IP Library Granted Patent US 10,030,293
Granted Patent B2
US 10,030,293 · App. 14/338,652 · Granted Jul 24, 2018

Aluminum material having improved precipitation hardening

Inventor: Frank Palm (Unterhaching, DE)
Assignee: Airbus Defence and Space GmbH
C22F1/04C22C1/03C22C21/00C22F1/02B22F1/00B22F1/0085B22F3/15B22F9/04B22F2998/10B61D17/041B63B2231/10B64C2001/0081C22C1/0416
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Quick Facts
Patent No.
US 10,030,293
App. No.
14/338,652
Granted
Jul 24, 2018
Kind
B2
Abstract

An aluminum material for producing light-weight components includes aluminum (Al), scandium (Sc), zirconium (Zr) and ytterbium (Yb), where a weight ratio of scandium (Sc) to zirconium (Zr) to ytterbium (Yb) [Sc/Zr/Yb] is in a range from 10/5/2.5 to 10/2.5/1.25.

Claims (22)

1. A method for producing an aluminum material, the method comprising the steps:

a) providing an aluminum (AD-scandium (Sc)-zirconium (Zr) base alloy;

b) adding ytterbium (Yb) to the AlScZr base alloy from step a) to produce a molten aluminum (Al)-scandium(Se)-zirconium(Zr)-ytterbium (Yb) alloy;

c) cooling the molten AlScZrYb alloy obtained in step b) in a temperature interval T liquidus to T 350° C. at a cooling rate of ≥100 K/sec to produce a solidified AlScZrYb alloy; and

d) heat treating the solidified AlScZrYb alloy in a temperature range from 250 to 500° C.,

wherein a weight ratio of scandium (Sc) to zirconium (Zr) to ytterbium (Yb) [Sc/Zr/Yb] is in a range from 10/5/2.5 to 10/2.5/1.25.

2. The method of claim 1 , wherein the AlScZr base alloy is obtained by previously adding zirconium (Zr) to an aluminum (Al)-scandium (Sc) base alloy.

3. The method of claim 1 , wherein an AlScZr base alloy or an AlSc base alloy is used, which comprises at least one further alloying element selected from the group consisting of Mg, Zn, Cu, Mn, Si, Li, Ag in an amount from 0.5 to 10.0% by weight, Ti, Nb, Ta, Hf, Fe, Ni, Co, Cr, V and/or at least one further alloying element selected from the group of lanthanides comprising Y, La, Eu, Nd, Gd, Tb, Dy, Er, Pr and Ce in an amount from 0.05 to 2.0% by weight, based on the total weight of the AlScZr or AlSc base alloy, per element.

4. The method of claim 1 , wherein the AlScZr base alloy and/or the AlSc base alloy are present

a) in powder or wire form, or

b) as sintered, cast, rolled or extruded molded parts.

5. The method of claim 1 , wherein the melting of the AlScZrYb alloy in step b) is carried out

a) by way of a laser beam, an electron beam or an arc,

b) by way of a chemical exothermic reaction, and/or

c) capacitively, conductively or inductively.

6. The method of claim 1 , wherein the molten AlScZrYb alloy is cooled in the temperature interval T liquidus to T 350° C. at a cooling rate of ≥150 K/sec.

7. The method of claim 1 , wherein the AlScZrYb alloy is cooled to room temperature.

8. The method of claim 1 , wherein the heat treatment of the solidified AlScZrYb alloy is carried out for a duration from 10 minutes to 100 hours and/or takes place in multiple stages and/or steps.

9. The method of claim 1 , wherein the heat-treated AlScZrYb alloy is subjected to cooling to room temperature and the cooling rate is ≥10 K/sec.

10. The method of claim 1 , wherein, following the heat treatment from step d), at least one further heat treatment process is carried out

a) in air, protective gas or under vacuum in a temperature range from 300 to 400° C. for a duration from 10 minutes to 100 hours and/or in multiple stages and/or steps, or

b) by way of hot isostatic pressing in a temperature range from 300 to 400° C. and a pressure range from 100 to 10000 bar and/or in multiple stages and/or steps.

Assignments (1)
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Aug 21, 2014
From: PALM, FRANK
To: AIRBUS DEFENCE AND SPACE GMBH
Reel/Frame 033582/0380 →
Priority Claims (1)
DE 10 2013 012 259 · Jul 24, 2013 · national
Continuity (1)
Related Publication 20150027595A1 · Jan 29, 2015
Cited By (2)
US 12,522,896 US 12,695,002