The 2001 NASA Seal/Secondary Air System Workshop covered the following topics: (i) overview of NASA's Vision for 21st Century Aircraft; (ii) overview of NASA-sponsored Ultra-Efficient Engine Technology (UEET); (iii) reviews of sealing concepts, test results, experimental facilities, and numerical predictions; and (iv) reviews of material development programs relevant to advanced seals development. The NASA UEET overview illustrates for the reader the importance of advanced technologies, including seals, in meeting future turbine engine system efficiency and emission goals. The NASA UEET program goals include an 8-to 15-percent reduction in fuel burn, a 15-percent reduction in CO2, a 70-percent reduction in NOx, CO, and unburned hydrocarbons...
Low-leakage, long-life turbomachinery seals are important to both Space and Aeronautics Missions. (1...
Design and performance of gas-film and oil-film lubricated self sealing mainshaft seals for gas turb...
The author will present results obtained to date of a secondary flow study currently being conducted...
The 2002 NASA Seal/Secondary Air System Workshop covered the following topics: (i) Overview of NASA ...
The 2000 NASA Seal/Secondary Air System Workshop covered four main areas: (1) overviews of NASA-spon...
NASA Glenn hosted the Seals/Secondary Air System Workshop on October 28-29, 1999. Each year NASA and...
The 2005 NASA Seal/Secondary Air System workshop covered the following topics: (i) Overview of NASA ...
The 1998 NASA Seal/Secondary Air System Workshop was divided into three major areas with limited mat...
Current NASA program goals for aircraft engines and vehicle performance include reducing direct oper...
Cycle studies have shown the benefits of increasing engine pressure ratios and cycle temperatures to...
The Seal Team is divided into four primary areas. These areas include turbine engine seal developmen...
NASA Glenn is currently performing seal research supporting both advanced turbine engine development...
Seal technology development is an important part of the Air Force's participation in the Integrated ...
High temperature, dynamic structural seals are required in advanced hypersonic engines to seal the p...
Efforts are in progress to develop advanced sealing for large utility industrial gas turbine engines...
Low-leakage, long-life turbomachinery seals are important to both Space and Aeronautics Missions. (1...
Design and performance of gas-film and oil-film lubricated self sealing mainshaft seals for gas turb...
The author will present results obtained to date of a secondary flow study currently being conducted...
The 2002 NASA Seal/Secondary Air System Workshop covered the following topics: (i) Overview of NASA ...
The 2000 NASA Seal/Secondary Air System Workshop covered four main areas: (1) overviews of NASA-spon...
NASA Glenn hosted the Seals/Secondary Air System Workshop on October 28-29, 1999. Each year NASA and...
The 2005 NASA Seal/Secondary Air System workshop covered the following topics: (i) Overview of NASA ...
The 1998 NASA Seal/Secondary Air System Workshop was divided into three major areas with limited mat...
Current NASA program goals for aircraft engines and vehicle performance include reducing direct oper...
Cycle studies have shown the benefits of increasing engine pressure ratios and cycle temperatures to...
The Seal Team is divided into four primary areas. These areas include turbine engine seal developmen...
NASA Glenn is currently performing seal research supporting both advanced turbine engine development...
Seal technology development is an important part of the Air Force's participation in the Integrated ...
High temperature, dynamic structural seals are required in advanced hypersonic engines to seal the p...
Efforts are in progress to develop advanced sealing for large utility industrial gas turbine engines...
Low-leakage, long-life turbomachinery seals are important to both Space and Aeronautics Missions. (1...
Design and performance of gas-film and oil-film lubricated self sealing mainshaft seals for gas turb...
The author will present results obtained to date of a secondary flow study currently being conducted...