NASA Logo

NTRS

NTRS - NASA Technical Reports Server

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

Back to Results
Abrasive tip treatment for use on compressor bladesA co-spray process was used which simultaneously but separately introduces abrasive grits and metal matrix powder into the plasma stream and entraps the abrasive grits within a molten matrix to form an abrasive coating as the matrix material solidifies on test specimen surfaces. Spray trials were conducted to optimize spray parameter settings for the various matrix/grit combinations before actual spraying of the test specimens. Rub, erosion, and bond adhesion tests were conducted on the coated specimens in the as-sprayed condition as well as on coated specimens that were aged for 100 hours at a temperature of 866K (1100 F). Microscopic examinations were performed to determine the coating abrasive-particle content, the size and shape of the adhesive particles in the coating, and the extent of compositional or morphological changes resulting from the aging process. A nickel chromium/aluminum composite with No. 150 size (0.002 to 0.005 inch) silicon carbide grits was selected as the best matrix/abrasive combination of the candidates surveyed for coating compressor blade tips.
Document ID
19840016997
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Pedersen, H. C.
(United Technologies Research Center East Hartford, CT, United States)
Date Acquired
September 4, 2013
Publication Date
January 1, 1984
Subject Category
Mechanical Engineering
Report/Patent Number
PWA-5833-37
NASA-CR-174666
NAS 1.26:174666
Report Number: PWA-5833-37
Report Number: NASA-CR-174666
Report Number: NAS 1.26:174666
Accession Number
84N25065
Funding Number(s)
PROJECT: DA PROJ. 1L1-61102-AH-45
PROJECT: RTOP 505-33-5A
CONTRACT_GRANT: NAS3-22813
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
No Preview Available