NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Press Enter or click the Search button to begin your search.

Back to Results
Fluctuating pressures in pump diffuser and collector scrolls, part 1The cracking of scroll liners on the SSME High Pressure Fuel Turbo Pump (HPFTP) on hot gas engine test firings has prompted a study into the nature of pressure fluctuations in centrifugal pump states. The amplitudes of these fluctuations and where they originate in the pump stage are quantified. To accomplish this, a test program was conducted to map the pressure pulsation activity in a centrifugal pump stage. This stage is based on typical commercial (or generic) pump design practice and not the specialized design of the HPFTP. Measurements made in the various elements comprising the stage indicate that pulsation activity is dominated by synchronous related phenomena. Pulsation amplitudes measured in the scroll are low, on the order of 2 to 7 percent of the impeller exit tip speed velocity head. Significant non-sychronous pressure fluctuations occur at low flow, and while of interest to commercial pump designers, have little meaning to the HPFTP experience. Results obtained with the generic components do provide insights into possible pulsation related scroll failures on the HPFTP, and provide a basis for further study.
Document ID
19910015241
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Sloteman, Donald P.
(Ingersoll-Rand Co. Phillipsburg, NJ, United States)
Date Acquired
September 6, 2013
Publication Date
August 1, 1989
Subject Category
Fluid Mechanics And Heat Transfer
Report/Patent Number
NAS 1.26:183781
NASA-CR-183781
Report Number: NAS 1.26:183781
Report Number: NASA-CR-183781
Accession Number
91N24554
Funding Number(s)
CONTRACT_GRANT: NAS8-36223
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
No Preview Available