NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Back to Results
Seals/Secondary Fluid Flows Workshop 1997; Volume II: HSR Engine Special SessionThe High Speed Civil Transport (HSCT) will be the largest engine ever built and operated at maximum conditions for long periods of time. It is being developed collaboratively with NASA, FAA, Boeing-McDonnell Douglas, Pratt & Whitney, and General Electric. This document provides an initial step toward defining high speed research (HSR) sealing needs. The overview for HSR seals includes defining objectives, summarizing sealing and material requirements, presenting relevant seal cross-sections, and identifying technology needs. Overview presentations are given for the inlet, turbomachinery, combustor and nozzle. The HSCT and HSR seal issues center on durability and efficiency of rotating equipment seals, structural seals and high speed bearing and sump seals. Tighter clearances, propulsion system size and thermal requirements challenge component designers.
Document ID
20080003276
Acquisition Source
Glenn Research Center
Document Type
Conference Proceedings
Authors
Hendricks, Robert C.
(NASA Glenn Research Center Cleveland, OH, United States)
Date Acquired
August 24, 2013
Publication Date
May 1, 2006
Subject Category
Aircraft Propulsion And Power
Report/Patent Number
NASA/CP-2006-214329/VOL2
E-15561-2
Meeting Information
Meeting: Seals/Secondary Fluid Flows Workshop 1997
Location: Cleveland, OH
Country: United States
Start Date: October 15, 1997
End Date: October 16, 1997
Sponsors: NASA Glenn Research Center
Funding Number(s)
WBS: WBS 22-714-09-46
CONTRACT_GRANT: NAS3-27235
Distribution Limits
Public
Copyright
Public Use Permitted.
No Preview Available