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Cooled variable-area radial turbine technology programThe objective of this study was a conceptual evaluation and design analyses of a cooled variable-area radial turbine capable of maintaining nearly constant high efficiency when operated at a constant speed and pressure ratio over a range of flows corresponding to 50- to 100-percent maximum engine power. The results showed that a 1589K (2400 F) turbine was feasible that would satisfy a 4000-hour duty cycle life goal. The final design feasibility is based on 1988 material technology goals. A peak aerodynamic stage total efficiency of 0.88 was predicted at 100 percent power. Two candidate stators were identified: an articulated trailing-edge and a locally movable sidewall. Both concepts must be experimentally evaluated to determine the optimum configuration. A follow-on test program is proposed for this evaluation.
Document ID
19820011347
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Large, G. D.
(Garrett Turbine Engine Co. Phoenix, AZ, United States)
Meyer, L. J.
(Garrett Turbine Engine Co. Phoenix, AZ, United States)
Date Acquired
September 4, 2013
Publication Date
January 1, 1982
Subject Category
Aircraft Propulsion And Power
Report/Patent Number
NASA-CR-165408
Report Number: NASA-CR-165408
Accession Number
82N19221
Funding Number(s)
CONTRACT_GRANT: NAS3-22004
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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