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Injected Water Augments Cooling In Turboshaft EngineReport describes experiments in which water injected into compressor-bleed cooling air of aircraft turboshaft engine. Injection of water previously suggested as way to provide additional cooling needed to sustain operation at power levels higher than usual. Involves turbine-inlet temperatures high enough to shorten lives of first-stage high-pressure turbine blades. Latent heat of vaporization of injected water serves as additional heat sink to maintain blades at design operating temperatures during high-power operation.
Document ID
19890000090
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Tech Brief
Authors
Biesiadny, Thomas J.
(NASA Lewis Research Center, Cleveland, OH.)
Berger, Brett
(Army Aviation Research and Technology Activity)
Klann, Gary A.
(Army Aviation Research and Technology Activity)
Clark, David A.
(Army Aviation Research and Technology Activity)
Date Acquired
August 13, 2013
Publication Date
February 1, 1989
Publication Information
Publication: NASA Tech Briefs
Volume: 13
Issue: 2
ISSN: 0145-319X
Subject Category
Machinery
Report/Patent Number
LEW-14706
Accession Number
89B10090
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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