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. (SDW)
Aircraft Battle Damage Repair of Transparencies
1990
61 pages
Report
No indication
English
Aircraft , Composite Materials , Adhesives & Sealants , Adhesive bonding , Aircraft canopies , Laminates , Repair , Transparencies , Air pressure , Ammunition damage , Battles , Bonding , Coatings , Cockpits , Cycles , Field conditions , Fusion(Melting) , Induction heating , Methodology , Plastics , Rates , Surface to air , Surface to surface , Composite materials , Aircraft construction materials
Battle Damage Repair of Aircraft Transparencies
British Library Conference Proceedings | 1995
|Engineering Index Backfile | 1943
Emerald Group Publishing | 1964
Vision through Aircraft Transparencies
NTIS | 1988
|Aging of Aircraft Transparencies
British Library Conference Proceedings | 1999
|