Superplastic Forming of Aluminum (Task C)

Abstract

This report covers the work under Task C of Contract F33615-83-C- 3208. An SPF based A-10 nose landing gear door was designed using Supral 220 alloy: The part count for the basic door was reduced to 4 components as compared to 52 for the conventional construction method. The superplastic pan comprising the stiffening structure of the door was assembled to the external skin using the ultrasonic weldbonding process. The SPF based door and conventional door were supplied to AFFDL for static testing. Test results show that the two doors are approximately equivalent in strength. Economic analysis indicates that the SPF door is less than half the cost of the conventional door for production quantities larger than 100.

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Document Details

Document Type
Technical Report
Publication Date
Mar 01, 1989
Accession Number
ADA207282

Entities

People

  • T. Renshaw

Tags

Communities of Interest

  • Air Platforms
  • Energy and Power Technologies
  • Space

DTIC Thesaurus Topics

  • Air Force Facilities
  • Aircrafts
  • Aluminum Alloys
  • Contracts
  • Fabrication
  • Failure Mode And Effect Analysis
  • Landing Gear
  • Landing Gear Doors
  • Manufacturing
  • Materials
  • Plastic Explosives
  • Production
  • Spars
  • Strain Gages
  • Tensile Strength
  • Test And Evaluation
  • United States

Readers

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  • Metallurgy
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