CYCOM® EP2190
This highly toughened resin is formulated with the most advanced epoxy chemistry. Optimized for structurally efficient structure with excellent resistance to impact and delamination growth under fatigue. Designed to provide excellent cure robustness and cure stability. A 177°C (350°F) curing toughened resin system with a service temperature range of -59°C t o 107°C (-75°F t o 225°F). Typical applications for CYCOM® EP2190 include primary and secondary aircraft structures. Recommended for both thin and t hick structures.
CYCOM® EP2190 is available with carbon reinforcement in unidirectional tape, woven fabric and slit tape forms.
The following products are compatible and are suggested for use with CYCOM® EP2190: FM® 309-1 adhesives, FusePly™100, Surface Master® 905.
Features and Benefits
Minimum 15+ days handling l ife at 21°C (70°F)
12 months storage at -12°C (10°F)
Controlled f low
Very high i mpact resistance
177°C (350°F) autoclave cure t emperature
Excellent cured surface finish
Good for multiple cure cycles
NCAMP database i n development
Thermo-chemical modelling in Raven Software
High-rate manufacturing-ready with automated processing and reduced cure cycle time
Markets
| Segments | Applications | End uses |
|---|---|---|
| Advanced Air Mobility | Air Taxis / Heavy Goods Cargos | Structures |
| Rotocraft | Fixed Primary Structures | |
| Defense | Rotorcrafts | |
| Fixed Wing Aircraft | Structures | Fuselages |
Processing Method
- Autoclave
Chemical categories
| Chemical category | Chemical family | Chemical product |
|---|---|---|
| Composite materials | Thermoset composite | Epoxy |
Region of availability
- Africa & Middle East
- Asia Pacific
- Europe
- Latin America
- North America