High temperature composites. Status and future directions
Technical Report
·
OSTI ID:6315345
A summary of research investigations of manufacturing methods, fabrication methods, and testing of high temperature composites for use in gas turbine engines is presented. Ceramic/ceramic, ceramic/metal, and metal/metal composites are considered. Directional solidification of superalloys and eutectic alloys, fiber reinforced metal and ceramic composites, ceramic fibers and whiskers, refractory coatings, metal fiber/metal composites, matrix metal selection, and the preparation of test specimens are discussed.
- Research Organization:
- National Aeronautics and Space Administration, Cleveland, OH (USA). Lewis Research Center
- OSTI ID:
- 6315345
- Report Number(s):
- N-8230336; CONF-821023-2
- Country of Publication:
- United States
- Language:
- English
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Related Subjects
33 ADVANCED PROPULSION SYSTEMS
330103 -- Internal Combustion Engines-- Turbine
36 MATERIALS SCIENCE
360301* -- Composite Materials-- Preparation & Fabrication-- (-1987)
CERAMICS
COMPOSITE MATERIALS
ENGINES
EUTECTOIDS
GAS TURBINE ENGINES
HEAT ENGINES
HEAT RESISTANT MATERIALS
INTERNAL COMBUSTION ENGINES
MATERIALS
PLANNING
REFRACTORIES
REINFORCED MATERIALS
TECHNOLOGY ASSESSMENT
330103 -- Internal Combustion Engines-- Turbine
36 MATERIALS SCIENCE
360301* -- Composite Materials-- Preparation & Fabrication-- (-1987)
CERAMICS
COMPOSITE MATERIALS
ENGINES
EUTECTOIDS
GAS TURBINE ENGINES
HEAT ENGINES
HEAT RESISTANT MATERIALS
INTERNAL COMBUSTION ENGINES
MATERIALS
PLANNING
REFRACTORIES
REINFORCED MATERIALS
TECHNOLOGY ASSESSMENT