Method of preparing beta titanium-fiber reinforced composite lam

Details Method of preparing beta titanium-fiber reinforced composite lam Method of preparing beta titanium-fiber reinforced composite lam

1996-08-01

1997-12-02

Sheehan, John

Metal treatment

Process of modifying or maintaining internal physical...

Producing or treating layered, bonded, welded, or...

148518, 148527, 4273881, 4273718, 156153, 156281, 156330, C23C 1600, C23C 2802

Patent

active

056931573

ABSTRACT:
A method of preparing a beta titanium-fiber reinforced composite laminate comprising the steps of, first, providing a beta titanium alloy having a first yield strength to modulus of elasticity ratio; then, heating the beta titanium alloy at a first preselected temperature for a first preselected time to produce a beta titanium alloy having a second yield strength to modulus of elasticity ratio; and then, adhering a fiber reinforced composite having a strength to modulus of elasticity ratio to the beta titanium alloy to produce a beta titanium-fiber reinforced composite laminate; wherein the first preselected temperature and the first preselected time are preselected such that the second yield strength to modulus of elasticity ratio of the beta titanium alloy is substantially similar to the strength to modulus of elasticity ratio of the fiber reinforced composite.

REFERENCES:
patent: 3758234 (1973-09-01), Goodwin
patent: 3888661 (1975-06-01), Levitt et al.
patent: 3936277 (1976-02-01), Jakway et al.
patent: 3991928 (1976-11-01), Friedrich et al.
patent: 4029838 (1977-06-01), Chamis et al.
patent: 4115611 (1978-09-01), Stoltze et al.
patent: 4132828 (1979-01-01), Nakamura et al.
patent: 4137370 (1979-01-01), Fujishiro et al.
patent: 4141802 (1979-02-01), Duparque et al.
patent: 4356678 (1982-11-01), Andrews et al.
patent: 4411380 (1983-10-01), McWithey et al.
patent: 4473446 (1984-09-01), Locke et al.
patent: 4489123 (1984-12-01), Schijve et al.
patent: 4500589 (1985-02-01), Schijve et al.
patent: 4624897 (1986-11-01), Ito
patent: 4753850 (1988-06-01), Ibe et al.
patent: 4775602 (1988-10-01), Rasch
patent: 4777098 (1988-10-01), Takamura et al.
patent: 4816347 (1989-03-01), Rosenthal et al.
patent: 4917968 (1990-04-01), Tuffias et al.
patent: 4935291 (1990-06-01), Gunnink
patent: 4956026 (1990-09-01), Bell
patent: 4992323 (1991-02-01), Vogelesang et al.
patent: 5006419 (1991-04-01), Grunke et al.
patent: 5008157 (1991-04-01), Paxos
patent: 5009966 (1991-04-01), Garg et al.
patent: 5039571 (1991-08-01), Vogelesang et al.
patent: 5076875 (1991-12-01), Padden
patent: 5079101 (1992-01-01), Murayama
patent: 5100737 (1992-03-01), Colombier et al.
patent: 5104460 (1992-04-01), Smith, Jr. et al.
patent: 5122422 (1992-06-01), Rodhammer et al.
patent: 5160771 (1992-11-01), Lambing et al.
patent: 5200004 (1993-04-01), Verhoeven et al.
patent: 5213904 (1993-05-01), Banker
patent: 5215832 (1993-06-01), Hughes et al.
patent: 5232525 (1993-08-01), Smith et al.
patent: 5242759 (1993-09-01), Hall
patent: 5260137 (1993-11-01), Rosenthal et al.
patent: 5403411 (1995-04-01), Smith et al.
patent: 5429877 (1995-07-01), Eylon
patent: 5460774 (1995-10-01), Bachelet
NASA CR-1859, "Analytical and Experimental Investigation of Aircraft Metal Structures Reinforced with Filamentary Composites--Phase I--Concept Development and Feasibility," S. Oken and R.R. June, 129 pp. (1969-1970).
NASA CR-2039, "Analytical and Experimental Investigation of Aircraft Metal Structures Reinforced with Filamentary Composites--Phase II--Structural Fatigue, Thermal Cycling Creep, and Residual Strength," B. Blichfeldt and J.E. McCarty, 111 pp. (1969-1970).

Affiliated with

Also associated with

Rating

Method of preparing beta titanium-fiber reinforced composite lam does not yet have a rating. At this time, there are no reviews or comments for this patent.

If you have personal experience with Method of preparing beta titanium-fiber reinforced composite lam, we encourage you to share that experience with our LandOfFree.com community. Your opinion is very important and Method of preparing beta titanium-fiber reinforced composite lam will most certainly appreciate the feedback.

Rate now

Comments { 0 }

Profile ID: LFUS-PAI-O-797997