DUCTILE TITANIUM ALLOY MATRIX FIBER REINFORCED COMPOSITES
Assignee
UNITED TECHNOLOGIES CORPORATION
Filed
Apr 1, 1993
Granted
Apr 16, 1996
Location
GLASTONBURY CT US
Abstract
A titanium alloy matrix fiber reinforced composite made from titanium alloy sheet processed to have ductility up to about 35%. Of particular usefulness is the composite having a Ti3 Al titanium aluminide having this level of ductility. The composites have good resistance to thermal cyclic fatigue.
Source: Google Patents
35 USC §181 Secrecy Order
Imposed
Apr 8, 1994
Rescinded
Jul 29, 1994
Duration
3 months
Inventor
- 1GARY D. LINSEY
Record Details
- Patent number
- US 5508115
- Application
- 08041087
- Aerospace match
- No
- Dataset source
- 35 USC §181 SO records
Browse by Assignee
UNITED TECHNOLOGIES CORPORATIONMore from this assignee
COOLED AIRFOILS FOR A GAS TURBINE ENGINE
UNITED TECHNOLOGIES CORPORATION
ENHANCED FILM COOLING SLOT FOR TURBINE BLADE OUTER AIR SEALS
UNITED TECHNOLOGIES CORPORATION
AIRFOIL HAVING EXPANDED WALL PORTIONS TO ACCOMMODATE FILM COOLING HOLES
UNITED TECHNOLOGIES CORPORATION
LOW OBSERVABLE ENGINE AIR INLET SYSTEM
UNITED TECHNOLOGIES CORPORATION
TIP SEAL AND ANTI-CONTAMINATION FOR TURBINE BLADES
UNITED TECHNOLOGIES CORPORATION
TURBINE AIRFOIL SUCTION AIDED FILM COOLING MEANS
UNITED TECHNOLOGIES CORPORATION