- Fire seals
- Fire seals
Turbine Case Cooling (TCC)
Engine nacelle/engine interface seal, compliant with AC 20-135 / ISO 2685 fire resistance requirements, capable of withstanding large displacements.
Main Benefits
Fireproof seal (1,100°C for 15 min)
Controlled tightening to match customer requirements
Retainer integrated to facilitate assembly and disassembly
Permits high displacement
Key features
Safety
In the event of a fire, Hutchinson's system creates a barrier to temporarily impede the fire, allowing more time for exceptional pilot reaction.
Excellence
An extremely robust solution, this fire seal is installed in the engine compartment to allow bleed air to escape from the turbine for improved air and oil cooling.
Applications
Technology mainly used for engines, nacelles, APU, pylon, and karman environments. Often linked with cross-contamination requirements for nacelle purposes.
Applications

Customization
Can be customized and adjusted to customer requirements for a wide range of aircraft: commercial, business jet, regional jet, or helicopters (civil or military programs).

Performance
TCC function is critical to ensure a high level of performance for the engine and nacelle.
Commercial Aviation
Business and General aviation
Rotary Wing
Aerospace defense
Advanced air mobility