Turbine Engine Composite Preforms: Design of MAGNAWEAVE Loom for 3-D Braiding Net Shapes

Abstract

Three dimensional braiding technology should fabricate integrally braided preforms for turbine engine parts. Using MAGNASWIRL technology, a circular 3D braiding machine design was proposed. Design requirements were defined in terms of anticipated performance requirements for gas turbine rotors. Preliminary designs were generated for a 30-ring, 360 slot/ring MAGNASWIRL machine, capable of preform fabrication for (1) test discs, (2) 2- or 4-bladed discs, (3) 36 bladed discs. Silicon carbides (continuous filament) were the fibers of design. Loom loadings were developed to provide continuous and constant fiber volume; machine motion sequences were developed for integrally fabricating body and turbine blades.

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Document Details

Document Type
Technical Report
Publication Date
Aug 01, 1991
Accession Number
ADA239294

Entities

People

  • George Pestolozzi
  • Niles Logue
  • Robert A. Florentine

Tags

Communities of Interest

  • Advanced Electronics
  • Air Platforms
  • Energy and Power Technologies
  • Weapons Technologies

DTIC Thesaurus Topics

  • Air Force
  • Composite Materials
  • Construction
  • Fabrication
  • Fiber Reinforced Composites
  • Gas Turbines
  • Manufacturing
  • Materials Processing
  • Mechanical Properties
  • Mechanical Working
  • Polymer Matrix Composites
  • Silicon Carbide
  • Tensile Strength
  • Three Dimensional
  • Turbine Wheels
  • Turbines
  • Two Dimensional

Fields of Study

  • Physics

Readers

  • Aerodynamics.
  • Reinforced Composite Materials