NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Back to Results
Noncontacting measuring device to indicate deflection of turbopump internal rotating partsNoncontacting, nondestructive techniques to measure vibrations and deflections of parts in future LOX and LH2 multistage turbopump prototypes are reported. The measurements include shaft vibration, vibration of turbine wheel and blades, blade clearance, vibration of impellers, value component flutter, and vibration of face seal components. Three techniques were selected for development: ultrasonic Doppler devices, flash X-ray, and light-pipe reflectance.
Document ID
19720006808
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Hamilton, D. B.
(Battelle Memorial Inst. Columbus, OH, United States)
Grieser, D. R.
(Battelle Memorial Inst. Columbus, OH, United States)
Plummer, A. M.
(Battelle Memorial Inst. Columbus, OH, United States)
Ensminger, D.
(Battelle Memorial Inst. Columbus, OH, United States)
Saccacio, E. J.
(Battelle Memorial Inst. Columbus, OH, United States)
Kissel, J. W.
(Battelle Memorial Inst. Columbus, OH, United States)
Date Acquired
September 2, 2013
Publication Date
September 20, 1971
Subject Category
Instrumentation And Photography
Report/Patent Number
NASA-CR-121060
QR-2
Report Number: NASA-CR-121060
Report Number: QR-2
Accession Number
72N14457
Funding Number(s)
CONTRACT_GRANT: NAS8-26903
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
No Preview Available