AirFrame

AirCraft Materials

Aero Dynamics

Avionics & Electrical Systems

Propulsion

Weapon Systems

AirFrame Design and Analysis

AirFrame Components

Aero elastic Analysis

Structural Testing

Integrated Testing

 

AirFrame Components

• Wing
• Fuselage
• Fin
• Control surfaces
• Drop tanks

Wing

• multi spar construction
• monolithic wing skins
• integral fuel tank
• damage tolerant design concept

Fuselage

• thin walled, integrally stiffened structure

• sustain internal pressure without stiffener debonding

• complex shapes and contours

• large scale use of integral structures

• helped meet weight targets

Fin

• state of the art co-curing, co-bonding  technology

• reduced part count, manufacturing & assembly time

• multi - pronged processing involving filament winding, lay-up, thermal  expansion molding & autoclave curing weight saving – 20%, cost saving – 80%