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US4978585A Expired / Lapsed US ⏱️ 0.0 years remaining

Silicon carbide fiber-reinforced titanium base composites of improved tensile properties

Assignee: General Electric Co
•
Filing: 1990-01-02
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Granted: 1990-12-18
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Expires: 2010-01-02
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Abstract

Abstract A method of altering the crystal form of an alloy is disclosed. To accomplish this change in crystal form, the concentrations of the more volatile constituents of the alloy are reduced and the concentration of the less volatile constituents is increased on a relative basis. The process may be carried out in forming a reinforced structure. For this purpose, an improved reinforced matrix and a method of forming it are taught. The reinforcement may be silicon carbide filaments or other reinforcing filaments. The matrix is a titanium 1421 alloy nominally containing 14 weight percent of aluminum and 21 weight percent of niobium. The matrix is formed by plasma-spray forming a powder of the alloy to impart to the alloy particles a superheat during the plasma-spraying as the particles traverse the plasma plume. As a result of the superheat, the alloy is changed in its composition to reduce the aluminum concentration and to increase the niobium and titanium concentrations on a relative basis. As a result of the change in composition the crystal form of the spray deposited matrix is altered to increase the amount of the beta-phase crystal form of the alloy which is present and to decrease the amount of the alpha-2 crystal form of the alloy which is present. The result is the formation of a matrix which is less subject to cracking and which has greater strength.

Inventors

  • 👤 Ann M. Ritter
  • 👤 Paul A. Siemers
  • 👤 Donald R. Spriggs

Bibliographic Details

Application Number —
Jurisdiction US
Data Source google_patents
Last Synchronized 2026-11-05 05:47
CPC Classifications
C; C22; C22C; C22C47/00; C22C47/16; C22C47/18; C23; C23C; C23C4/00; C23C4/04; C23C4/06; C23C4/08; C23C4/12; C23C4/134; Y; Y10; Y10S; Y10S428/00; Y10S428/922; Y10S428/9335; Y10S428/937; Y10T; Y10T428/00; Y10T428/12; Y10T428/12014; Y10T428/1216; Y10T428/12167; Y10T428/12486

Claims Analysis

Total Claims: 9
Claim 1
Independent Claim 104 words
A method for forming a reinforced composite member which comprises providing a set of reinforcement strands, mounting said strands on a substrate to receive a plasma-sprayed matrix, providing a powdered sample of Ti-1421 alloy, plasma-spray depositing said powder onto said strands and onto said substrate with an RF plasma gun to form a matrix of Ti-1421 alloy, and modifying the aluminum concentration of said Ti-1421 alloy as it is being plasma-spray deposited by increasing the superheat of the particles of said alloy as the particles traverse the plume of said RF plasma thereby increasing the amount of beta crystal phase in the deposited matrix.
Claim 2
Independent Claim 104 words
A method for forming a reinforced composite member which comprises providing a set of reinforcement strands, mounting said strands on a substrate to receive a plasma-sprayed matrix, providing a powdered sample of Ti-1421 alloy, plasma-spray depositing said powder onto said strands and onto said substrate with an RF plasma gun to form a matrix of Ti-1421 alloy, and modifying the aluminum concentration of said Ti-1421 alloy as it is being plasma-spray deposited by increasing the superheat of the particles of said alloy as the particles traverse the plume of said RF plasma thereby increasing the amount of beta crystal phase in the deposited matrix.
Claim 3
Dependent Claim 17 words
The method of claim 1, in which the plasma gas contains up to 6 volume percent hydrogen.
Claim 4
Dependent Claim 17 words
The method of claim 1, in which the plasma gas contains up to 3 volume percent hydrogen.
Claim 5
Dependent Claim 16 words
The method of claim 1, in which the plasma gas contains about 1.5 volume percent hydrogen.
Claim 6
Dependent Claim 22 words
The method of claim 1, in which the superheat is increased by reducing the particle size of the powder being plasma sprayed.
Claim 7
Dependent Claim 62 words
As an article of manufacture, a fiber reinforced metal monotape which comprises, a plurality of silicon carbide filaments, said filaments having disposed thereabout a plasma spray deposited Ti-1421 alloy, and said alloy displaying a higher percentage of beta crystal form than normal plasma spray deposited Ti-1421 such that there are larger semicontinuous regions of the beta-phase or transformed beta-phase in the matrix.
Claim 8
Dependent Claim 62 words
As an article of manufacture, a fiber reinforced metal monotape which comprises, a plurality of silicon carbide filaments, said filaments having disposed thereabout a plasma spray deposited Ti-1421 alloy, and said alloy displaying a higher percentage of beta crystal form than normal plasma spray deposited Ti-1421 such that there are larger semicontinuous regions of the beta-phase or transformed beta-phase in the matrix.
Claim 9
Dependent Claim 12 words
The monotape of claim 6, in which the filaments are axially aligned.

References Cited (Backward Citations)

US4499156A Cited
US4782884A Cited
US4786566A Cited
US4805294A Cited
US4838337A Cited

USPTO Annuity & Maintenance Windows

Annuity Stage Window Opens Payment Deadline Surcharge Period Until Estimated Fee Status
3.5 Years (Year 4) 1993-12-17 1994-06-18 1994-12-18 $2000.00 Window Closed / Lapsed
7.5 Years (Year 8) 1997-12-17 1998-06-18 1998-12-18 $3760.00 Window Closed / Lapsed
11.5 Years (Year 12) 2001-12-17 2002-06-18 2002-12-18 $7700.00 Window Closed / Lapsed

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