METHOD FOR DISSOLVABLE ALUMINUM ALLOYS
20210252574 ยท 2021-08-19
Assignee
Inventors
- Jianhui Xu (Katy, TX, US)
- Timothy Dunne (Pearland, TX, US)
- Yu SANG (Chengdu, CN)
- Yi SONG (Chengdu, CN)
- Wenhan YUE (Chengdu, CN)
- Yu Liu (Beijing, CN)
- Xiongwen Yang (Beijing, CN)
Cpc classification
B21C23/001
PERFORMING OPERATIONS; TRANSPORTING
B21C23/01
PERFORMING OPERATIONS; TRANSPORTING
International classification
Abstract
The method for equal channel angular extrusion increases yield strength and ultimate tensile strength of a dissolvable aluminum alloy. A billet of a dissolvable aluminum alloy is wrapped with a sheet cover so as to form a wrapped billet. The wrapped billet is extruded through an equal channel angular extrusion die with an extrusion angle ranging 90-135 degrees so as to form an extruded billet. The step of extruding is at a temperature ranging 150-250 degrees C., an extrusion rate ranging 0.003-0.010 inches per second, and a back pressure ranging 200-10000 psi. The dissolvable aluminum alloy of the extruded billet has a yield strength and ultimate tensile strength 50% greater than the initial yield strength and initial ultimate tensile strength.
Claims
1. A method for equal channel angular extrusion, comprising the steps of: wrapping a billet with a sheet cover so as to form a wrapped billet, said billet being comprised of a dissolvable aluminum alloy with an initial tensile yield strength; and extruding said wrapped billet through an equal channel angular extrusion die with an extrusion angle ranging 90-135 degrees so as to form an extruded billet, wherein the step of extruding is at a temperature ranging 150-250 degrees C., wherein the step of extruding is at an extrusion rate ranging 0.003-0.010 inches per second, wherein the step of extruding is at a back pressure ranging 200-10000 psi, and wherein said extruded billet has an extruded tensile yield strength 50% greater than said initial tensile yield strength.
2. The method of claim 1, wherein said temperature is 200 degrees C.
3. The method of claim 1, wherein said extrusion rate is 0.005 inches per second.
4. The method of claim 1, wherein said back pressure is 8000 psi.
5. The method of claim 1, wherein said sheet cover is comprised of one of a group consisting of brass and graphite.
6. A method for equal channel angular extrusion, comprising the steps of: wrapping a billet with a sheet cover so as to form a wrapped billet, said billet being comprised of a dissolvable aluminum alloy with an initial tensile ultimate strength; and extruding said wrapped billet through an equal channel angular extrusion die with an extrusion angle ranging 90-135 degrees so as to form an extruded billet, wherein the step of extruding is at a temperature ranging 150-250 degrees C., wherein the step of extruding is at an extrusion rate ranging 0.003-0.010 inches per second, wherein the step of extruding is at a back pressure ranging 200-10000 psi, and wherein said extruded billet has an extruded tensile ultimate strength 50% greater than said initial tensile ultimate strength.
7. The method of claim 6, wherein said temperature is 200 degrees C.
8. The method of claim 6, wherein said extrusion rate is 0.005 inches per second.
9. The method of claim 6, wherein said back pressure is 8000 psi.
10. The method of claim 6, wherein said sheet cover is comprised of one of a group consisting of brass and graphite.
11. A method for equal channel angular extrusion, comprising the steps of: wrapping a billet with a sheet cover so as to form a wrapped billet, said billet being comprised of a dissolvable aluminum alloy with an initial tensile elongation; and extruding said wrapped billet through an equal channel angular extrusion die with an extrusion angle ranging 90-135 degrees so as to form an extruded billet, wherein the step of extruding is at a temperature ranging 150-250 degrees C., wherein the step of extruding is at an extrusion rate ranging 0.003-0.010 inches per second, wherein the step of extruding is at a back pressure ranging 200-10000 psi, and wherein said extruded billet has an extruded tensile elongation 50% greater than said initial tensile elongation.
12. The method of claim 11, wherein said temperature is 200 degrees C.
13. The method of claim 11, wherein said extrusion rate is 0.005 inches per second.
14. The method of claim 11, wherein said back pressure is 8000 psi.
15. The method of claim 11, wherein said sheet cover is comprised of one of group consisting of brass and graphite.
Description
BRIEF DESCRIPTION OF THE SEVERAL VIEWS OF THE DRAWINGS
[0017]
[0018]
[0019]
[0020]
[0021]
[0022]
[0023]
[0024]
[0025]
DETAILED DESCRIPTION OF THE INVENTION
[0026]
[0027]
TABLE-US-00001 TABLE 1 results for temperature, extrusion rate, back pressure, and wrapping Back Temperature Extrusion Rate Pressure Critical FIG. (degrees C.) (inches/sec) (psi) Wrapping Fail 2 (a), 4(a) 250 0.01 200 YES YES 3 (a) 100 0.005 200 YES YES 3 (b), 4 200 0.005 200 YES NO (b), 5 (a) 5 (b) 200 0.005 4000 YES NO 5 (c) 200 0.005 8000 YES NO 6 (a) 330 0.005 0 NO YES 6 (b) 330 0.005 4000 YES NO 7-AA 200 0.005 8000 YES NO 7-AC 200 0.005 8000 YES NO 7-AG 200 0.005 8000 YES NO 7-AH 200 0.005 8000 YES NO
[0028] There is a critical range of the temperature.
[0029] There is a critical range of the extrusion rate.
[0030] Back pressure can also be a critical ECAE condition. Table 1 shows failures between 0-200 psi, while
[0031]
[0032] Table 1 identifies the critical ranges as now claimed. The temperature has a range of 150-250 degrees C. with an extrusion rate range of 0.003-0.010 inches per second and a back pressure range of 200-10000 psi. Additionally, these conditions require wrapping. The present invention indicates the critical ranges interacting to avoid fractures in the extruded dissolvable aluminum alloy.
[0033] Beyond achieving a functional extruded dissolvable aluminum alloy, the method of the present invention further includes unexpected performance. Simply avoiding complete structural failure is important for components of downhole tools, but there is a further benefit beyond forming an extruded dissolvable aluminum alloy.
TABLE-US-00002 TABLE 2 results of FIG. 7 for increased strengths and sometimes elongation. Tensile Tensile Tensile Tensile Ultimate Ultimate Tensile Tensile Yield Strength Yield Strength Strength Strength Elongation Elongation BEFORE AFTER BEFORE AFTER BEFORE AFTER Sample (MPa) (MPa) (MPa) (MPa) (%) (%) AA 137 275 190 325 3.3 8.7 AC 122 265 190 290 4.7 2.9 AG 153 273 187 320 1.4 2.1 AH 125 252 225 290 7.0 6.5
[0034] After identifying the ECAE conditions of the present invention, dissolvable aluminum materials were processed successfully, as shown in
[0035] In the present invention, just to achieve extruded dissolvable aluminum alloy that does not fracture is surpassed by the additional findings of Table 2. There are actual improvements to mechanical properties beyond just being able to form components of downhole tools without fractures.
[0036] The present invention provides a method for processing dissolvable aluminum alloy. After being cast, the dissolvable aluminum alloy must be formed into shapes that correspond to components of downhole tools. Being brittle makes the formation of parts difficult. Once formed, the component must have the necessary strength for downhole conditions, while remaining dissolvable. The present invention improves the strengths of a dissolvable aluminum alloy in a post processing treatment of dissolvable aluminum alloy. Previously unusable or at least time consuming and expensive processing for downhole tool components can be avoided. The method for an equal channel angular extrusion has been modified to be compatible with dissolvable aluminum alloys. Regular alloys do not require such modifications, and there are critical ranges to avoid fracturing and failure of the extruded material. The present invention identifies these critical ranges to avoid failure and further achieves an unexpected improvement in strengths.
[0037] The foregoing disclosure and description of the invention is illustrative and explanatory thereof. Various changes in the details of the illustrated structures, construction and method can be made without departing from the true spirit of the invention.