NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Back to Results
Erosion/corrosion of turbine airfoil materials in the high-velocity effluent of a pressurized fluidized coal combustorFour candidate turbine airfoil superalloys were exposed to the effluent of a pressurized fluidized bed with a solids loading of 2 to 4 g/scm for up to 100 hours at two gas velocities, 150 and 270 m/sec, and two temperatures, 730 deg and 795 C. Under these conditions, both erosion and corrosion occurred. The damaged specimens were examined by cross-section measurements, scanning electron and light microscopy, and X-ray analysis to evaluate the effects of temperature, velocity, particle loading, and alloy material. Results indicate that for a given solids loading the extent of erosion is primarily dependent on gas velocity. Corrosion occurred only at the higher temperature. There was little difference in the erosion/corrosion damage to the four alloys tested under these severe conditions.
Document ID
19780020282
Acquisition Source
Legacy CDMS
Document Type
Technical Publication (TP)
Authors
Zellars, G. R.
(NASA Lewis Research Center Cleveland, OH, United States)
Rowe, A. P.
(NASA Lewis Research Center Cleveland, OH, United States)
Lowell, C. E.
(NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 3, 2013
Publication Date
July 1, 1978
Subject Category
Metallic Materials
Report/Patent Number
NASA-TP-1274
E-9507
Accession Number
78N28225
Funding Number(s)
PROJECT: RTOP 778-83
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
No Preview Available