The Need for New Materials in Aging Aircraft Structures

Abstract

The end of the Cold War and political and economic considerations has resulted in an effort to extend the life of many aircraft that are the backbone of NATO operational forces. Although some are designated to be replaced with new aircraft, the replacement schedule of many often requires an unprecedented life span of between 40 to 60 years before retirement. Many of the older aircraft have encountered, or can be expected to encounter, aging problems such as fatigue cracking, stress corrosion cracking, corrosion and wear. In order to ensure continued airworthiness and flight safety the structural components undergoing these problems will have to be repaired or replaced. Alloy development that has taken place since a large percentage of the older aircraft were put into service has resulted in several new materials, heat treatments and processing technology that can be used for appropriate longer lasting and higher performing airframe components thus reducing life-cycle costs. This paper describes some of these materials and their advantages over those suffering from "aging problems".

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Document Details

Document Type
Technical Report
Publication Date
Apr 01, 2000
Accession Number
ADP010408

Entities

People

  • C. J. Warren
  • E. A. Starke Jr.
  • R. J. Bucci

Organizations

  • Alcoa

Tags

Communities of Interest

  • Air Platforms

DTIC Thesaurus Topics

  • Air Force
  • Aircrafts
  • Airframes
  • Corrosion Resistance
  • Damage Tolerance
  • Fuselages
  • Heat Treatment
  • Life Cycle Costs
  • Life Cycles
  • Materials
  • Materials Science
  • Mechanical Properties
  • Mechanical Working
  • Resistance
  • Stress Corrosion
  • Stress Corrosion Cracking
  • Structural Components

Readers

  • Aerospace Engineering
  • Materials Science and Engineering.
  • Strategic Security Studies