Metal treatment – Stock – Age or precipitation hardened or strengthened
Reexamination Certificate
2000-09-28
2002-06-18
Wyszomierski, George (Department: 1742)
Metal treatment
Stock
Age or precipitation hardened or strengthened
C148S416000, C148S417000
Reexamination Certificate
active
06406567
ABSTRACT:
BACKGROUND OF THE INVENTION
1. Field of the Invention
The invention relates to a method of stress relieving an age hardenable aluminium alloy product by a permanent cold plastic deformation operation after solution heat treatment and quenching. The invention also relates to a stress relieved product of an age hardenable aluminium alloy, and to uses of such a product.
2. Description of the Prior Art
Manufacture of age hardenable aluminium alloy products requires solution heat treatment and quenching of the product. Since residual stresses due to the quenching operation do not allow for machining operations without simultaneous distortion of the machined parts, the products are stress relieved. In case of flat products (e.g. rolled plate) this has been accomplished by a stretching operation using a permanent plastic deformation of a few percent of the original dimension. Usually this stretching is done in the length direction which is normally also the rolling direction.
U.S. Pat. No. 4,294,625 for example describes a process in which aluminium alloy is cast, hot worked into plate, solution treated, quenched, pre-aged, cold rolled to reduce thickness by 11±2% and then stretched for stress relieving prior to ageing. The product is for use in aircraft. WO 95/24514 similarly briefly mentions stretching a quenched thick aluminium alloy product to improve flatness and reduce residual stress. JP-A-54-102214 describes manufacture of aluminium alloy pipe or rod with low residual stress, by hardening followed by stretch levelling by 0.5-1.0%, then roll levelling and further stretch levelling by 0.5-1.0%, followed by tempering at 210-250° C. for 1-2 hours to relieve stress further.
It has also been proposed to employ cold compression as a stress-relieving step. GB-A-2025818 discusses manufacture of aluminium alloy rings by hot ring rolling, solution heat treatment, quenching, cold rolling for stress relieving and ageing. The diameter expansion in the cold rolling is 1 to 3%. Similarly JP-A-3-2359 describes cold compression of a complex shaped hollow conical billet of aluminium alloy, after solution heat treatment and prior to ageing. JP-A-4-187747 describes two-axis cold compression carried out on an aluminium alloy block of complex shape having insert parts located in apertures.
In conventional cold stretching, if the cross-section of the product (plate) is large (e.g. very thick or very wide plate) the strength of the stretcher machine may be insufficient to achieve the desired stretching degree. This of course depends not only on the dimensions of the plate but also on the plate alloy or—more precisely—on the flow stress of the plate material in the solutionized and quenched condition.
SUMMARY OF THE INVENTION
The object of the invention is therefore to provide a method of stress relieving of an age hardenable aluminium alloy product which is especially applicable to alloy product of large cross-section.
According to the invention in one aspect there is provided a method of stress relieving an age hardenable aluminium alloy product after solution heat treatment and quenching, comprising applying a permanent cold plastic deformation by the steps of:
(a) applying a stress-relieving cold mechanical stretch to the product, and
(b) applying a stress-relieving cold compression to the product.
In another aspect, the invention provides a method of manufacture of a product of an age hardenable aluminium alloy comprising the steps of:
(i) casting said age hardenable alloy
(ii) shaping the cast alloy to form a shaped product
(iii) solution heat treating said shaped product
(iv) quenching the solution heat treated product
(v) performing stress relieving of the quenched product by applying a permanent cold plastic deformation by the steps of
(a) applying a stress-relieving cold mechanical stretch to said product, and
(b) applying a stress-relieving cold compression to said product.
In this method, the age hardening may be natural ageing or artificial ageing.
In a preferred embodiment the product is a plate product, having length, width and thickness directions, which is stretched in the length direction and compressed in the thickness reduction.
It has been found, as will be shown below, that replacement of the conventional mechanical stretching as a stress relieving method by cold compression alone results in loss of strength and toughness properties of the final product, although distortion after machining is improved. By applying combined stretching and compression the loss of properties is recovered while at the same time the improved distortion is retained.
To obtain full advantage of the invention the stress relieving permanent deformation by stretching, defined as the permanent elongation in the direction of stretching should be not more than 15%, should more preferably be in the range of 0.3-5%, and most preferably be in the range of 0.5-3%.
Similarly preferably the stress relieving permanent deformation by compression, defined as the permanent reduction in the direction of compression should be in the range of 0.2-5%, and should more preferably be in the range of 0.5-3%.
In practice the cold compression may be given by forging, e.g. by a forging tool in overlapping steps. The stress relieving stretching of the product preferably takes place before the compression. The deformation is preferably given before substantially any age hardening after quenching.
Full advantage of the invention is obtained when the product is a thick plate having a final thickness of 2 inches (5 cm) or more, preferably 4 inches (10 cm) or more and most preferably 6 inches (15 cm) or more.
The invention is particularly effective in meeting requirements of strength and toughness properties and distortion when the aluminium alloy belongs to the Aluminium Association AA 2XXX, the AA 6XXX or the AA 7XXX series.
The invention also consists in the product of the method of the invention described above.
In another aspect the invention provides a product made of an age hardenable aluminium alloy suitable for use in an aircraft construction and being stress relieved after solution heat treatment and quenching by a combination of a cold mechanical stretching and a cold compression, having in the age hardened condition, as compared with a product which has been stress relieved by said cold mechanical stretching only but has otherwise the same manufacturing history, similar strength and toughness properties and an improved property of distortion after machining.
In still another aspect the invention provides a product made of an age hardenable aluminium alloy suitable for use in one of a tooling construction and a moulding construction and being stress relieved after solution heat treatment and quenching by a combination of a cold mechanical stretching and a cold compression, having in the age hardened condition, as compared with a product which has been stress relieved by said cold compression only but has otherwise the same manufacturing history, improved strength and toughness properties and a similar property of distortion after machining.
Preferably the distortion after machining is less than 50 &mgr;m.
REFERENCES:
patent: 4294625 (1981-10-01), Hyatt et al.
patent: 4968359 (1990-11-01), Hebel, Jr. et al.
patent: 5277719 (1994-01-01), Kuhlman et al.
patent: 5413650 (1995-05-01), Jarrett et al.
patent: 2025818 (1980-01-01), None
patent: 54102214 (1979-08-01), None
patent: 54102214 (1979-08-01), None
patent: 03002359 (1991-01-01), None
patent: 04187747 (1992-07-01), None
patent: 9524514 (1995-09-01), None
Altschuler, et al., “Relief of Residual Stresses in a High- Strength Aluminum Alloy by Cold Working”, ASTM Spec. Tech. Publ. (1988) (from the text Mechanical Relaxation of Residual Stresses, edited by Leonard Mordfin), 19-29, ISSN: 0066-0558, 1988.
Metals Handbook, vol. 14, ASM International, pp. 680-687 (1988).
Haszler Alfred Johann Peter
Heinz Alfred Ludwig
Müller Otmar Martin
Combs Morillo Janelle
Corus Aluminium Walzprodukte GmbH
Stevens Davis Miller & Mosher LLP
Wyszomierski George
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