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Referencia: 34/38
Palas del rotor de cola Juego de 2 palaslongitud = 130 mmancho = 35 mm13 gsimétricopara portacuchillas con portacuchillas de 5 mm (¡no para portacuchillas Vario!), 1 orificio, Ø 3 mmcompatible con NHP
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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: 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...
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.
Reference: 641/16
right / leftThis exhaust system is designed for the Air-Crane with turbine power system.
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: 429/16
Stainless steel exhaust manufactured specifically for the Bell 429