Titanium-based intermetallic alloy

US10119180B2 · US · B2

Patent metadata
FieldValue
Publication numberUS-10119180-B2
Application numberUS-201515538119-A
CountryUS
Kind codeB2
Filing dateDec 14, 2015
Priority dateDec 22, 2014
Publication dateNov 6, 2018
Grant dateNov 6, 2018

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  1. Title

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  2. Abstract

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  3. Assignees and inventors

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  4. Key dates

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  5. First independent claim

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  6. CPC / IPC classifications

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  7. Citations and related patents

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Abstract

Official abstract text for this publication.

A titanium-based intermetallic alloy includes, in atomic percent, 16% to 26% Al, 18% to 28% Nb, 0% to 3% of a metal M selected from Mo, W, Hf, and V, 0.1% to 2% of Si, 0% to 2% of Ta, 1% to 4% of Zr, with the condition Fe+Ni≤400 ppm, the balance being Ti, the alloy also presenting an Al/Nb ratio in atomic percent lying in the range 1.05 to 1.15.

First claim

Opening claim text (preview).

The invention claimed is: 1. A titanium-based intermetallic alloy comprising, in atomic percent, 19.3% to 26% Al, 18% to 24.3% Nb, 0% to 3% of a metal M selected from Mo, W, Hf, and V, 0.1% to 2% of Si, 0% to 2% of Ta, 1% to 4% of Zr, with the condition Fe+Ni≤400 ppm, the balance being Ti, the alloy also presenting an Al/Nb ratio in atomic percent of about 1.07. 2. An alloy according to claim 1 , comprising 20% to 22% Nb, in atomic percent. 3. An alloy according to claim 1 , comprising 23% to 24% Al, in atomic percent. 4. An alloy according to claim 1 , comprising 0.1% to 0.8% Si, in atomic percent. 5. An alloy according to claim 1 claim 1 , comprising 0.8% to 3% of M, in atomic percent. 6. An alloy according to claim 1 , comprising 1% to 3% Zr, in atomic percent. 7. An intermetallic alloy according to claim 1 , wherein: the content of Al lies in the range 20% to 25%, in atomic percent; the content of Nb lies in the range 20% to 22%, in atomic percent; the content of M lies in the range 0.8% to 3%, in atomic percent; and the content of Zr lies in the range 1% to 3%, in atomic percent. 8. A turbomachine including a part including an alloy according to claim 1 . 9. An engine including a turbomachine according to claim 8 . 10. An aircraft including an engine according to claim 9 .

Assignees

Inventors

Classifications

  • of titanium or alloys based thereon · CPC title

  • C22C14/00Primary

    Alloys based on titanium · CPC title

  • Alloys based on titanium, zirconium or hafnium · CPC title

  • Chemistry & Metallurgy · mapped topic

  • Selecting particular materials; {Particular measures relating thereto;} Measures against erosion or corrosion · CPC title

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What does patent US10119180B2 cover?
A titanium-based intermetallic alloy includes, in atomic percent, 16% to 26% Al, 18% to 28% Nb, 0% to 3% of a metal M selected from Mo, W, Hf, and V, 0.1% to 2% of Si, 0% to 2% of Ta, 1% to 4% of Zr, with the condition Fe+Ni≤400 ppm, the balance being Ti, the alloy also presenting an Al/Nb ratio in atomic percent lying in the range 1.05 to 1.15.
Who is the assignee on this patent?
Safran Aircraft Engines
What technology area does this patent fall under?
Primary CPC classification C22C14/00. Mapped technology areas include Chemistry & Metallurgy.
When was this patent published?
Publication date Tue Nov 06 2018 00:00:00 GMT+0000 (Coordinated Universal Time) (B2). Legal status and post-grant events are not shown on this page.
What related patents are in patentsdb?
We list 8 related publications on this page (citations in our corpus or others sharing the same primary CPC).