U.S. patents available from 1976 to present.
U.S. patent applications available from 2005 to present.

Hybrid titanium alloy matrix composites

Patent 4816347 Issued on March 28, 1989. Estimated Expiration Date: Icon_subject May 29, 2007. Estimated Expiration Date is calculated based on simple USPTO term provisions. It does not account for terminal disclaimers, term adjustments, failure to pay maintenance fees, or other factors which might affect the term of a patent.

Patent References

3556837

3676293

3849080

Method of fabricating a filament-reinforced composite article
Patent #: 4010884
Issued on: 03/08/1977
Inventor: Rothman

Fibre-reinforced metal panels and production thereof
Patent #: 4141802
Issued on: 02/27/1979
Inventor: Duparque ,   et al.

Titanium metal-matrix composites
Patent #: 4499156
Issued on: 02/12/1985
Inventor: Smith ,   et al.

Inorganic fiber-reinforced metallic composite material Patent #: 4622270
Issued on: 11/11/1986
Inventor: Yamamura ,   et al.

Inventors

Assignee

Application

No. 07/055415 filed on 05/29/1987

US Classes:

428/615, Composite; i.e., plural, adjacent, spatially distinct metal components (e.g., layers, joint, etc.)428/607, Composite428/608, Embodying fibers interengaged or between layers (e.g., paper, etc.)428/614Laterally noncoextensive components (e.g., embedded, etc.)

Examiners

Primary: Roy, Upendra

Attorney, Agent or Firm

International Classes

B32B 15/01 (20060101)
C22C 47/00 (20060101)
C22C 47/20 (20060101)
C22C 49/11 (20060101)
C22C 49/12 (20060101)
C22C 49/00 (20060101)

Abstract

A combination of unique properties of (i) high strength and stiffness at temperatures up to about of 1500° F., (ii) good room temperature mechanical properties including good ductility and (iii) improved resistance to matrix cracking is achieved in a titanium structure by forming a hybrid titanium alloy matrix composite in which the matrix consists of layers of at least two alloys, i.e. a high temperature-resistant titanium aluminide alloy and a ductile, lower modulus titanium alloy, that are bonded metallurgically to each other in various embodiments. A reinforcing material in the form of filaments, fibers or wiskers, e.g. silicon carbide, can be embedded within either or both types of the titanium layers.

Other References

  • Petrova et al., in Ti and Ti-Alloys, vol. 3, ed.: Williams et al., Plenum, N.Y., 1976, p. 2419
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