Effect of Very Low Sulfur in JP-5 Fuel on Hot Corrosion,

Abstract

The report discusses an investigation to determine whether the present limit of 0.4 per cent by weight (4,000 ppm) of sulfur in JP-5 fuel is a safe level for the protection of turbine-blade materials from hot corrosion in high-performance engines when operated in a marine environment. The present study shows that a 100-fold reduction in the sulfur limit to 40 ppm would not reduce hot corrosion significantly. Such reductions in the sulfur limit would drastically curtail fuel availability, since they approach the mean and the minimum of current production, and could cause critical problems in logistics. It was found that the use of an essentially sulfur-free fuel, containing only 4 ppm sulfur, significantly decreased both the surface scale on specimens and the weight lost by specimens of a wide variety of superalloys and superalloy-coating systems when exposed under conditions which simulate those in an aircraft-turbine engine ingesting air with 1 ppm sea salt. Thus, indications are that the sulfur in fuel must be below a 'threshold' concentration to improve the durability of turbine-blade materials. (Author)

Document Details

Document Type
Technical Report
Publication Date
May 20, 1971
Accession Number
AD0725619

Entities

People

  • Harold T. Quigg
  • Robert M. Schirmer

Tags

Communities of Interest

  • Air Platforms

DTIC Thesaurus Topics

  • Aircrafts
  • Corrosion
  • Engines
  • Materials
  • Propulsion Systems
  • Superalloys
  • Turbine Blades
  • Turbines
  • Turbomachinery

Readers

  • Petroleum Engineering