A Kinetic Study of Lubricant Antioxidant Depletion in Aircraft Gas Turbine Engines.

Abstract

The kinetics of lubricant depletion in an aircraft gas turbine engine were treated as those of a stirred flow reactor. Depletion rates of p,p'-dioctylamine and phenyl-alpha-naphthylamine, based on zero and first order reaction models, were calculated. First order reaction rates most closely fit the engine test data. (Author)

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Document Details

Document Type
Technical Report
Publication Date
Nov 17, 1982
Accession Number
ADA121431

Entities

People

  • P. J. Sniegoski

Organizations

  • United States Naval Research Laboratory

Tags

Communities of Interest

  • Air Platforms

DTIC Thesaurus Topics

  • Additives (Chemicals)
  • Aircrafts
  • Antioxidants
  • Chemical Kinetics
  • Engine Components
  • Engineering
  • Engines
  • Equations
  • Gas Turbines
  • Jet Engines
  • Kinetics
  • Lubricants
  • Steady State
  • Steam Turbines
  • Turbine Components
  • Turbines
  • Turboshaft Engines

Readers

  • Mathematics or Statistics
  • Petroleum Engineering
  • Quantum Chemistry