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Energy efficient engine high-pressure turbine component rig performance test reportA rig test of the cooled high-pressure turbine component for the Energy Efficient Engine was successfully completed. The principal objective of this test was to substantiate the turbine design point performance as well as determine off-design performance with the interaction of the secondary flow system. The measured efficiency of the cooled turbine component was 88.5 percent, which surpassed the rig design goal of 86.5 percent. The secondary flow system in the turbine performed according to the design intent. Characterization studies showed that secondary flow system performance is insensitive to flow and pressure variations. Overall, this test has demonstrated that a highly-loaded, transonic, single-stage turbine can achieve a high level of operating efficiency.
Document ID
19850021643
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Leach, K. P.
(Pratt and Whitney Aircraft Group East Hartford, CT, United States)
Date Acquired
September 5, 2013
Publication Date
May 1, 1983
Subject Category
Aircraft Propulsion And Power
Report/Patent Number
NASA-CR-168189
NAS 1.26:168189
PWA-5594-243
Report Number: NASA-CR-168189
Report Number: NAS 1.26:168189
Report Number: PWA-5594-243
Accession Number
85N29955
Funding Number(s)
CONTRACT_GRANT: NAS3-20646
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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