Ninguna marca
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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Reference: 350/17
When the turbine of a full-size helicopter is not running, the engine is protected with an exhaust cover which prevents foreign objects finding their way inside the turbine. This exhaust cover for model turbines is suitable for the Lama, Alouette III and any other machine with a 90 mm Ø exhaust pipe. Caution: it is essential to allow the exhaust pipes to...
Reference: 641/16
right / leftThis exhaust system is designed for the Air-Crane with turbine power system.
Reference: 340/16
This exhaust system is designed for the Lama with turbine power system.
Reference: 429/16
Stainless steel exhaust manufactured specifically for the Bell 429
Reference: 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.
Reference: 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.
Reference: 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.
Reference: 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
Reference: 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.
