Exhaust for Lama

Reference: 206/16

Exhaust for UH-1D

This exhaust system is designed for the UH-1D with turbine power system.Exhaust tubes for turbines are always designed for the specified model. It is important that no forward thrust emerges from the system. Should this still occur, the forward thrust produced is minimal.Turbine exhaust tubes are designed as exhaust-gas diffusers, i.e. opens wider towards...

Reference: 342/16

Exhaust for Gazelle

Not available

Reference: 930/16

Exhaust gas efflux for Mil Mi-2

right / leftThis exhaust system is designed for the Mil Mi-2 with turbine power system.

Reference: 641/16

Exhaust system for Air-Crane

right / leftThis exhaust system is designed for the Air-Crane with turbine power system.

Reference: 268/16

Exhaust for XL-C

Exhaust tubes for turbines are always designed for the specified model. It is important that no forward thrust emerges from the system. Should this still occur, the forward thrust produced is minimal.Turbine exhaust tubes are designed as exhaust-gas diffusers, i.e. opens wider towards the rear.

Reference: 344/16

Exhaust for "Starwood" Lama

Not available

Reference: 530/17

Tapa de escape Ø 55 mm

Reference: 134/16

Exhaust tube for turbine, EC 135

On the EC the forward thrust is eliminated by the scale division of the exhaust tube (enlarging of the cross-section) and exhausting up through the rotor disc.

Reference: 412/16

Stainless steel exhaust

Not available

Reference: 120/16

EC 120 turbine exhaust pipe

Not available

Reference: 25/9

Heat reflective mat

Between fuselage and exhaust tube a heat-reflecting mat avoids melting of the fibreglass. Even in smaller fuselages where conventional silencer systems are close to the inside surface, the heat reflective mat is useful as a heat shield.Heat reflective matheat rejectingsize approx. 300 x 700 mmmat thickness approx. 3 mm

Reference: 144/16

Exhaust for EC 145 Turbine

stainless steelfor turbine 

Reference: 530/16

Exhaust efflux for CH-53

right / left

Reference: 9/26

Ceramic band 50x3x1000 mm

Not available

Reference: 214/16

Exhaust for Bell 212 Twin Jet

Exhaust tubes for turbines are always designed for the specified model. It is important that no forward thrust emerges from the system. Should this still occur, the forward thrust produced is minimal.Turbine exhaust tubes are designed as exhaust-gas diffusers, i.e. opens wider towards the rear.

Reference: 350/16

Exhaust system for Alouette III

Not available