Z-Pin Stubble Technology Advanced Research (ZSTAR)

Abstract

Z-pins are small-diameter carbon rods that are ultrasonically inserted through composite laminates in the z-direction to provide extra resistance to crack growth and delamination. They are normally inserted through co-cured composites, but this report presents an experimental study on a new z-pin stubble manufacturing technique that is compatible with the co-bonding process. Early researchers were limited to an exposed stubble height of 0.030 inch, which would not provide all of the benefits of a full-depth co-cured z-pin reinforced joint. This report describes a study in which the stubble lengths were increased to 0.250 inch. Double cantilever beam specimens were used to characterize the effect of stubble diameter and height on the Mode I crack resistance. It was found that increasing the stubble height from 0.040 inch to 0.125 inch resulted in a significant improvement in Mode I properties. Z-pins are small diameter carbon rods that are ultrasonically inserted through composite laminates in the z-direction to provide extra resistance to crack growth and delamination. They are normally inserted through co-cured composites, but this paper presents an experimental study on a new z-pin stubble manufacturing technique that is compatible with the co-bonding process. Z-pin stubble is created by inserting pins through the thickness of an uncured laminate and trimming the pins to a certain height above the surface. After initial cure, another uncured composite part is cured on the exposed stubble. Early researchers were limited to an exposed stubble height of 0.030 inch, which would not provide all of the benefits of a full-depth co-cured z-pin reinforced joint. This paper describes a study in which the stubble lengths were increased to 0.250 inch. Double cantilever beam (DCB) specimens were used to characterize the effect of stubble diameter and height

Open PDF

Document Details

Document Type
Technical Report
Publication Date
Apr 01, 2008
Accession Number
ADA483021

Entities

People

  • Amanda K. Pommer
  • Stephen B. Clay

Organizations

  • Air Force Research Laboratory

Tags

Communities of Interest

  • Energy and Power Technologies

DTIC Thesaurus Topics

  • Air Force
  • Air Force Research Laboratories
  • Aircrafts
  • Cantilever Beams
  • Composite Material Fabrication
  • Composite Materials
  • Delamination
  • Fabrication
  • Failure Mode And Effect Analysis
  • Laminates
  • Manufacturing
  • Materials
  • Materials Laboratories
  • Materials Processing
  • Measurement
  • Resistance
  • Structural Components

Fields of Study

  • Materials science

Readers

  • Electrical Engineering
  • Neurotoxicology
  • ballistics.