TITANIUM-BASE ALLOYS AND METHODS OF MANUFACTURING SUCH ALLOYS

Abstract: Creep resistant titanium alloys containing : Al---5,0 - 7,0 % Zr---2,0 - 7,0 % Mo 0,1 - 2,5 % Ge---0,01 - 10,0 % and optionally one or more of the following elements: Sn 2,0 - 6,0 % Nb 0,1 - 2,0 % C 0,02 - 0,1 % Si 0,1 - 2,0 %

Description: This invention relates to titanium base alloys. All percentages are weight percentages. According to the present invention we provide a titanium base alloy consisting of 5.0-7.0% aluminium, 2.0-7.0% zirconium, 0.1-2.5% molybdenum and 0.01-10.0 germanium and optionally one or more of the following elements: tin 2.0-6.0%, niobium 0.1-2.0%, carbon 0.02-0.1% and silicon 0.1-2.0%; the balance being titanium apart from incidental impurities. The aluminium content may be in the range 5.0-­ 6.0% or 5.0-6.5%. The zirconium content may be in the range 2.0-­ 4.0%, 2.0-6.0% or 3.0-7.0%. The molybdenum content may be in the range 0.1-0.6%, 0.25-0.75% or 2.0-2.5%. The germanium content may be in the range 0.01-5.0%, 0.01-0.2%, 0.01-0.5%, 0.1-2.0% or 2.0-5.0%. More particularly, the alloy may consist of 5.3-6.1% aluminium, 3.5-4.5% tin, 3.0-4.0% zirconium, 0.5-1.0% niobium, 0.2-0.7% molybdenum, 0.1-0.5% silicon, 0.03-0.10% carbon and 0.3-3.0% germanium, the balance being titanium apart from incidental impurities. Alternatively, the alloy may consist of 5.3-6.1% aluminium, 3.5-4.5% tin, 3.0-4.0% zirconium, 0.5-1.0% niobium, 0.2-0.7% molybdenum, 0.03-0.10% carbon and 0.3-3.0% germanium, the balance being titanium apart from incidental impurities. Alternatively, the alloy may consist of 5.6-6.0% aluminium, 3.5-4.5% tin, 3.0-4.0% zirconium, 0.6-0.8% niobium, 0.3-0.6% molybdenum, 0.03-0.10% carbon, 0.15-0.5% silicon and 0.5-2.5% germanium, the balance being titanium apart from incidental impurities. Alternatively, the alloy may consist of 5.6-6.0% aluminium, 3.5-4.5% tin, 3.0-4.0% zirconium, 0.6-0.8% niobium, 0.3-0.6% molybdenum, 0.03-0.10% carbon and 1.0-3.0% germanium, the balance being titanium apart from incidental impurities. The alloys according to the invention are preferably heat-treated and subsequently cooled. The alloys are then preferably aged by heating to a selected temperature for a predetermined period of time and then cooled. The aging temperature may be in excess of 600°C and may be as high as 700°C. Examples of an alloy according to the invention are now provided. The alloys set out in Table 1 below were prepared: The prepared alloys were then each heat treated at 1030°C for 2 hours and then air cooled. Subsequently each alloy was aged by heating at 700°C for 2 hours. The mechanical properties for each alloy are set out in Table 2 below. The creep exposure was 100 hours at 600°C at 125MPa for each sample. Test A was at room temperature; Test B was at an elevated temperature of 700°C; Test C was at room temperature after the creep exposure referred to above. The increase in yield stress for these alloys aged at 700°C shows significant improvements over a comparable alloy containing silicon but with no germanium, ie. the increase in yield stress which might have been expected, if silicon and germanium had precisely the same effect as one another, has been significantly reduced. The alloys in accordance with the invention possess excellent creep resistance particularly at temperatures above 540°C which makes them particularly valuable in gas turbine engine applications.

Claims: 1. A titanium base alloy consisting of 5.0-7.0% aluminium, 2.0-7.0% zirconium, 0.1-2.5% molybdenum and 0.01-10.0 germanium and optionally one or more of the following elements: tin 2.0-6.0%, niobium 0.1-2.0%, carbon 0.02-0.1% and silicon 0.1-2.0%; the balance being titanium apart from incidental impurities. 2. A titanium base alloy as claimed in claim 1 in which the aluminium content is in the range 5.0-6.0% or 5.0-6.5%. 3. A titanium base alloy as claimed in claim 1 or claim 2 in which the zirconium content is in the range 2.0-4.0%, 2.0-6.0% or 3.0-7.0%. 4. A titanium base alloy as claimed in any preceding claim in which the molybdenum content is in the range 0.1-0.6%, 0.25-0.75% or 2.0-2.5%. 5. A titanium base alloy as claimed in any preceding claim in which the germanium content is in the range 0.01-5.0%, 0.01-0.2%, 0.01-0.5%, 0.1-2.0% or 2.0-5.0%. 6. A titanium base alloy as claimed in claim 1 in which the alloy consists of 5.3-6.1% aluminium, 3.5-4.5% tin, 3.0-4.0% zirconium, 0.5-1.0% niobium, 0.2-0.7% molybdenum, 0.1-0.5% silicon, 0.03-0.10% carbon and 0.3-3.0% germanium, the balance being titanium apart from incidental impurities. 7. A titanium base alloy as claimed in claim 1 in which the alloy consists of 5.3-6.1% aluminium, 3.5-4.5% tin, 3.0-4.0% zirconium, 0.5-1.0% niobium, 0.2-0.7% molybdenum, 0.03-0.10% carbon and 0.3-3.0% germanium, the balance being titanium apart from incidental impurities. 8. A titanium base alloy as claimed in claim 1 in which the alloy consists of 5.6-6.0% aluminium, 3.5-4.5% tin, 3.0-4.0% zirconium, 0.6-0.8% niobium, 0.3-0.6% molybdenum, 0.03-0.10% carbon, 0.15-0.5% silicon and 0.5-2.5% germanium, the balance being titanium apart from incidental impurities. 9. A titanium base alloy as claimed in claim 1 in which the alloy consists of 5.6-6.0% aluminium, 3.5-4.5% tin, 3.0-4.0% zirconium, 0.6-0.8% niobium, 0.3-0.6% molybdenum, 0.03-0.10% carbon and 1.0-3.0% germanium, the balance being titanium apart from incidental impurities. 10. A titanium base alloy as claimed in any preceding claim in which the alloy has been heat treated, subsequently cooled, and then aged by heating to a selected temperature for a predetermined period of time and is subsequently cooled.

Inventors: BARBER, ANTHONY CLIFFORD
Applicants: IMI TITANIUM LIMITED
Application year: 1987
Main classification: C22C14
IPC codes: C22C14