Various combinations of fiber and matrix materials were fabricated and evaluated for the purpose of selecting a specific combination that exhibited the best overall properties for a turbine blade application. A total of seven matrix alloys, including Hastelloy X, Nimonic 80A, Inconel 600, Inconel 625, IN-102, FeCrA1Y, were investigated reinforced with either 218CS tungsten, or W-Hf-C fibers. Based on preliminary screening studies, FeCrA1Y, Inconel 600 and Inconel 625 matrix composites systems were selected for extended thermal cycle tests and for property evaluations which included stress rupture, impact, and oxidation resistance. Of those investigated, the FeCrA1Y matrix composite system exhibited the best overall properties required for a...
This preliminary design study evaluated the potential of fiber-reinforced superalloys (FRS) for hot-...
High-pressure turbopumps for advanced reusable liquid-propellant rocket engines such as that for the...
Resin matrix composites having improved resistance to foreign object damage in gas turbine engine fa...
W-Hf-C/superalloy composites were found to be potentially useful for turbine blade applications on t...
A tungsten alloy wire reinforced high temperature alloy composite is being developed for potential a...
Evaluation of tungsten alloy fiber-nickel base alloy composites for turbojet engine applicatio
Metal fiber reinforced superalloys are being considered for construction of critical components in t...
Fabrication methods for tungsten fiber reinforced nickel-base superalloy composites were investigate...
Improved performance of heat engines is largely dependent upon maximum cycle temperatures. Tungsten ...
Tungsten fiber-reinforced nickel superalloy combines the strength of refractory metals with the oxid...
The miniature Izod and Charpy impact strengths of copper, copper-nickel, and nickel-base superalloy ...
Superalloy has 1000-hour strength of 37,000 psi at 2000 degrees F. The strength to density ratio of ...
Studies of advanced aircraft propulsion systems have indicated that performance gains and operating ...
Impact properties determined for pure copper, copper-nickel alloy, and superalloy metal matrix compo...
Stress-rupture and tensile tests were conducted at 816 C (1500 F) to determine the effect of matrix ...
This preliminary design study evaluated the potential of fiber-reinforced superalloys (FRS) for hot-...
High-pressure turbopumps for advanced reusable liquid-propellant rocket engines such as that for the...
Resin matrix composites having improved resistance to foreign object damage in gas turbine engine fa...
W-Hf-C/superalloy composites were found to be potentially useful for turbine blade applications on t...
A tungsten alloy wire reinforced high temperature alloy composite is being developed for potential a...
Evaluation of tungsten alloy fiber-nickel base alloy composites for turbojet engine applicatio
Metal fiber reinforced superalloys are being considered for construction of critical components in t...
Fabrication methods for tungsten fiber reinforced nickel-base superalloy composites were investigate...
Improved performance of heat engines is largely dependent upon maximum cycle temperatures. Tungsten ...
Tungsten fiber-reinforced nickel superalloy combines the strength of refractory metals with the oxid...
The miniature Izod and Charpy impact strengths of copper, copper-nickel, and nickel-base superalloy ...
Superalloy has 1000-hour strength of 37,000 psi at 2000 degrees F. The strength to density ratio of ...
Studies of advanced aircraft propulsion systems have indicated that performance gains and operating ...
Impact properties determined for pure copper, copper-nickel alloy, and superalloy metal matrix compo...
Stress-rupture and tensile tests were conducted at 816 C (1500 F) to determine the effect of matrix ...
This preliminary design study evaluated the potential of fiber-reinforced superalloys (FRS) for hot-...
High-pressure turbopumps for advanced reusable liquid-propellant rocket engines such as that for the...
Resin matrix composites having improved resistance to foreign object damage in gas turbine engine fa...