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US4134758A Expired / Lapsed US ⏱️ 0.0 years remaining

Titanium alloy with high internal friction and method of heat-treating the same

Assignee: Kobe Steel Ltd
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Filing: 1977-04-26
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Granted: 1979-01-16
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Expires: 1997-04-26
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Abstract

Abstract A titanium alloy having a high degree of internal friction and suitable for rotating blades of turbomachines is composed of 5.5 - 6.75% Al, 1 - 5% V, 1 - 5% Mo, V plus Mo being greater than or equal to 5%, and the balance Ti and usual impurities, all by weight. A method of heat-treating the alloy comprises maintaining the same at a temperature not lower than 125° C below its β transformation point for a predetermined period of time and then rapidly cooling the alloy.

Inventors

  • 👤 Nobuyuki Nagai
  • 👤 Yasuo Moriguchi
  • 👤 Yoshimasa Itoh
  • 👤 Shoji Ueda
  • 👤 Yorimasa Takeda
  • 👤 Akira Hiromoto

Bibliographic Details

Application Number —
Jurisdiction US
Data Source google_patents
Last Synchronized 2026-10-27 17:29
CPC Classifications
C; C22; C22C; C22C14/00

Claims Analysis

Total Claims: 4
Claim 1
Independent Claim 76 words
A heat-treated titanium alloy with a high internal friction suitable for rotating blades of turbomachines and consisting essentially of, by weight, 5.5-6.75% Al, 1-5% V, 1-5% Mo, V plus Mo being greater than 6%, and the balance being Ti, the alloy having been solution heat treated at a temperature not lower than 125° C. below the β transformation point of the alloy, the alloy having a minimum damping capacity of about 5 × 10 -3 .
Claim 2
Dependent Claim 76 words
A heat-treated titanium alloy with a high internal friction suitable for rotating blades of turbomachines and consisting essentially of, by weight, 5.5-6.75% Al, 1-5% V, 1-5% Mo, V plus Mo being greater than 6%, and the balance being Ti, the alloy having been solution heat treated at a temperature not lower than 125° C. below the β transformation point of the alloy, the alloy having a minimum damping capacity of about 5 × 10 -3 .
Claim 3
Independent Claim 94 words
A method of solution heat-treating a titanium alloy with a high internal friction suitable for rotating blades of turbomachines, which comprises heating and maintaining a titanium alloy consisting essentially of, by weight, 5.5-6.75% Al, 1-5% V, 1-5% Mo, V plus Mo being greater than 6%, and the balance being Ti at a temperature not lower than 125° C. below the β transformation point of the alloy for a predetermined period of time, and then rapidly cooling the same to produce an alloy having a minimum damping capacity of about 5 × 10 -3 .
Claim 4
Independent Claim 94 words
A method of solution heat-treating a titanium alloy with a high internal friction suitable for rotating blades of turbomachines, which comprises heating and maintaining a titanium alloy consisting essentially of, by weight, 5.5-6.75% Al, 1-5% V, 1-5% Mo, V plus Mo being greater than 6%, and the balance being Ti at a temperature not lower than 125° C. below the β transformation point of the alloy for a predetermined period of time, and then rapidly cooling the same to produce an alloy having a minimum damping capacity of about 5 × 10 -3 .

References Cited (Backward Citations)

GB772339A Cited
US2918367A Cited
US2754204A Cited
US2804409A Cited

USPTO Annuity & Maintenance Windows

Annuity Stage Window Opens Payment Deadline Surcharge Period Until Estimated Fee Status
3.5 Years (Year 4) 1982-01-15 1982-07-17 1983-01-16 $2000.00 Window Closed / Lapsed
7.5 Years (Year 8) 1986-01-15 1986-07-17 1987-01-16 $3760.00 Window Closed / Lapsed
11.5 Years (Year 12) 1990-01-15 1990-07-17 1991-01-16 $7700.00 Window Closed / Lapsed

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