US4094706A
Expired / Lapsed
US
⏱️ 0.0 years remaining
Preparation of zirconium alloys
Assignee: Atomic Energy of Canada Ltd AECL
•
Filing: 1976-08-04
•
Granted: 1978-06-13
•
Expires: 1996-08-04
Abstract
Abstract High tensile strength, creep and corrosion resistant zirconium alloys containing 7.0-10.0 wt% aluminum, 0-3 wt% in total of one or more elements selected from the group consisting of magnesium, tin, chromium, iron, carbon, silicon, yttrium, niobium, molybdenum and beryllium, the balance zirconium and incidental impurities, are produced by annealing cast alloys at a temperature below about 992° C for a period of time sufficient to produce alloys having a substantially continuous matrix of the ordered intermetallic compound Zr 3 Al. The alloys may initially be hot worked at temperatures above about 1000° C, while in the βZr-Zr 2 Al two phase region, prior to annealing. Preferred alloys contain 7.5-9.5% aluminum, the balance zirconium and incidental impurities.
Inventors
- 👤 Erland Maxwell Schulson
- 👤 Donald James Cameron
Bibliographic Details
Application Number
—
Jurisdiction
US
Data Source
google_patents
Last Synchronized
2026-11-07 07:36
CPC Classifications
G; G21; G21C; G21C3/00; G21C3/02; G21C3/04; G21C3/06; G21C3/07; C; C22; C22C; C22C16/00; G21C1/00; G21C1/04; G21C1/06; G21C1/14; G21C1/16; G21C1/18; G21C1/20; Y; Y02; Y02E; Y02E30/00; Y02E30/30; Y10; Y10S; Y10S376/00; Y10S376/90
Claims Analysis
Total Claims: 20
Claim 1
Independent Claim
95 words
A method of producing a high tensile strength, creep and corrosion resistant zirconium alloy, consisting essentially of 7.0-10.0 wt.% Al, 0-3 wt.% in total of one or more elements selected from the group consisting of magnesium, tin, chromium, iron, carbon, silicon, yttrium, niobium, molybdenum and beryllium, balance zirconium and incidental impurities, comprising annealing said alloy, in a state substantially devoid of untransformable Zr 2 Al particles, at a temperature below about 992° C for a period of time sufficient to produce a substantially continuous matrix of the intermetallic compound Zr 3 Al in said alloy
Claim 2
Independent Claim
95 words
A method of producing a high tensile strength, creep and corrosion resistant zirconium alloy, consisting essentially of 7.0-10.0 wt.% Al, 0-3 wt.% in total of one or more elements selected from the group consisting of magnesium, tin, chromium, iron, carbon, silicon, yttrium, niobium, molybdenum and beryllium, balance zirconium and incidental impurities, comprising annealing said alloy, in a state substantially devoid of untransformable Zr 2 Al particles, at a temperature below about 992° C for a period of time sufficient to produce a substantially continuous matrix of the intermetallic compound Zr 3 Al in said alloy
Claim 3
Dependent Claim
21 words
A method as claimed in claim 1 wherein said alloy consists essentially of 7.5-9.5 wt.% Al, balance zirconium and incidental impurities.
Claim 4
Dependent Claim
26 words
A method as claimed in claim 2 wherein said alloy is annealed at a temperature in the range 700°-975° C for between 2 and 100 hours.
Claim 5
Dependent Claim
20 words
A method as claimed in claim 3 wherein said alloy is annealed at a temperature in the range 825°-950° C.
Claim 6
Dependent Claim
15 words
A method as claimed in claim 1, wherein said annealing is carried out in vacuo.
Claim 7
Dependent Claim
27 words
A method as claimed in claim 1, wherein said alloy is subjected to working at temperatures in the range up to about 975° C, prior to annealing.
Claim 8
Dependent Claim
60 words
A method as claimed in claim 1, wherein said alloy is subjected to working at temperatures in the range up to about 975° C and subsequently annealed at a temperature between about 500° and 975° C for a time sufficient to develop a selected combination of mechanical properties intermediate those of said alloy in hot worked and fully annealed conditions.
Claim 9
Dependent Claim
36 words
A method as claimed in claim 1, wherein the alloy is initially heat-treated in the β Zr solid solution region at a temperature above 1200° C to homogenize the alloy, the alloy cooled and then annealed.
Claim 10
Dependent Claim
42 words
A method as claimed in claim 8 wherein said alloy is homogenized at a temperature in the β Zr solid solution region, rapidly cooled, subjected to working in the Zr(Al)-Zr 2 Al region, and subsequently annealed at a temperature below 975° C.
Claim 11
Dependent Claim
59 words
A method as claimed in claim 1, wherein the alloy is heat soaked in the β Zr-Zr 2 Al two phase region and then subjected to working at a temperature above about 1000° C, and then subjected to solution treatment in the β Zr single phase region and rapid cooling prior to annealing at a temperature below 975° C.
Claim 12
Dependent Claim
44 words
A method as claimed in claim 1 wherein the alloy is heat soaked in the β Zr-Zr 2 Al two phase region and then subjected to working at a temperature above about 1000° C, cooled and then annealed at a temperature below 975° C.
Claim 13
Dependent Claim
47 words
A method as claimed in claim 1 wherein the alloy is heat soaked in the β Zr-Zr 2 Al two phase region and subjected to working at a temperature in the range between about 1000° C up to the melting temperature of the alloy, prior to annealing.
Claim 14
Dependent Claim
22 words
A method according to claim 12 wherein the working in the β Zr-Zr 2 Al region is by extrusion of the alloy.
Claim 15
Dependent Claim
14 words
A method according to claim 13 wherein the alloy is extruded to form tubes.
Claim 16
Dependent Claim
25 words
A method according to claim 12 wherein the working in the β Zr-Zr 2 Al region is by rolling or by forging of the alloy.
Claim 17
Dependent Claim
20 words
A method according to claim 12 wherein the alloy consists essentially of 7.6-9.0 wt.% Al, balance zirconium and incidental impurities.
Claim 18
Dependent Claim
27 words
A method according to claim 12 wherein the β Zr-Zr 2 Al two phase region contains about 50 - 60% by volume Zr 2 Al fine precipitates.
Claim 19
Dependent Claim
74 words
A method as claimed in claim 1 wherein the alloy consists essentially of 7.6-9 wt.% Al, balance zirconium and incidental impurities, and is heat soaked in the β Zr-Zr 2 Al two phase region, said two phase region containing about 50 - 60% by volume Zr 2 Al precipitates, and subjected to working at a temperature in the range between about 1000° C up to the melting temperature of the alloy prior to annealing.
Claim 20
Dependent Claim
57 words
A method as claimed in claim 1 wherein the Zr 2 Al particles present in the alloy prior to annealing have an average diameter of approximately 4 μm or smaller and the annealing is carried out at a temperature in the range of about 880° - 900° C for a period of about 8 - 16 hours.
References Cited (Backward Citations)
USPTO Annuity & Maintenance Windows
| Annuity Stage | Window Opens | Payment Deadline | Surcharge Period Until | Estimated Fee | Status |
|---|---|---|---|---|---|
| 3.5 Years (Year 4) | 1981-06-12 | 1981-12-12 | 1982-06-13 | $2000.00 | Window Closed / Lapsed |
| 7.5 Years (Year 8) | 1985-06-12 | 1985-12-12 | 1986-06-13 | $3760.00 | Window Closed / Lapsed |
| 11.5 Years (Year 12) | 1989-06-12 | 1989-12-12 | 1990-06-13 | $7700.00 | Window Closed / Lapsed |