Salida de gases, acero inoxidable

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: 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: 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: 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: 429/16

Exhaust Bell 429

Stainless steel exhaust manufactured specifically for the Bell 429

Reference: 350/16

Exhaust system for Alouette III

Not available

Reference: 520/16

Exhaust tube for turbine

The outlets on the left and right hand sides offer the necessary cross-section and greatly reduce the forward thrust.This keeps the scale rear outlet while only discharging a small amount of the total exhaust gas.

Reference: 344/16

Exhaust for "Starwood" Lama

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: 412/16

Stainless steel exhaust

Not available

Reference: 144/16

Exhaust for EC 145 Turbine

stainless steelfor turbine 

Reference: 120/16

EC 120 turbine exhaust pipe

Not available

Reference: 904/16

Exhaust tube for turbine, Hughes

The shape and dimensions of the Hughes fuselages allow for the installation of a three outlet exhaust. The outlets on the left and right hand sides offer the necessary cross-section and greatly reduce the forward thrust. This keeps the scale rear outlet while only discharging a small amount of the total exhaust gas.

Reference: 530/17

Tapa de escape Ø 55 mm

Reference: 530/16

Exhaust efflux for CH-53

right / left

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.