Accession Number : AD0845310
Title : Testing and Evaluation of Impact-Abrasion-Erosion Resistant Aircraft Coatings.
Descriptive Note : Final technical rept. May 66-Oct 68,
Corporate Author : ROCKWELL INTERNATIONAL COLUMBUS OH COLUMBUS DIV
Personal Author(s) : Michael, Harold J.
Report Date : OCT 1968
Pagination or Media Count : 202
Abstract : An impact-abrasion erosion system was developed for evaluating candidate erosion and corrosion resistant materials as prospective coatings for aircraft metal leading edges, inlet ducts, and jet engine compressor components. The coatings were compared at various temperatures. Best leading edge coatings were: 1) a plasma sprayed intermetallic with an organic cover coat, and 2) electroplated nickel. Best compressor component coating in both erosion and corrosion resistance was a fired on slurry type cermet applied during austenitizing. Materials evaluated were ceramic, cermet, polymeric, elastomeric, metallic, intermetallic and composite (Fibeglass-plastic laminate). (Author, modified-PL).
Descriptors : (*AIRCRAFT FINISHES, ACCEPTABILITY), RADOMES, LEADING EDGES, HIGH TEMPERATURE, EROSION, CORROSION INHIBITION, IMPACT TESTS, ABRASIVE BLASTING, SALT SPRAY TESTS, THERMAL STABILITY, CERMETS, WATER IMPINGEMENT, CHROMIUM ALLOYS, NICKEL ALLOYS.
Subject Categories : Coatings, Colorants and Finishes
Distribution Statement : APPROVED FOR PUBLIC RELEASE