Intermetallic and ceramic matrix composites for 815 to 1370 C (1500 to 2500F) gas turbine engine applications

Technical Report · Sun Jan 01 00:00:00 EST 1989

OSTI ID:5067404

Stephens, J R

Light weight and potential high temperature capability of intermetallic compounds, such as the aluminides, and structural ceramics, such as the carbides and nitrides, make these materials attractive for gas turbine engine applications. In terms of specific fuel consumption and specific thrust, revolutionary improvements over current technology are being sought by realizing the potential of these materials through their use as matrices combined with high strength, high temperature fibers. The U.S. along with other countries throughout the world have major research and development programs underway to characterize these composites materials; improve their reliability; identify and develop new processing techniques, new matrix compositions, and new fiber compositions; and to predict their life and failure mechanisms under engine operating conditions. The status is summarized of NASA's Advanced High Temperature Engine Materials Technology Program (HITEMP) and the potential benefits are described to be gained in 21st century transport aircraft by utilizing intermetallic and ceramic matrix composite materials.

• Research Organization: National Aeronautics and Space Administration, Cleveland, OH (USA). Lewis Research Center
• OSTI ID: 5067404
• Report Number(s): N-89-29490; NASA-TM-102326; E-5027; NAS-1.15:102326
• Country of Publication: United States
• Language: English

Related Subjects

36 MATERIALS SCIENCE
COMPOSITE MATERIALS
RESEARCH PROGRAMS
GAS TURBINE ENGINES
MATERIALS
MATRIX MATERIALS
ALUMINIUM BASE ALLOYS
CARBIDES
CERAMICS
FIBERS
INTERMETALLIC COMPOUNDS
NITRIDES
SERVICE LIFE
TEMPERATURE EFFECTS
ALLOYS
ALUMINIUM ALLOYS
CARBON COMPOUNDS
ENGINES
HEAT ENGINES
INTERNAL COMBUSTION ENGINES
NITROGEN COMPOUNDS
PNICTIDES
360600* - Other Materials