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Small, high-pressure ratio compressor mechanical acceptance test, volume 2The fabrication and mechanical testing of the high-pressure-ratio compressor are reported. Mechanical testing was performed to demonstrate overspeed capability, adequate rotor dynamics, electrical isolation of the gas bearing trunnion mounted diffuser and shroud and the effect of operating parameters (speed and pressure ratio) on clearance of the compressor test rig. The speed range covered was 20 to 120 percent of rated speed (80,000 rpm). Following these tests an acceptance test which consisted of a 5 hour run at 80,000 rpm was made with approximately design impeller to shroud clearances. For Vol. 1, see N73-26483.
Document ID
19730020731
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Metty, G. R.
(AiResearch Mfg. Co. Phoenix, AZ, United States)
Shoup, W. I.
(AiResearch Mfg. Co. Phoenix, AZ, United States)
Date Acquired
September 2, 2013
Publication Date
June 1, 1973
Subject Category
Machine Elements And Processes
Report/Patent Number
APS-5404-R-VOL-2
NASA-CR-121193
Report Number: APS-5404-R-VOL-2
Report Number: NASA-CR-121193
Accession Number
73N29463
Funding Number(s)
CONTRACT_GRANT: NAS3-14306
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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