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Engine Seal Technology Requirements to Meet NASA's Advanced Subsonic Technology Program GoalsCycle 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 generation 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
19940029454
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
September 6, 2013
Publication Date
June 1, 1994
Subject Category
Mechanical Engineering
Report/Patent Number
E-8842
NASA-TM-106582
NAS 1.15:106582
AIAA PAPER 94-2698
Report Number: E-8842
Report Number: NASA-TM-106582
Report Number: NAS 1.15:106582
Report Number: AIAA PAPER 94-2698
Meeting Information
Meeting: Joint Propulsion Conference
Location: Indianapolis, IN
Country: United States
Start Date: June 27, 1994
End Date: June 29, 1994
Sponsors: AIAA, ASME, SAE, and ASEE
Accession Number
94N33960
Funding Number(s)
PROJECT: RTOP 505-630-5B
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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