Exhaust tube for turbine

Reference: 144/16

Exhaust for EC 145 Turbine

stainless steelfor turbine 

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: 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: 791/16

Exhaust tube for turbine, Cobra

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: 641/16

Exhaust system for Air-Crane

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

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: 342/16

Exhaust for Gazelle

Not available

Reference: 344/16

Exhaust for "Starwood" Lama

Not available

Reference: 900/16

Exhaust, stainless steel

Exhaust, stainless steel, for Ecureuil

Reference: 340/16

Exhaust for Lama

This exhaust system is designed for the Lama with turbine power system.

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: 120/16

EC 120 turbine exhaust pipe

Not available

Reference: 434/16

Exhaust tube for turbine, AIRWOLF, Bell 230 und Bell 430

On the AIRWOLF, Bell 230 and Bell 430 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: 770/16

Exhaust tube for turbine, BK 117

On the BK 117 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: 530/17

Tapa de escape Ø 55 mm

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.