Salidad de gases de turbina para Aloutte II

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: 530/16

Exhaust efflux for CH-53

right / left

Reference: 144/16

Exhaust for EC 145 Turbine

stainless steelfor turbine 

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: 412/16

Stainless steel exhaust

Not available

Reference: 342/16

Exhaust for Gazelle

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: 641/16

Exhaust system for Air-Crane

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

Reference: 120/16

EC 120 turbine exhaust pipe

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: 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: 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: 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: 429/16

Exhaust Bell 429

Stainless steel exhaust manufactured specifically for the Bell 429

Reference: 900/16

Exhaust, stainless steel

Exhaust, stainless steel, for Ecureuil

Reference: 530/17

Tapa de escape Ø 55 mm