Aircraft Battle Damage Repair of Transparencies
Abstract
Both induction heating and adhesive bonding techniques were used to perform rapid repairs on aircraft transparencies under 'field' conditions. Patches were applied on various plastic laminated materials and were tested both for air leak rate and structural durability (cockpit air pressure representing ground-air-ground cycles). Keywords: Aircraft canopy, Transparency, Fusion bonding, Adhesive bonding, Coatings, Induction heating.
Document Details
- Document Type
- Technical Report
- Publication Date
- Apr 01, 1990
- Accession Number
- ADA224168
Entities
People
- Susan S. Saliba
Organizations
- University of Dayton