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Aerospace Seal RequirementsCycle studies have shown the benefits of increasing engine pressure ratios and cycle temperatures to decrease engine weight and improve performance of commercial turbine engines. NASA is working with industry to define technology requirements of advanced engines and engine technology to meet the goals of NASA's Advanced Subsonic Technology Initiative. As engine operating conditions become more severe and customers demand lower operating costs, NASA and engine manufacturers are investigating methods of improving engine efficiency and reducing operating costs. A number of new technologies are being examined that will allow next generations engines to operate at higher pressures and temperatures. Improving seal performance - reducing leakage and increasing service life while operating under more demanding conditions - will play an important role in meeting overall program goals of reducing specific fuel consumption and ultimately reducing direct operating costs. This paper provides an overview of the Advanced Subsonic Technology Program goals discusses the motivation for advanced seal development, and highlights seal technology requirements to meet future engine performance goals.
Document ID
19960020371
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Steinetz, Bruce M.
(NASA Lewis Research Center Cleveland, OH United States)
Hendricks, Robert C.
(NASA Lewis Research Center Cleveland, OH United States)
Date Acquired
August 17, 2013
Publication Date
March 1, 1996
Publication Information
Publication: Seals Code Development Workshop
Subject Category
Aircraft Propulsion And Power
Accession Number
96N23949
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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