Ninguna marca
Referencia: 92/91
Brida rodamientos autolubricantes 6 x 10 x 3 mm
Política de seguridad
Política de envío
Política de devolución
No hay reseñas de clientes en este momento.
Référence: 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.
Référence: 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.
Référence: 25/9
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
Référence: 429/16
Stainless steel exhaust manufactured specifically for the Bell 429
Référence: 340/16
This exhaust system is designed for the Lama with turbine power system.
Référence: 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.
Référence: 134/16
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.
Référence: 641/16
right / leftThis exhaust system is designed for the Air-Crane with turbine power system.
Référence: 520/16
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.
Référence: 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...
Référence: 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.
