normal practice of carrying out the heat treatment in a furnace at a slightly superatmospheric pressure, which eliminates or greatly reduces leakage of air into the atmosphere during performance of the process.
The test results given above are only for a binary Al-Li alloy, parallel tests on ternary Al-Li-Mg arid Al-Li;Cu alloys and quaternary Al-Li-Mg-Cu alloys yield similar results. This would in any event be expected since at the higher temperatures most or all of the Li content of the alloy would be rapidly redissolved in the aluminium matrix and not be present in the form of a precipitated intermetallic phase.
Claims (4)
1. A method of reducing the loss of lithium by oxidation in the heat treatment of Al alloys, having a substantial content of lithium, which comprises carrying out the heat treatment in an atmosphere of carbon dioxide and water vapour, the partial pressure of water vapour in such atmosphere being at least 4 torr.
2. A method according to claim 1 further characterised in that the partial pressure of water vapour in said atmosphere is maintained at a value in the range of 4-250 torr.
3. A method according to claim 1 further characterised in that the partial pressure of water vapour in said atmosphere is maintained at a value in the range of 10-50 torr.
4. A method according to any of claims 1 to 3 further characterised in that total nitrogen and oxygen impurity content of said atmosphere is held below 1%.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| GB08407904A GB2137666B (en) | 1983-04-06 | 1984-03-27 | Heat treatment of al-li alloys |
Applications Claiming Priority (2)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| GB838309349A GB8309349D0 (en) | 1983-04-06 | 1983-04-06 | Heat treatment of aluminium alloys containing lithium |
| GB08407904A GB2137666B (en) | 1983-04-06 | 1984-03-27 | Heat treatment of al-li alloys |
Publications (3)
| Publication Number | Publication Date |
|---|---|
| GB8407904D0 GB8407904D0 (en) | 1984-05-02 |
| GB2137666A true GB2137666A (en) | 1984-10-10 |
| GB2137666B GB2137666B (en) | 1986-04-23 |
Family
ID=26285751
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| GB08407904A Expired GB2137666B (en) | 1983-04-06 | 1984-03-27 | Heat treatment of al-li alloys |
Country Status (1)
| Country | Link |
|---|---|
| GB (1) | GB2137666B (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US5061328A (en) * | 1990-07-05 | 1991-10-29 | Grummann Aerospace Corporation | Coating method to suppress porosity in Al-Li alloys |
| US5154778A (en) * | 1990-09-17 | 1992-10-13 | Grumman Aerospace Corporation | Lithium loss suppression in alloys using hydrogen atmosphere |
-
1984
- 1984-03-27 GB GB08407904A patent/GB2137666B/en not_active Expired
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US5061328A (en) * | 1990-07-05 | 1991-10-29 | Grummann Aerospace Corporation | Coating method to suppress porosity in Al-Li alloys |
| US5154778A (en) * | 1990-09-17 | 1992-10-13 | Grumman Aerospace Corporation | Lithium loss suppression in alloys using hydrogen atmosphere |
Also Published As
| Publication number | Publication date |
|---|---|
| GB8407904D0 (en) | 1984-05-02 |
| GB2137666B (en) | 1986-04-23 |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| PCNP | Patent ceased through non-payment of renewal fee |
Effective date: 19930327 |