Referencia: 92/91
Rodamiento con orejuela de 6 x 10 x 3 mm
Brida rodamientos autolubricantes 6 x 10 x 3 mm
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Referencia: 92/91
Brida rodamientos autolubricantes 6 x 10 x 3 mm
Política de seguridad
Política de envío
Política de devolución
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Riferimento: 770/16
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.
Riferimento: 930/16
right / leftThis exhaust system is designed for the Mil Mi-2 with turbine power system.
Riferimento: 214/16
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.
Riferimento: 429/16
Stainless steel exhaust manufactured specifically for the Bell 429
Riferimento: 434/16
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.
Riferimento: 206/16
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...
Riferimento: 641/16
right / leftThis exhaust system is designed for the Air-Crane with turbine power system.
Riferimento: 791/16
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.
Riferimento: 268/16
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.