Add to ORKGThe Materials for Advanced Turbine Engine (MATE) Program managed by the NASA Lewis Research Center is supporting two projects to evaluate the potential of oxide dispersion strengthened (ODS) alloys for aircraft gas turbine applications. One project involves the evaluation of Incoloy (TM) MA-956 for application as a combustor liner material. An assessment of advanced engine potential will be conducted by means of a test in a P&WA 2037 turbofan engine. The other project involves the evaluation of Inconel (TM) MA 6000 for application as a high pressure turbine blade material and includes a test in a Garrett TFE 731 turbofan engine. Both projects are progressing toward these engine tests in 1984
Studies are in progress to establish the fundamental processes by which treatment and composition co...
The development of power and propulsion system technology is discussed. Specific emphasis is placed ...
The next generation of subsonic commercial aircraft will require engines with improved efficiency an...
Recent activities of the Lewis Research Center are reviewed which are directed toward developing mat...
Oxide-Dispersion-strengthened (ODS) Ni-Cr-Al alloy systems were exploited for turbine engine vanes w...
Development of high temperature alloys, dispersion strengthened materials, composites, and coatings ...
Several oxide dispersion strengthened (ODS) alloys were tested for cyclic, high velocity, oxidation,...
This study shows the effects of new materials for gas turbines and techniques for blade coating. The...
A wide range of programs are being conducted for improving the environmental resistance to oxidation...
Advanced high pressure O2/H2 propulsion systems as exemplified by the Space Shuttle Main Engine (SSM...
Material categories as well as coatings and recent turbine cooling developments are reviewed. Curren...
The potential role of superalloys, refractory alloys, and ceramics in the hottest sections of engine...
Aggressive fuel burn and carbon dioxide emission reduction goals for future gas turbine engines will...
NASA sponsored the Turbine Engine Hot Section Technology (HOST) Project to address the need for impr...
The objective of Project 4 was to develop a high-temperature, uncooled gas turbine blade using MA600...
Studies are in progress to establish the fundamental processes by which treatment and composition co...
The development of power and propulsion system technology is discussed. Specific emphasis is placed ...
The next generation of subsonic commercial aircraft will require engines with improved efficiency an...
Recent activities of the Lewis Research Center are reviewed which are directed toward developing mat...
Oxide-Dispersion-strengthened (ODS) Ni-Cr-Al alloy systems were exploited for turbine engine vanes w...
Development of high temperature alloys, dispersion strengthened materials, composites, and coatings ...
Several oxide dispersion strengthened (ODS) alloys were tested for cyclic, high velocity, oxidation,...
This study shows the effects of new materials for gas turbines and techniques for blade coating. The...
A wide range of programs are being conducted for improving the environmental resistance to oxidation...
Advanced high pressure O2/H2 propulsion systems as exemplified by the Space Shuttle Main Engine (SSM...
Material categories as well as coatings and recent turbine cooling developments are reviewed. Curren...
The potential role of superalloys, refractory alloys, and ceramics in the hottest sections of engine...
Aggressive fuel burn and carbon dioxide emission reduction goals for future gas turbine engines will...
NASA sponsored the Turbine Engine Hot Section Technology (HOST) Project to address the need for impr...
The objective of Project 4 was to develop a high-temperature, uncooled gas turbine blade using MA600...
Studies are in progress to establish the fundamental processes by which treatment and composition co...
The development of power and propulsion system technology is discussed. Specific emphasis is placed ...
The next generation of subsonic commercial aircraft will require engines with improved efficiency an...